US20100218932A1 - Thermally conducting foam interface materials - Google Patents

Thermally conducting foam interface materials Download PDF

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Publication number
US20100218932A1
US20100218932A1 US12/778,510 US77851010A US2010218932A1 US 20100218932 A1 US20100218932 A1 US 20100218932A1 US 77851010 A US77851010 A US 77851010A US 2010218932 A1 US2010218932 A1 US 2010218932A1
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US
United States
Prior art keywords
thermal interface
thermally conductive
interface material
foam
foam thermal
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
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US12/778,510
Inventor
Patrick J. Fischer
James J. Kobe
Cameron T. Murray
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3M Innovative Properties Co
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3M Innovative Properties Co
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Publication date
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Priority to US12/778,510 priority Critical patent/US20100218932A1/en
Publication of US20100218932A1 publication Critical patent/US20100218932A1/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/18Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00Layered products comprising a layer of synthetic resin
    • B32B27/18Layered products comprising a layer of synthetic resin characterised by the use of special additives
    • B32B27/20Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents
    • B32B27/205Layered products comprising a layer of synthetic resin characterised by the use of special additives using fillers, pigments, thixotroping agents the fillers creating voids or cavities, e.g. by stretching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/18Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
    • B32B5/20Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material foamed in situ
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/06Interconnection of layers permitting easy separation
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J11/00Features of adhesives not provided for in group C09J9/00, e.g. additives
    • C09J11/02Non-macromolecular additives
    • C09J11/04Non-macromolecular additives inorganic
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J5/00Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers
    • C09J5/08Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers using foamed adhesives
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J7/00Adhesives in the form of films or foils
    • C09J7/10Adhesives in the form of films or foils without carriers
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J7/00Adhesives in the form of films or foils
    • C09J7/20Adhesives in the form of films or foils characterised by their carriers
    • C09J7/22Plastics; Metallised plastics
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J7/00Adhesives in the form of films or foils
    • C09J7/30Adhesives in the form of films or foils characterised by the adhesive composition
    • C09J7/38Pressure-sensitive adhesives [PSA]
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B32B37/1207Heat-activated adhesive
    • B32B2037/1215Hot-melt adhesive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/0012Mechanical treatment, e.g. roughening, deforming, stretching
    • B32B2038/0028Stretching, elongating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/30Properties of the layers or laminate having particular thermal properties
    • B32B2307/306Resistant to heat
    • B32B2307/3065Flame resistant or retardant, fire resistant or retardant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2310/00Treatment by energy or chemical effects
    • B32B2310/08Treatment by energy or chemical effects by wave energy or particle radiation
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K2201/00Specific properties of additives
    • C08K2201/001Conductive additives
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/18Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/20Oxides; Hydroxides
    • C08K3/22Oxides; Hydroxides of metals
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2203/00Applications of adhesives in processes or use of adhesives in the form of films or foils
    • C09J2203/326Applications of adhesives in processes or use of adhesives in the form of films or foils for bonding electronic components such as wafers, chips or semiconductors
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2301/00Additional features of adhesives in the form of films or foils
    • C09J2301/20Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive itself
    • C09J2301/208Additional features of adhesives in the form of films or foils characterized by the structural features of the adhesive itself the adhesive layer being constituted by at least two or more adjacent or superposed adhesive layers, e.g. multilayer adhesive
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2301/00Additional features of adhesives in the form of films or foils
    • C09J2301/30Additional features of adhesives in the form of films or foils characterized by the chemical, physicochemical or physical properties of the adhesive or the carrier
    • C09J2301/308Additional features of adhesives in the form of films or foils characterized by the chemical, physicochemical or physical properties of the adhesive or the carrier the adhesive tape or sheet losing adhesive strength when being stretched, e.g. stretch adhesive
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2301/00Additional features of adhesives in the form of films or foils
    • C09J2301/30Additional features of adhesives in the form of films or foils characterized by the chemical, physicochemical or physical properties of the adhesive or the carrier
    • C09J2301/314Additional features of adhesives in the form of films or foils characterized by the chemical, physicochemical or physical properties of the adhesive or the carrier the adhesive layer and/or the carrier being conductive
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2421/00Presence of unspecified rubber
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2423/00Presence of polyolefin
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2433/00Presence of (meth)acrylic polymer
    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09JADHESIVES; NON-MECHANICAL ASPECTS OF ADHESIVE PROCESSES IN GENERAL; ADHESIVE PROCESSES NOT PROVIDED FOR ELSEWHERE; USE OF MATERIALS AS ADHESIVES
    • C09J2453/00Presence of block copolymer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F13/00Arrangements for modifying heat-transfer, e.g. increasing, decreasing
    • F28F2013/005Thermal joints
    • F28F2013/006Heat conductive materials
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L2924/00Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
    • H01L2924/0001Technical content checked by a classifier
    • H01L2924/0002Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249953Composite having voids in a component [e.g., porous, cellular, etc.]
    • Y10T428/249982With component specified as adhesive or bonding agent
    • Y10T428/249983As outermost component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
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    • Y10T428/249986Void-containing component contains also a solid fiber or solid particle
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y10T428/249987With nonvoid component of specified composition
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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    • Y10T428/2891Adhesive compositions including addition polymer from unsaturated monomer including addition polymer from alpha-beta unsaturated carboxylic acid [e.g., acrylic acid, methacrylic acid, etc.] Or derivative thereof

Definitions

  • Integrated circuits, active and passive components, optical disk drives, and the like generate heat under use conditions that must be diffused to allow continuous use of the heat generating component.
  • Heat sinks in the form of finned metal blocks and heat spreaders containing heat pipes are commonly attached to these heat generating components to allow excess heat to be conducted away and radiated into the atmosphere.
  • Materials useful for providing a thermal bridge between the heat generating components and heat sinks/heat spreaders are known. Many of these materials are based on gel masses, liquid to solid phase change compounds, greases, or pads that must be mechanically clamped between a printed circuit board (PCB) and heat sink.
  • PCB printed circuit board
  • thermally conductive materials incorporating adhesives have been introduced. These thermally conductive adhesive materials typically form an adhesive bond between the heat generating component and heat sink/heat spreader so that no mechanical clamping is required. Both heat-activated (hot melt) and pressure sensitive adhesives have been used in thermally conductive adhesives. In all cases, these thermal interface materials need to be thermally enhanced (compared with unfilled or lightly filled polymer compositions), be dimensionally stable at elevated temperatures (heat generating components often run at 50° C. or higher), and be soft and conformable enough to provide good contact (wet-out) between the substrates. Typically, such thermally conductive adhesives have compromised thermal conductivity for softness/conformability or vice versa.
  • Articles incorporating a polymer foam core are characterized by the density of the foamed polymer being lower than the density of the pre-foamed polymeric matrix.
  • the lowered density for the foam may be achieved in several known ways such as by foaming with chemical blowing agents or by interspersing microspheres within the matrix, the microspheres typically being made of glass or of certain polymeric materials, the former being detrimental to the softness/conformability of the foam.
  • Foams have been used to join two rigid substrates, or substrates with uneven or rough surfaces. However, heretofore, foams have not been used for thermal interface materials. It was believed that discontinuous voids in the thermal interface material should be avoided due to the insulating nature of such voids. Thus thermal conductivity was compromised.
  • a fire retardant feature may be needed and/or may be required by applicable regulations.
  • tapes to be used in electric or electronic applications may be directly exposed to electrical current, to short circuits, and/or to heat generated from the use of the associated electronic component or electrical device. Consequently, industry standards or regulations may impose conditions on the use of such tape articles that require qualifying tests be performed such as burn tests, and the like.
  • the industry standard flammability test is Underwriters Laboratories (UL 94 “Standard for Tests for Flammability of Plastic Materials for Parts in Devices and Appliances”).
  • thermally conductive foams and thermally conductive adhesive interfaces that have acceptable thermal conductivity and are soft/conformable and methods for the manufacture of the thermal interface materials. It is also desirable to provide the foregoing thermally conductive articles in a fire retardant construction which optionally has stretch releasable properties.
  • the invention provides a foam thermal interface material comprising a foamed film, the film comprising a blend of polymeric hot melt pressure sensitive adhesive having a number average molecular weight of greater than 25,000 and at least 25 percent by weight of thermally conductive filler, said film having a void volume of at least 5 percent of the volume of said foamed film.
  • the invention provides a thermal interface composition
  • a thermal interface composition comprising polymeric hot melt pressure sensitive adhesive having a number average molecular weight of greater than 25,000, at least 25 percent by weight of thermally conductive filler, and an effective amount of a foaming agent.
  • foam thermal interface materials and compositions of the invention may further comprise fire retardant and/or microfiber forming material.
  • the invention provides a method for preparing a foam thermal interface material, comprising:
  • the foaming agent can be activated after extruding the extrudable composition.
  • FIG. 1 is a perspective drawing showing a thermal interface material of the invention.
  • FIG. 2 is a perspective drawing showing a second thermal interface material.
  • FIG. 3 is a perspective drawing of a thermal interface material featuring a continuous film combined with a thermally conductive adhesive layer.
  • FIG. 4 is a schematic drawing of an extrusion processor for preparing articles according to the invention.
  • FIG. 5 is a schematic diagram of the thin-heater test apparatus used in the Examples.
  • FIG. 6 is a plot of thermal impedance (Z corr. ) versus thickness (t) used to calculate bulk thermal conductivity in the Examples.
  • Vehicle volume refers to the voids that there are present in the adhesive that are formed by activating a foaming agent contained in the adhesive.
  • Fire retardant refers to a substance that when applied to or incorporated within a combustible material, reduces or eliminates the tendency of the material to ignite and/or reduces the tendency to continue burning once ignited, when exposed to heat or flame.
  • “Stretch release” refers to the property of an adhesive article characterized in that, when the article is pulled and elongated from a substrate surface at a rate of 30 centimeters/minute and at an angle of 45° or less, the article detaches from a substrate surface without leaving a significant amount of visible residue on the substrate or when the article has been used between two rigid substrates, the article is pulled and elongated at a rate of 30 centimeters/minute and at an angle of 5° or less, the article detaches from a substrate surface without leaving a significant amount of visible residue on at least one of the rigid substrates.
  • substantially continuous refers to a microfiber that is unbroken for at least about 0.5 cm in the machine direction.
  • substantially free refers to a component that is present in a thermal interface material (TIM) of the invention at levels of less than 0.1, 0.09, or 0.08 percent by weight, based on the weight of the polymeric hot melt PSA.
  • foam thermal interface materials comprising a thermally conductive filler and a hot melt pressure sensitive adhesive (PSA) polymer foam (or foamed film) that is desirably substantially free or free of oligomers or low molecular weight polymers, other than residuals resulting from polymerization of the PSA, (that is, ⁇ 25,000 number average molecular weight), N-tert-butylacrylamide, organic solvent, added free radical initiators, and crosslinking agents.
  • PSA hot melt pressure sensitive adhesive
  • the foamed film may also comprise one or more polymer microspheres capable of further expansion when heated.
  • the outer surface of the foamed film may be substantially smooth or it may be patterned, and the foamed film may be provided in any of a variety of configurations including sheets, rods, or cylinders. At least a portion of the outer surface may serve as a substrate for films, adhesive layers, and the like, thus providing any of a variety of tape/TIMs.
  • the foamed film of the TIMs of the invention contain at least about 5 percent void volume as determined by the test method described herein.
  • the desired characteristics of a foam TIM according to the invention include one or more of the following: (1) bulk thermal conductivity of at least about 0.5 Watts/meter-K; (2) Shore A hardness less than about 60; (3) static shear strength at 22° C. or 70° C. of at least about 10,000 minutes when tested according to the test methods described below; and (4) when the TIM comprises viscoelastic microfibers, the tensile break strength of at least about 150% of the yield strength of the TIM with an elongation greater than about 200%, and less than about 50% recovery after being elongated 100%, and when the TIM comprises elastic microfibers, the TIM has an elongation greater than about 200% and have greater than about 50% recovery after being elongated 100%.
  • Foam TIMs comprising the continuous adhesive film and/or the optional skin adhesive layer(s) applied to the surfaces of the foam PSA film can have a high adhesion when applied to a panel, such as 90 degree peel adhesion of greater than about 0.0438 kN/m (4 oz/in), in other embodiments, greater than about 0.176 kN/m, or greater than about 0.352 kN/m.
  • the polymeric hot melt PSA useful in the invention has a number average molecular weight of greater than 25,000, particularly, a number average molecular weight of greater than 100,000, and more particularly a number average molecular weight of greater than 200,000, and even more particularly a number average molecular weight of greater than 400,000 (as defined in Introduction to Physical Polymer Science , Chapter 1, page 6, L. H. Sperling ISBN 0-471-89092-8).
  • the polymeric hot melt PSA may be selected from any of a variety of polymeric materials, such as rubbers, elastomers, thermoplastic polyurethanes, thermoplastic elastomers, poly-alpha-olefins, synthetic rubbers, acrylate polymers and methacrylate polymers, acrylate and methacrylate copolymers, and combinations of the foregoing.
  • the optional thermally conductive adhesive layer may be a PSA, such as, for example, poly-alpha-olefin adhesive, acrylic acid adhesive, a rubber based adhesive, a silicone adhesive, a blend of rubber based adhesive and acrylic adhesive, and combinations thereof.
  • the optional thermally conductive adhesive layer may be a heat-activated adhesive.
  • the continuous foamed film and/or the optional thermally conductive adhesive layer may be provided with substantially continuous, individual polymeric microfibers therein and oriented in the machine direction, the microfibers imparting stretch release properties to the article.
  • the continuous film and/or optional thermally conductive adhesive layer may comprise a fire retardant.
  • the foam TIM 10 comprises a foamed film 11 having a first flat surface 12 and a second surface (not shown) opposite the first surface 12 .
  • at least one thermally conductive filler 15 is interspersed throughout a polymeric adhesive matrix 16 .
  • the foamed film 11 comprises a polymer adhesive matrix 16 with a plurality of voids 14 interspersed within the matrix.
  • the voids 14 are the result of the foaming process used in the manufacture of the film 11 and may be created through the use, for example, of blowing agents or by the inclusion of expandable polymeric microspheres or combinations thereof. If expandable microspheres are included in the manufacture of the foamed film 11 , the voids 14 typically comprise the polymer microspheres in an expanded and unbroken form and provide a void volume of at least 5%.
  • a layer of a thermally conductive skin adhesive may first be applied to the first surface 12 to bond the additional layers or structures to the surface 12 .
  • the foamed film 11 may be provided as a two-sided tape TIM having another adhesive layer, in particular a thermally conductive adhesive layer, on surface opposite the first surface 12 .
  • a release liner or the like may be associated with the thermally conductive skin adhesive(s) on either or both of the surfaces of the foamed film 11 .
  • FIG. 2 shows foam TIM 100 in the form of a foamed film 101 having a first surface 102 and a second surface opposite the first surface (not shown).
  • foam TIM 100 comprises a foamed film 101 comprising at least one thermally conductive filler 105 , a plurality of voids 104 , and individual, substantially continuous viscoelastic and/or elastic microfibers 108 interspersed throughout polymeric adhesive matrix 106 and oriented in the machine direction.
  • Microfibers 108 are typically formed in situ during the manufacture of the TIM and are oriented in the machine direction. It will be appreciated that other layers and/or structures may be applied or affixed to the surfaces 102 of the foamed film 101 .
  • the polymeric hot melt PSAs (prior to compounding with thermally conductive filler) useful in the invention have a number average molecular weight of greater than 25,000 and is tacky at room temperature (about 22° C.).
  • PSAs are a distinct category of adhesives which in dry (solvent-free) form are permanently tacky at room temperature. They firmly adhere to a variety of dissimilar surfaces upon mere contact without the need of more than finger or hand pressure. PSAs require no activation by water, solvent, or heat to exert a relatively strong adhesive holding force.
  • PSAs can be quantitatively described using the “Dahlquist criteria” which maintains that the elastic modulus of these materials is less than 10 6 dynes/cm 2 at room temperature. See Pocius, A.
  • the foams of the invention may comprise one or more PSAs. It may be desirable to use two or more PSA polymers having different compositions to achieve unique foam properties. A wide range of foam physical properties can be obtained by selectively choosing the PSA component types and concentrations. A particular polymer may be selected based upon the desired properties of a final material.
  • the hot melt PSA may be any of a variety of different polymer materials including elastomers, rubbers, thermoplastic elastomers, poly-alpha-olefin adhesives, acrylic adhesives, and blends thereof.
  • the polymer resins are of the type that are suitable for melt extrusion processing, as described in U.S. Pat. No. 6,103,152, incorporated in its entirety herein by reference thereto. It may be desirable to blend two or more polymers having chemically different compositions.
  • the physical properties of the foam can be optimized by varying the types of components used in creating the foam and by varying their relative concentrations.
  • a particular hot melt PSA is generally chosen or selected based upon the desired properties of the final thermal interface material. It is recognized that the polymer material used to prepare the hot melt PSA may contain residual amounts of free radical initiators, oligomers or low molecular weight polymers ( ⁇ 25,000 number average molecular weight), or organic solvent.
  • Suitable materials for producing a useful hot melt PSA include acrylate and methacrylate polymers or co-polymers.
  • Such polymers can be formed by polymerizing 50 to 100 parts by weight of one or more monomeric acrylic or methacrylic esters of non-tertiary alkyl alcohols, with the alkyl groups having from 1 to 20 carbon atoms (e.g., from 3 to 18 carbon atoms).
  • Suitable acrylate monomers include methyl acrylate, ethyl acrylate, n-butyl acrylate, lauryl acrylate, 2-ethylhexyl acrylate, cyclohexyl acrylate, iso-octyl acrylate, octadecyl acrylate, nonyl acrylate, decyl acrylate, isobornyl acrylate, and dodecyl acrylate. Also useful are aromatic acrylates, e.g., benzyl acrylate and cyclobenzyl acrylate. In some applications, it may be desirable to use less than 50 parts by weight of the monomeric acrylic or methacrylic esters.
  • one or more monoethylenically unsaturated co-monomers may be polymerized with the acrylate monomers in amounts from about 0 to 50 parts co-monomer.
  • One class of useful co-monomers includes those having a homopolymer glass transition temperature greater than the glass transition temperature of the acrylate homopolymer.
  • suitable co-monomers falling within this class include acrylic acid, acrylamide, methacrylamide, substituted acrylamides, such as N,N-dimethyl acrylamide, itaconic acid, methacrylic acid, acrylonitrile, methacrylonitrile, vinyl acetate, N-vinyl pyrrolidone, isobornyl acrylate, cyano ethyl acrylate, N-vinylcaprolactam, maleic anhydride, hydroxyalkylacrylates, N,N-dimethyl aminoethyl(meth)acrylate, N,N-diethylacrylamide, beta-carboxyethyl acrylate, vinyl esters of neodecanoic, neononanoic, neopentanoic, 2-ethylhexanoic, or propionic acids (e.g., available from Union Carbide Corp. of Danbury, Conn., under the designation VYNATES), vinylidene chloride
  • a second class of useful co-monomers includes those having a homopolymer glass transition temperature less than the glass transition temperature of the acrylate homopolymer.
  • polymers useful in the present invention includes pressure sensitive and hot melt adhesives prepared from non-photopolymerizable monomers.
  • Such polymers can be adhesive polymers (i.e., polymers that are inherently adhesive), or polymers that are not inherently adhesive but are capable of forming adhesive compositions when compounded with tackifiers.
  • Specific examples include polyurethanes, poly-alpha-olefins (e.g., polyoctene, polyhexene, and atactic polypropylene), block copolymer-based adhesives, natural and synthetic rubbers, silicone adhesives, ethylene-vinyl acetate, and epoxy-containing structural adhesive blends (e.g., epoxy-acrylate and epoxy-polyester blends), and combinations thereof.
  • the adhesive has a high service temperature (i.e., up to or greater than 70° C.).
  • a high service temperature i.e., up to or greater than 70° C.
  • acrylic based adhesives can be crosslinked by irradiation by electron beam (E-beam), gamma, and the like.
  • Block copolymer-based adhesives can have their elevated temperature performance improved through the addition of polyphenylene oxide (PPO) or an end block reinforcing resin to the block copolymer as described in U.S. Pat. No. 6,277,488, which is incorporated herein by reference.
  • PPO polyphenylene oxide
  • thermally conductive fillers are suitable for use in the adhesives of the invention.
  • the thermally conductive filler is selected from a variety of materials having a bulk conductivity of between about 5 and 1000 Watts/meter-K as measured according to ASTM D1530.
  • suitable thermally conductive fillers include but are not limited to, aluminum oxide, beryllia, zirconia, aluminum titanate, silicon carbide, boron carbide, silicon nitride, aluminum hydroxide, magnesium hydroxide, titanium dioxide, aluminum nitride, boron nitride, titanium nitride, and the like, and combinations thereof.
  • fillers are found in a variety of shapes/forms (spherical, flakes, agglomerates, crystals, acicular, fumed). The choice of shape is dependent upon the rheology of the selected adhesive resin and ease of processing of the final hot melt PSA/particle mix. Fillers may be available in several crystal types (e.g., hexagonal and rhombic boron nitride) and the type of crystal chosen will depend upon the thermal conductivity of the crystal (including the anisotropic nature of the conductivity along different crystal axes), effect of crystal type on final mechanical properties and cost.
  • crystal types e.g., hexagonal and rhombic boron nitride
  • particle size and distribution will also affect mechanical and adhesive properties, so particle size selection should accommodate the final adhesive property requirements.
  • the particle size of the filler (or mixture of fillers) and particle loading are selected to produce suitable thermal conductance while retaining adequate mechanical properties.
  • useful thermally conductive particles have an average particle size in the range of from about 0.5 micrometers ( ⁇ m) to about 250 micrometers.
  • the thermally conductive particles may range in average size from about 1 to about 100 micrometers and from about 10 to about 70 micrometers.
  • the particles may range in average size in any range between 0.5 and 250 micrometers and may be any average size between 0.5 and 250 micrometers.
  • the adhesive may contain thermally conductive particles that can bridge the adhesive and/or thermal interface matrix and be exposed through the matrix to a degree increasing with their size. Thus, particles are contained within the PSA and improve thermal conductivity in the path between the heat-source substrate and heat-conducting article, such as a heat sink article.
  • These particles are of sufficient size to impinge near or against base of heat sink article such that they impress into or onto its surface prior to or after the heat sink article is placed in service.
  • increasing the size of these particles to the same adhesive thickness will increase the thermal conductivity between a heat-source substrate and the heat-conducting article.
  • particle size depends on the application. For example, particles having a major dimension of at least about 1-2 ⁇ m and about 30 ⁇ m or below and in other embodiments, between about 5 and 20 ⁇ m, are suitable when the bond line will be in the 25 to 100 ⁇ m range (such as found between a central processing unit (CPU) and a heat sink). Particles larger than about 20 to 30 ⁇ m, such as 50 to 250 ⁇ m, are used where a larger gap exists between the hot and cold substrates. In addition, combinations of different particle size materials can be used. Larger conductive filler particle size results in higher bulk conductivity. When at least some of the selected particles are capable of being plastically deformed during heat sink article attachment, these particle sizes can be even larger than the sizes mentioned above.
  • thermally conductive fillers have been shown to provide equivalent thermal performance at reduced costs by substituting a portion of an expensive filler (for example, boron nitride) with a less expensive filler (for example, silicon carbide).
  • thermally conductive fillers often have anisotropic thermal conductivity along various crystal planes, so filler orientation via known methods can be used to enhance thermal performance.
  • the thermally conductive particles may be present in the adhesive compositions of the invention in an amount of at least 25 percent by weight of the total composition. In other embodiments of the invention, the thermally conductive filler is present in an amount of at least about 30 weight percent, at least about 40 weight percent, and in some embodiments of the invention, at least about 50 weight percent. In other embodiments, thermally conductive fillers may be present in the adhesive blends of the invention in a range of from 25 to 80 weight percent, 30 to 80 weight percent, 40 to 80 weight percent, 50 to 80 weight percent, or any range between 25 and 80 weight percent.
  • thermally conductive filler While the maximum of thermally conductive filler is selected based on the final properties (e.g., hardness, conformability, adhesion, and thermal conductivity) of the article, the thermally conductive filler is generally present is an amount less than about 80 weight percent.
  • the foam thermal interface material has a bulk conductivity of at least about 0.5 Watts/meter-K; in other embodiments, the foam thermal interface material has a bulk conductivity of at least about 0.6 Watts/meter-K; and in other embodiments, at least about 0.8 Watts/meter-K.
  • Useful foaming agents include entrained gases/high pressure injectable gases; blowing agents, such as chemical blowing agents and physical blowing agents; expanded or unexpanded polymeric bubbles; and combinations thereof.
  • High pressure injectable gases are gases that are added to sealed mixing systems (e.g., a sealed extruder) at a pressure of greater than 20.67 MPa (3000 psi) to generate a foam upon existing the sealed system.
  • sealed mixing systems e.g., a sealed extruder
  • high pressure injectable gases include nitrogen, air, carbon dioxide (CO 2 ), and other compatible gases, and combinations thereof.
  • a physical blowing agent useful in the present invention is any naturally occurring atmospheric material which is a vapor at the temperature and pressure at which the foamed film exits the die.
  • the physical blowing agent may be introduced into the polymeric material as a gas, liquid, or supercritical fluid.
  • the physical blowing agent may be injected into the extruder system.
  • a physical blowing agent is usually in a supercritical state at the conditions existing in the extruder during the process. If a physical blowing agent is used, it is preferable that it is soluble in the polymeric material being used.
  • the physical blowing agents used will depend on the properties sought in the resulting foam articles. Other factors considered in choosing a blowing agent are its toxicity, vapor pressure profile, and ease of handling.
  • Blowing agents such as pentane, butane, and other organic materials, such as hydrofluorocarbons (HFC) and hydrochlorofluorocarbons (HCFC) may be used, but non-flammable, non-toxic, non-ozone depleting blowing agents are preferred because they are easier to use, e.g., fewer environmental and safety concerns.
  • HFC hydrofluorocarbons
  • HCFC hydrochlorofluorocarbons
  • Suitable physical blowing agents include, for example, carbon dioxide, nitrogen, SF6, nitrous oxide, perfluorinated fluids, such as C 2 F 6 , argon, helium, noble gases, such as xenon, air (nitrogen and oxygen blend), and blends of these materials, hydrofluorocarbons (HFC), hydrochlorofluorocarbons (HCFC), and hydrofluoroethers (HFE).
  • perfluorinated fluids such as C 2 F 6 , argon, helium
  • noble gases such as xenon, air (nitrogen and oxygen blend
  • HFC hydrofluorocarbons
  • HCFC hydrochlorofluorocarbons
  • HFE hydrofluoroethers
  • Chemical blowing agents do not require an injection system as does a physical blowing agent and they can be used in virtually any extrusion system.
  • Examples of chemical blowing agents include water and azo-, carbonate-, and hydrazide-based molecules including, e.g., 4,4′-oxybis(benzenesulfonyl)hydrazide, such as CELOGEN OT (available from Uniroyal Chemical Company, Inc., Middlebury, Conn.), 4,4′-oxybenzenesulfonyl semicarbazide, p-toluenesulfonyl semicarbazide, p-toluenesulfonyl hydrazide, oxalic acid hydrazide, diphenyloxide-4,4′-disulphohydrazide, benzenesulfonhydrazide, azodicarbonamide, azodicarbonamide(1,1′-azobisformamide), meta-modified azodicarbonides,
  • silicon carbide available from Washington Mills Electro Minerals Corp., Niagara Falls, N.Y., under the trade designation of SILCARIDE G-21 Silicon Carbide Grade P240 functions as a chemical blowing agent as well as a thermally conductive filler. Additional chemical blowing agents are described in Klempner, D., Frisch, K.C. (editors), Handbook of Polymeric Foams and Foam Technology , Chapter 17, (Hansen, N.Y., 1991).
  • One or more expandable polymeric microsphere can be used as the foaming agent in the foamed thermally conductive film of the invention.
  • An expandable polymeric microsphere comprises a polymer shell and a core material in the form of a gas, liquid, or combination thereof. Upon heating to a temperature at or below the melt or flow temperature of the polymeric shell, the polymer shell will expand. Examples of suitable core materials include propane, butane, pentane, isobutane, neopentane, or similar material, and combinations thereof.
  • the identity of the thermoplastic resin used for the polymer microsphere shell can influence the mechanical properties of the foam, and the properties of the foam may be adjusted by the choice of microsphere, or by using mixtures of different types of microspheres.
  • acrylonitrile-containing resins are useful where high tensile and cohesive strength are desired in a low density foam article. This is especially true where the acrylonitrile content is at least 50 weight percent of the resin used in the polymer shell, generally at least 60 weight percent, and typically at least 70 weight percent.
  • suitable thermoplastic resins which may be used as the shell include acrylic and methacrylic acid esters, such as polyacrylate; acrylate-acrylonitrile copolymer; and methacrylate-acrylic acid copolymer.
  • Vinylidene chloride-containing polymers such as vinylidene chloride-methacrylate copolymer, vinylidene chloride-acrylonitrile copolymer, acrylonitrile-vinylidene chloride-methacrylonitrile-methyl acrylate copolymer, and acrylonitrile-vinylidene chloride-methacrylonitrile-methyl methacrylate copolymer may also be used, but may not be desired if high strength is sought. In general, where high strength is desired, the microsphere shell will have no more than 20 weight percent vinylidene chloride and typically no more than 15 weight percent vinylidene chloride. High strength applications may require microspheres with essentially no vinylidene chloride.
  • Halogen free microspheres may also be used in the foams of the invention.
  • suitable commercially available expandable polymeric microspheres include those available from Pierce Stevens (Buffalo, N.Y.) under the designations F-30D, F-50D, F-80SD, and F-100D.
  • expandable polymeric microspheres available from Expancel, Inc. (Duluth, Ga.) under the designations EXPANCEL 551, EXPANCEL 461, EXPANCEL 091, and EXPANCEL 092 MB 120.
  • the selection of expandable polymeric microsphere is typically based on its expansion temperature and on the thermally conductive filler used.
  • the amount of foaming agent is selected to provide a void volume constituting at least 5% of the volume of the foamed film.
  • the higher the foaming agent concentration the lower the density of the foamed film and the lower the thermal conductivity. That is, the higher the void volume, the lower the thermal conductivity of the foamed film.
  • the amount of microspheres in the polymer resin typically ranges from about 0.1 parts by weight to about 10 parts by weight (based upon 100 parts of polymer), in other embodiments, from about 0.5 parts by weight to about 5 parts by weight, and in other embodiments, from about 0.5 parts by weight to about 2 parts by weight.
  • the foam TIM contains at least about 5 percent void volume as determined by the test method described herein. In another embodiment, the foam TIM contains at least about 10 percent void volume as determined by the test method described herein. Generally, the foam TIM contains less than about 75 percent void volume, less than about 60 percent, or less than about 50 percent void volume due to influence of voids on thermally conductivity.
  • a fire retardant feature may be needed and/or may be required by applicable regulations.
  • tapes to be used in electric or electronic applications may be directly exposed to electrical current, to short circuits, and/or to heat generated from the use of the associated electronic component or electrical device. Consequently, industry standards or regulations may impose conditions on the use of such tape articles that require qualifying tests be performed, such as burn tests, and the like.
  • the industry standard flammability test is Underwriters Laboratories (UL 94 “Standard for Tests for Flammability of Plastic Materials for Parts in Devices and Appliances”). It is preferable that the foam TIM will pass UL 94 V-2 flammability rating and in other embodiments, will pass a UL 94 V-0 flammability rating.
  • Fire retardants suitable for inclusion in the foam TIMs of the present invention include any type of fire retardant which are generally present in the film at a concentration of between about 5 weight percent and about 40 weight percent based on the total weight of the foam TIM.
  • the fire retardants can be intumescent fire retardants and/or non-intumescent fire retardants.
  • the fire retardants are non-halogen containing and antimony-free.
  • suitable fire retardants for use in the foam TIMs described herein include those commercially available from Clariant Corporation of Charlotte, N.C., under the designation EXOLIT, including those designated IFR 23, AP 750, EXOLIT OP grade materials based on organophosphorous compounds, and EXOLIT RP grades of red phosphorus materials non-halogenated fire retardants, such as FIREBRAKE ZB and BORGARD ZB, and FR 370 (tris(tribromoneopentyl) phosphate), available from Dead Sea Bromine Group, Beer Shiva, Israel.
  • suitable fire retardants that also function as thermally conductive fillers include aluminum hydroxide and magnesium hydroxide.
  • Blends of one or more fire retardants and/or a synergist may also be used in the foam TIMs of the invention. Selection of the fire retardant system will be determined by various parameters, for example, the industry standard for the desired application, and by composition of the foamed film polymer matrix.
  • the foam TIMs of the invention may contain smoke suppressants, such as those available under the trade designation Kemgard HPSS, 911A, 911B, and 911 C, available from Sherwin-Williams Chemicals, Cleveland, Ohio.
  • the thermally conductive film, the thermally conductive skin adhesive or both the film and the skin adhesive will include microfiber forming materials that form viscoelastic and/or elastic microfibers formed in situ during the manufacturing process described herein.
  • the individual microfibers are individual substantially continuous and dispersed throughout the adhesive polymer matrix and oriented in the machine direction of the film. It has been found that suitable microfibers include those formulated according to the teachings of pending U.S. Patent. Publication No. 02-0187294-A1, incorporated in its entirety herein by reference thereto.
  • the individual microfibers are unbroken for at least about 0.5 centimeters (cm) in the machine direction, in other embodiments, at least about 2 cm, about 5 cm, or about 8 cm.
  • the individuals substantially continuous microfibers generally have a maximum diameter of about 0.05 to about 5 micrometers, typically from about 0.1 to about 1 micrometer and the aspect ratio (i.e., the ratio of the length to the diameter) of the individual substantially continuous microfibers is greater than about 1000.
  • the foam TIM may also include a number of other additives other than materials expressly excluded above.
  • suitable additives include tackifiers (e.g., rosin esters, terpenes, phenols, and aliphatic, aromatic, or mixtures of aliphatic and aromatic synthetic hydrocarbon resins), pigments, reinforcing agents, hydrophobic or hydrophilic silica, calcium carbonate, toughening agents, fibers, fillers, antioxidants, stabilizers, and combinations thereof.
  • tackifiers e.g., rosin esters, terpenes, phenols, and aliphatic, aromatic, or mixtures of aliphatic and aromatic synthetic hydrocarbon resins
  • pigments e.g., rosin esters, terpenes, phenols, and aliphatic, aromatic, or mixtures of aliphatic and aromatic synthetic hydrocarbon resins
  • pigments e.g., rosin esters, terpenes, phenols, and
  • backing materials are thermally conductive. Such backing materials can be inherently thermally conductive or may contain additive(s), such as those described under “Thermally Conductive Fillers” above, to impart thermal conductivity.
  • suitable backing materials include cellulosic materials, such as paper and cloth (woven and nonwoven); films, such as polyester, polyvinyl chloride, polyurethane, polypropylene, and nylon; thermally conductive foam materials, such as polyethylene foams and acrylic foams; scrims; and metal foils, such as aluminum foil.
  • the backing material can be a release liner. In this embodiment, the backing does not need to be thermally conductive.
  • the release liner can be coated on one or both sides with a release coating.
  • the backing may also be provided as multiple layers.
  • Multilayer foam TIMs can also be prepared by laminating polymer or nonpolymer layers to a foamed film, or by layering extruded foamed films as they exit their respective shaping orifices, with the use of some affixing means, such as an adhesive.
  • Other techniques that can be used include extrusion coating and inclusion coextrusion, which is described in, for example, U.S. Pat. No. 5,429,856, incorporated herein by reference.
  • FIG. 3 depicts yet another TIM 200 in which a thermally conductive skin adhesive layer 220 is provided on one of the surfaces 202 of the foamed film 201 .
  • Foamed film 201 comprises a polymer adhesive matrix 206 with a plurality of voids 204 and thermally conductive particles 205 interspersed within the matrix.
  • the skin adhesive layer 220 may comprise any of a variety of adhesive materials and thermally conductive fillers as are further described herein.
  • the skin adhesive layer 220 is a thermally conductive PSA formulated without fire retardant materials therein.
  • a release liner (not shown) may optionally be included to protect the adhesive layer 220 prior to the application of the adhesive 220 to another substrate or the like.
  • the aforementioned thermally conductive skin adhesive layer may be associated with the foamed film by, for example, co-extruding the extrudable foaming agent containing composition with one or more extrudable adhesive compositions, as described in greater detail, below.
  • the thermally conductive adhesive compositions are generally formulated and/or selected without fire retardant to provide an adhesive article, such as a tape wherein the continuous foamed film forms the substrate for the tape.
  • the adhesive may be applied to a portion of the surface of the continuous foamed film (e.g., on one of the major surfaces thereof), leaving a portion of the surface (a second major surface) of the foamed film as a substrate to support additional layers or structures.
  • the skin adhesive can also be laminated to a surface of the foamed film, or the foamed film can be directly extruded or coated onto the skin adhesive layer after the skin adhesive layer has been applied to a release liner.
  • the skin adhesive layer may employ multiple adhesive layers.
  • the skin adhesive layer has a lower concentration of thermally conductive filler than the foamed film so that adhesion can be maximized. In general, as the amount of thermally conductive filler increases, adhesive properties decrease.
  • an extrusion process 300 is shown for preparing a foam TIM according to the invention.
  • hot melt PSA polymer is fed into a first extruder 310 (typically a single screw extruder) to soften and mix the polymer into a form suitable for extrusion.
  • the resulting polymer will be used to form the polymer matrix of the foamed film.
  • the polymer may be added to the extruder 310 in any convenient form, such as pellets, billets, packages, strands, pouches, and ropes.
  • the thermally conductive filler, and when present, tackifying resin, fire retardant, microfiber forming material, and other additives are fed to a second extruder 312 (e.g., typically a twin screw extruder).
  • the hot melt PSA polymer may be fed directly from the extruder 310 into second extruder 312 through the first port 311 .
  • the thermally conductive filler and other additives can be fed into any port and are typically fed into the second extruder 312 at entrance 313 which is typically at a point prior to the mixing/dispersing section of the extruder 312 .
  • the hot melt PSA polymer and additives are well mixed in extruder 312 .
  • the order of component addition and mixing conditions are selected to achieve optimum mixing. Generally, mixing is carried out at a temperature below the threshold temperature required to expand the microspheres, when such microspheres are present. However, temperatures higher than the microsphere expansion temperature may be used, in which case the temperature is typically decreased following mixing and prior to the addition of the microspheres to the extruder 312 . It will be appreciated that if the hot melt PSA polymer is provided in a form suitable for extrusion, the first extrusion step may be omitted and the polymer added directly to extruder 312 .
  • the filler is added to the extruder through multiple addition ports (i.e., split feed, not shown) and that vacuum via port 309 be used to remove entrapped air.
  • void volume may be caused by entrapped gases, chemical blowing agents, physical blowing agents, and microspheres.
  • the expandable polymeric microspheres may be added to the second extruder 312 , typically in a separate zone at downstream entrance 313 typically immediately prior to a conveying zone of extruder 312 .
  • the thermally conductive filler, expandable polymeric microspheres, the hot melt PSA polymer, and the optional fire retardant and/or microfiber forming material are melt-mixed in the conveying zone to form an expandable extrudable composition.
  • the purpose of the melt-mixing step is to prepare an expandable extrudable composition in which the thermally conductive filler, microspheres and other additives, if present, are distributed throughout the molten polymer.
  • melt-mixing operation uses one conveying block downstream from entrance 313 to obtain adequate mixing, although kneading elements may be used as well.
  • the temperature, pressure, shear rate, and mixing time employed during melt-mixing are selected to prepare an expandable extrudable composition without causing the microspheres to expand or break.
  • zone temperatures, pressures, shear rates, and mixing times are selected based upon the particular chemical compositions being processed, and the selection of these conditions is within the skill of those practicing in the field.
  • the expandable extrudable composition is metered into extrusion die 314 (e.g., a contact or drop die) through transfer tubing 318 using a gear pump 316 .
  • the temperature within multi-layer die 314 is maintained at substantially the same temperature as the temperature within transfer tubing 318 .
  • the temperature within die 314 is at or above the temperature required to cause expansion of the expandable microspheres. While extrusion die 314 is shown in FIG. 4 as a multi-layer die, it is understood that die 314 can be a single layer die.
  • the pressure within the transfer tubing 318 is usually high enough to prevent the microspheres from expanding during the time they reside within the tubing 318 .
  • the volume within the die 314 is greater than the volume within the tubing 318 so that material flowing from the tubing 318 into the die 314 experiences a pressure drop to a pressure below that within transfer tubing 318 .
  • the expandable extrudable composition enters the die 314 , the drop in pressure and the heat within the die 314 will cause the polymeric microspheres to begin expanding. As the microspheres begin to expand, the expandable extrudable composition forms a foam.
  • the pressure within the die 314 will continue to decrease as the expandable extrudable composition approaches the exit port 315 of the die 314 .
  • the continued decrease of pressure contributes to the further expansion of the microspheres within the die.
  • the flow rate of polymer through the extruder 312 and the die 314 are maintained to keep the pressure in the die cavity sufficiently low to promote the expansion of the expandable microspheres before the expandable polymer composition exits the die 314 .
  • the shape of die 314 may be chosen or fashioned to provide a desired shape for the foam TIM. Any of a variety of foam shapes may be produced, including continuous or discontinuous sheets or films. Those skilled in the art will appreciate that chemical blowing agents and the like are also useful in the manufacture of foams according to the invention, either in place of the expandable microspheres or in combination with the microspheres.
  • the smoothness of one or both of the foamed film surfaces can be increased by using nip roll 317 to press the foamed film against a chill roll 319 after the foamed film exits die 314 , or by using smooth liners on each of the foamed film surfaces and passing the composite article through a nip. Smoothness of the surface(s) is beneficial for good surface contact and adhesion. It is also possible to emboss a pattern on one or both surfaces of the foamed film by contacting the foam with a patterned roll after it exits die 314 or by using a patterned or microstructured liner, such as those described in, for example, U.S. Pat. No. 6,197,397 B1.
  • Non-contact or non-bonded areas do not conduct heat and reduce the overall thermal conductivity of the foam TIM.
  • Patterned foam TIMs facilitate egress of air and result in improved adhesive contact.
  • the improved softness and conformability of a foam TIM versus a non-foam TIM also contributes to improved adhesive contact.
  • the extrusion process can also be used to prepare patterned foamed films having areas of different densities.
  • the film can be selectively heated, e.g., using a patterned roll or infrared mask, to cause differential or regional expansion of microspheres within designated areas of the foamed film.
  • the thermally conductive foamed film is combined with one or more skin adhesive layers; in other embodiments, one or more thermally conductive skin adhesive layers, applied to the outer surfaces of the foamed film.
  • the thickness of the skin adhesive layer is typically from about 0.025 mm (1 mil) to about 0.125 mm (5 mils); and in other embodiments, from about 0.025 mm (1 mil) to about 0.076 mm (3 mils).
  • FIG. 4 shows such a co-extrusion process.
  • Adhesive for the skin adhesive layer is introduced to the system by adding an adhesive polymer to the extruder 330 (e.g., a single screw extruder) where the polymer is softened before it is fed to a second extruder 332 (e.g., typically a twin screw extruder) where the polymer is mixed with thermally conductive filler and other additives, if any.
  • the adhesive typically a PSA
  • the thermally conductive adhesive is formulated without adding other additives that diminish the adhesive properties or the tackiness of the adhesive.
  • fire retardant materials are normally excluded from the formulation for the adhesive, small amounts of fire retardant may also be included within the adhesive at concentrations that are effective to impart fire retardant properties to the adhesive, while not significantly diminishing the tack of the adhesive. Specifically, it may be desirable to add a small amount of fire retardant to the skin adhesive in very thin (i.e., ⁇ 0.635 mm ( ⁇ 0.025 inches)) thermally conductive fire retardant foam TIMs.
  • the amount of fire retardant added to the skin adhesive layer is no greater than about 30 weight percent of the total weight of skin adhesive, no greater than about 20 weight percent, no greater than about 10 weight percent, or no greater than about 5 weight percent.
  • a formable or extrudable adhesive composition is metered from the extruder 332 to the appropriate chambers of die 314 through transfer tubing 334 using a gear pump 336 .
  • the adhesive is co-extruded with the foam through an exit port 315 on the die 314 so that the adhesive is applied directly to the outer surface of the foamed film.
  • the foamed film is provided in a sheet form having two major outer surfaces thereon, the adhesive may be applied to the foamed film on either or both of the major outer surfaces.
  • Co-extrusion methods for coating an article with adhesive are known to those in the art and need not be further explained here. Other methods can be used for applying the skin adhesive layer, such as for example, direct coating, spray coating, pattern coating, laminating, and the like.
  • the resulting foam TIM is a three-layer article featuring a foamed film core with a skin adhesive layer on each of the major surfaces of the foamed film.
  • a skin adhesive layer for a three layer A/B/C construction (adhesive A/foam B/adhesive C)
  • another extruder and related equipment can be employed to permit another thermally conductive skin adhesive to be applied to the other major surface of the foam.
  • the major surfaces of the foam TIM may be adhered to any of a variety of surfaces for use in applications where the thermally conductive properties of the foam TIM are desired and/or required.
  • the absence of fire retardant in the skin adhesive layer allows the thermally conductive foamed film to be adhered to a surface or substrate with the maximum degree of adhesion provided by the particular skin adhesive used.
  • Suitable skin adhesives for use in the articles of the present invention include any adhesive that provides acceptable adhesion to a variety of polar and/or non-polar substrates.
  • PSAs are generally acceptable.
  • Suitable PSAs include those based on acrylic polymers, polyurethanes, thermoplastic elastomers, such as those commercially available under the trade designation KRATON (e.g., styrene-isoprene-styrene, styrene-butadiene-styrene, and combinations thereof) and other block copolymers, polyolefins, such as poly-alpha-olefins and amorphous polyolefins, silicones, rubber based adhesives (including natural rubber, polyisoprene, polyisobutylene, butyl rubber, etc.) as well as combinations or blends of these adhesives.
  • KRATON e.g., styrene-isoprene-styrene,
  • the thermally conductive skin adhesive may contain tackifiers, reinforcing resins, plasticizers, rheology modifiers, fillers, fibers, crosslinkers, antioxidants, dyes, colorants, as well as active components, such as an antimicrobial agent.
  • a group of PSAs known to be useful in the present invention are, for example, the acrylate copolymers described in, for example, U.S. Pat. No. RE 24,906, incorporated herein by reference, and particularly a copolymer comprising a weight ratio of from about 90:10 to about 98:2 iso-octyl acrylate:acrylic acid copolymer. Also acceptable is a copolymer comprising a weight ratio of about 90:10 to about 98:2 2-ethylhexyl acrylate:acrylic acid copolymer, and a 65:35 2-ethylhexyl acrylate:isobornyl acrylate copolymer.
  • Useful adhesives are described in, for example, U.S.
  • a release liner 320 may be applied to the thermally conductive skin adhesive layer or layers disposed on either or both of the major surfaces of the foam.
  • the liner 320 can be dispensed from a feed roll 322 .
  • Suitable materials for liner 320 include silicone release liners, release coated polyester films (e.g., polyethylene terephthalate films), and polyolefin films (e.g., polyethylene films). The liner and the foam are then laminated together between nip rollers 324 .
  • Optional release liner 340 can be added to the opposing surface of the foam by positioning optional second feed roll 342 near one of the nip rolls 324 .
  • the second release liner 340 may be the same as or different from the release liner 320 .
  • the second release liner 340 may be provided with a layer of a thermally conductive adhesive coated or applied to one surface of the release liner 340 .
  • a second thermally conductive adhesive layer (not shown) may be applied to the second major surface of the foam material.
  • the second thermally conductive skin adhesive layer may be the same as or different from the aforementioned co-extruded adhesive.
  • the thermally conductive skin adhesive layers will comprise thermally conductive PSAs.
  • Release liners 320 , 340 may also be provided with a layer of a thermally conductive adhesive coated or applied to one of its surfaces.
  • multilayered foam TIMs are to be considered within the scope of the invention.
  • the foregoing co-extrusion process can be conducted so that a one or two-layer TIM is produced, or to produce TIMs having three or more layers (e.g., 10-100 layers or more) by equipping a single layer die with an appropriate feed block, or by using a multi-vaned or a multi-manifold die.
  • Multilayered TIMs can also be prepared by laminating additional layers (e.g., polymer layers, metals, metal foils, scrims, paper, cloth, adhesives coated on a release liner, etc.) to the foamed film, or to any of the co-extruded polymer layers after the article exits die 314 .
  • additional layers e.g., polymer layers, metals, metal foils, scrims, paper, cloth, adhesives coated on a release liner, etc.
  • Other techniques which can be used include pattern coating.
  • the thermally conductive foam film(s) in the TIMs of the invention can be thick, i.e., greater than or equal to 0.25 mm (0.010 inches) or thin (i.e., ⁇ 0.025 mm (0.010 inches).
  • the foam TIM is optionally exposed to radiation from an E-beam source 326 to crosslink the foam TIM for improved cohesive strength.
  • E-beam source 326 Radial Beam source 326
  • Other sources of radiation e.g., ion beam and gamma radiation
  • the optional second release liner 340 can be rolled up onto a take-up roll 329 , and the laminate is rolled up onto a take-up roll 328 .
  • the TIM could be gamma irradiated after being wound into a roll.
  • the release liners are typically coated with release agents, such as fluorochemicals or silicones.
  • release agents such as fluorochemicals or silicones.
  • U.S. Pat. No. 4,472,480 describes low surface energy perfluorochemical liners.
  • Suitable release liners include papers, polyolefin films, or polyester films coated with silicone release materials. Polyolefin films may not require release coatings when used with acrylic based PSAs. Examples of commercially available silicone coated release liners are POLYSLIKTM silicone release papers (available from James River Co., H. P. Smith Division, Bedford Park, Ill.) and silicone release papers supplied by DCP-Lohja (Dixon, Ill.) now known as Loparex, Inc. (Willowbrook, Ill.).
  • Other types of E-beam stable, contaminant free release liners are also useful in the invention, such as those described in pending, for example, U.S. Patent Publication No. 02-0155243-A1, assigned to the assignee of this application, and incorporated in its entirety herein by reference.
  • the foam TIMs of the invention may be used in a variety of applications, including aerospace, automotive, electronic, and medical applications.
  • the foam TIMs of the invention are typically used to join processors and components to heat dissipating devices (for example, heat sinks and spreaders).
  • the properties of the TIMs may be tailored to meet the demands of the desired applications. Specific examples of applications include adhesive tapes, pads, or sheets, vibration damping articles, tape backings, gaskets, spacers, and sealants.
  • sample dimensions are approximate except for the width wherein the width was measured to the accuracy of the cutting tool.
  • Density was determined according to ASTM D 792-86 “Standard Test Method for Density and Specific Gravity (Relative Density) of Plastics by Displacement.” Samples were cut into approximately 2.54 cm ⁇ 2.54 cm (1 inch (in) ⁇ 1 inch (in)) specimens and weighed on a high precision balance available as Model AG245 from Mettler-Toledo, Gillersee, Switzerland. The volume of each sample was obtained by measuring the mass of water displaced at room temperature (23° C.+/ ⁇ 1° C.). The buoyancy of each sample was measured in grams (g) using a special attachment for the balance. The density (D meas. ) of the sample was taken to be its mass divided by its buoyancy, assuming the density of water at 23° C. to be 1 g/cc.
  • composition (weight percent adhesive component ⁇ D meas. of adhesive component)+(weight percent first filler component ⁇ D theor. of first filler component)+(weight percent second filler component ⁇ D theor. of second filler component)+(weight percent third filler component ⁇ D theor. of third filler component), etc.
  • the reported % Void Volume includes the void volume contribution of expanded polymeric microspheres and/or entrapped gas and/or chemical blowing agents and/or physical blowing agents.
  • a 2.54 cm (1 in) wide by about 3.81 cm (1.5 in) long sample was cut from the article to be tested and pressed onto a solvent-washed (one wash of acetone followed by three washes of heptane), dry, 0.508 cm (2 in) wide by 7.62 cm (3 in) long, Type 304 stainless steel substrate panel and the sample was centered on one end of the panel.
  • the 5.1 cm (2 in) tab was then folded around a triangular clip, wrapped with masking tape, and stapled so that a weight could be attached to the test specimen.
  • a 1000 g weight was used to test samples at room temperature and a 500 g weight was used to test samples at 70° C. (158° F.). The sample thus prepared was allowed to dwell at room temperature and approximately 50% relative humidity for approximately 24 to 72 hours.
  • the test specimen was then placed in a Static Shear standard fixture having a 2 degree angle back slant. The fixtured specimen was then either tested at room temperature (about 22° C.) or in a forced air oven set at 70° C. ⁇ 3° C. (158° F.). The elevated temperature test specimen was then given a 10 minute warm up period before attaching the 500 g weight. The test was run until the test specimen failed or 10,000 minutes elapsed. Failure time was recorded.
  • Tensile and elongation was determined according to ASTM D412-98a “Standard Test Methods for Vulcanized Rubber and Thermoplastic Elastomers-Tension.”
  • a silicone release liner was applied to the exposed surface of the article which already had a liner on one side.
  • a sample was cut using Die E in the machine direction from the article to be tested to form the test specimen.
  • Sample thickness was measured in the center of each specimen using an AMES gauge having a force of 0.1 kg (3.5 oz) and a 0.0635 cm (0.25 in) diameter foot.
  • the tensile tester was set up with the following conditions:
  • the initial gauge length was set at 8.89 cm (3.5 in) by separating the instrument clamping jaws to this length and the sample was centered horizontally between the jaws so that an approximate equal length of sample was held by each jaw.
  • the sample was tested at a crosshead speed of 51 cm/min (20 in/min) until the sample broke or reached the maximum extension of the machine (101.6 cm (40 in)).
  • the tensile strength in pounds (and later converted to kilograms) and elongation distance were recorded.
  • the percent elongation was determined by dividing the elongation distance by the initial gap distance times 100. Eleven replicates were tested, except where noted, and averaged to provide the thickness, Peak Load, Peak Stress, Percent (%) Strain at Peak Stress, Break Load, % Strain at Break, Energy at Break, and Modulus.
  • a silicone release liner was applied to the non-liner side of the article.
  • a 1.27 cm (0.5 in) wide by about 12.7 cm (5 in) long sample was cut in the machine direction from the article to be tested to form the test specimen.
  • One liner was removed and a 2.54 cm (1.0 in) length was measured and marked in the center of test specimen to provide the initial gap distance.
  • a 2.54 cm (1 in) wide by about 7.62 cm (3 in) piece of masking tape was placed across the foam article by positioning the tape edge on the both marks so that the 2.54 cm (1 in) long section that was marked off did not have tape covering it.
  • the other liner was then removed and masking tape was wrapped completely around the article, making sure to keep the masking tape aligned across the article.
  • the tape was used to prevent the sample from adhering to the INSTRON jaws and prevent the sample from breaking at the point where it was clamped by the jaws.
  • the INSTRON was set up with the following conditions:
  • test specimen was then positioned in the INSTRON jaws so that the jaws lined up with the edge of the masking tape.
  • the sample was tested at a crosshead speed of 25.4 cm/min (10 in/min) until the sample broke.
  • the tensile break strength or peak load was recorded in pounds (and later converted to kilograms) and elongation distance was recorded.
  • the percent elongation at break was determined by dividing the elongation distance by the initial gap distance times 100. One specimen per sample was tested.
  • a 25.4 mm (1 in) or a 12.7 mm (0.5 in) wide by about 127 mm (5 in) long sample was cut from the article to be tested and laminated to an about 15.24 mm (6 in) long by about 28.6 mm (1.125 in) wide by 0.025 mm (0.001 in) thick primed polyester film by rolling down the article onto the primed side of the polyester film, taking care not to trap air bubbles between the film and the article.
  • the 12.7 mm (0.5 in) wide sample was similarly laminated to an about 152.4 mm (6 in) long by about 15.8 mm (0.625 in) wide by 0.025 mm (0.001 in) thick primed polyester film.
  • the laminate was then positioned on either a solvent-washed (one wash of acetone followed by three washes of heptane), dry, 51 mm (2 in) wide by about 127 mm (5 in) long, Type 6061-T6 alloy bare standard aluminum panel or a solvent-washed (three washes of isopropyl alcohol), dry 51 mm (2 in) wide by about 127 mm (5 in) long polypropylene panel, so that the laminate was centered on the panel with a portion of the laminate extending off the panel to serve as a tab.
  • the laminate was rolled down onto the panel using a 2 kg (4.5 lb) hard rubber roller, with one pass in each direction. Care was taken not to trap bubbles between the panel and the laminate.
  • the sample thus prepared was allowed to dwell at room temperature (about 22° C.) for about 24 hours. Then the sample was tested at room temperature (about 22° C.) for 90 Degree Peel Adhesion by Method A (for polypropylene panels) or Method B (for aluminum panels) described below.
  • Method A The sample was tested at crosshead speed of 30 cm/min (12 in/min) using an IMASS tester fitted with a 4.5 kg (10 lb) load cell. The peel value obtained from the first 0.51 cm (0.2 in) length of peel was ignored. The peel value of the next 5.08 cm (2 in) or “peel area” was recorded as an integrated average value. The values reported were the average of 3 replicates.
  • Method B The sample was tested at crosshead speed of 30 cm/min (12 in/min) using a SINTECH 5/GL Instron tester fitted with a 45 kg (100 lb) load cell. The peel value obtained from the first 1.27 cm (0.5 in) length of peel was ignored. The integrated average peel value of the next 89 mm (3.5 in) or “peel area” was recorded. The values reported were the integrated average peel adhesion values of three replicates.
  • a 12.5 mm (0.5 in) wide by 127 mm (5 in) long strip was cut from the test sample such that the length was cut in the machine direction of the sample.
  • One strip was laminated to a 50.8 mm (2 in) wide ⁇ 127 mm (5 in) long aluminum or glass panel such that the strip was approximately 0.635 cm (0.25 in) from one of the long edges of the panel and approximately 25.4 mm (1.0 in) of the strip extends beyond the end of the panel. Care was taken to ensure maximum wet-out of or contact between the strip and the panel. It was desired that 100% contact be achieved.
  • a second like panel i.e., aluminum to aluminum or glass to glass
  • the bonded sample was allowed to dwell for between 24 hours and 72 hours at room temperature (about 22° C.).
  • test strips were pulled by hand at a speed of about 30 cm/min (about 12 in/min) in a direction substantially parallel to the panels to initiate stretch release removal until the bond failed. Only the glass panels were visually examined for the presence of residue and the failure mode was recorded. A sample was rated as “Pass” if there was complete removal from the panel. A sample was rated as “Fail” if the sample could not be completely removed.
  • the thermal impedance of single layers of the disclosed invention was measured according to ASTM C-1114 Test Method “Steady-State Thermal Transmission Properties by Means of the Thin-Heater Apparatus.”
  • FIG. 5 A diagram of the Thin-Heater Apparatus 500 is shown in FIG. 5 .
  • a small resistor 502 was used as the thin-heater.
  • the resistor used was a 10 ohm resistor in TO-220 package with an area of 0.806 cm 2 (0.125 in 2 ) (such as Caddock Electronics MP930).
  • a small hole was drilled through the back of the resistor into which a thin-wire thermocouple 504 was placed to measure the hot side temperature, T h .
  • a know amount of power, Q, was supplied from the precision power supply 506 (such as Hewlett Packard E3611A) by setting the current and voltage (Power current ⁇ voltage).
  • the sample to be tested 508 was placed onto a disposable test surface 509 and between the thin-heater and the cold aluminum test block 510 , cooled by running cold water through a cooling block 511 .
  • the cold test block had a thermocouple 512 for measuring the cold side temperature, T c .
  • the resistor was powered up and the temperature of the resistor was allowed to come to equilibrium. Temperatures T h and T c were recorded and the impedance and conductivity calculated according to ASTM C 1114 using the following relationships:
  • the thermal impedance was corrected for any heat loss off the top (horizontal) surface of the resistor (but not the sides of the sample) and reported as Z corr .
  • Z corr. Z uncorr. ⁇ [convective heat loss value of the resistor ⁇ (surface temperature T h of the resistor ⁇ room temperature)]
  • the thermal impedance (Z corr. ) was measured according to the above test method for samples of different thickness. The data was then plotted allowing for a finite value of the interfacial impedance. This plot method can be expressed as an equation:
  • Thermal bulk conductivity (k) was then calculated from slope of the line.
  • VA-24 film VA-24 film 0.0635 mm thick heat sealable, CT Film of Dallas, ethylene vinyl acetate TX copolymer film having 6% vinyl acetate Filler
  • BN boron nitride thermally conductive particle, Advanced Ceramics hexagonal form; theoretical Corporation, density of 1.80 Cleveland, OH; now known as GE Advanced Ceramics SiC silicon carbide thermally conductive filler; Washington Mills (SILICARIDE theoretical density of 3.10 Electro Minerals G-21, Grade p240) Corp., Niagara Falls, NY Al(OH) 3 Martinal ON 320 aluminum hydroxide, particle Albemarle size 20 microns, theoretical Corporation, Baton density of 2.40 Rouge, LA Mg(OH) 2 magnesium thermally conductive filler; Albemarle hydroxide theoretical density 2.40 Corporation F-100D Micropearl TM expandable polymeric Pierce Stevens, F-100D microspheres having a shell Buffalo, NY composition containing acrylonitrile and methacrylonitrile Exact 3040 Exact TM 3040 ethylene
  • PSA-A Pressure Sensitive Adhesive A
  • a pressure sensitive adhesive composition was prepared by mixing 95 parts 2-EHA, 5 part AA, 0.15 parts IRG 651, and 0.02 parts IOTG.
  • composition was placed into VA-24 film packages measuring approximately 100 mm by 50 mm by 5 mm thick, immersed in a water bath and exposed to UV radiation as described in U.S. Pat. No. 5,804,610.
  • Viscosity of PSA-A was 3980.73 Poise (P) as tested according to test method above.
  • This adhesive is believed to have a weight average molecular weight (M W ) of about 700,000 to about 1,200,000.
  • M W weight average molecular weight
  • the density of PSA-A was 0.98 g/cc.
  • PSA-A was fed to the feed port in barrel section 1 of a 30 mm co-rotating twin screw extruder with four ports (Werner Pfleider) operating at a screw speed set point of 200 rpm (actual speed about 176 rpm) via a 51 mm single screw extruder (Bonnot).
  • the temperature for all zones in the Bonnot extruder was set at 149° C. (300° F.).
  • Thermally conductive fillers as specified in Table 1 (parts by weight as specified in Table 1 per 100 parts by weight of PSA-A plus thermally conductive filler) were added as dry solids in one portion to a feed port in barrel section 5 of the twin screw extruder with a total flow rate of thermally conductive filler and PSA-A of about 3.18 kg/hr (7 lb/hr). F-100D microspheres at a concentration of 0.5 parts by weight per 100 parts by weight of PSA-A were added downstream to barrel section 7 . In all six temperature zones in the twin screw extruder, the temperature was set at 93.5° C. (200° F.). A vacuum (in a range from about ⁇ 77.9+/ ⁇ 10.2 newtons/sq.
  • the extrudate was pumped via the heated hose to a (15.24 cm (6 in) wide single layer drop die with a gap of about 0.114 cm (0.045 in).
  • the die temperature was set at 182° C. (360° F.).
  • the line speed was adjusted to provide the target thickness as specified in Table 1.
  • the extruded sheet was cast into a nip formed by a two chill rolls (one metal and one rubber), between two silicone coated polyester release liners. The temperatures of the chill rolls were set at 7.5° C. (45° F.). Each liner was a 0.051 mm (0.002 in) thick two sided, silicone-coated polyester liner, having different release materials (identified as 5035 and 7200) on each side, available from DCP-LOHJA Inc., Willowbrook, Ill., as 2-2PESTR(P2)-5035 and 7200. The extruded sheet contacted the 7200 side of one liner and the 5035 side of the other liner. The liner having 7200 release material in contact with the extruded sheet was removed and the resulting article was wound into a roll for subsequent crosslinking
  • the resultant article was then tested for physical properties, the Test Method outlined above.
  • the Thermal Bulk Conductivity for Examples 1-4 was 0.82, 0.95, 0.60, and 0.85 Watts/meter-K respectively.
  • An acrylic thermal interface composition was prepared using a blend of two thermally conductive fillers that also functioned as the foaming agent.
  • a thermally interface composition was prepared according to Examples 1-4 except that the conductive filler was a dry blend of 82 parts by weight of SiC and 18 parts by weight of BN and no expandable polymeric microspheres were used.
  • Example 5 The Thermal Bulk Conductivity of Example 5 was 0.97 Watts/meter-K.
  • thermoplastic elastomeric TIM was prepared using the blend of two thermally conductive fillers of Example 5.
  • the silicon carbide also acted as a chemical blowing agent.
  • the composition was coated at several thicknesses. The resultant article was not subjected to irradiation.
  • the total flow rate of the adhesive (i.e., Kraton D1107, WINGTACK PLUS tackifying resin, and SHELLFLEX 371N) was about 3.18 kg/hr (7 lb/hr).
  • the density of the adhesive was 0.96 g/cc.
  • Thermally conductive fillers as specified in Table 5 and 3 parts IRGANOX 1010 were added as a dry blend in one portion to a feed port in barrel section 5 at a flow rate of 2.60 kg/hr (5.73 lb/hr).
  • Zone 1 at 149° C. (300° F.), Zone 2 at 154.4° C. (310° F.), and Zones 3 to 6 at 160° C. (320° F.).
  • a vacuum in a range from about ⁇ 77.9+/ ⁇ 10.2 N/m 2 ( ⁇ 23+/ ⁇ 3 inches of mercury (Hg)) was applied through a port in barrel section 9 .
  • the temperature in the extruder adapters and the flexible hose at the exit end of the extruder were set at 160° C. (320° F.).
  • the flow rate was controlled with a heated Zenith melt pump, nominally 10.3 cc/rev, set at 160° C. (320° F.).
  • the extrudate was pumped via the heated hose to the single layer drop die of Examples 1-4.
  • the temperature of the die was set at 163° C. ⁇ 14° C. (325° F. ⁇ 25° F.).
  • the line speed was adjusted to provide the target thickness as specified in Table 5.
  • the extruded sheet was cast into a nip formed by a two chill rolls (one metal and one rubber), between two silicone coated polyester release liners of Examples 1-4.
  • the temperature of the chill rolls was set at 7.5° C. (45° F.).
  • One liner was removed and the resulting article was wound into a roll.
  • the TIM was then tested for physical properties according to the Test Methods outlined above. Results are given in Table 6. For the density calculation, the density of the thermoplastic elastomeric adhesive without thermally conductive filler was measured as 0.96 g/cc. The Thermal Bulk Conductivity of Example 6 was 0.84 Watts/meter-K.
  • Acrylic thermal interface compositions were prepared using various thermally conductive fillers.
  • PSA-B Pressure Sensitive Adhesive B
  • PSA-B A pressure sensitive adhesive composition (PSA-B) was prepared according to the preparation of PSA-A except that 97 parts 2-EHA, 3 part AA, and 0.01 parts IOTG was used in place of 95 parts 2-EHA, 5 parts AA, and 0.02 parts IOTG. Viscosity of PSA-B was 2215.2 P as tested according to test method above. This adhesive is believed to have a weight average molecular weight (M W ) of about 800,000 to about 1,300,000. The density of PSA-B was 0.98 g/cc.
  • the thermally conductive fillers were fed as dry solids into barrels 2 and 4 of the twin screw extruder, at feed rates of 2.27 kg/hr (4 lb/hr) and 2.73 kg/hr (6 lb/hr) respectively, using gravimetric feeders (K-Tron model T20, K-Tron, Pitman, N.Y.). Table 7 below provides amount and type of conductive filled added. This split feed arrangement was used to successfully obtain the required loading levels of the low bulk density filler. In addition, the vertical drop distances were kept as short as possible to avoid excess air entrapment. Each extrusion screw was composed of self-wiping and square channel double-flighted conveying elements of varying pitch (60 mm, 40 mm, and 30 mm).
  • the screws also contained 5-paddled kneading blocks, 50 mm in length, offset in three different arrangements: (1) 45 degrees in a forward (LI) direction, (2) 45 degrees in a reverse (RE) direction, or (3) 90 degrees in a neutral pattern.
  • the first 370 millimeters of the screw was composed of forward conveying, self-wiping elements (pitches of 30 and 60).
  • the first kneading section was located between 370-520 mm of the screw and consists of a forward, neutral, and reverse kneading block.
  • a conveying section (520-770 mm) and another kneading segment (770-920 mm) follow. This kneading section was composed of two forward blocks followed by a reverse block.
  • the remainder of the screw (920-1600 mm) is composed of self-wiping and square channel forward conveying elements of various pitches, generally following a declining trend in pitch (60 mm, 40 mm, 30 mm).
  • the twin screw extruder was operated with a screw speed set point of 200 rpm (actual speed about 200 rpm) at a temperature of 125° C. (257° F.) in all zones.
  • a vacuum (about ⁇ 94.81 kN/m2 ( ⁇ 28 inches of mercury (Hg)) was applied through an open port in Zone 8 to remove any volatiles and/or moisture.
  • large pitch forward conveying elements were used in the vacuum area to provide a lower degree of fill thereby maximizing polymer surface area.
  • the extrudate was pumped via a heated Normag melt pump, nominally 10.3 cc/rev, set at 125° C. (257° F.) through a 1.905 cm (0.75 in) diameter stainless steel neck tube set at 154.4° C. (310° F.) to the middle/center layer of a 4.17 cm (10 in) wide 3-layer Cloeren drop die, having a 0.102 cm (0.040 in) gap (available from The Cloeren Company, Orange, Tex.). The die temperature was set at 177° C. (350° F.). The line speed was adjusted to provide the target thickness as specified in Table 7.
  • the extruded sheet was cast onto the two side, silicone coated, polyester liner of Examples 1-4 in contact with a chilled cast roll.
  • the sheet was cast onto the 5035 side of 2-2PESTR(P2)-5035 and 7200 release liner.
  • the temperature of the cast roll was set at 7.5° C. (54° F.).
  • the resulting article was wound into a roll for subsequent crosslinking.
  • Samples were subjected to gamma radiation and were passed through the gamma processing unit of Examples 1-4.
  • Two sample pieces each received a target (actual measured) gamma dose of between about 30 kGy (31.6-31.7 kGy), 45 kGy (44.4-45.9 kGy), or 60 kGy (58.8-59.7 kGy).
  • Acrylic thermal interface compositions having stretch release properties provided by in situ microfiber formation were prepared using varying amounts of Exact 3040. Each composition was coated at several thicknesses.
  • PSA-B of Example 7 was fed to the feed port in barrel section 3 of the twin screw extruder of Examples 1-4 operating at a screw speed set point of 225 rpm (actual speed about 201 rpm) via Bonnot extruder of Examples 1-4 at a feed rate of 1.95 kg/hr (4.28 lb/hr).
  • the temperature for all zones in the Bonnot extruder was set at 149° C. (300° F.).
  • Thermally conductive fillers as specified in Table 10 (parts by weight as specified in Table 10 per 100 parts by weight of PSA-B plus thermally conductive filler) were added as dry solids in one portion to a feed port in barrel section 1 of the twin screw extruder of Examples 1-4.
  • the feed rates of thermally conductive filler and Exact 3040 were 2.12 kg/hr (4.67 lb/hr) and 0.65 kg/hr (1.43 lb/hr), respectively.
  • the flow rates of thermally conductive filler and Exact 3040 were 2.27 kg/hr (5.00 lb/hr) and 0.83 kg/hr (1.83 lb/hr), respectively.
  • the temperature was set at 149° C. (300° F.) except for Zone 4 which was set at 93.5° C. (200° F.).
  • a vacuum in a range from about ⁇ 77.9+/ ⁇ 10.2 N/cm 2 ( ⁇ 23+/ ⁇ 3 inches of mercury (Hg)) was applied through a port in barrel section 10 .
  • the temperatures in the three extruder adapters were 149° C. (300° F.) and the flexible hose at the exit end of the extruder were all set at 165.5° C. (330° F.).
  • the flow rate was controlled with a heated Zenith melt pump, nominally 10.3 cc/rev, set at 149° C. (300° F.).
  • the extrudate was pumped via the heated hose to the single layer drop die of Examples 1-4.
  • the die temperature was set at 182° C. (360° F.).
  • the line speed was adjusted to provide the target thickness as specified in Table 10.
  • the extruded sheet was cast into a nip formed by a two chill rolls (one metal and one rubber), between two silicone coated polyester release liners as in Examples 1-4.
  • the temperature of the chill rolls was set at 7.5° C. (45° F.).
  • One liner was removed as in Examples 1-4 and the resulting article was wound into a roll for subsequent crosslinking.
  • the resultant roll was subjected to gamma radiation at a measured gamma dose between 33.4 to 35.3 kGy (target was 30 kGy).

Abstract

In one aspect, the invention provides a foam thermal interface material comprising a foamed film, the film comprising a blend of polymeric hot melt pressure sensitive adhesive having a number average molecular weight of greater than 25,000 and at least 25 percent by weight of thermally conductive filler, said film having a void volume of at least 5 percent of the volume of said foamed film.

Description

    CROSS REFERENCE TO RELATED APPLICATIONS
  • This application is a continuation of U.S. application Ser. No. 10/449,679, filed May 30, 2003, now allowed, the disclosure of which is incorporated by reference in its entirety herein.
  • BACKGROUND
  • Integrated circuits, active and passive components, optical disk drives, and the like generate heat under use conditions that must be diffused to allow continuous use of the heat generating component. Heat sinks in the form of finned metal blocks and heat spreaders containing heat pipes are commonly attached to these heat generating components to allow excess heat to be conducted away and radiated into the atmosphere. Materials useful for providing a thermal bridge between the heat generating components and heat sinks/heat spreaders are known. Many of these materials are based on gel masses, liquid to solid phase change compounds, greases, or pads that must be mechanically clamped between a printed circuit board (PCB) and heat sink.
  • More recently, thermally conductive materials incorporating adhesives have been introduced. These thermally conductive adhesive materials typically form an adhesive bond between the heat generating component and heat sink/heat spreader so that no mechanical clamping is required. Both heat-activated (hot melt) and pressure sensitive adhesives have been used in thermally conductive adhesives. In all cases, these thermal interface materials need to be thermally enhanced (compared with unfilled or lightly filled polymer compositions), be dimensionally stable at elevated temperatures (heat generating components often run at 50° C. or higher), and be soft and conformable enough to provide good contact (wet-out) between the substrates. Typically, such thermally conductive adhesives have compromised thermal conductivity for softness/conformability or vice versa.
  • Articles incorporating a polymer foam core are characterized by the density of the foamed polymer being lower than the density of the pre-foamed polymeric matrix. The lowered density for the foam may be achieved in several known ways such as by foaming with chemical blowing agents or by interspersing microspheres within the matrix, the microspheres typically being made of glass or of certain polymeric materials, the former being detrimental to the softness/conformability of the foam.
  • Foams have been used to join two rigid substrates, or substrates with uneven or rough surfaces. However, heretofore, foams have not been used for thermal interface materials. It was believed that discontinuous voids in the thermal interface material should be avoided due to the insulating nature of such voids. Thus thermal conductivity was compromised.
  • In certain applications, a fire retardant feature may be needed and/or may be required by applicable regulations. For example, tapes to be used in electric or electronic applications may be directly exposed to electrical current, to short circuits, and/or to heat generated from the use of the associated electronic component or electrical device. Consequently, industry standards or regulations may impose conditions on the use of such tape articles that require qualifying tests be performed such as burn tests, and the like. For electrical and electronics applications, the industry standard flammability test is Underwriters Laboratories (UL 94 “Standard for Tests for Flammability of Plastic Materials for Parts in Devices and Appliances”).
  • In other applications, there is a need for rework/and or repair, such as for example, attaching an aluminum frame to a plasma display panel (PDP). In these applications, an easily removable attachment system such as a stretch-releasable attachment system would be beneficial.
  • Consequently, it is desirable to provide thermally conductive foams and thermally conductive adhesive interfaces that have acceptable thermal conductivity and are soft/conformable and methods for the manufacture of the thermal interface materials. It is also desirable to provide the foregoing thermally conductive articles in a fire retardant construction which optionally has stretch releasable properties.
  • SUMMARY
  • In one aspect, the invention provides a foam thermal interface material comprising a foamed film, the film comprising a blend of polymeric hot melt pressure sensitive adhesive having a number average molecular weight of greater than 25,000 and at least 25 percent by weight of thermally conductive filler, said film having a void volume of at least 5 percent of the volume of said foamed film.
  • In another aspect, the invention provides a thermal interface composition comprising polymeric hot melt pressure sensitive adhesive having a number average molecular weight of greater than 25,000, at least 25 percent by weight of thermally conductive filler, and an effective amount of a foaming agent.
  • In other aspects, the foam thermal interface materials and compositions of the invention may further comprise fire retardant and/or microfiber forming material.
  • In another aspect, the invention provides a method for preparing a foam thermal interface material, comprising:
      • (a) melt mixing a pressure sensitive adhesive (PSA) polymer, thermally conductive particles, and a foaming agent to form an expandable formable composition;
      • (b) activating the foaming agent;
      • (c) forming the formable composition into a foamed film having an outer surface; and
      • (d) optionally applying a thermally conductive adhesive composition onto the outer surface of the foamed film.
  • In still another aspect of the invention, the foaming agent can be activated after extruding the extrudable composition.
  • Other features and advantages of the invention will be apparent to those practicing in the art upon consideration of the Detailed Description, and from the appended claims.
  • BRIEF DESCRIPTION OF THE FIGURES
  • In describing the various features of the preferred embodiment, reference is made to the various figures, in which like reference numerals indicate like features and wherein:
  • FIG. 1 is a perspective drawing showing a thermal interface material of the invention.
  • FIG. 2 is a perspective drawing showing a second thermal interface material.
  • FIG. 3 is a perspective drawing of a thermal interface material featuring a continuous film combined with a thermally conductive adhesive layer.
  • FIG. 4 is a schematic drawing of an extrusion processor for preparing articles according to the invention.
  • FIG. 5 is a schematic diagram of the thin-heater test apparatus used in the Examples.
  • FIG. 6 is a plot of thermal impedance (Zcorr.) versus thickness (t) used to calculate bulk thermal conductivity in the Examples.
  • DETAILED DESCRIPTION
  • Certain terms are used herein in describing the preferred embodiment of the invention. All such terms are intended to be interpreted in a manner consistent with their usage by those skilled in the art. For convenience, by way of example and not limitation, the following meanings are set forth:
  • “Void volume” refers to the voids that there are present in the adhesive that are formed by activating a foaming agent contained in the adhesive.
  • “Fire retardant” refers to a substance that when applied to or incorporated within a combustible material, reduces or eliminates the tendency of the material to ignite and/or reduces the tendency to continue burning once ignited, when exposed to heat or flame.
  • “Stretch release” refers to the property of an adhesive article characterized in that, when the article is pulled and elongated from a substrate surface at a rate of 30 centimeters/minute and at an angle of 45° or less, the article detaches from a substrate surface without leaving a significant amount of visible residue on the substrate or when the article has been used between two rigid substrates, the article is pulled and elongated at a rate of 30 centimeters/minute and at an angle of 5° or less, the article detaches from a substrate surface without leaving a significant amount of visible residue on at least one of the rigid substrates.
  • “Substantially continuous” refers to a microfiber that is unbroken for at least about 0.5 cm in the machine direction.
  • “Substantially free” refers to a component that is present in a thermal interface material (TIM) of the invention at levels of less than 0.1, 0.09, or 0.08 percent by weight, based on the weight of the polymeric hot melt PSA.
  • The invention provides foam thermal interface materials (foam TIMs) comprising a thermally conductive filler and a hot melt pressure sensitive adhesive (PSA) polymer foam (or foamed film) that is desirably substantially free or free of oligomers or low molecular weight polymers, other than residuals resulting from polymerization of the PSA, (that is, <25,000 number average molecular weight), N-tert-butylacrylamide, organic solvent, added free radical initiators, and crosslinking agents. The foamed film may also comprise one or more polymer microspheres capable of further expansion when heated. The outer surface of the foamed film may be substantially smooth or it may be patterned, and the foamed film may be provided in any of a variety of configurations including sheets, rods, or cylinders. At least a portion of the outer surface may serve as a substrate for films, adhesive layers, and the like, thus providing any of a variety of tape/TIMs. The foamed film of the TIMs of the invention contain at least about 5 percent void volume as determined by the test method described herein.
  • The desired characteristics of a foam TIM according to the invention include one or more of the following: (1) bulk thermal conductivity of at least about 0.5 Watts/meter-K; (2) Shore A hardness less than about 60; (3) static shear strength at 22° C. or 70° C. of at least about 10,000 minutes when tested according to the test methods described below; and (4) when the TIM comprises viscoelastic microfibers, the tensile break strength of at least about 150% of the yield strength of the TIM with an elongation greater than about 200%, and less than about 50% recovery after being elongated 100%, and when the TIM comprises elastic microfibers, the TIM has an elongation greater than about 200% and have greater than about 50% recovery after being elongated 100%. Foam TIMs comprising the continuous adhesive film and/or the optional skin adhesive layer(s) applied to the surfaces of the foam PSA film can have a high adhesion when applied to a panel, such as 90 degree peel adhesion of greater than about 0.0438 kN/m (4 oz/in), in other embodiments, greater than about 0.176 kN/m, or greater than about 0.352 kN/m.
  • The polymeric hot melt PSA useful in the invention has a number average molecular weight of greater than 25,000, particularly, a number average molecular weight of greater than 100,000, and more particularly a number average molecular weight of greater than 200,000, and even more particularly a number average molecular weight of greater than 400,000 (as defined in Introduction to Physical Polymer Science, Chapter 1, page 6, L. H. Sperling ISBN 0-471-89092-8). The polymeric hot melt PSA may be selected from any of a variety of polymeric materials, such as rubbers, elastomers, thermoplastic polyurethanes, thermoplastic elastomers, poly-alpha-olefins, synthetic rubbers, acrylate polymers and methacrylate polymers, acrylate and methacrylate copolymers, and combinations of the foregoing. The optional thermally conductive adhesive layer may be a PSA, such as, for example, poly-alpha-olefin adhesive, acrylic acid adhesive, a rubber based adhesive, a silicone adhesive, a blend of rubber based adhesive and acrylic adhesive, and combinations thereof. Likewise, the optional thermally conductive adhesive layer may be a heat-activated adhesive. The continuous foamed film and/or the optional thermally conductive adhesive layer may be provided with substantially continuous, individual polymeric microfibers therein and oriented in the machine direction, the microfibers imparting stretch release properties to the article. In addition, the continuous film and/or optional thermally conductive adhesive layer may comprise a fire retardant.
  • One example of a foam TIM according to the invention is shown in FIG. 1. The foam TIM 10 comprises a foamed film 11 having a first flat surface 12 and a second surface (not shown) opposite the first surface 12. According to the invention, at least one thermally conductive filler 15 is interspersed throughout a polymeric adhesive matrix 16. The foamed film 11 comprises a polymer adhesive matrix 16 with a plurality of voids 14 interspersed within the matrix. The voids 14 are the result of the foaming process used in the manufacture of the film 11 and may be created through the use, for example, of blowing agents or by the inclusion of expandable polymeric microspheres or combinations thereof. If expandable microspheres are included in the manufacture of the foamed film 11, the voids 14 typically comprise the polymer microspheres in an expanded and unbroken form and provide a void volume of at least 5%.
  • It will be appreciated that other layers and/or structures may be applied or affixed to the first surface 12 of the foamed film 11. In associating other layers or structures with the surface 12, a layer of a thermally conductive skin adhesive may first be applied to the first surface 12 to bond the additional layers or structures to the surface 12. Likewise, the foamed film 11 may be provided as a two-sided tape TIM having another adhesive layer, in particular a thermally conductive adhesive layer, on surface opposite the first surface 12. A release liner or the like may be associated with the thermally conductive skin adhesive(s) on either or both of the surfaces of the foamed film 11.
  • FIG. 2 shows foam TIM 100 in the form of a foamed film 101 having a first surface 102 and a second surface opposite the first surface (not shown). According to this embodiment of the invention, foam TIM 100 comprises a foamed film 101 comprising at least one thermally conductive filler 105, a plurality of voids 104, and individual, substantially continuous viscoelastic and/or elastic microfibers 108 interspersed throughout polymeric adhesive matrix 106 and oriented in the machine direction. Microfibers 108 are typically formed in situ during the manufacture of the TIM and are oriented in the machine direction. It will be appreciated that other layers and/or structures may be applied or affixed to the surfaces 102 of the foamed film 101.
  • The polymeric hot melt PSAs (prior to compounding with thermally conductive filler) useful in the invention have a number average molecular weight of greater than 25,000 and is tacky at room temperature (about 22° C.). PSAs are a distinct category of adhesives which in dry (solvent-free) form are permanently tacky at room temperature. They firmly adhere to a variety of dissimilar surfaces upon mere contact without the need of more than finger or hand pressure. PSAs require no activation by water, solvent, or heat to exert a relatively strong adhesive holding force. PSAs can be quantitatively described using the “Dahlquist criteria” which maintains that the elastic modulus of these materials is less than 106 dynes/cm2 at room temperature. See Pocius, A. V., Adhesion & Adhesives: An Introduction, Hanser Publishers, New York, N.Y., First Edition, 1997. The foams of the invention may comprise one or more PSAs. It may be desirable to use two or more PSA polymers having different compositions to achieve unique foam properties. A wide range of foam physical properties can be obtained by selectively choosing the PSA component types and concentrations. A particular polymer may be selected based upon the desired properties of a final material.
  • The hot melt PSA may be any of a variety of different polymer materials including elastomers, rubbers, thermoplastic elastomers, poly-alpha-olefin adhesives, acrylic adhesives, and blends thereof. Typically, the polymer resins are of the type that are suitable for melt extrusion processing, as described in U.S. Pat. No. 6,103,152, incorporated in its entirety herein by reference thereto. It may be desirable to blend two or more polymers having chemically different compositions. The physical properties of the foam can be optimized by varying the types of components used in creating the foam and by varying their relative concentrations. A particular hot melt PSA is generally chosen or selected based upon the desired properties of the final thermal interface material. It is recognized that the polymer material used to prepare the hot melt PSA may contain residual amounts of free radical initiators, oligomers or low molecular weight polymers (<25,000 number average molecular weight), or organic solvent.
  • Suitable materials for producing a useful hot melt PSA include acrylate and methacrylate polymers or co-polymers. Such polymers can be formed by polymerizing 50 to 100 parts by weight of one or more monomeric acrylic or methacrylic esters of non-tertiary alkyl alcohols, with the alkyl groups having from 1 to 20 carbon atoms (e.g., from 3 to 18 carbon atoms). Suitable acrylate monomers include methyl acrylate, ethyl acrylate, n-butyl acrylate, lauryl acrylate, 2-ethylhexyl acrylate, cyclohexyl acrylate, iso-octyl acrylate, octadecyl acrylate, nonyl acrylate, decyl acrylate, isobornyl acrylate, and dodecyl acrylate. Also useful are aromatic acrylates, e.g., benzyl acrylate and cyclobenzyl acrylate. In some applications, it may be desirable to use less than 50 parts by weight of the monomeric acrylic or methacrylic esters. Optionally, one or more monoethylenically unsaturated co-monomers may be polymerized with the acrylate monomers in amounts from about 0 to 50 parts co-monomer. One class of useful co-monomers includes those having a homopolymer glass transition temperature greater than the glass transition temperature of the acrylate homopolymer. Examples of suitable co-monomers falling within this class include acrylic acid, acrylamide, methacrylamide, substituted acrylamides, such as N,N-dimethyl acrylamide, itaconic acid, methacrylic acid, acrylonitrile, methacrylonitrile, vinyl acetate, N-vinyl pyrrolidone, isobornyl acrylate, cyano ethyl acrylate, N-vinylcaprolactam, maleic anhydride, hydroxyalkylacrylates, N,N-dimethyl aminoethyl(meth)acrylate, N,N-diethylacrylamide, beta-carboxyethyl acrylate, vinyl esters of neodecanoic, neononanoic, neopentanoic, 2-ethylhexanoic, or propionic acids (e.g., available from Union Carbide Corp. of Danbury, Conn., under the designation VYNATES), vinylidene chloride, styrene, vinyl toluene, and alkyl vinyl ethers.
  • A second class of useful co-monomers includes those having a homopolymer glass transition temperature less than the glass transition temperature of the acrylate homopolymer. Examples of suitable co-monomers falling within this class include ethoxyethoxy ethyl acrylate (Tg=−71° C.) and methoxypolyethylene glycol 400 acrylate (Tg=−65° C., available from Shin Nakamura Chemical Co., Ltd., under the designation NK Ester AM-90G).
  • Another group of polymers useful in the present invention includes pressure sensitive and hot melt adhesives prepared from non-photopolymerizable monomers. Such polymers can be adhesive polymers (i.e., polymers that are inherently adhesive), or polymers that are not inherently adhesive but are capable of forming adhesive compositions when compounded with tackifiers. Specific examples include polyurethanes, poly-alpha-olefins (e.g., polyoctene, polyhexene, and atactic polypropylene), block copolymer-based adhesives, natural and synthetic rubbers, silicone adhesives, ethylene-vinyl acetate, and epoxy-containing structural adhesive blends (e.g., epoxy-acrylate and epoxy-polyester blends), and combinations thereof.
  • In some instances, it may be desirable that the adhesive has a high service temperature (i.e., up to or greater than 70° C.). This can be accomplished in several known methods. For example, acrylic based adhesives can be crosslinked by irradiation by electron beam (E-beam), gamma, and the like. Block copolymer-based adhesives can have their elevated temperature performance improved through the addition of polyphenylene oxide (PPO) or an end block reinforcing resin to the block copolymer as described in U.S. Pat. No. 6,277,488, which is incorporated herein by reference.
  • A number of thermally conductive fillers are suitable for use in the adhesives of the invention. The thermally conductive filler is selected from a variety of materials having a bulk conductivity of between about 5 and 1000 Watts/meter-K as measured according to ASTM D1530. Examples of suitable thermally conductive fillers include but are not limited to, aluminum oxide, beryllia, zirconia, aluminum titanate, silicon carbide, boron carbide, silicon nitride, aluminum hydroxide, magnesium hydroxide, titanium dioxide, aluminum nitride, boron nitride, titanium nitride, and the like, and combinations thereof. These fillers are found in a variety of shapes/forms (spherical, flakes, agglomerates, crystals, acicular, fumed). The choice of shape is dependent upon the rheology of the selected adhesive resin and ease of processing of the final hot melt PSA/particle mix. Fillers may be available in several crystal types (e.g., hexagonal and rhombic boron nitride) and the type of crystal chosen will depend upon the thermal conductivity of the crystal (including the anisotropic nature of the conductivity along different crystal axes), effect of crystal type on final mechanical properties and cost.
  • Particle size and distribution will also affect mechanical and adhesive properties, so particle size selection should accommodate the final adhesive property requirements. In other embodiments, the particle size of the filler (or mixture of fillers) and particle loading are selected to produce suitable thermal conductance while retaining adequate mechanical properties.
  • Typically, useful thermally conductive particles have an average particle size in the range of from about 0.5 micrometers (μm) to about 250 micrometers. In other embodiments, the thermally conductive particles may range in average size from about 1 to about 100 micrometers and from about 10 to about 70 micrometers. The particles may range in average size in any range between 0.5 and 250 micrometers and may be any average size between 0.5 and 250 micrometers. The adhesive may contain thermally conductive particles that can bridge the adhesive and/or thermal interface matrix and be exposed through the matrix to a degree increasing with their size. Thus, particles are contained within the PSA and improve thermal conductivity in the path between the heat-source substrate and heat-conducting article, such as a heat sink article. These particles are of sufficient size to impinge near or against base of heat sink article such that they impress into or onto its surface prior to or after the heat sink article is placed in service. Generally, increasing the size of these particles to the same adhesive thickness will increase the thermal conductivity between a heat-source substrate and the heat-conducting article.
  • The choice of particle size depends on the application. For example, particles having a major dimension of at least about 1-2 μm and about 30 μm or below and in other embodiments, between about 5 and 20 μm, are suitable when the bond line will be in the 25 to 100 μm range (such as found between a central processing unit (CPU) and a heat sink). Particles larger than about 20 to 30 μm, such as 50 to 250 μm, are used where a larger gap exists between the hot and cold substrates. In addition, combinations of different particle size materials can be used. Larger conductive filler particle size results in higher bulk conductivity. When at least some of the selected particles are capable of being plastically deformed during heat sink article attachment, these particle sizes can be even larger than the sizes mentioned above. A mixture of particle sizes can result in improved packing density which improves the resultant conductivity. Combinations of different thermally conductive fillers have been shown to provide equivalent thermal performance at reduced costs by substituting a portion of an expensive filler (for example, boron nitride) with a less expensive filler (for example, silicon carbide). Thermally conductive fillers often have anisotropic thermal conductivity along various crystal planes, so filler orientation via known methods can be used to enhance thermal performance.
  • The thermally conductive particles may be present in the adhesive compositions of the invention in an amount of at least 25 percent by weight of the total composition. In other embodiments of the invention, the thermally conductive filler is present in an amount of at least about 30 weight percent, at least about 40 weight percent, and in some embodiments of the invention, at least about 50 weight percent. In other embodiments, thermally conductive fillers may be present in the adhesive blends of the invention in a range of from 25 to 80 weight percent, 30 to 80 weight percent, 40 to 80 weight percent, 50 to 80 weight percent, or any range between 25 and 80 weight percent.
  • While the maximum of thermally conductive filler is selected based on the final properties (e.g., hardness, conformability, adhesion, and thermal conductivity) of the article, the thermally conductive filler is generally present is an amount less than about 80 weight percent.
  • The foam thermal interface material has a bulk conductivity of at least about 0.5 Watts/meter-K; in other embodiments, the foam thermal interface material has a bulk conductivity of at least about 0.6 Watts/meter-K; and in other embodiments, at least about 0.8 Watts/meter-K.
  • Useful foaming agents include entrained gases/high pressure injectable gases; blowing agents, such as chemical blowing agents and physical blowing agents; expanded or unexpanded polymeric bubbles; and combinations thereof.
  • High pressure injectable gases are gases that are added to sealed mixing systems (e.g., a sealed extruder) at a pressure of greater than 20.67 MPa (3000 psi) to generate a foam upon existing the sealed system. Examples of high pressure injectable gases include nitrogen, air, carbon dioxide (CO2), and other compatible gases, and combinations thereof.
  • A physical blowing agent useful in the present invention is any naturally occurring atmospheric material which is a vapor at the temperature and pressure at which the foamed film exits the die. The physical blowing agent may be introduced into the polymeric material as a gas, liquid, or supercritical fluid. The physical blowing agent may be injected into the extruder system. A physical blowing agent is usually in a supercritical state at the conditions existing in the extruder during the process. If a physical blowing agent is used, it is preferable that it is soluble in the polymeric material being used. The physical blowing agents used will depend on the properties sought in the resulting foam articles. Other factors considered in choosing a blowing agent are its toxicity, vapor pressure profile, and ease of handling. Blowing agents, such as pentane, butane, and other organic materials, such as hydrofluorocarbons (HFC) and hydrochlorofluorocarbons (HCFC) may be used, but non-flammable, non-toxic, non-ozone depleting blowing agents are preferred because they are easier to use, e.g., fewer environmental and safety concerns. Suitable physical blowing agents include, for example, carbon dioxide, nitrogen, SF6, nitrous oxide, perfluorinated fluids, such as C2F6, argon, helium, noble gases, such as xenon, air (nitrogen and oxygen blend), and blends of these materials, hydrofluorocarbons (HFC), hydrochlorofluorocarbons (HCFC), and hydrofluoroethers (HFE).
  • Chemical blowing agents do not require an injection system as does a physical blowing agent and they can be used in virtually any extrusion system. Examples of chemical blowing agents include water and azo-, carbonate-, and hydrazide-based molecules including, e.g., 4,4′-oxybis(benzenesulfonyl)hydrazide, such as CELOGEN OT (available from Uniroyal Chemical Company, Inc., Middlebury, Conn.), 4,4′-oxybenzenesulfonyl semicarbazide, p-toluenesulfonyl semicarbazide, p-toluenesulfonyl hydrazide, oxalic acid hydrazide, diphenyloxide-4,4′-disulphohydrazide, benzenesulfonhydrazide, azodicarbonamide, azodicarbonamide(1,1′-azobisformamide), meta-modified azodicarbonides, 5-phenyltetrazole, 5-phenyltetrazole analogues, hydrazocarboxylates, diisopropylhydrazodicarboxylate, barium azodicarboxylate, 5-phenyl-3,6-dihydro-1,3,4-oxadiazin-2-one, sodium borohydride, azodiisobutyronitrile, trihydrazinotriazine, metal salts of azodicarboxylic acids, tetrazole compounds, sodium bicarbonate, ammonium bicarbonate, preparations of carbonate compounds and polycarbonic acids, and mixtures of citric acid and sodium bicarbonate, N,N′-dimethyl-N,N′-dinitroso-terephthalamide, N,N′-dinitrosopentamethylenetetramine, and combinations thereof. It has been found that silicon carbide available from Washington Mills Electro Minerals Corp., Niagara Falls, N.Y., under the trade designation of SILCARIDE G-21 Silicon Carbide Grade P240, functions as a chemical blowing agent as well as a thermally conductive filler. Additional chemical blowing agents are described in Klempner, D., Frisch, K.C. (editors), Handbook of Polymeric Foams and Foam Technology, Chapter 17, (Hansen, N.Y., 1991).
  • One or more expandable polymeric microsphere can be used as the foaming agent in the foamed thermally conductive film of the invention. An expandable polymeric microsphere comprises a polymer shell and a core material in the form of a gas, liquid, or combination thereof. Upon heating to a temperature at or below the melt or flow temperature of the polymeric shell, the polymer shell will expand. Examples of suitable core materials include propane, butane, pentane, isobutane, neopentane, or similar material, and combinations thereof. The identity of the thermoplastic resin used for the polymer microsphere shell can influence the mechanical properties of the foam, and the properties of the foam may be adjusted by the choice of microsphere, or by using mixtures of different types of microspheres. For example, acrylonitrile-containing resins are useful where high tensile and cohesive strength are desired in a low density foam article. This is especially true where the acrylonitrile content is at least 50 weight percent of the resin used in the polymer shell, generally at least 60 weight percent, and typically at least 70 weight percent. Examples of suitable thermoplastic resins which may be used as the shell include acrylic and methacrylic acid esters, such as polyacrylate; acrylate-acrylonitrile copolymer; and methacrylate-acrylic acid copolymer. Vinylidene chloride-containing polymers, such as vinylidene chloride-methacrylate copolymer, vinylidene chloride-acrylonitrile copolymer, acrylonitrile-vinylidene chloride-methacrylonitrile-methyl acrylate copolymer, and acrylonitrile-vinylidene chloride-methacrylonitrile-methyl methacrylate copolymer may also be used, but may not be desired if high strength is sought. In general, where high strength is desired, the microsphere shell will have no more than 20 weight percent vinylidene chloride and typically no more than 15 weight percent vinylidene chloride. High strength applications may require microspheres with essentially no vinylidene chloride. Halogen free microspheres may also be used in the foams of the invention. Examples of suitable commercially available expandable polymeric microspheres include those available from Pierce Stevens (Buffalo, N.Y.) under the designations F-30D, F-50D, F-80SD, and F-100D. Also suitable are expandable polymeric microspheres available from Expancel, Inc. (Duluth, Ga.) under the designations EXPANCEL 551, EXPANCEL 461, EXPANCEL 091, and EXPANCEL 092 MB 120. The selection of expandable polymeric microsphere is typically based on its expansion temperature and on the thermally conductive filler used.
  • The amount of foaming agent is selected to provide a void volume constituting at least 5% of the volume of the foamed film. In general, the higher the foaming agent concentration, the lower the density of the foamed film and the lower the thermal conductivity. That is, the higher the void volume, the lower the thermal conductivity of the foamed film. For example, the amount of microspheres in the polymer resin typically ranges from about 0.1 parts by weight to about 10 parts by weight (based upon 100 parts of polymer), in other embodiments, from about 0.5 parts by weight to about 5 parts by weight, and in other embodiments, from about 0.5 parts by weight to about 2 parts by weight.
  • The foam TIM contains at least about 5 percent void volume as determined by the test method described herein. In another embodiment, the foam TIM contains at least about 10 percent void volume as determined by the test method described herein. Generally, the foam TIM contains less than about 75 percent void volume, less than about 60 percent, or less than about 50 percent void volume due to influence of voids on thermally conductivity.
  • In certain applications, a fire retardant feature may be needed and/or may be required by applicable regulations. For example, tapes to be used in electric or electronic applications may be directly exposed to electrical current, to short circuits, and/or to heat generated from the use of the associated electronic component or electrical device. Consequently, industry standards or regulations may impose conditions on the use of such tape articles that require qualifying tests be performed, such as burn tests, and the like. For electrical and electronics applications, the industry standard flammability test is Underwriters Laboratories (UL 94 “Standard for Tests for Flammability of Plastic Materials for Parts in Devices and Appliances”). It is preferable that the foam TIM will pass UL 94 V-2 flammability rating and in other embodiments, will pass a UL 94 V-0 flammability rating.
  • Fire retardants suitable for inclusion in the foam TIMs of the present invention include any type of fire retardant which are generally present in the film at a concentration of between about 5 weight percent and about 40 weight percent based on the total weight of the foam TIM. The fire retardants can be intumescent fire retardants and/or non-intumescent fire retardants. Typically, the fire retardants are non-halogen containing and antimony-free. Examples of suitable fire retardants for use in the foam TIMs described herein include those commercially available from Clariant Corporation of Charlotte, N.C., under the designation EXOLIT, including those designated IFR 23, AP 750, EXOLIT OP grade materials based on organophosphorous compounds, and EXOLIT RP grades of red phosphorus materials non-halogenated fire retardants, such as FIREBRAKE ZB and BORGARD ZB, and FR 370 (tris(tribromoneopentyl) phosphate), available from Dead Sea Bromine Group, Beer Shiva, Israel. Examples of suitable fire retardants that also function as thermally conductive fillers include aluminum hydroxide and magnesium hydroxide.
  • Blends of one or more fire retardants and/or a synergist may also be used in the foam TIMs of the invention. Selection of the fire retardant system will be determined by various parameters, for example, the industry standard for the desired application, and by composition of the foamed film polymer matrix. In addition, the foam TIMs of the invention may contain smoke suppressants, such as those available under the trade designation Kemgard HPSS, 911A, 911B, and 911C, available from Sherwin-Williams Chemicals, Cleveland, Ohio.
  • To provide stretch release properties and to further reinforce the foam TIMs of the invention, the thermally conductive film, the thermally conductive skin adhesive or both the film and the skin adhesive will include microfiber forming materials that form viscoelastic and/or elastic microfibers formed in situ during the manufacturing process described herein. The individual microfibers are individual substantially continuous and dispersed throughout the adhesive polymer matrix and oriented in the machine direction of the film. It has been found that suitable microfibers include those formulated according to the teachings of pending U.S. Patent. Publication No. 02-0187294-A1, incorporated in its entirety herein by reference thereto. In foam TIMs of the invention, the individual microfibers are unbroken for at least about 0.5 centimeters (cm) in the machine direction, in other embodiments, at least about 2 cm, about 5 cm, or about 8 cm. In another aspect, the individuals substantially continuous microfibers generally have a maximum diameter of about 0.05 to about 5 micrometers, typically from about 0.1 to about 1 micrometer and the aspect ratio (i.e., the ratio of the length to the diameter) of the individual substantially continuous microfibers is greater than about 1000.
  • The foam TIM may also include a number of other additives other than materials expressly excluded above. Examples of suitable additives include tackifiers (e.g., rosin esters, terpenes, phenols, and aliphatic, aromatic, or mixtures of aliphatic and aromatic synthetic hydrocarbon resins), pigments, reinforcing agents, hydrophobic or hydrophilic silica, calcium carbonate, toughening agents, fibers, fillers, antioxidants, stabilizers, and combinations thereof. The foregoing additional agents and components are generally added in amounts sufficient to obtain an article having the desired end properties, in particular, adhesive properties. For good conformability and surface contact, it is preferred that the TIM has a hardness less than about 60 Shore A.
  • Other embodiments of the invention include tapes and transfer tapes. Useful backing materials are thermally conductive. Such backing materials can be inherently thermally conductive or may contain additive(s), such as those described under “Thermally Conductive Fillers” above, to impart thermal conductivity. Examples of suitable backing materials include cellulosic materials, such as paper and cloth (woven and nonwoven); films, such as polyester, polyvinyl chloride, polyurethane, polypropylene, and nylon; thermally conductive foam materials, such as polyethylene foams and acrylic foams; scrims; and metal foils, such as aluminum foil. In another embodiment, the backing material can be a release liner. In this embodiment, the backing does not need to be thermally conductive. The release liner can be coated on one or both sides with a release coating. The backing may also be provided as multiple layers.
  • Multilayer foam TIMs can also be prepared by laminating polymer or nonpolymer layers to a foamed film, or by layering extruded foamed films as they exit their respective shaping orifices, with the use of some affixing means, such as an adhesive. Other techniques that can be used include extrusion coating and inclusion coextrusion, which is described in, for example, U.S. Pat. No. 5,429,856, incorporated herein by reference.
  • FIG. 3 depicts yet another TIM 200 in which a thermally conductive skin adhesive layer 220 is provided on one of the surfaces 202 of the foamed film 201. Foamed film 201 comprises a polymer adhesive matrix 206 with a plurality of voids 204 and thermally conductive particles 205 interspersed within the matrix. The skin adhesive layer 220 may comprise any of a variety of adhesive materials and thermally conductive fillers as are further described herein. Typically, the skin adhesive layer 220 is a thermally conductive PSA formulated without fire retardant materials therein. A release liner (not shown) may optionally be included to protect the adhesive layer 220 prior to the application of the adhesive 220 to another substrate or the like.
  • In accordance with the principals of the invention, the aforementioned thermally conductive skin adhesive layer may be associated with the foamed film by, for example, co-extruding the extrudable foaming agent containing composition with one or more extrudable adhesive compositions, as described in greater detail, below. The thermally conductive adhesive compositions are generally formulated and/or selected without fire retardant to provide an adhesive article, such as a tape wherein the continuous foamed film forms the substrate for the tape. The adhesive may be applied to a portion of the surface of the continuous foamed film (e.g., on one of the major surfaces thereof), leaving a portion of the surface (a second major surface) of the foamed film as a substrate to support additional layers or structures. The skin adhesive can also be laminated to a surface of the foamed film, or the foamed film can be directly extruded or coated onto the skin adhesive layer after the skin adhesive layer has been applied to a release liner. The skin adhesive layer may employ multiple adhesive layers. Typically, the skin adhesive layer has a lower concentration of thermally conductive filler than the foamed film so that adhesion can be maximized. In general, as the amount of thermally conductive filler increases, adhesive properties decrease.
  • Referring to FIG. 4, an extrusion process 300 is shown for preparing a foam TIM according to the invention. According to the process of the invention, hot melt PSA polymer is fed into a first extruder 310 (typically a single screw extruder) to soften and mix the polymer into a form suitable for extrusion. The resulting polymer will be used to form the polymer matrix of the foamed film. The polymer may be added to the extruder 310 in any convenient form, such as pellets, billets, packages, strands, pouches, and ropes.
  • Next, the thermally conductive filler, and when present, tackifying resin, fire retardant, microfiber forming material, and other additives (except the expandable microspheres if present) are fed to a second extruder 312 (e.g., typically a twin screw extruder). The hot melt PSA polymer may be fed directly from the extruder 310 into second extruder 312 through the first port 311. The thermally conductive filler and other additives can be fed into any port and are typically fed into the second extruder 312 at entrance 313 which is typically at a point prior to the mixing/dispersing section of the extruder 312. Once combined, the hot melt PSA polymer and additives are well mixed in extruder 312. The order of component addition and mixing conditions (e.g., screw speed, screw length, and temperature) are selected to achieve optimum mixing. Generally, mixing is carried out at a temperature below the threshold temperature required to expand the microspheres, when such microspheres are present. However, temperatures higher than the microsphere expansion temperature may be used, in which case the temperature is typically decreased following mixing and prior to the addition of the microspheres to the extruder 312. It will be appreciated that if the hot melt PSA polymer is provided in a form suitable for extrusion, the first extrusion step may be omitted and the polymer added directly to extruder 312. When incorporating high amounts of thermally conductive filler, it is desirable that the filler is added to the extruder through multiple addition ports (i.e., split feed, not shown) and that vacuum via port 309 be used to remove entrapped air. Generally, void volume may be caused by entrapped gases, chemical blowing agents, physical blowing agents, and microspheres.
  • The expandable polymeric microspheres may be added to the second extruder 312, typically in a separate zone at downstream entrance 313 typically immediately prior to a conveying zone of extruder 312. Once added, the thermally conductive filler, expandable polymeric microspheres, the hot melt PSA polymer, and the optional fire retardant and/or microfiber forming material are melt-mixed in the conveying zone to form an expandable extrudable composition. The purpose of the melt-mixing step is to prepare an expandable extrudable composition in which the thermally conductive filler, microspheres and other additives, if present, are distributed throughout the molten polymer. Typically, the melt-mixing operation uses one conveying block downstream from entrance 313 to obtain adequate mixing, although kneading elements may be used as well. The temperature, pressure, shear rate, and mixing time employed during melt-mixing are selected to prepare an expandable extrudable composition without causing the microspheres to expand or break. Specific order of addition, zone temperatures, pressures, shear rates, and mixing times are selected based upon the particular chemical compositions being processed, and the selection of these conditions is within the skill of those practicing in the field.
  • Following melt-mixing, the expandable extrudable composition is metered into extrusion die 314 (e.g., a contact or drop die) through transfer tubing 318 using a gear pump 316. The temperature within multi-layer die 314 is maintained at substantially the same temperature as the temperature within transfer tubing 318. The temperature within die 314 is at or above the temperature required to cause expansion of the expandable microspheres. While extrusion die 314 is shown in FIG. 4 as a multi-layer die, it is understood that die 314 can be a single layer die. While the temperature within the transfer tubing 318 will also be at or above the threshold temperature required to initiate microsphere expansion, the pressure within the transfer tubing 318 is usually high enough to prevent the microspheres from expanding during the time they reside within the tubing 318. The volume within the die 314 is greater than the volume within the tubing 318 so that material flowing from the tubing 318 into the die 314 experiences a pressure drop to a pressure below that within transfer tubing 318. When the expandable extrudable composition enters the die 314, the drop in pressure and the heat within the die 314 will cause the polymeric microspheres to begin expanding. As the microspheres begin to expand, the expandable extrudable composition forms a foam. Most of the microsphere expansion will normally occur before the microspheres exit the die 314. The pressure within the die 314 will continue to decrease as the expandable extrudable composition approaches the exit port 315 of the die 314. The continued decrease of pressure contributes to the further expansion of the microspheres within the die. The flow rate of polymer through the extruder 312 and the die 314 are maintained to keep the pressure in the die cavity sufficiently low to promote the expansion of the expandable microspheres before the expandable polymer composition exits the die 314. The shape of die 314 may be chosen or fashioned to provide a desired shape for the foam TIM. Any of a variety of foam shapes may be produced, including continuous or discontinuous sheets or films. Those skilled in the art will appreciate that chemical blowing agents and the like are also useful in the manufacture of foams according to the invention, either in place of the expandable microspheres or in combination with the microspheres.
  • If desired, the smoothness of one or both of the foamed film surfaces can be increased by using nip roll 317 to press the foamed film against a chill roll 319 after the foamed film exits die 314, or by using smooth liners on each of the foamed film surfaces and passing the composite article through a nip. Smoothness of the surface(s) is beneficial for good surface contact and adhesion. It is also possible to emboss a pattern on one or both surfaces of the foamed film by contacting the foam with a patterned roll after it exits die 314 or by using a patterned or microstructured liner, such as those described in, for example, U.S. Pat. No. 6,197,397 B1.
  • For good thermal conductivity, especially when bonding rigid substrates having large attachment areas, it is desirable that there is no air entrapment between the foam TIM and the substrate. Non-contact or non-bonded areas do not conduct heat and reduce the overall thermal conductivity of the foam TIM. Patterned foam TIMs facilitate egress of air and result in improved adhesive contact. The improved softness and conformability of a foam TIM versus a non-foam TIM, also contributes to improved adhesive contact.
  • The extrusion process can also be used to prepare patterned foamed films having areas of different densities. For example, downstream of the point at which the film exits the die 314 (FIG. 4), the film can be selectively heated, e.g., using a patterned roll or infrared mask, to cause differential or regional expansion of microspheres within designated areas of the foamed film.
  • In applications requiring improved adhesive properties, the thermally conductive foamed film is combined with one or more skin adhesive layers; in other embodiments, one or more thermally conductive skin adhesive layers, applied to the outer surfaces of the foamed film. The thickness of the skin adhesive layer is typically from about 0.025 mm (1 mil) to about 0.125 mm (5 mils); and in other embodiments, from about 0.025 mm (1 mil) to about 0.076 mm (3 mils). FIG. 4 shows such a co-extrusion process. Adhesive for the skin adhesive layer is introduced to the system by adding an adhesive polymer to the extruder 330 (e.g., a single screw extruder) where the polymer is softened before it is fed to a second extruder 332 (e.g., typically a twin screw extruder) where the polymer is mixed with thermally conductive filler and other additives, if any. The adhesive, typically a PSA, is processed through the system to provide a resulting foam TIM having a skin layer that will be useful as a tape, for example. For such applications, the thermally conductive adhesive is formulated without adding other additives that diminish the adhesive properties or the tackiness of the adhesive.
  • Although fire retardant materials are normally excluded from the formulation for the adhesive, small amounts of fire retardant may also be included within the adhesive at concentrations that are effective to impart fire retardant properties to the adhesive, while not significantly diminishing the tack of the adhesive. Specifically, it may be desirable to add a small amount of fire retardant to the skin adhesive in very thin (i.e., <0.635 mm (<0.025 inches)) thermally conductive fire retardant foam TIMs. The amount of fire retardant added to the skin adhesive layer is no greater than about 30 weight percent of the total weight of skin adhesive, no greater than about 20 weight percent, no greater than about 10 weight percent, or no greater than about 5 weight percent.
  • A formable or extrudable adhesive composition is metered from the extruder 332 to the appropriate chambers of die 314 through transfer tubing 334 using a gear pump 336. The adhesive is co-extruded with the foam through an exit port 315 on the die 314 so that the adhesive is applied directly to the outer surface of the foamed film. Where the foamed film is provided in a sheet form having two major outer surfaces thereon, the adhesive may be applied to the foamed film on either or both of the major outer surfaces. Co-extrusion methods for coating an article with adhesive are known to those in the art and need not be further explained here. Other methods can be used for applying the skin adhesive layer, such as for example, direct coating, spray coating, pattern coating, laminating, and the like.
  • If a skin adhesive layer is applied to both of the major outer foamed film surfaces, the resulting foam TIM is a three-layer article featuring a foamed film core with a skin adhesive layer on each of the major surfaces of the foamed film. For a three layer A/B/C construction (adhesive A/foam B/adhesive C), another extruder and related equipment can be employed to permit another thermally conductive skin adhesive to be applied to the other major surface of the foam. In this construction, the major surfaces of the foam TIM may be adhered to any of a variety of surfaces for use in applications where the thermally conductive properties of the foam TIM are desired and/or required. Moreover, the absence of fire retardant in the skin adhesive layer allows the thermally conductive foamed film to be adhered to a surface or substrate with the maximum degree of adhesion provided by the particular skin adhesive used.
  • Suitable skin adhesives for use in the articles of the present invention include any adhesive that provides acceptable adhesion to a variety of polar and/or non-polar substrates. PSAs are generally acceptable. Suitable PSAs include those based on acrylic polymers, polyurethanes, thermoplastic elastomers, such as those commercially available under the trade designation KRATON (e.g., styrene-isoprene-styrene, styrene-butadiene-styrene, and combinations thereof) and other block copolymers, polyolefins, such as poly-alpha-olefins and amorphous polyolefins, silicones, rubber based adhesives (including natural rubber, polyisoprene, polyisobutylene, butyl rubber, etc.) as well as combinations or blends of these adhesives. The thermally conductive skin adhesive may contain tackifiers, reinforcing resins, plasticizers, rheology modifiers, fillers, fibers, crosslinkers, antioxidants, dyes, colorants, as well as active components, such as an antimicrobial agent.
  • A group of PSAs known to be useful in the present invention are, for example, the acrylate copolymers described in, for example, U.S. Pat. No. RE 24,906, incorporated herein by reference, and particularly a copolymer comprising a weight ratio of from about 90:10 to about 98:2 iso-octyl acrylate:acrylic acid copolymer. Also acceptable is a copolymer comprising a weight ratio of about 90:10 to about 98:2 2-ethylhexyl acrylate:acrylic acid copolymer, and a 65:35 2-ethylhexyl acrylate:isobornyl acrylate copolymer. Useful adhesives are described in, for example, U.S. Pat. Nos. 5,804,610 and 5,932,298, both of which are incorporated herein in their entireties by reference thereto. The inclusion of antimicrobial agents in the adhesive is also contemplated, such as is described in, for example, U.S. Pat. Nos. 4,310,509 and 4,323,557, both of which are incorporated in their entireties herein by reference thereto. Blends of acrylic adhesives and rubber based adhesives may also be used such as is described in WO 01/57152, which is incorporated in its entirety herein by reference thereto.
  • A release liner 320 may be applied to the thermally conductive skin adhesive layer or layers disposed on either or both of the major surfaces of the foam. The liner 320 can be dispensed from a feed roll 322. Suitable materials for liner 320 include silicone release liners, release coated polyester films (e.g., polyethylene terephthalate films), and polyolefin films (e.g., polyethylene films). The liner and the foam are then laminated together between nip rollers 324.
  • Optional release liner 340 can be added to the opposing surface of the foam by positioning optional second feed roll 342 near one of the nip rolls 324. The second release liner 340 may be the same as or different from the release liner 320. Moreover, the second release liner 340 may be provided with a layer of a thermally conductive adhesive coated or applied to one surface of the release liner 340. In this manner, a second thermally conductive adhesive layer (not shown) may be applied to the second major surface of the foam material. The second thermally conductive skin adhesive layer may be the same as or different from the aforementioned co-extruded adhesive. Typically, the thermally conductive skin adhesive layers will comprise thermally conductive PSAs. Release liners 320, 340 may also be provided with a layer of a thermally conductive adhesive coated or applied to one of its surfaces.
  • Variations to the foregoing process and to the equipment used will be known to those skilled in the art, and the invention is not limited by the described apparatus of FIG. 4 herein.
  • Other methods for the manufacture of multilayered foam TIMs are to be considered within the scope of the invention. For example, the foregoing co-extrusion process can be conducted so that a one or two-layer TIM is produced, or to produce TIMs having three or more layers (e.g., 10-100 layers or more) by equipping a single layer die with an appropriate feed block, or by using a multi-vaned or a multi-manifold die. Multilayered TIMs can also be prepared by laminating additional layers (e.g., polymer layers, metals, metal foils, scrims, paper, cloth, adhesives coated on a release liner, etc.) to the foamed film, or to any of the co-extruded polymer layers after the article exits die 314. Other techniques which can be used include pattern coating. The thermally conductive foam film(s) in the TIMs of the invention can be thick, i.e., greater than or equal to 0.25 mm (0.010 inches) or thin (i.e., <0.025 mm (0.010 inches).
  • Following lamination, the foam TIM is optionally exposed to radiation from an E-beam source 326 to crosslink the foam TIM for improved cohesive strength. Other sources of radiation (e.g., ion beam and gamma radiation) may be used as long as the radiation is energetic enough to penetrate the thickness of the foam TIM to initiate and to sufficiently crosslink the foam TIM throughout its thickness. Following E-beam exposure, the optional second release liner 340 can be rolled up onto a take-up roll 329, and the laminate is rolled up onto a take-up roll 328. For foam TIMs, it may be necessary to E-beam irradiate the foamed film through both major surfaces to sufficiently penetrate the material to induce more complete crosslinking. Alternatively, the TIM could be gamma irradiated after being wound into a roll.
  • The release liners are typically coated with release agents, such as fluorochemicals or silicones. For example, U.S. Pat. No. 4,472,480 describes low surface energy perfluorochemical liners. Suitable release liners include papers, polyolefin films, or polyester films coated with silicone release materials. Polyolefin films may not require release coatings when used with acrylic based PSAs. Examples of commercially available silicone coated release liners are POLYSLIK™ silicone release papers (available from James River Co., H. P. Smith Division, Bedford Park, Ill.) and silicone release papers supplied by DCP-Lohja (Dixon, Ill.) now known as Loparex, Inc. (Willowbrook, Ill.). A particular release liner that is known by the designation 1-60BKG-157, a super calendared Kraft paper with a water-based silicone release surface, is available from DCP-Lohja. Other types of E-beam stable, contaminant free release liners are also useful in the invention, such as those described in pending, for example, U.S. Patent Publication No. 02-0155243-A1, assigned to the assignee of this application, and incorporated in its entirety herein by reference.
  • The foam TIMs of the invention may be used in a variety of applications, including aerospace, automotive, electronic, and medical applications. The foam TIMs of the invention are typically used to join processors and components to heat dissipating devices (for example, heat sinks and spreaders). The properties of the TIMs may be tailored to meet the demands of the desired applications. Specific examples of applications include adhesive tapes, pads, or sheets, vibration damping articles, tape backings, gaskets, spacers, and sealants.
  • The features of the embodiments of the invention are further illustrated in the following non-limiting examples.
  • EXAMPLES
  • In the test methods and examples below, the sample dimensions (typically the length) are approximate except for the width wherein the width was measured to the accuracy of the cutting tool.
  • These examples are merely for illustrative purposes only and are not meant to be limiting on the scope of the appended claims. All parts, percentages, ratios, etc. in the examples and the rest of the specification are by weight unless indicated otherwise.
  • Test Methods Density and Determination of Void Volume
  • Density was determined according to ASTM D 792-86 “Standard Test Method for Density and Specific Gravity (Relative Density) of Plastics by Displacement.” Samples were cut into approximately 2.54 cm×2.54 cm (1 inch (in)×1 inch (in)) specimens and weighed on a high precision balance available as Model AG245 from Mettler-Toledo, Greifensee, Switzerland. The volume of each sample was obtained by measuring the mass of water displaced at room temperature (23° C.+/−1° C.). The buoyancy of each sample was measured in grams (g) using a special attachment for the balance. The density (Dmeas.) of the sample was taken to be its mass divided by its buoyancy, assuming the density of water at 23° C. to be 1 g/cc.
  • The theoretical density (Dtheor.) of the composition (before foaming) was determined from the following:
  • Dtheor.of composition=(weight percent adhesive component×Dmeas.of adhesive component)+(weight percent first filler component×Dtheor.of first filler component)+(weight percent second filler component×Dtheor.of second filler component)+(weight percent third filler component×Dtheor.of third filler component), etc.
  • And from this, the Void Volume was calculated as:
  • % Void Volume = ( 1 - D meas . of composition D theor . of composition ) × 100
  • The reported % Void Volume includes the void volume contribution of expanded polymeric microspheres and/or entrapped gas and/or chemical blowing agents and/or physical blowing agents.
  • Hardness Test
  • The thickness of an article (about 3.81 cm (1.5 in) by 2.54 cm (1.0 in)) sample was measured and recorded. The sample was then laminated to a clean, dry glass panel taking care to avoid trapping air bubbles between the sample and the glass. Additional pieces of article sample were laminated to the first article in the same manner until a total thickness of at least 0.34 cm (0.135 in) was achieved. Using a Shore A Hardness Tester (Model CV Stand and Durometer Type A ASTM D2240 Gauge, available from Shore Instrument Mfg. Co. Inc., Freeport, N.Y.), the initial hardness reading from the instrument was taken at three locations on each sample piece and those values were averaged.
  • Viscosity
  • The changes in viscosity were measured using Rheometrics RDA II, available from Rheometrics. The adhesive was put in 25 mm diameter parallel plates with the thickness of 1 mm. The data was plotted as complex viscosity versus temperature and shear rate at 180° C. The viscosity at a frequency of 1 radian/second was reported.
  • Static Shear Strength Test
  • A 2.54 cm (1 in) wide by about 3.81 cm (1.5 in) long sample was cut from the article to be tested and pressed onto a solvent-washed (one wash of acetone followed by three washes of heptane), dry, 0.508 cm (2 in) wide by 7.62 cm (3 in) long, Type 304 stainless steel substrate panel and the sample was centered on one end of the panel. An about 10.16 cm (4 in) long by about 3.175 cm (1.25 in) wide by 0.0025 cm (0.001 in) thick sheet of primed polyester film was adhered to the sample by rolling down the primed side of the polyester film onto the sample using a 2 kg (4.5 lb) hard rubber roller, with two passes in each direction, taking care not to trap air bubbles between the film and the sample, with approximately 5.1 cm (2 in) of the polyester film extended off the panel to serve as a tab. The laminate on the panel was then cut to a 2.54 cm (1 in) length so that the resultant bonded area was 2.54 cm×2.54 cm (1 in ×1 in). The 5.1 cm (2 in) tab was then folded around a triangular clip, wrapped with masking tape, and stapled so that a weight could be attached to the test specimen. A 1000 g weight was used to test samples at room temperature and a 500 g weight was used to test samples at 70° C. (158° F.). The sample thus prepared was allowed to dwell at room temperature and approximately 50% relative humidity for approximately 24 to 72 hours. The test specimen was then placed in a Static Shear standard fixture having a 2 degree angle back slant. The fixtured specimen was then either tested at room temperature (about 22° C.) or in a forced air oven set at 70° C.±3° C. (158° F.). The elevated temperature test specimen was then given a 10 minute warm up period before attaching the 500 g weight. The test was run until the test specimen failed or 10,000 minutes elapsed. Failure time was recorded.
  • Tensile Break Strength and Elongation Test (Method I)
  • Tensile and elongation was determined according to ASTM D412-98a “Standard Test Methods for Vulcanized Rubber and Thermoplastic Elastomers-Tension.” A silicone release liner was applied to the exposed surface of the article which already had a liner on one side. A sample was cut using Die E in the machine direction from the article to be tested to form the test specimen. Sample thickness was measured in the center of each specimen using an AMES gauge having a force of 0.1 kg (3.5 oz) and a 0.0635 cm (0.25 in) diameter foot. The tensile tester was set up with the following conditions:
      • Jaw Gap: 8.89 cm (3.5 in)
      • Crosshead Speed: 51 cm/min (20 in/min)
      • Load cell: 45 kg (100 lb)
  • The initial gauge length was set at 8.89 cm (3.5 in) by separating the instrument clamping jaws to this length and the sample was centered horizontally between the jaws so that an approximate equal length of sample was held by each jaw. The sample was tested at a crosshead speed of 51 cm/min (20 in/min) until the sample broke or reached the maximum extension of the machine (101.6 cm (40 in)). The tensile strength in pounds (and later converted to kilograms) and elongation distance were recorded. The percent elongation was determined by dividing the elongation distance by the initial gap distance times 100. Eleven replicates were tested, except where noted, and averaged to provide the thickness, Peak Load, Peak Stress, Percent (%) Strain at Peak Stress, Break Load, % Strain at Break, Energy at Break, and Modulus.
  • Tensile Break Strength and Elongation (at Break) Test (Method II)
  • A silicone release liner was applied to the non-liner side of the article. A 1.27 cm (0.5 in) wide by about 12.7 cm (5 in) long sample was cut in the machine direction from the article to be tested to form the test specimen. One liner was removed and a 2.54 cm (1.0 in) length was measured and marked in the center of test specimen to provide the initial gap distance. A 2.54 cm (1 in) wide by about 7.62 cm (3 in) piece of masking tape was placed across the foam article by positioning the tape edge on the both marks so that the 2.54 cm (1 in) long section that was marked off did not have tape covering it. The other liner was then removed and masking tape was wrapped completely around the article, making sure to keep the masking tape aligned across the article. The tape was used to prevent the sample from adhering to the INSTRON jaws and prevent the sample from breaking at the point where it was clamped by the jaws. The INSTRON was set up with the following conditions:
      • Jaw Gap: 2.54 cm (1.0 in)
      • Crosshead Speed: 25.4 cm/min (10 in/min)
  • The test specimen was then positioned in the INSTRON jaws so that the jaws lined up with the edge of the masking tape. The sample was tested at a crosshead speed of 25.4 cm/min (10 in/min) until the sample broke. The tensile break strength or peak load was recorded in pounds (and later converted to kilograms) and elongation distance was recorded. The percent elongation at break was determined by dividing the elongation distance by the initial gap distance times 100. One specimen per sample was tested.
  • 90 Degree Peel Adhesion Test
  • A 25.4 mm (1 in) or a 12.7 mm (0.5 in) wide by about 127 mm (5 in) long sample was cut from the article to be tested and laminated to an about 15.24 mm (6 in) long by about 28.6 mm (1.125 in) wide by 0.025 mm (0.001 in) thick primed polyester film by rolling down the article onto the primed side of the polyester film, taking care not to trap air bubbles between the film and the article. The 12.7 mm (0.5 in) wide sample was similarly laminated to an about 152.4 mm (6 in) long by about 15.8 mm (0.625 in) wide by 0.025 mm (0.001 in) thick primed polyester film. The laminate was then positioned on either a solvent-washed (one wash of acetone followed by three washes of heptane), dry, 51 mm (2 in) wide by about 127 mm (5 in) long, Type 6061-T6 alloy bare standard aluminum panel or a solvent-washed (three washes of isopropyl alcohol), dry 51 mm (2 in) wide by about 127 mm (5 in) long polypropylene panel, so that the laminate was centered on the panel with a portion of the laminate extending off the panel to serve as a tab. The laminate was rolled down onto the panel using a 2 kg (4.5 lb) hard rubber roller, with one pass in each direction. Care was taken not to trap bubbles between the panel and the laminate. The sample thus prepared was allowed to dwell at room temperature (about 22° C.) for about 24 hours. Then the sample was tested at room temperature (about 22° C.) for 90 Degree Peel Adhesion by Method A (for polypropylene panels) or Method B (for aluminum panels) described below.
  • Method A: The sample was tested at crosshead speed of 30 cm/min (12 in/min) using an IMASS tester fitted with a 4.5 kg (10 lb) load cell. The peel value obtained from the first 0.51 cm (0.2 in) length of peel was ignored. The peel value of the next 5.08 cm (2 in) or “peel area” was recorded as an integrated average value. The values reported were the average of 3 replicates.
  • Method B: The sample was tested at crosshead speed of 30 cm/min (12 in/min) using a SINTECH 5/GL Instron tester fitted with a 45 kg (100 lb) load cell. The peel value obtained from the first 1.27 cm (0.5 in) length of peel was ignored. The integrated average peel value of the next 89 mm (3.5 in) or “peel area” was recorded. The values reported were the integrated average peel adhesion values of three replicates.
  • Stretch Release Test
  • A 12.5 mm (0.5 in) wide by 127 mm (5 in) long strip was cut from the test sample such that the length was cut in the machine direction of the sample.
  • One strip was laminated to a 50.8 mm (2 in) wide×127 mm (5 in) long aluminum or glass panel such that the strip was approximately 0.635 cm (0.25 in) from one of the long edges of the panel and approximately 25.4 mm (1.0 in) of the strip extends beyond the end of the panel. Care was taken to ensure maximum wet-out of or contact between the strip and the panel. It was desired that 100% contact be achieved.
  • Similarly, a strip from a different example was laminated along the other edge of the glass panel.
  • Then a second like panel (i.e., aluminum to aluminum or glass to glass) was laminated directly over the first panel making sure not to entrap air bubbles between the strips and the second panel. The bonded sample was allowed to dwell for between 24 hours and 72 hours at room temperature (about 22° C.).
  • The free end of the test strips were pulled by hand at a speed of about 30 cm/min (about 12 in/min) in a direction substantially parallel to the panels to initiate stretch release removal until the bond failed. Only the glass panels were visually examined for the presence of residue and the failure mode was recorded. A sample was rated as “Pass” if there was complete removal from the panel. A sample was rated as “Fail” if the sample could not be completely removed.
  • Thermal Impedance Measurement
  • The thermal impedance of single layers of the disclosed invention was measured according to ASTM C-1114 Test Method “Steady-State Thermal Transmission Properties by Means of the Thin-Heater Apparatus.”
  • A diagram of the Thin-Heater Apparatus 500 is shown in FIG. 5.
  • A small resistor 502 was used as the thin-heater. The resistor used was a 10 ohm resistor in TO-220 package with an area of 0.806 cm2 (0.125 in2) (such as Caddock Electronics MP930). A small hole was drilled through the back of the resistor into which a thin-wire thermocouple 504 was placed to measure the hot side temperature, Th.
  • A know amount of power, Q, was supplied from the precision power supply 506 (such as Hewlett Packard E3611A) by setting the current and voltage (Power=current×voltage).
  • The sample to be tested 508 was placed onto a disposable test surface 509 and between the thin-heater and the cold aluminum test block 510, cooled by running cold water through a cooling block 511. The cold test block had a thermocouple 512 for measuring the cold side temperature, Tc. The resistor was powered up and the temperature of the resistor was allowed to come to equilibrium. Temperatures Th and Tc were recorded and the impedance and conductivity calculated according to ASTM C 1114 using the following relationships:
  • A=area of thin heater
  • Power, Q=voltage×current supplied
  • Rate of heat flux, q=Q/A
  • Delta T=Th−Tc
  • Thermal resistance (R)=Delta T/q
  • Thermal impedance (Zuncorr.)=R×A
  • The thermal impedance was corrected for any heat loss off the top (horizontal) surface of the resistor (but not the sides of the sample) and reported as Zcorr.
  • Zcorr.=Zuncorr.−[convective heat loss value of the resistor×(surface temperature Th of the resistor−room temperature)]
  • where the convective heat loss value for TO-220 type resistor=0.011 Watts.
  • Further discussion can be found in the article “Factors Affecting Convection Heat Transfer”, Heat Transfer, Watlow Education Series, Book One, 1995, pages 16-17. The convection heat loss value is taken from FIG. 17 on page 17 based upon the size of the test resistor.
  • Thermal Bulk Conductivity Measurement
  • An impedance plot method was used to thermal bulk conductivity (k). The samples were obtained by either extruding material at different thicknesses or by combining multiple layers of a single sample to obtain different thicknesses.
  • The thermal impedance (Zcorr.) was measured according to the above test method for samples of different thickness. The data was then plotted allowing for a finite value of the interfacial impedance. This plot method can be expressed as an equation:

  • Z corr. =Z interface +t/k
  • As illustrated in FIG. 6, a plot of corrected thermal impedance (Zcorr.) versus thickness (t) resulted in a line having a slope=1/k and an intercept at t=0 equal to Zinterface. Thermal bulk conductivity (k) was then calculated from slope of the line.
  • Materials Used in the Examples
    Component Trade Name Description Source
    Adhesive
    2-EHA 2-Ethyl hexyl acrylate monomer BASF Corp., Mount
    acrylate Olive, NJ
    AA acrylic acid acrylate monomer BASF Corp.
    IOTG isooctyl chain transfer agent BASF Corp.
    thioglycolate
    Kraton Kraton ™ D1107 styrene-isoprene-styrene linear Kraton Polymers
    D1107 thermoplastic elastomer, U.S. LLC, Houston,
    nominal molecular weight of TX
    229,000
    SHELLFLEX SHELLFLEX ™ refined petroleum oil Shell Lubricants,
    371N 371N Houston, TX
    IRGANOX IRGANOX ™ antioxidant Ciba Specialty
    1010 1010 Chemicals Corp,
    Tarrytown, NY
    WINGTACK Wingtack ™ Plus tackifying resin, nominal Goodyear Tire &
    PLUS average molecular weight of Rubber Co, Chemical
    1070 Division, Akron, OH
    IRG 651 Irgacure ™ 651 2,2-dimethoxy-2- Ciba Specialty
    phenylacetophenone Chemicals Corp.
    VA-24 film VA-24 film 0.0635 mm thick heat sealable, CT Film of Dallas,
    ethylene vinyl acetate TX
    copolymer film having 6%
    vinyl acetate
    Filler
    BN boron nitride thermally conductive particle, Advanced Ceramics
    hexagonal form; theoretical Corporation,
    density of 1.80 Cleveland, OH; now
    known as GE
    Advanced Ceramics
    SiC silicon carbide thermally conductive filler; Washington Mills
    (SILICARIDE theoretical density of 3.10 Electro Minerals
    G-21, Grade p240) Corp., Niagara Falls, NY
    Al(OH)3 Martinal ON 320 aluminum hydroxide, particle Albemarle
    size 20 microns, theoretical Corporation, Baton
    density of 2.40 Rouge, LA
    Mg(OH)2 magnesium thermally conductive filler; Albemarle
    hydroxide theoretical density 2.40 Corporation
    F-100D Micropearl ™ expandable polymeric Pierce Stevens,
    F-100D microspheres having a shell Buffalo, NY
    composition containing
    acrylonitrile and
    methacrylonitrile
    Exact 3040 Exact ™ 3040 ethylene-based hexene ExxonMobil
    copolymer, nominal tensile Chemical Company,
    yield strength (MD) 5.4 MPa Houston, TX
    (780 psi), tensile break
    strength (MD) 51.6 MPa (7490
    psi), elongation at break (MD)
    460%, MI 16.5, density 0.900
    g/cm3, peak melting
    temperature 96° C. (205° F.)
  • Examples 1-4
  • Four acrylic TIMs were prepared using expandable polymeric microspheres (F-100D) and varying amounts of thermally conductive fillers. Each composition was coated at several thicknesses.
  • Preparation of Pressure Sensitive Adhesive A (PSA-A):
  • A pressure sensitive adhesive composition was prepared by mixing 95 parts 2-EHA, 5 part AA, 0.15 parts IRG 651, and 0.02 parts IOTG.
  • The composition was placed into VA-24 film packages measuring approximately 100 mm by 50 mm by 5 mm thick, immersed in a water bath and exposed to UV radiation as described in U.S. Pat. No. 5,804,610. Viscosity of PSA-A was 3980.73 Poise (P) as tested according to test method above. This adhesive is believed to have a weight average molecular weight (MW) of about 700,000 to about 1,200,000. The density of PSA-A was 0.98 g/cc.
  • Preparation of TIM:
  • PSA-A was fed to the feed port in barrel section 1 of a 30 mm co-rotating twin screw extruder with four ports (Werner Pfleider) operating at a screw speed set point of 200 rpm (actual speed about 176 rpm) via a 51 mm single screw extruder (Bonnot). The temperature for all zones in the Bonnot extruder was set at 149° C. (300° F.). Thermally conductive fillers as specified in Table 1 (parts by weight as specified in Table 1 per 100 parts by weight of PSA-A plus thermally conductive filler) were added as dry solids in one portion to a feed port in barrel section 5 of the twin screw extruder with a total flow rate of thermally conductive filler and PSA-A of about 3.18 kg/hr (7 lb/hr). F-100D microspheres at a concentration of 0.5 parts by weight per 100 parts by weight of PSA-A were added downstream to barrel section 7. In all six temperature zones in the twin screw extruder, the temperature was set at 93.5° C. (200° F.). A vacuum (in a range from about −77.9+/−10.2 newtons/sq. meter (N/m2) (−23+/−3 inches of mercury (Hg)) was applied through a port in barrel section 9. The temperatures in the extruder adapters and the flexible hose at the exit end of the extruder were all set at 113° C. (235° F.). The flow rate was controlled with a heated Zenith melt pump, nominally 10.3 cc/rev, set at 113° C. (235° F.).
  • The extrudate was pumped via the heated hose to a (15.24 cm (6 in) wide single layer drop die with a gap of about 0.114 cm (0.045 in). The die temperature was set at 182° C. (360° F.). The line speed was adjusted to provide the target thickness as specified in Table 1.
  • The extruded sheet was cast into a nip formed by a two chill rolls (one metal and one rubber), between two silicone coated polyester release liners. The temperatures of the chill rolls were set at 7.5° C. (45° F.). Each liner was a 0.051 mm (0.002 in) thick two sided, silicone-coated polyester liner, having different release materials (identified as 5035 and 7200) on each side, available from DCP-LOHJA Inc., Willowbrook, Ill., as 2-2PESTR(P2)-5035 and 7200. The extruded sheet contacted the 7200 side of one liner and the 5035 side of the other liner. The liner having 7200 release material in contact with the extruded sheet was removed and the resulting article was wound into a roll for subsequent crosslinking
  • TABLE 1
    Weight Percent Target Measured
    Ex. Conductive Conductive Thickness, cm Thickness, cm
    No. Filler Filler (mils) (mils)
    1 BN 40 0.0508 (20) 0.0439 (17.3)
    2 BN 50 0.0508 (20) 0.0538 (21.2)
    3 Al(OH)3 40 0.0508 (20) 0.0569 (22.4)
    4 Al(OH)3 50 0.0508 (20) 0.0462 (18.2)
  • Two approximately 0.46 meter (m) (18 in) long pieces were cut from the above sample roll. 2-2PESTR(P2)-5035 and 7200 release liner was carefully laminated to the uncovered side of each piece with the 7200 silicone coated side contacting the uncovered side. The extruded sheets with liners on both sides were then subjected to gamma radiation as described below.
  • Samples were passed through a gamma processing unit (Research Loop of Panasonic Industrial Irradiator JS 7500, Cobalt 60 Wet Storage, available from M. D. S, Nordion, Kanota, Ontario, Canada). Each piece received a measured gamma dose between 31.6 to 36.4 kilograys (kGy) (target dose 30 kGy).
  • The resultant article was then tested for physical properties, the Test Method outlined above. The Thermal Bulk Conductivity for Examples 1-4 was 0.82, 0.95, 0.60, and 0.85 Watts/meter-K respectively.
  • Results are given in Table 2.
  • TABLE 2
    Density, Peel Impedance, ° C.-
    g/cm3 Adhesion, Static Shear, cm2/W
    Ex. (measured/ % Void kN/m (oz/in) Minutes (° C.-in2/W)
    No. theoretical) Volume Al PP 22° C. 70° C. Zuncorr. Zcorr.
    1 1.106/1.30 14.9 0.601 0.069 10,000+ 10,000+ 8.32 9.03
    (54.9) (6.3) (1.29) (1.40)
    2 1.206/1.38 12.6 0.426 0.0722 10,000+ 10,000+ 7.61 8.26
    (38.9) (6.6) (1.18) (1.28)
    3 1.081/1.55 30.3 0.380 0.118 10,000+ 10,000+ 14.32 16.71
    (34.7) (10.8) (2.22) (2.59)
    4 1.221/1.69 27.8 0.420 0.0996 10,000+ 10,000+ 10.39 11.48
    (38.4) (9.1) (1.61) (1.78)
  • Example 5
  • An acrylic thermal interface composition was prepared using a blend of two thermally conductive fillers that also functioned as the foaming agent.
  • Preparation of Thermal Interface Composition:
  • A thermally interface composition was prepared according to Examples 1-4 except that the conductive filler was a dry blend of 82 parts by weight of SiC and 18 parts by weight of BN and no expandable polymeric microspheres were used.
  • TABLE 3
    Weight Percent Target Measured
    Ex. Conductive Conductive Thickness, cm Thickness, cm
    No. Filler Filler (mils) (mils)
    5 82:18 SiC:BN 60 0.0508 (20) 0.0549 (21.6)
  • Samples were subjected to gamma radiation as in Examples 1-4.
  • The TIM was then tested for physical properties according to the Test Methods outlined above. The Thermal Bulk Conductivity of Example 5 was 0.97 Watts/meter-K.
  • Results are given in Table 4.
  • TABLE 4
    Density, Impedance, ° C.-
    g/cm3 Peel Adhesion, Static Shear, cm2/W
    Ex. (measured/ % Void kN/m (oz/in) Minutes (° C.-in2/W)
    No. theoretical) Volume Al PP 22° C. 70° C. Zuncorr. Zcorr.
    5 1.43/2.11 32.2 0.730 0.172 10,000+ 10,000+ 8.06 8.84
    (66.7) (15.7) (1.25) (1.37)
  • Example 6
  • A thermoplastic elastomeric TIM was prepared using the blend of two thermally conductive fillers of Example 5. The silicon carbide also acted as a chemical blowing agent. There was no premixing of a PSA composition. The composition was coated at several thicknesses. The resultant article was not subjected to irradiation.
  • Preparation of TIM:
  • 100 parts Kraton D1107 were added to the feed port in barrel section 1 of the twin screw extruder of Examples 1-4 at a feed rate of 2.60 kg/hr (5.73 lbs/hr). 179 parts WINGTACK PLUS tackifying resin was melted in a Helicon Mixer (tank set at 149° C. (300° F.), pump and hose set at 163° C. (325° F.)) and pumped to feed port in barrel section 3 at a feed rate of 1.87 kg/hr (4.11 lb/hr). 23 parts SHELLFLEX 371N oil was added through a feed port in barrel section 5 using a Zenith pump at a feed rate of 0.24 kg/hr (0.528 lb/hr). The total flow rate of the adhesive (i.e., Kraton D1107, WINGTACK PLUS tackifying resin, and SHELLFLEX 371N) was about 3.18 kg/hr (7 lb/hr). The density of the adhesive was 0.96 g/cc.
  • Thermally conductive fillers as specified in Table 5 and 3 parts IRGANOX 1010 were added as a dry blend in one portion to a feed port in barrel section 5 at a flow rate of 2.60 kg/hr (5.73 lb/hr).
  • The six temperature zones in the twin screw extruder were set as follows: Zone 1 at 149° C. (300° F.), Zone 2 at 154.4° C. (310° F.), and Zones 3 to 6 at 160° C. (320° F.). A vacuum (in a range from about −77.9+/−10.2 N/m2 (−23+/−3 inches of mercury (Hg)) was applied through a port in barrel section 9. The temperature in the extruder adapters and the flexible hose at the exit end of the extruder were set at 160° C. (320° F.). The flow rate was controlled with a heated Zenith melt pump, nominally 10.3 cc/rev, set at 160° C. (320° F.).
  • The extrudate was pumped via the heated hose to the single layer drop die of Examples 1-4. The temperature of the die was set at 163° C.±14° C. (325° F.±25° F.). The line speed was adjusted to provide the target thickness as specified in Table 5. The extruded sheet was cast into a nip formed by a two chill rolls (one metal and one rubber), between two silicone coated polyester release liners of Examples 1-4. The temperature of the chill rolls was set at 7.5° C. (45° F.). One liner was removed and the resulting article was wound into a roll.
  • TABLE 5
    Weight Percent Target Measured
    Ex. Conductive Conductive Thickness, cm Thickness, cm
    No. Filler Filler (mils) (mils)
    6 82:18 SiC:BN 45 0.0508 (20) 0.0424 (16.7)
  • The TIM was then tested for physical properties according to the Test Methods outlined above. Results are given in Table 6. For the density calculation, the density of the thermoplastic elastomeric adhesive without thermally conductive filler was measured as 0.96 g/cc. The Thermal Bulk Conductivity of Example 6 was 0.84 Watts/meter-K.
  • TABLE 6
    Density, Impedance, ° C.-
    g/cm3 Peel Adhesion, Static Shear, cm2/W
    Ex. (measured/ % Void kN/m (oz/in) Minutes (° C.-in2/W)
    No. theoretical) Volume Al PP 22° C. 70° C. Zuncorr. Zcorr.
    6 1.32/1.83 27.9 1.103 1.600 10,000+ 98.5 10.84 12.39
    (100.8) (146.2) (1.68) (1.92)
  • Example 7 Preparation of Thermal Interface Composition
  • Acrylic thermal interface compositions were prepared using various thermally conductive fillers.
  • Preparation of Pressure Sensitive Adhesive B (PSA-B):
  • A pressure sensitive adhesive composition (PSA-B) was prepared according to the preparation of PSA-A except that 97 parts 2-EHA, 3 part AA, and 0.01 parts IOTG was used in place of 95 parts 2-EHA, 5 parts AA, and 0.02 parts IOTG. Viscosity of PSA-B was 2215.2 P as tested according to test method above. This adhesive is believed to have a weight average molecular weight (MW) of about 800,000 to about 1,300,000. The density of PSA-B was 0.98 g/cc.
  • Preparation of TIM:
  • PSA-B was fed at a feed rate of 4.55 kg/hr (10 lb/hr) via the Bonnet extruder of Examples 1-4 into barrel 1 of a co-rotating twin screw extruder (40 mm Berstorff ZE-40, L/D=40, 10 barrels). All temperature zones of the Bonnot extruder were set at 149° C. (300° F.) except for Zone 1, which was set at 135° C. (275° F.). The thermally conductive fillers were fed as dry solids into barrels 2 and 4 of the twin screw extruder, at feed rates of 2.27 kg/hr (4 lb/hr) and 2.73 kg/hr (6 lb/hr) respectively, using gravimetric feeders (K-Tron model T20, K-Tron, Pitman, N.Y.). Table 7 below provides amount and type of conductive filled added. This split feed arrangement was used to successfully obtain the required loading levels of the low bulk density filler. In addition, the vertical drop distances were kept as short as possible to avoid excess air entrapment. Each extrusion screw was composed of self-wiping and square channel double-flighted conveying elements of varying pitch (60 mm, 40 mm, and 30 mm). The screws also contained 5-paddled kneading blocks, 50 mm in length, offset in three different arrangements: (1) 45 degrees in a forward (LI) direction, (2) 45 degrees in a reverse (RE) direction, or (3) 90 degrees in a neutral pattern. The first 370 millimeters of the screw was composed of forward conveying, self-wiping elements (pitches of 30 and 60). The first kneading section was located between 370-520 mm of the screw and consists of a forward, neutral, and reverse kneading block. A conveying section (520-770 mm) and another kneading segment (770-920 mm) follow. This kneading section was composed of two forward blocks followed by a reverse block. The remainder of the screw (920-1600 mm) is composed of self-wiping and square channel forward conveying elements of various pitches, generally following a declining trend in pitch (60 mm, 40 mm, 30 mm). The twin screw extruder was operated with a screw speed set point of 200 rpm (actual speed about 200 rpm) at a temperature of 125° C. (257° F.) in all zones. A vacuum (about −94.81 kN/m2 (−28 inches of mercury (Hg)) was applied through an open port in Zone 8 to remove any volatiles and/or moisture. As noted in the screw design, large pitch forward conveying elements were used in the vacuum area to provide a lower degree of fill thereby maximizing polymer surface area. The extrudate was pumped via a heated Normag melt pump, nominally 10.3 cc/rev, set at 125° C. (257° F.) through a 1.905 cm (0.75 in) diameter stainless steel neck tube set at 154.4° C. (310° F.) to the middle/center layer of a 4.17 cm (10 in) wide 3-layer Cloeren drop die, having a 0.102 cm (0.040 in) gap (available from The Cloeren Company, Orange, Tex.). The die temperature was set at 177° C. (350° F.). The line speed was adjusted to provide the target thickness as specified in Table 7.
  • TABLE 7
    Weight Percent Target Measured
    Ex. Conductive Conductive Thickness, cm Thickness, cm
    No. Filler Filler (mils) (mils)
    7a 82:18 SiC:BN 50 0.0508 (20) 0.0406 (16)
    7b 82:18 SiC:BN 50 0.0762 (30) 0.0762 (30)
    7c 82:18 SiC:BN 50 0.1016 (40) 0.0991 (39)
  • The extruded sheet was cast onto the two side, silicone coated, polyester liner of Examples 1-4 in contact with a chilled cast roll. The sheet was cast onto the 5035 side of 2-2PESTR(P2)-5035 and 7200 release liner. The temperature of the cast roll was set at 7.5° C. (54° F.). The resulting article was wound into a roll for subsequent crosslinking.
  • Eight approximately 0.46 m (18 in) long pieces were cut from the above sample roll. 2-2PESTR(P2)-5035 and 7200 release liner was carefully laminated to the uncovered side of each piece with the 7200 silicone coated side contacting the uncovered side. The extruded sheets with liners on both sides were then subjected to gamma radiation as described below.
  • Samples were subjected to gamma radiation and were passed through the gamma processing unit of Examples 1-4. Two sample pieces each received a target (actual measured) gamma dose of between about 30 kGy (31.6-31.7 kGy), 45 kGy (44.4-45.9 kGy), or 60 kGy (58.8-59.7 kGy).
  • The resultant articles were then tested for physical properties, and adhesive performance properties according to the Test Methods outlined above. Results are given in Tables 8 and 9. The test method used was Tensile Break Strength and Elongation Test (Method I).
  • TABLE 8
    Density, % Peel Impedance, ° C.-
    g/cm3 Volume Radiation Adhesion, Static Shear, cm2/W Thermal
    Ex. (measured/ Gas Type and kN/m (oz/in) Minutes (° C.-in2/W) Bulk
    No. theoretical) Hardness Phase Amount Al 22° C. 70° C. Zuncorr. Zcorr. Conductivity
    7a 1.347(a)/ NT 29.82 Gamma, NT 10,000+ 10,000+ NT NT 1.12
    1.92 30 kGys
    7b 1.461(a)/ NT 23.93 Gamma, NT 10,000+ 10,000+ NT NT
    1.92 30 kGys
    7c 1.478/ 24 (b) 23.04 Gamma, 0.727 NT NT NT NT
    1.92 45 kGys (66.4)
    (a) Measured on samples that had received 45 kGys dose of Gamma radiation
    (b) Measured on 40 mil thick sample that had received 30 kGys dose of gamma radiation
  • TABLE 9
    Peak Peak % Break Energy
    Radiation Load, Stress, Strain Break Stress, % at Break, Modulus,
    Ex. Type and Thickness, kg MPa at Peak Load, MPa Strain at cm-kg MPa
    No. Amount cm (mils) (lb) (psi) Load kg (lb) (psi) Break (in-lb) (psi)
    7c Gamma,    0.0864 0.409    0.738 408.9 0.409 0.728 433.6 11.74 0.344
    45 kGy (34) (0.9) (107) (0.9) (105.6) (10.17) (49.87)
  • Examples 8-9
  • Acrylic thermal interface compositions having stretch release properties provided by in situ microfiber formation were prepared using varying amounts of Exact 3040. Each composition was coated at several thicknesses.
  • Preparation of TIM:
  • PSA-B of Example 7 was fed to the feed port in barrel section 3 of the twin screw extruder of Examples 1-4 operating at a screw speed set point of 225 rpm (actual speed about 201 rpm) via Bonnot extruder of Examples 1-4 at a feed rate of 1.95 kg/hr (4.28 lb/hr). The temperature for all zones in the Bonnot extruder was set at 149° C. (300° F.). Thermally conductive fillers as specified in Table 10 (parts by weight as specified in Table 10 per 100 parts by weight of PSA-B plus thermally conductive filler) were added as dry solids in one portion to a feed port in barrel section 1 of the twin screw extruder of Examples 1-4.
  • For examples containing 25 weight percent of Exact 3040, the feed rates of thermally conductive filler and Exact 3040 were 2.12 kg/hr (4.67 lb/hr) and 0.65 kg/hr (1.43 lb/hr), respectively. For examples containing 30 percent by weight of Exact 3040, the flow rates of thermally conductive filler and Exact 3040 were 2.27 kg/hr (5.00 lb/hr) and 0.83 kg/hr (1.83 lb/hr), respectively. F-100D microspheres, at a concentration of 0.93 parts by weight per 100 parts by weight of PSA-B, were added downstream to barrel section 7 at a feed rate of 0.3 g/min.
  • In all six temperature zones in the twin screw extruder, the temperature was set at 149° C. (300° F.) except for Zone 4 which was set at 93.5° C. (200° F.). A vacuum (in a range from about −77.9+/−10.2 N/cm2 (−23+/−3 inches of mercury (Hg)) was applied through a port in barrel section 10. The temperatures in the three extruder adapters were 149° C. (300° F.) and the flexible hose at the exit end of the extruder were all set at 165.5° C. (330° F.). The flow rate was controlled with a heated Zenith melt pump, nominally 10.3 cc/rev, set at 149° C. (300° F.).
  • The extrudate was pumped via the heated hose to the single layer drop die of Examples 1-4. The die temperature was set at 182° C. (360° F.). The line speed was adjusted to provide the target thickness as specified in Table 10.
  • The extruded sheet was cast into a nip formed by a two chill rolls (one metal and one rubber), between two silicone coated polyester release liners as in Examples 1-4. The temperature of the chill rolls was set at 7.5° C. (45° F.). One liner was removed as in Examples 1-4 and the resulting article was wound into a roll for subsequent crosslinking.
  • TABLE 10
    Wt. % Wt. % Target Measured
    Conductive Conductive Exact Wt. % Thickness, Thickness, cm
    Ex. No. Filler Filler 3040 F-100D cm (mils) (mils)
    8 95/5 45 25 0.93 0.1016 (40) 0.0724 (28.50)
    Mg(OH)2/
    Al(OH)3
    9 95/5 45 30 0.93 0.1016 (40) 0.0965 (38.0)
    Mg(OH)2/
    Al(OH)3
  • The resultant roll was subjected to gamma radiation at a measured gamma dose between 33.4 to 35.3 kGy (target was 30 kGy).
  • Samples were cut from the irradiated roll and tested for physical properties, and adhesive performance properties according to the Test Methods outlined above with the exception for Dtheor.for which the contribution of expandable microspheres was assumed to be negligible and was not included in the calculation. Results are given in Tables 11 and 12. The test method used was Tensile Break Strength and Elongation Test (Method II).
  • TABLE 11
    Peel
    Density, Adhesion, Impedance, ° C.-
    g/cm3 % kN/m Static Shear, cm2/W
    Ex. (measured/ Void (lb/0.5 in) Minutes (° C.-in2/W)
    No. theoretical) Volume Hardness Al 22° C. 70° C. Zuncorr. Zcorr.
    8 1.314/1.608 18.3 56.0 NT 10,000+ 10,000+ 14.90 18.13
    (2.31) (2.81)
    9 1.263/1.606 21.4 56.5 NT 10,000+ 10,000+ 17.29 22.06
    (2.68) (3.42)
    (a) VLR = very light residue
    LR = light residue
    SB = sample broke, but was still removable
    P = Pass
  • TABLE 12
    Ex. Thickness, Peak Load, % Elongation
    No. cm (mils) kg (lb) at Break
    8 15.7 (40) 5.45 (12.0) 570
    9 16.5 (42) 7.05 (15.5) 1000
  • While the various features of the preferred embodiment of the invention have been described in detail, changes to these features and to the described embodiment may be apparent to those skilled in the art. Such changes or modifications are believed to be within the scope and spirit of the invention, as set forth in the following claims.

Claims (20)

1. A foam thermal interface material comprising a foamed film, the foamed film comprising a blend of polymeric hot melt PSA having a number average molecular weight of greater than 25,000, individual microfibers which are unbroken for at least 0.5 cm in the machine direction, and at least 25 percent by weight of thermally conductive filler, said film having a void volume of at least 5 percent of the volume of said foamed film.
2. The foam thermal interface material of claim 1 wherein the foamed film further comprises a fire retardant.
3. The foam thermal interface material of claim 1 wherein the material has stretch release properties.
4. The foam thermal interface material of claim 1 wherein the microfibers imparting stretch release properties have been formed in situ.
5. The foam thermal interface material of claim 2 wherein the material will pass UL 94 V-2 rating.
6. The foam thermal interface material of claim 1 wherein the void volume ranges from 5 to 75 volume percent of the material.
7. The foam thermal interface material of claim 1 wherein the thermally conductive filler is selected from the group consisting of ceramics, metal oxides, metal hydroxides, and combinations thereof.
8. The foam thermal interface material of claim 1 wherein the polymeric hot melt PSA is selected from acrylic polymer, thermoplastic elastomer, rubber, block copolymer, poly-alpha-olefins, and blends thereof.
9. The foam thermal interface material of claim 1 wherein the thermally conductive filler is selected from the group consisting of boron nitride, silicon nitride, aluminum nitride, titanium nitride, aluminum oxide, beryllia, zirconia, silicon carbide, boron carbide, magnesium hydroxide, magnesium oxide, aluminum hydroxide, and combinations thereof.
10. The foam thermal interface material of claim 1 wherein the thermally conductive filler is present in the foamed film in an amount of at least 40 weight percent.
11. The foam thermal interface material of claim 1 further having a backing adjacent to said foamed film.
12. The foam thermal interface material of claim 11 wherein the backing is thermally conductive.
13. The foam thermal interface material of claim 1 further having at least one adhesive skin layer attached to at least a portion of said foamed film.
14. The foam thermal interface material of claim 13 wherein the at least one adhesive skin layer contains thermally conductive filler.
15. The foam thermal interface material of claim 1 having a bulk conductivity of at least 0.5 Watts/meter-K.
16. A method of conducting heat from an electrical component to a heat sink material comprising the steps of: providing a foam thermal interface material of claim 1; and contacting the foam thermal interface material with an electrical component and a heat sink material such that the foam thermal interface material is between the electrical component and the heat sink material.
17. A thermal interface composition comprising polymeric hot melt PSA having a number average molecular weight of greater than 25,000, individual microfibers which are unbroken for at least 0.5 cm in the machine direction and at least 25 percent by weight of thermally conductive filler, and an effective amount of a foaming agent.
18. The thermal interface composition of claim 17, wherein the thermally conductive filler is selected from the group consisting of ceramics, metal oxides, metal hydroxides, and combinations thereof.
19. The thermal interface composition of claim 17 wherein the polymeric hot melt PSA is selected from acrylic polymer, thermoplastic elastomer, rubber, block copolymer, poly-alpha-olefin, and blends thereof.
20. The thermal interface material of claim 17, wherein the foaming agent is selected from the group consisting of expandable microspheres, physical blowing agents, chemical blowing agents, and combinations thereof.
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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8056257B2 (en) * 2006-11-21 2011-11-15 Tokyo Electron Limited Substrate processing apparatus and substrate processing method
US20110281964A1 (en) * 2008-12-08 2011-11-17 Tesa Se Process for preparing foamable polymer compositions, process for preparing foamed polymer compositions therefrom, foamed polymer compositions and adhesive tape therewith
US20150029671A1 (en) * 2012-01-19 2015-01-29 Sew-Eurodrive Gmbh & Co. Kg Electric Device
US20150275031A1 (en) * 2012-12-18 2015-10-01 Hilti Aktiengesellschaft Insulating layer-forming composition and use thereof
EP2975096A1 (en) * 2014-07-17 2016-01-20 3M Innovative Properties Company Pressure sensitive adhesive assembly suitable for bonding to uneven substrates
EP2975097A1 (en) * 2014-07-17 2016-01-20 3M Innovative Properties Company Pressure sensitive adhesive assembly comprising thermoplastic filler material
US9268366B2 (en) 2013-09-30 2016-02-23 Google Inc. Apparatus related to a structure of a base portion of a computing device
US9430006B1 (en) 2013-09-30 2016-08-30 Google Inc. Computing device with heat spreader
US9442514B1 (en) 2014-07-23 2016-09-13 Google Inc. Graphite layer between carbon layers
US9606587B2 (en) * 2012-10-26 2017-03-28 Google Inc. Insulator module having structure enclosing atomspheric pressure gas
CN107525424A (en) * 2016-06-21 2017-12-29 株式会社西部技研 Heat exchanger and its manufacture method
US20190225054A1 (en) * 2018-01-23 2019-07-25 Borgwarner Ludwigsburg Gmbh Heating device and method for producing a heating rod
WO2020056243A1 (en) * 2018-09-13 2020-03-19 3M Innovative Properties Company Polymeric membrane useful as a commercial roofing membrane

Families Citing this family (97)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7744991B2 (en) * 2003-05-30 2010-06-29 3M Innovative Properties Company Thermally conducting foam interface materials
KR100528925B1 (en) * 2003-09-09 2005-11-15 삼성에스디아이 주식회사 Heat dissipating sheet and plasma display device having the same
JP5068919B2 (en) * 2003-09-25 2012-11-07 スリーエム イノベイティブ プロパティズ カンパニー Foam sheet-forming composition, thermally conductive foam sheet and method for producing the same
KR20060127049A (en) * 2003-12-18 2006-12-11 제온 코포레이션 Thermally conductive pressure-sensitive adhesive composition, thermally conductive sheet-form molded foam, and process for producing the same
DE10361475B4 (en) 2003-12-23 2011-06-09 Lohmann Gmbh & Co Kg Self-adhesive sealing tape for bonding vapor barrier and vapor barrier films, as well as methods of manufacture and use thereof
US20100326645A1 (en) * 2004-01-21 2010-12-30 Wei Fan Thermal pyrolytic graphite laminates with vias
US20050167194A1 (en) * 2004-02-03 2005-08-04 Arner Investments Inc Accoustical Absorption Coating and Process
KR100564620B1 (en) * 2004-03-31 2006-03-29 삼성전자주식회사 Memory module, socket for memory module and mounting method using the same for improving a heat spread characteristics
TWM261006U (en) * 2004-05-28 2005-04-01 Au Optronics Corp Heatsink sheet of optic-electric apparatus
JP2006213845A (en) * 2005-02-04 2006-08-17 Nippon Zeon Co Ltd Heat-conductive pressure-sensitive adhesive sheet-like foamed shaped article and method for producing the same
US20060228542A1 (en) * 2005-04-08 2006-10-12 Saint-Gobain Performance Plastics Corporation Thermal interface material having spheroidal particulate filler
KR100700346B1 (en) * 2005-08-05 2007-03-29 쓰리엠 이노베이티브 프로퍼티즈 캄파니 Heat-transferring adhesive tape with improved functionality
WO2007059264A2 (en) * 2005-11-16 2007-05-24 P.H. Glatfelter Company Marine flexible laminate system
JP4206501B2 (en) * 2006-03-01 2009-01-14 ヤスハラケミカル株式会社 Thermally conductive hot melt adhesive composition
JP5004538B2 (en) * 2006-09-12 2012-08-22 日立化成ポリマー株式会社 Thermally conductive moisture-curing adhesive and its construction method
DE102006062247A1 (en) * 2006-12-22 2008-06-26 Tesa Ag Adhesive layer for bubble-free bonding
US7579686B2 (en) * 2006-12-29 2009-08-25 Intel Corporation Thermal interface material with hotspot heat remover
TWI371833B (en) * 2007-05-24 2012-09-01 Advanced Semiconductor Eng Package structure and electronic device using the same
KR100945039B1 (en) * 2007-06-25 2010-03-05 (주)해은켐텍 Manufacturing method of FPCB
US7965506B1 (en) * 2007-08-22 2011-06-21 Nvidia Corporation Heat sink apparatus and method for allowing air to flow directly to an integrated circuit package thereunder
US8545987B2 (en) * 2007-11-05 2013-10-01 Laird Technologies, Inc. Thermal interface material with thin transfer film or metallization
US9795059B2 (en) 2007-11-05 2017-10-17 Laird Technologies, Inc. Thermal interface materials with thin film or metallization
JP2009263542A (en) * 2008-04-25 2009-11-12 Three M Innovative Properties Co (meth)acrylic adhesive foam and method for producing the same
DE102009001145A1 (en) * 2009-02-25 2010-09-09 Leibniz-Institut Für Polymerforschung Dresden E.V. Method for curing and surface functionalization of molded parts
DE102009015233A1 (en) * 2009-04-01 2010-10-14 Tesa Se Process for producing a foamed mass system
MX2011008921A (en) * 2009-05-05 2011-11-18 Parker Hannifin Corp Thermally conductive foam product.
KR101266195B1 (en) 2009-09-16 2013-05-21 주식회사 엘지화학 Double-sided pressure-sensitive adhesive tape, preparation method thereof and touch panel
WO2011084804A2 (en) * 2009-12-21 2011-07-14 Saint-Gobain Performance Plastics Corporation Thermally conductive foam material
US20140183403A1 (en) 2012-12-27 2014-07-03 Peterson Chemical Technology, Inc. Increasing the Heat Flow of Flexible Cellular Foam Through the Incorporation of Highly Thermally Conductive Solids
US20110265973A1 (en) * 2010-05-03 2011-11-03 Scalia Jr William Henry Passive Heat Exchanger Comprising Thermally Conductive Foam
US9695343B2 (en) 2010-09-30 2017-07-04 3M Innovative Properties Company Hot melt processable pressure sensitive adhesives containing fibrous materials
US20120085391A1 (en) * 2010-10-06 2012-04-12 Uday Varde Structure and method for mounting a photovoltaic material
US10347559B2 (en) 2011-03-16 2019-07-09 Momentive Performance Materials Inc. High thermal conductivity/low coefficient of thermal expansion composites
WO2013155362A1 (en) * 2012-04-13 2013-10-17 3M Innovative Properties Company Pressure sensitive adhesive foams and articles therefrom
US9205605B2 (en) 2012-04-25 2015-12-08 Textron Innovations Inc. Multi-function detection liner for manufacturing of composites
EP2669073A1 (en) * 2012-05-29 2013-12-04 Basf Se Method for producing at least two-layer thermoplastic foam panels by gluing
US20130344712A1 (en) * 2012-06-22 2013-12-26 Apple Inc. Interconnections between flexible and rigid components
US9520378B2 (en) * 2012-12-21 2016-12-13 Intel Corporation Thermal matched composite die
CN103398305B (en) * 2013-07-25 2015-11-25 宁波市爱使电器有限公司 The LED of a kind of high sealing height heat radiation
CN105899714B (en) 2013-12-05 2018-09-21 霍尼韦尔国际公司 Stannous methanesulfonate solution with pH after the adjustment
US9826662B2 (en) * 2013-12-12 2017-11-21 General Electric Company Reusable phase-change thermal interface structures
TWI657132B (en) 2013-12-19 2019-04-21 德商漢高智慧財產控股公司 Compositions having a matrix and encapsulated phase change materials dispersed therein, and electronic devices assembled therewith
US20150218425A1 (en) * 2014-02-05 2015-08-06 Apple Inc. Stretch release conductive adhesive
US10155894B2 (en) 2014-07-07 2018-12-18 Honeywell International Inc. Thermal interface material with ion scavenger
EP3227399B1 (en) 2014-12-05 2021-07-14 Honeywell International Inc. High performance thermal interface materials with low thermal impedance
WO2016103783A1 (en) * 2014-12-26 2016-06-30 リンテック株式会社 Thermally conductive adhesive sheet, method for manufacturing same, and electronic device using same
ES2914973T3 (en) * 2015-03-05 2022-06-20 Henkel Ag & Co Kgaa thermally conductive adhesive
EP3075772B1 (en) * 2015-04-02 2020-08-26 tesa SE Removable adhesive tape
DE102015206076A1 (en) * 2015-04-02 2016-10-06 Tesa Se Removable pressure-sensitive adhesive strip
CN106158790B (en) * 2015-04-10 2018-11-16 台达电子工业股份有限公司 power module and its thermal interface structure
US9828539B2 (en) 2015-06-30 2017-11-28 Laird Technologies, Inc. Thermal interface materials with low secant modulus of elasticity and high thermal conductivity
US10155896B2 (en) 2015-06-30 2018-12-18 Laird Technologies, Inc. Thermal interface materials with low secant modulus of elasticity and high thermal conductivity
US10692797B2 (en) 2015-06-30 2020-06-23 Laird Technologies, Inc. Thermal interface materials with low secant modulus of elasticity and high thermal conductivity
EP3127973B1 (en) * 2015-08-07 2019-04-03 3M Innovative Properties Company Thermally conductive pressure sensitive adhesive
US10312177B2 (en) 2015-11-17 2019-06-04 Honeywell International Inc. Thermal interface materials including a coloring agent
CN105349063B (en) * 2015-12-03 2017-08-04 杭州汉高新材料科技有限公司 Automobile hot-melt foaming pressure sensitive adhesive and its manufacture method
JP6786221B2 (en) * 2016-01-28 2020-11-18 日東電工株式会社 Adhesive sheet
MX2018010819A (en) 2016-03-08 2019-01-14 Honeywell Int Inc Phase change material.
JP2017183617A (en) * 2016-03-31 2017-10-05 積水化学工業株式会社 Foaming composite sheet
US10501671B2 (en) 2016-07-26 2019-12-10 Honeywell International Inc. Gel-type thermal interface material
JP6769801B2 (en) * 2016-09-21 2020-10-14 日東電工株式会社 Manufacturing method for foaming members, electrical and electronic equipment, and foaming materials
KR101832938B1 (en) 2016-11-18 2018-03-23 대준이앤씨 주식회사 Inner and outer wall panel of building with temperature sensitivity
JP6620736B2 (en) * 2016-12-28 2019-12-18 トヨタ自動車株式会社 Composite material and manufacturing method thereof
WO2018136453A1 (en) * 2017-01-17 2018-07-26 Laird Technologies, Inc. Compressible foamed thermal interface materials and methods of making the same
KR101919906B1 (en) * 2017-02-16 2018-11-19 한국과학기술원 Bio-inspired, highly stretchable and conductive dry adhesive, method of manufacturing the same and wearable device including the same
US11041103B2 (en) 2017-09-08 2021-06-22 Honeywell International Inc. Silicone-free thermal gel
US10385469B2 (en) * 2017-09-11 2019-08-20 Toyota Motor Engineering & Manufacturing North America, Inc. Thermal stress compensation bonding layers and power electronics assemblies incorporating the same
US10428256B2 (en) 2017-10-23 2019-10-01 Honeywell International Inc. Releasable thermal gel
US10927228B2 (en) 2017-11-16 2021-02-23 3M Innovative Properties Company Polymer matrix composites comprising intumescent particles and methods of making the same
CN111357061B (en) 2017-11-16 2022-04-12 3M创新有限公司 Polymer matrix composites comprising dielectric particles and methods of making the same
WO2019097445A1 (en) 2017-11-16 2019-05-23 3M Innovative Properties Company Polymer matrix composites comprising thermally conductive particles and methods of making the same
US10913834B2 (en) 2017-11-16 2021-02-09 3M Innovative Properties Company Polymer matrix composites comprising indicator particles and methods of making the same
US11745167B2 (en) 2017-11-16 2023-09-05 3M Innovative Properties Company Polymer matrix composites comprising functional particles and methods of making the same
US11807732B2 (en) 2017-11-16 2023-11-07 3M Innovative Properties Company Method of making polymer matrix composites
US10836873B2 (en) 2017-11-16 2020-11-17 3M Innovative Properties Company Polymer matrix composites comprising thermally insulating particles and methods of making the same
CN108342168B (en) * 2017-12-26 2020-08-07 苏州环明电子科技有限公司 Heat-conducting pressure-sensitive adhesive tape and preparation method and application method thereof
WO2019136151A2 (en) * 2018-01-05 2019-07-11 Neograf Solutions, Llc Thermal interface material
CN110055038A (en) 2018-01-19 2019-07-26 天津莱尔德电子材料有限公司 The non-silicone putty of highly conforming properties and the thermal interfacial material comprising it
US11072706B2 (en) 2018-02-15 2021-07-27 Honeywell International Inc. Gel-type thermal interface material
US11141823B2 (en) * 2018-04-28 2021-10-12 Laird Technologies, Inc. Systems and methods of applying materials to components
US11193016B2 (en) 2018-05-09 2021-12-07 3M Innovative Properties Company Curable and cured compositions
EP3814445B1 (en) 2018-06-14 2023-04-19 3M Innovative Properties Company Method of treating a surface, surface-modified abrasive particles, and resin-bond abrasive articles
EP3807371B1 (en) 2018-06-14 2022-07-27 3M Innovative Properties Company Adhesion promoters for curable compositions
CN109112855A (en) * 2018-07-03 2019-01-01 绍兴百立盛新材料科技有限公司 A kind of concentrator and its preparation method and application with cooling effect
EP3830175B1 (en) 2018-07-30 2022-06-15 3M Innovative Properties Company Foams and methods of making
US10672679B2 (en) * 2018-08-31 2020-06-02 Micron Technology, Inc. Heat spreaders for multiple semiconductor device modules
US11505143B2 (en) * 2019-02-27 2022-11-22 Ford Global Technologies, Llc Supercapacitor mounting assemblies and vehicle mounting locations
US11373921B2 (en) 2019-04-23 2022-06-28 Honeywell International Inc. Gel-type thermal interface material with low pre-curing viscosity and elastic properties post-curing
WO2020229967A1 (en) * 2019-05-15 2020-11-19 3M Innovative Properties Company (co)polymer matrix composites comprising thermally-conductive particles and intumescent particles and methods of making the same
EP3969506A1 (en) * 2019-05-15 2022-03-23 3M Innovative Properties Company (co)polymer matrix composites comprising thermally-conductive particles and endothermic particles and methods of making the same
DE112020005651T5 (en) * 2020-02-21 2022-10-13 Sekisui Polymatech Co., Ltd. HEAT CONDUCTING FOIL AND METHOD OF MAKING THEM
EP4118162A4 (en) * 2020-03-13 2023-11-29 DDP Specialty Electronic Materials US, LLC Thermal interface material comprising magnesium hydroxide
US11814566B2 (en) 2020-07-13 2023-11-14 L&P Property Management Company Thermally conductive nanomaterials in flexible foam
US11597862B2 (en) 2021-03-10 2023-03-07 L&P Property Management Company Thermally conductive nanomaterial coatings on flexible foam or fabrics
CN113444363B (en) * 2021-07-16 2023-03-10 福建三盛实业有限公司 TPE supercritical micropore foaming material and preparation method thereof
US20230160646A1 (en) * 2021-11-19 2023-05-25 Amulaire Thermal Technology, Inc. Immersion heat dissipation structure
CN117374029A (en) * 2023-12-07 2024-01-09 深圳平创半导体有限公司 Silicon carbide device with double-sided heat dissipation structure, method and vehicle electric drive device

Citations (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE24906E (en) * 1955-11-18 1960-12-13 Pressure-sensitive adhesive sheet material
US3725115A (en) * 1970-06-18 1973-04-03 Ppg Industries Inc Pressure-sensitive adhesive articles and method of making same
US4059714A (en) * 1976-08-02 1977-11-22 Nordson Corporation Hot melt thermoplastic adhesive foam system
US4234662A (en) * 1979-04-26 1980-11-18 National Starch And Chemical Corporation Pressure sensitive hot melt adhesive curable by exposure to electron beam radiation
US4310509A (en) * 1979-07-31 1982-01-12 Minnesota Mining And Manufacturing Company Pressure-sensitive adhesive having a broad spectrum antimicrobial therein
US4323557A (en) * 1979-07-31 1982-04-06 Minnesota Mining & Manufacturing Company Pressure-sensitive adhesive containing iodine
US4361663A (en) * 1981-11-09 1982-11-30 Exxon Research And Engineering Co. Pressure sensitive adhesive compositions
US4472480A (en) * 1982-07-02 1984-09-18 Minnesota Mining And Manufacturing Company Low surface energy liner of perfluoropolyether
US4606962A (en) * 1983-06-13 1986-08-19 Minnesota Mining And Manufacturing Company Electrically and thermally conductive adhesive transfer tape
US4851278A (en) * 1986-08-11 1989-07-25 Minnesota Mining And Manufacturing Company Acrylate hot melt adhesive containing zinc carboxylate
US5026742A (en) * 1988-08-20 1991-06-25 Basf Aktiengesellschaft Radiation-crosslinkable contact adhesive mixtures
US5049085A (en) * 1989-12-22 1991-09-17 Minnesota Mining And Manufacturing Company Anisotropically conductive polymeric matrix
US5100728A (en) * 1987-07-01 1992-03-31 Avery Dennison Corporation High performance pressure sensitive adhesive tapes and process for making the same
US5187235A (en) * 1986-10-08 1993-02-16 Avery Dennison Corporation Energy-curable acrylic pressure-sensitive adhesives
US5194455A (en) * 1989-12-21 1993-03-16 Beiersdorf Aktiengesellschaft Acrylate-based hot-melt pressure-sensitive adhesives
US5232970A (en) * 1990-08-31 1993-08-03 The Dow Chemical Company Ceramic-filled thermally-conductive-composites containing fusible semi-crystalline polyamide and/or polybenzocyclobutenes for use in microelectronic applications
US5399416A (en) * 1991-04-24 1995-03-21 Ciba-Geigy Corporation Heat-conductive adhesive films, laminates with heat-conductive adhesive layer and the use thereof
US5416127A (en) * 1993-01-28 1995-05-16 National Starch And Chemical Investment Holding Corporation Radiation curable hot melt pressure sensitive adhesives
US5429856A (en) * 1990-03-30 1995-07-04 Minnesota Mining And Manufacturing Company Composite materials and process
US5550175A (en) * 1992-11-06 1996-08-27 Minnesota Mining And Manufacturing Company Solventless compounding and coating of non-thermoplastic hydrocarbon elastomers
US5738936A (en) * 1996-06-27 1998-04-14 W. L. Gore & Associates, Inc. Thermally conductive polytetrafluoroethylene article
US5753362A (en) * 1994-08-12 1998-05-19 Soken Chemical & Engineering Co., Ltd. Acrylic sheet, acrylic adhesive sheet and processes for preparing the sheets
US5804610A (en) * 1994-09-09 1998-09-08 Minnesota Mining And Manufacturing Company Methods of making packaged viscoelastic compositions
US5890915A (en) * 1996-05-17 1999-04-06 Minnesota Mining And Manufacturing Company Electrical and thermal conducting structure with resilient conducting paths
US5904796A (en) * 1996-12-05 1999-05-18 Power Devices, Inc. Adhesive thermal interface and method of making the same
US6054198A (en) * 1996-04-29 2000-04-25 Parker-Hannifin Corporation Conformal thermal interface material for electronic components
US6103152A (en) * 1998-07-31 2000-08-15 3M Innovative Properties Co. Articles that include a polymer foam and method for preparing same
US6197397B1 (en) * 1996-12-31 2001-03-06 3M Innovative Properties Company Adhesives having a microreplicated topography and methods of making and using same
US6207272B1 (en) * 1997-05-16 2001-03-27 Nitto Denko Corporation Peelable heat-conductive and pressure-sensitive adhesive and adhesive sheet containing the same
US6277488B1 (en) * 1998-10-28 2001-08-21 3M Innovative Properties Company Adhesive composition containing a block copolymer composition and polyphenylene oxide resin and products thereof
US20010055678A1 (en) * 2000-05-15 2001-12-27 Nitto Denko Corporation Heat-peelable pressure-sensitive adhesive sheet
US6432497B2 (en) * 1997-07-28 2002-08-13 Parker-Hannifin Corporation Double-side thermally conductive adhesive tape for plastic-packaged electronic components
US20020128336A1 (en) * 2001-01-08 2002-09-12 Kolb Brant U. Foam including surface-modified nanoparticles
US20020155243A1 (en) * 2001-02-02 2002-10-24 Kobe James J. Adhesive article and method of preparing
US20020165477A1 (en) * 2001-05-02 2002-11-07 Dunshee Wayne K. Tapered stretch removable adhesive articles and methods
US20020187294A1 (en) * 2001-01-17 2002-12-12 3M Innovative Properties Company Pressure sensitive adhesives with a fibrous reinforcing material
US20040241410A1 (en) * 2003-05-30 2004-12-02 Fischer Patrick J. Thermal interface materials and method of making thermal interface materials
US6866928B2 (en) * 2002-04-08 2005-03-15 3M Innovative Properties Company Cleanly removable tapes and methods for the manufacture thereof
US7063887B2 (en) * 2002-02-04 2006-06-20 3M Innovative Properties Company Stretch releasable foams, articles including same and methods for the manufacture thereof
US7744991B2 (en) * 2003-05-30 2010-06-29 3M Innovative Properties Company Thermally conducting foam interface materials

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2093191A1 (en) 1992-04-15 1993-10-16 Richard J. Webb Psa containing thermally conductive, electrically insulative particles and a transfer tape from this psa
CA2273289A1 (en) 1996-11-29 1998-06-04 Takao Yoshikawa Thermally conductive pressure-sensitive adhesive and adhesive sheet containing the same
DE19851166C2 (en) 1998-11-06 2000-11-30 Hermann Otto Gmbh Foamable, electrically and thermally conductive sealants and adhesives, processes for production and their use
JP2001284859A (en) * 2000-03-31 2001-10-12 Jsr Corp Heat-conductive sheet and application thereof
US6630531B1 (en) 2000-02-02 2003-10-07 3M Innovative Properties Company Adhesive for bonding to low surface energy surfaces
JP2001279196A (en) * 2000-03-30 2001-10-10 Sliontec Corp Substrate-free, thermally conductive pressure-sensitive adhesive tape or sheet and method for manufacturing the same
JP2001291807A (en) 2000-04-10 2001-10-19 Three M Innovative Properties Co Thermo-conductive sheet
JP2001311008A (en) * 2000-04-28 2001-11-09 Three M Innovative Properties Co Thermal conductive sheet
JP2002030212A (en) * 2000-06-29 2002-01-31 Three M Innovative Properties Co Thermally conductive sheet
JP2002080817A (en) * 2000-09-04 2002-03-22 Three M Innovative Properties Co Crosslinked, expanded adhesive and its preparation process
JP4584439B2 (en) * 2000-10-30 2010-11-24 アキレス株式会社 Heat dissipation resin sheet
JP2002128931A (en) 2000-10-30 2002-05-09 Sekisui Chem Co Ltd Thermally conductive resin sheet
US7078582B2 (en) * 2001-01-17 2006-07-18 3M Innovative Properties Company Stretch removable adhesive articles and methods
JP4660949B2 (en) * 2001-03-27 2011-03-30 日本ゼオン株式会社 Pressure-sensitive adhesive composition and sheet using the same
JP2002294192A (en) * 2001-03-29 2002-10-09 Three M Innovative Properties Co Thermally conductive flame-retardant pressure- sensitive adhesive and sheet by forming the same
JP2002317064A (en) * 2001-04-20 2002-10-31 Sekisui Chem Co Ltd Thermoconductive material
JP2003049144A (en) 2001-08-08 2003-02-21 Sekisui Chem Co Ltd Heat-conductive pressure-sensitive adhesive and heat- conductive pressure-sensitive adhesive sheet
US20030175497A1 (en) 2002-02-04 2003-09-18 3M Innovative Properties Company Flame retardant foams, articles including same and methods for the manufacture thereof
DE10259451A1 (en) 2002-12-19 2004-07-08 Tesa Ag PSA article with at least one layer of a thermally conductive PSA and process for its production
EP1433829A1 (en) 2002-12-23 2004-06-30 3M Innovative Properties Company Thermally-formable and cross-linkable precursor of a thermally conductive material

Patent Citations (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE24906E (en) * 1955-11-18 1960-12-13 Pressure-sensitive adhesive sheet material
US3725115A (en) * 1970-06-18 1973-04-03 Ppg Industries Inc Pressure-sensitive adhesive articles and method of making same
US4059714A (en) * 1976-08-02 1977-11-22 Nordson Corporation Hot melt thermoplastic adhesive foam system
US4234662A (en) * 1979-04-26 1980-11-18 National Starch And Chemical Corporation Pressure sensitive hot melt adhesive curable by exposure to electron beam radiation
US4310509A (en) * 1979-07-31 1982-01-12 Minnesota Mining And Manufacturing Company Pressure-sensitive adhesive having a broad spectrum antimicrobial therein
US4323557A (en) * 1979-07-31 1982-04-06 Minnesota Mining & Manufacturing Company Pressure-sensitive adhesive containing iodine
US4361663A (en) * 1981-11-09 1982-11-30 Exxon Research And Engineering Co. Pressure sensitive adhesive compositions
US4472480A (en) * 1982-07-02 1984-09-18 Minnesota Mining And Manufacturing Company Low surface energy liner of perfluoropolyether
US4606962A (en) * 1983-06-13 1986-08-19 Minnesota Mining And Manufacturing Company Electrically and thermally conductive adhesive transfer tape
US4851278A (en) * 1986-08-11 1989-07-25 Minnesota Mining And Manufacturing Company Acrylate hot melt adhesive containing zinc carboxylate
US5187235A (en) * 1986-10-08 1993-02-16 Avery Dennison Corporation Energy-curable acrylic pressure-sensitive adhesives
US5100728A (en) * 1987-07-01 1992-03-31 Avery Dennison Corporation High performance pressure sensitive adhesive tapes and process for making the same
US5026742A (en) * 1988-08-20 1991-06-25 Basf Aktiengesellschaft Radiation-crosslinkable contact adhesive mixtures
US5194455A (en) * 1989-12-21 1993-03-16 Beiersdorf Aktiengesellschaft Acrylate-based hot-melt pressure-sensitive adhesives
US5049085A (en) * 1989-12-22 1991-09-17 Minnesota Mining And Manufacturing Company Anisotropically conductive polymeric matrix
US5429856A (en) * 1990-03-30 1995-07-04 Minnesota Mining And Manufacturing Company Composite materials and process
US5232970A (en) * 1990-08-31 1993-08-03 The Dow Chemical Company Ceramic-filled thermally-conductive-composites containing fusible semi-crystalline polyamide and/or polybenzocyclobutenes for use in microelectronic applications
US5399416A (en) * 1991-04-24 1995-03-21 Ciba-Geigy Corporation Heat-conductive adhesive films, laminates with heat-conductive adhesive layer and the use thereof
US5550175A (en) * 1992-11-06 1996-08-27 Minnesota Mining And Manufacturing Company Solventless compounding and coating of non-thermoplastic hydrocarbon elastomers
US5416127A (en) * 1993-01-28 1995-05-16 National Starch And Chemical Investment Holding Corporation Radiation curable hot melt pressure sensitive adhesives
US5753362A (en) * 1994-08-12 1998-05-19 Soken Chemical & Engineering Co., Ltd. Acrylic sheet, acrylic adhesive sheet and processes for preparing the sheets
US5932298A (en) * 1994-09-09 1999-08-03 Minnesota Mining And Manufacturing Company Methods of making packaged viscoelastic compositions
US5804610A (en) * 1994-09-09 1998-09-08 Minnesota Mining And Manufacturing Company Methods of making packaged viscoelastic compositions
US6054198A (en) * 1996-04-29 2000-04-25 Parker-Hannifin Corporation Conformal thermal interface material for electronic components
US5890915A (en) * 1996-05-17 1999-04-06 Minnesota Mining And Manufacturing Company Electrical and thermal conducting structure with resilient conducting paths
US5738936A (en) * 1996-06-27 1998-04-14 W. L. Gore & Associates, Inc. Thermally conductive polytetrafluoroethylene article
US5904796A (en) * 1996-12-05 1999-05-18 Power Devices, Inc. Adhesive thermal interface and method of making the same
US6197397B1 (en) * 1996-12-31 2001-03-06 3M Innovative Properties Company Adhesives having a microreplicated topography and methods of making and using same
US6207272B1 (en) * 1997-05-16 2001-03-27 Nitto Denko Corporation Peelable heat-conductive and pressure-sensitive adhesive and adhesive sheet containing the same
US6432497B2 (en) * 1997-07-28 2002-08-13 Parker-Hannifin Corporation Double-side thermally conductive adhesive tape for plastic-packaged electronic components
US6103152A (en) * 1998-07-31 2000-08-15 3M Innovative Properties Co. Articles that include a polymer foam and method for preparing same
US6277488B1 (en) * 1998-10-28 2001-08-21 3M Innovative Properties Company Adhesive composition containing a block copolymer composition and polyphenylene oxide resin and products thereof
US20010055678A1 (en) * 2000-05-15 2001-12-27 Nitto Denko Corporation Heat-peelable pressure-sensitive adhesive sheet
US20020128336A1 (en) * 2001-01-08 2002-09-12 Kolb Brant U. Foam including surface-modified nanoparticles
US20020187294A1 (en) * 2001-01-17 2002-12-12 3M Innovative Properties Company Pressure sensitive adhesives with a fibrous reinforcing material
US20020155243A1 (en) * 2001-02-02 2002-10-24 Kobe James J. Adhesive article and method of preparing
US20020165477A1 (en) * 2001-05-02 2002-11-07 Dunshee Wayne K. Tapered stretch removable adhesive articles and methods
US7063887B2 (en) * 2002-02-04 2006-06-20 3M Innovative Properties Company Stretch releasable foams, articles including same and methods for the manufacture thereof
US6866928B2 (en) * 2002-04-08 2005-03-15 3M Innovative Properties Company Cleanly removable tapes and methods for the manufacture thereof
US20040241410A1 (en) * 2003-05-30 2004-12-02 Fischer Patrick J. Thermal interface materials and method of making thermal interface materials
US7229683B2 (en) * 2003-05-30 2007-06-12 3M Innovative Properties Company Thermal interface materials and method of making thermal interface materials
US7744991B2 (en) * 2003-05-30 2010-06-29 3M Innovative Properties Company Thermally conducting foam interface materials

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8056257B2 (en) * 2006-11-21 2011-11-15 Tokyo Electron Limited Substrate processing apparatus and substrate processing method
US20110281964A1 (en) * 2008-12-08 2011-11-17 Tesa Se Process for preparing foamable polymer compositions, process for preparing foamed polymer compositions therefrom, foamed polymer compositions and adhesive tape therewith
US9200129B2 (en) * 2010-12-08 2015-12-01 Tesa Se Process for preparing foamable polymer compositions, process for preparing foamed polymer compositions therefrom, foamed polymer compositions and adhesive tape therewith
US20150029671A1 (en) * 2012-01-19 2015-01-29 Sew-Eurodrive Gmbh & Co. Kg Electric Device
US9949404B2 (en) * 2012-01-19 2018-04-17 Sew-Eurodrive Gmbh & Co. Kg Electric device
US9606587B2 (en) * 2012-10-26 2017-03-28 Google Inc. Insulator module having structure enclosing atomspheric pressure gas
US20150275031A1 (en) * 2012-12-18 2015-10-01 Hilti Aktiengesellschaft Insulating layer-forming composition and use thereof
US10000659B2 (en) * 2012-12-18 2018-06-19 Hilti Aktiengesellschaft Insulating layer-forming composition and use thereof
US9430006B1 (en) 2013-09-30 2016-08-30 Google Inc. Computing device with heat spreader
US9268366B2 (en) 2013-09-30 2016-02-23 Google Inc. Apparatus related to a structure of a base portion of a computing device
EP2975097A1 (en) * 2014-07-17 2016-01-20 3M Innovative Properties Company Pressure sensitive adhesive assembly comprising thermoplastic filler material
US10501591B2 (en) 2014-07-17 2019-12-10 3M Innovative Properties Company Pressure sensitive adhesive assembly suitable for bonding to uneven substrates
WO2016011152A1 (en) * 2014-07-17 2016-01-21 3M Innovative Properties Company Pressure sensitive adhesive assembly suitable for bonding to uneven substrates
US11332648B2 (en) 2014-07-17 2022-05-17 3M Innovative Properties Company Pressure sensitive adhesive assembly comprising thermoplastic filler material
WO2016010803A1 (en) * 2014-07-17 2016-01-21 3M Innovative Properties Company Pressure sensitive adhesive assembly comprising thermoplastic filler material
EP2975096A1 (en) * 2014-07-17 2016-01-20 3M Innovative Properties Company Pressure sensitive adhesive assembly suitable for bonding to uneven substrates
US10633495B2 (en) 2014-07-17 2020-04-28 3M Innovative Properties Company Pressure sensitive adhesive assembly suitable for bonding to uneven substrates
US9442514B1 (en) 2014-07-23 2016-09-13 Google Inc. Graphite layer between carbon layers
CN107525424A (en) * 2016-06-21 2017-12-29 株式会社西部技研 Heat exchanger and its manufacture method
US20190225054A1 (en) * 2018-01-23 2019-07-25 Borgwarner Ludwigsburg Gmbh Heating device and method for producing a heating rod
WO2020056243A1 (en) * 2018-09-13 2020-03-19 3M Innovative Properties Company Polymeric membrane useful as a commercial roofing membrane
WO2020056238A1 (en) * 2018-09-13 2020-03-19 3M Innovative Properties Company Polymeric membrane useful as a commercial roofing membrane
WO2020056245A1 (en) * 2018-09-13 2020-03-19 3M Innovative Properties Company Polymeric membrane useful as a commercial roofing membrane
CN112639002A (en) * 2018-09-13 2021-04-09 3M创新有限公司 Foam composition and process for preparing the same
US20220055264A1 (en) * 2018-09-13 2022-02-24 3M Innovative Properties Company Polymeric Membrane Useful As A Commercial Roofing Membrane
EP3849801A4 (en) * 2018-09-13 2022-07-13 3M Innovative Properties Company Polymeric membrane useful as a commercial roofing membrane

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