US2378642A - Process of making fiber-body articles - Google Patents

Process of making fiber-body articles Download PDF

Info

Publication number
US2378642A
US2378642A US409220A US40922041A US2378642A US 2378642 A US2378642 A US 2378642A US 409220 A US409220 A US 409220A US 40922041 A US40922041 A US 40922041A US 2378642 A US2378642 A US 2378642A
Authority
US
United States
Prior art keywords
die
mat
work
binder
fibers
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.)
Expired - Lifetime
Application number
US409220A
Inventor
Karl J Kopplin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BURKART Manufacturing Co F
F BURKART MANUFACTURING Co
Original Assignee
BURKART Manufacturing Co F
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by BURKART Manufacturing Co F filed Critical BURKART Manufacturing Co F
Priority to US409220A priority Critical patent/US2378642A/en
Application granted granted Critical
Publication of US2378642A publication Critical patent/US2378642A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
    • B29C51/002Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor characterised by the choice of material
    • B29C51/004Textile or other fibrous material made from plastics fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
    • B29C51/08Deep drawing or matched-mould forming, i.e. using mechanical means only
    • B29C51/082Deep drawing or matched-mould forming, i.e. using mechanical means only by shaping between complementary mould parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D22/00Producing hollow articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2021/00Use of unspecified rubbers as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0854Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns in the form of a non-woven mat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2311/00Use of natural products or their composites, not provided for in groups B29K2201/00 - B29K2309/00, as reinforcement
    • B29K2311/10Natural fibres, e.g. wool or cotton
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/48Wearing apparel
    • B29L2031/4807Headwear
    • B29L2031/4814Hats
    • B29L2031/4821Helmets
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S264/00Plastic and nonmetallic article shaping or treating: processes
    • Y10S264/64Processes of using preform in molding

Definitions

  • My invention relates to the utilization of long fibers in the manufacture of hollow or deeply drawn products.
  • the principal object or the'invention is to devise a method whereby long fibers. such as raw sisal, can be drawn into hollow products of substantial tensile strength in various directions ready for divers uses such as foundations for upholstery, helmet linings or coverings and cushions for other articles, and as preforms" for further processing into resin bound articles.
  • the invention consists in the described and claimed. 1 V
  • FIE. 1 is a plan view and P18. 2 is a cross-sectional view of a fiber blank, Fig. 3 shows the blank or work-piece in its initial position relative to aforming die,
  • Fig. 5 illustrates the work-piece or preform in relation to the forming die with the plunger at the end of its forming stroke
  • Figs. 5 and 6 illustrate a preform in relation to a pressure die in its initial position and at the end of'its forward stroke. respectively
  • Fig. 'l is a view of a finished product, Fig.8isavieworafiatblankwitharinsof latex thereon;
  • Fig. 9 is a sectional view of a preform ready for entryinto the pressure die, and showing the distribution of the latex and. binder thereon.
  • the present process starts with a substantially fiat mat of long unwoven fiber, preferably raw sisal, laidloosely in layers, as by a camel-back machine, with the fibers of adjacent layers disposed in the same; general direction and criss-, cross in relation to the fibers of adjacent layers, thereby forming a loose mat that is somewhat compacted and stabilized by the operation or needling which forms some of the fibers into loops 'or bights that extend transversely through the ,mat and serve as transverse ties therefor.
  • many of the individual fibers which may be a yard or more long, zig-zag crosswise or the mat and, being loosely laid, are more 'or less crooked or curved.
  • a blank I of suitable size is cut from the stabllized or needled mat and the blank, without I further preparation or treatment, is laid over the end of the hollow member 2 of a forming die.
  • the plunger 3 of the forming die is then actuated to force the blank or work-piece I into the hollow oi the die to become a "preform" A or prodnot, depending on its use. Due to the facts that the fibers were crooked and loosely laid, and that process hereinafter there is no adhesive or binding material in the blank or work-piece, the long fibers of the workpiece adjust themselves to the shape of the mold and are held by friction in their adjusted positions.
  • the work-piece contracts circumferentially somewhat after the manner of a metal plate in the operation of drawing.
  • the structural looseness of the work-piece enable those fibers, that are disposed more or less radially with relation to the axis of the die, to crowd closer together by shifting their position circumferentially and thereby adapt themselves'to the die, while the same loosenes of the work-piece enables those fibers that are disposed more or less circumferentially to adapt themselves to the changing situation by bending or kinking individually and remaining relatively slack, at least in sections, in the product.
  • this die-forming In this die-forming.
  • the criss-cross arrangement '0! the fibers is an important factor in maintaining the 80 integrity of the work-piece and adequate strength thereof at all points and in all directions.
  • the operations hereinbefore described are carried out without applying any latexor bindingmaterial .to the work-piece, as, due to frictional engagement of the fibers, the preform thus produced has sufficient stability of shape and dimensions for convenient handling, such as entering into a pressure die.
  • the natural springiness of the sisal or other fibers tends to'enlarge the diameter of the hollow produced therein by the forming die and make the subsequent handling thereof somewhat more difilcult.
  • pressure plate I whose pressure is exerted by means of springs O that are preferably made ad- Justable to regulate the clamping pressure.
  • the proper clamping pressure is high enough to insure stretching or drawing ofthe work-piece quantity of thermo-plastic binder is helpful in stiffening and stabilizing the preform.
  • the present invention permits the use of long fibers in substantially their raw condition, that is, without disentangling the natural vascular bundles in which they occur. It requires a minimum Oi. preparation of the fibers, namely, merely carding, laying preferably with a camel-back machine, and needling.
  • the fibers in the mat are of their full natural length and the only cutting of the fibers is that due to the cutting of blanks from the mat and to the trimming of the work-piece.
  • the foregoing operation of die-forming the work-piece into a preform may slightlydecrease the thickness thereof but is not ordinarily relied upon for this purpose.
  • a suitable liquid binder is applied to the hollow portion and portion adjacent thereto and the "preform is then placed in a heated pressure die I, I and compressed to substantially decrease the thickness thereof, say, for instance, to about one-third its thickness before pressing.
  • the preform is thus converted into a resin-bound product which may be complete in itself or further processed if desired.
  • the binder is a thermo-setting synthetic resin and the die is heated so that, in the process of die-pressin the binder flows into the voids, or interstices between fibers, and sets and thereby stabilizes the work at the size, shape and thickness produced by the pressure die.
  • Synthetic thermo-setting resins suitable for this purpose include the phenolformaldehyde and ureaformaldehyde condensation products.
  • thermo-plastic binders such as ethyl-cellulose or vinyl chloride'resin, in-whioh case the temperature of the pressure die or mould is lowered below the softening point of the binder so as to set the binder before removal of the work-piece from the die.
  • binder in the proportion of ten percent of binder to ninety percent of fiber is sufllcient to stabilize the article for some uses. On the other hand, as much as fifty percent of binder may be required to obtain maximum moisture resistance and a high polish finish.
  • thermo-settin that is, heat hardenable, binder
  • a thermoplastic binder or a thermo-settin that is, heat hardenable, binder may be used, as above stated.
  • a thermo-plastlc binder is used in the manufacture of a deep drawn article, it is convenient to use some of the binder in the preforming operation by applying a small quantity thereof to the region of the fiat work-piece that lies adia-
  • Another important advantage is that all pulpin of the material is dispensed with.
  • the invention makes it practicable to use raw sisal fiber which has a remarkable tensile strength and is quite inexpensive.
  • the work-piece may be consideredas complete as soon as the initial shaping thereof is completed, that is, without being treated with a resinoid binder and die-pressed.
  • the shaped, but uncompressed, work without binder may be used as foundations for upholstery. particularly automobile arm rests, or as linings and covers for hats. helmets and containers or as cushions for other articles.
  • plastic-bound longfiber hollow articles which consists in starting with a loose unwoven mat of long fibers laid crisscross in layers, forming said mat in a hollow forming die after applying a binder to said mat in the form of a band that surrounds the hollow in said hollow forming die, then applying binder to the formed work and die pressing the same in a hollow die.
  • plastic-bound longfiberv hollow articles which consists in starting with a loose unwoven and relatively thick mat of, long sisal fibers laid cries-cross, applying a limited quantity of latex to a surface thereof in the form of a closed band, lightly pressing the portion of the mat surrounded by said band into a flaring hollow die of smaller radius than said band, applying liquid binder to the lightly pressed work at the rate of from about 1 ounce to about 2.5 ounces of binder per square foot of said work, and die pressing the lightly pressed work in a hot hollow die to a thickness of less than one third that of the loose mat.
  • plastic-bound longfiber hollow articles which comprises starting with a loose unwoven mat of long fibers loosely laid cries-cross, clamping said mat fiatwise against the end face of a hollow forming die tight enough to compel the mat to stretch under the pressure of a die but loose enough to permit slippage of the mat and prevent breaking of the fibers when the pressure of the die plunger exceeds a predetermined amount, after applying a band of liquid binder to the portion'ofthe mat shortlybeyond the margin of the hollow forming aiefriaanmaemtoe miermm die to produce a loose hollow blank, applying liquid 7 fiber hollow articles which comprises starting with a loose unwoven mat of long fibers loosely laid criss-cross, clamping said mat fiatwise against the end face of a hollow forming die tight enough to compel the mat to stretch under the pressure of a die but loose enough to permit slippage of the mat and prevent breaking of the fibers when the pressure of the die plunger exceeds a predetermined amount
  • plastic-bound longfiber hollow articles which consists in starting 'witha loose unwoven mat of long fibers laid in criss-cross layers, ⁇ orming said mat in a forming die after applying latex to said mat in the form of a band that surrounds and is of greater diameter than the main body of the forming die, then applying binder to the formed work and die pressing the same in a hollow'die.
  • plastic-bound long fiber hollow articles which comprises starting with a loose unwoven mat of long fibers loosely laid criss-cross, clamping said mat fiatwise against the end face of a hollow forming die tight enough to compel the mat to stretch under the

Description

June-19, 1945. K. J, KOPPLIN PROCESS OF MAKING FIBER-BODY ARTICLES Filed Sept. 2, 1941 2 Sheets-Sheet 1 MI l/gA/roe 4/5 flrroRMsYs.
June 19, 1945. K. J. KOPPLIN 2,378,642
PROCESS OF MAKING FIBER-BODY ARTICLES Filed Sept. 2, 1941 2 Sheets-Sheet 2 mama June 19, 1945 UNITED STATES, PATENT "oF'ncE Karl J. Kopplin, hlormandy hlm, aesignor to F.
Burks-rt Mann! tflfllll Company, St. Louis,
Mos a corporation of Missouri Application September a, 1941, Serial No. 409,220
1 Claims. (01. 1 -56),
My invention relates to the utilization of long fibers in the manufacture of hollow or deeply drawn products. The principal object or the'invention is to devise a method whereby long fibers. such as raw sisal, can be drawn into hollow products of substantial tensile strength in various directions ready for divers uses such as foundations for upholstery, helmet linings or coverings and cushions for other articles, and as preforms" for further processing into resin bound articles. The invention consists in the described and claimed. 1 V
In the accompanying drawings, wherein like reference numerals refer to like parts wherever theyoccur,
FIE. 1 is a plan view and P18. 2 is a cross-sectional view of a fiber blank, Fig. 3 shows the blank or work-piece in its initial position relative to aforming die,
Fig. 5 illustrates the work-piece or preform in relation to the forming die with the plunger at the end of its forming stroke,
.Figs. 5 and 6 illustrate a preform in relation to a pressure die in its initial position and at the end of'its forward stroke. respectively,
Fig. 'l is a view of a finished product, Fig.8isavieworafiatblankwitharinsof latex thereon; and
Fig. 9 is a sectional view of a preform ready for entryinto the pressure die, and showing the distribution of the latex and. binder thereon.
The present process starts with a substantially fiat mat of long unwoven fiber, preferably raw sisal, laidloosely in layers, as by a camel-back machine, with the fibers of adjacent layers disposed in the same; general direction and criss-, cross in relation to the fibers of adjacent layers, thereby forming a loose mat that is somewhat compacted and stabilized by the operation or needling which forms some of the fibers into loops 'or bights that extend transversely through the ,mat and serve as transverse ties therefor. In such I a mat, many of the individual fibers, which may be a yard or more long, zig-zag crosswise or the mat and, being loosely laid, are more 'or less crooked or curved.
A blank I of suitable sizeis cut from the stabllized or needled mat and the blank, without I further preparation or treatment, is laid over the end of the hollow member 2 of a forming die. The plunger 3 of the forming die is then actuated to force the blank or work-piece I into the hollow oi the die to become a "preform" A or prodnot, depending on its use. Due to the facts that the fibers were crooked and loosely laid, and that process hereinafter there is no adhesive or binding material in the blank or work-piece, the long fibers of the workpiece adjust themselves to the shape of the mold and are held by friction in their adjusted positions. Thus, the work-piece, as distinguished y .beyond the hollow oi the die, contracts circumferentially somewhat after the manner of a metal plate in the operation of drawing. The structural looseness of the work-piece enable those fibers, that are disposed more or less radially with relation to the axis of the die, to crowd closer together by shifting their position circumferentially and thereby adapt themselves'to the die, while the same loosenes of the work-piece enables those fibers that are disposed more or less circumferentially to adapt themselves to the changing situation by bending or kinking individually and remaining relatively slack, at least in sections, in the product. In this die-forming.
operation, the criss-cross arrangement '0! the fibers is an important factor in maintaining the 80 integrity of the work-piece and adequate strength thereof at all points and in all directions. Ordinarily, the operations hereinbefore described are carried out without applying any latexor bindingmaterial .to the work-piece, as, due to frictional engagement of the fibers, the preform thus produced has sufficient stability of shape and dimensions for convenient handling, such as entering into a pressure die. When, however, an untreated work-piece is deeply drawn, the natural springiness of the sisal or other fibers tends to'enlarge the diameter of the hollow produced therein by the forming die and make the subsequent handling thereof somewhat more difilcult. For this reason, it is desirable to spray a limited amount or liquid latex (say about /2 ounce of latex containing about fifty percent solids per square foot of surface) on one or both surfaces of the flat work-piece in the quickly evaporated and the small film or elastic latex remaining on the blank in the form of a band or ring ,does not seriously interfere with the ability of the fibers to adjust themselves to the mold, while, on the other hand, the ring of latex remainins in the "preform" acts as an elastic binder to stabilize and fix the dimensions of the hollow thereof. Instead of latex. other binder may be used that will not seriously interfere with the slippage or adjustment of the fibers; 1
c When the blank or work-piece is to be drawn only to a shallow depth. it is not necessary to clamp the edges thereof. But when the workpiece is to be deeply drawn, the edges thereof are clamped against the end face of the die by a' amass:
pressure plate I whose pressure is exerted by means of springs O that are preferably made ad- Justable to regulate the clamping pressure. The proper clamping pressure is high enough to insure stretching or drawing ofthe work-piece quantity of thermo-plastic binder is helpful in stiffening and stabilizing the preform.
In practice, it is convenient to trim the work piece while it is in the dieby means of a cutter t mounted on the die plunger.
Among the advantages of the present invention are the following: it permits the use of long fibers in substantially their raw condition, that is, without disentangling the natural vascular bundles in which they occur. It requires a minimum Oi. preparation of the fibers, namely, merely carding, laying preferably with a camel-back machine, and needling. The fibers in the mat are of their full natural length and the only cutting of the fibers is that due to the cutting of blanks from the mat and to the trimming of the work-piece.
to the required depth but low enough to permit 1 slippage of the work-piece when the tension therein, due to the force ofthe plunger, threatens to break the fibers.
The foregoing operation of die-forming the work-piece into a preform may slightlydecrease the thickness thereof but is not ordinarily relied upon for this purpose. After making the preform," a suitable liquid binder is applied to the hollow portion and portion adjacent thereto and the "preform is then placed in a heated pressure die I, I and compressed to substantially decrease the thickness thereof, say, for instance, to about one-third its thickness before pressing. The preform is thus converted into a resin-bound product which may be complete in itself or further processed if desired. Preferably the binder is a thermo-setting synthetic resin and the die is heated so that, in the process of die-pressin the binder flows into the voids, or interstices between fibers, and sets and thereby stabilizes the work at the size, shape and thickness produced by the pressure die. Synthetic thermo-setting resins suitable for this purpose include the phenolformaldehyde and ureaformaldehyde condensation products. In some instances it maybe desirable to use thermo-plastic binders, such as ethyl-cellulose or vinyl chloride'resin, in-whioh case the temperature of the pressure die or mould is lowered below the softening point of the binder so as to set the binder before removal of the work-piece from the die.
l The amount of binder required is dependent upon the characteristics desired in the finished article. For example, binder in the proportion of ten percent of binder to ninety percent of fiber is sufllcient to stabilize the article for some uses. On the other hand, as much as fifty percent of binder may be required to obtain maximum moisture resistance and a high polish finish.
In carrying out my process, either a thermoplastic binder or a thermo-settin that is, heat hardenable, binder may be used, as above stated. When a thermo-plastlc binder is used in the manufacture of a deep drawn article, it is convenient to use some of the binder in the preforming operation by applying a small quantity thereof to the region of the fiat work-piece that lies adia- Another important advantage is that all pulpin of the material is dispensed with. Another advantage is that the invention makes it practicable to use raw sisal fiber which has a remarkable tensile strength and is quite inexpensive.
For many uses, the work-piece may be consideredas complete as soon as the initial shaping thereof is completed, that is, without being treated with a resinoid binder and die-pressed. For instance, the shaped, but uncompressed, work without binder may be used as foundations for upholstery. particularly automobile arm rests, or as linings and covers for hats. helmets and containers or as cushions for other articles. For such uses, it is preferably to spray one Or both surfaces of the work-piecewith a limited amount of latex or like elastic material, say at the rate of about one ounce of liquid latex containing about fifty percent solids, per square foot of surface sufficient to stabilize the shape and serve as an elastic binder at and adjacent to one or both surfaces of the work-piece without filling the voids in such work-piece.
What I claim is: I r
1. The process of making plastic-bound longfiber hollow articles which consists in starting with a loose unwoven mat of long fibers laid crisscross in layers, forming said mat in a hollow forming die after applying a binder to said mat in the form of a band that surrounds the hollow in said hollow forming die, then applying binder to the formed work and die pressing the same in a hollow die.
2. The process of making plastic-bound longfiberv hollow articles which consists in starting with a loose unwoven and relatively thick mat of, long sisal fibers laid cries-cross, applying a limited quantity of latex to a surface thereof in the form of a closed band, lightly pressing the portion of the mat surrounded by said band into a flaring hollow die of smaller radius than said band, applying liquid binder to the lightly pressed work at the rate of from about 1 ounce to about 2.5 ounces of binder per square foot of said work, and die pressing the lightly pressed work in a hot hollow die to a thickness of less than one third that of the loose mat.
3. The process of making plastic-bound longfiber hollow articles which comprises starting with a loose unwoven mat of long fibers loosely laid cries-cross, clamping said mat fiatwise against the end face of a hollow forming die tight enough to compel the mat to stretch under the pressure of a die but loose enough to permit slippage of the mat and prevent breaking of the fibers when the pressure of the die plunger exceeds a predetermined amount, after applying a band of liquid binder to the portion'ofthe mat shortlybeyond the margin of the hollow forming aiefriaanmaemtoe miermm die to produce a loose hollow blank, applying liquid 7 fiber hollow articles which comprises starting with a loose unwoven mat of long fibers loosely laid criss-cross, clamping said mat fiatwise against the end face of a hollow forming die tight enough to compel the mat to stretch under the pressure of a die but loose enough to permit slippage of the mat and prevent breaking of the fibers when the pressure of the die plunger exceeds a predetermined amount, after applying a band of liquid binder to the portion 01' the mat shortly beyond the margin of the-hollow forming die, forcing said mat into said forming die to produce a loose hollow blank, applying thermo-setting binder to said loose blank and then compressing said loose blank.
5. The process which consists in forming an annular film of latex on the surface of a loose unwoven and relatively thick mat of long sisal fibers laid criss-cross and then die forming with light pressure the portion of the mat surrounded by said band. r
6. The process of making plastic-bound longfiber hollow articles which consists in starting 'witha loose unwoven mat of long fibers laid in criss-cross layers, {orming said mat in a forming die after applying latex to said mat in the form of a band that surrounds and is of greater diameter than the main body of the forming die, then applying binder to the formed work and die pressing the same in a hollow'die.
'7. The process of making plastic-bound long fiber hollow articles which comprises starting with a loose unwoven mat of long fibers loosely laid criss-cross, clamping said mat fiatwise against the end face of a hollow forming die tight enough to compel the mat to stretch under the
US409220A 1941-09-02 1941-09-02 Process of making fiber-body articles Expired - Lifetime US2378642A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US409220A US2378642A (en) 1941-09-02 1941-09-02 Process of making fiber-body articles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US409220A US2378642A (en) 1941-09-02 1941-09-02 Process of making fiber-body articles

Publications (1)

Publication Number Publication Date
US2378642A true US2378642A (en) 1945-06-19

Family

ID=23619551

Family Applications (1)

Application Number Title Priority Date Filing Date
US409220A Expired - Lifetime US2378642A (en) 1941-09-02 1941-09-02 Process of making fiber-body articles

Country Status (1)

Country Link
US (1) US2378642A (en)

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2444394A (en) * 1943-03-11 1948-06-29 Lane Wells Co Method of molding diaphragms
US2452999A (en) * 1944-06-28 1948-11-02 Us Rubber Co Method of making cellular thermoplastic receptacles
US2462940A (en) * 1946-10-02 1949-03-01 Columbian Rope Co Low-pressure molding
US2521985A (en) * 1948-09-16 1950-09-12 American Felt Co Process of making fibrous units
US2536713A (en) * 1947-11-17 1951-01-02 Berg John Wesley Method of making picture frames
US2672176A (en) * 1946-04-03 1954-03-16 Briggs Mfg Co Die apparatus for making laminated panels
US2681599A (en) * 1948-01-27 1954-06-22 American Cyanamid Co Molding pulp and impregnating the product
US2697057A (en) * 1948-12-23 1954-12-14 Ortho Pharma Corp Method of making a diaphragm
US2701893A (en) * 1951-08-06 1955-02-15 Joseph Lincoln Mfg Company Inc Apparatus for making hat covers
US2845699A (en) * 1955-12-13 1958-08-05 Lee L Woodard Sons Method of making contoured dished articles
US2854696A (en) * 1949-11-30 1958-10-07 Kreibaum Otto Method for the production of molded articles
US2951780A (en) * 1955-10-19 1960-09-06 Gen Am Transport Methods of making decorative glass fiber reinforced resin bodies
US3000429A (en) * 1956-06-22 1961-09-19 Studebaker Packard Corp Machine for prestressing and molding reinforced plastic members
US3018210A (en) * 1955-05-09 1962-01-23 Gentex Corp Ballistic helmet and method of making same
US3097125A (en) * 1960-02-02 1963-07-09 Plastic Age Sales Inc Method of fabricating a glass fiber reinforced plastic luminaire globe
US3122787A (en) * 1960-11-18 1964-03-03 Owens Illinois Glass Co Apparatus and method for molding cellular articles
US3205110A (en) * 1960-07-08 1965-09-07 Lonza Electric & Chem Works Method for producing shaped multilayer bodies
US3208104A (en) * 1961-01-28 1965-09-28 Ornapress A G Ornamentation of plastic articles
US3214319A (en) * 1959-03-17 1965-10-26 Robert N Williams Hollow plastic structure method and apparatus for the same
US3224658A (en) * 1963-08-12 1965-12-21 Kelsey Hayes Co Cold pressure welding apparatus
US3348549A (en) * 1964-07-06 1967-10-24 Du Pont Brassiere pad and process
US4025597A (en) * 1975-03-14 1977-05-24 Sawamoto Sangyo Kabushiki Kaisha Method of making brassiere cup
US4562026A (en) * 1984-03-15 1985-12-31 Motorola, Inc. Compression molding against an insert
US4708900A (en) * 1984-04-30 1987-11-24 Henkel Kommanditgesellschaft Auf Aktien Fibrous perfume carrier for artificial flowers and a process for its manufacture
EP0324714A2 (en) * 1988-01-12 1989-07-19 Textec Textil Engineering Und Consulting Gmbh Flat textile material
EP0433857A2 (en) * 1989-12-12 1991-06-26 The Dow Chemical Company Reaction injection molding apparatus for forming fibre-reinforced molded article
WO1996009927A1 (en) * 1994-09-27 1996-04-04 Empe-Werke Ernst Pelz Gmbh & Co. Kg Method of manufacturing a moulding for use in particular as interior trim, etc., in motor vehicles
US6671889B2 (en) 2001-11-14 2004-01-06 Michael R. Dennis Multi-layer, personnel-protective helmet shell with spray-fabricated inner and outer structural layers
DE102007046734A1 (en) * 2007-09-28 2009-04-02 Bayerische Motoren Werke Aktiengesellschaft Method for manufacturing fiber-reinforced plastic component, involves inserting one or multiple fiber mats into cavity of multipart forming tool, shaping fiber mats by forming tool, and evacuating forming tool
DE102007058727A1 (en) * 2007-12-06 2009-06-10 Airbus Deutschland Gmbh A method of making a FVW preform from a laminate having at least two prepreg layers and a manufacturing apparatus for such a method
US20120090768A1 (en) * 2009-04-14 2012-04-19 Airbus Operations Gmbh Apparatus and method for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material
US20140103585A1 (en) * 2012-10-12 2014-04-17 The Boeing Company Method and Apparatus for Forming Fuselage Stringers
DE19922799B4 (en) * 1999-05-18 2014-06-12 Bayerische Motoren Werke Aktiengesellschaft Process for producing a plastic molding
US20220361623A1 (en) * 2021-05-12 2022-11-17 Galvion Incorporated System for forming a deep drawn helmet and method therefor

Cited By (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2444394A (en) * 1943-03-11 1948-06-29 Lane Wells Co Method of molding diaphragms
US2452999A (en) * 1944-06-28 1948-11-02 Us Rubber Co Method of making cellular thermoplastic receptacles
US2672176A (en) * 1946-04-03 1954-03-16 Briggs Mfg Co Die apparatus for making laminated panels
US2462940A (en) * 1946-10-02 1949-03-01 Columbian Rope Co Low-pressure molding
US2536713A (en) * 1947-11-17 1951-01-02 Berg John Wesley Method of making picture frames
US2681599A (en) * 1948-01-27 1954-06-22 American Cyanamid Co Molding pulp and impregnating the product
US2521985A (en) * 1948-09-16 1950-09-12 American Felt Co Process of making fibrous units
US2697057A (en) * 1948-12-23 1954-12-14 Ortho Pharma Corp Method of making a diaphragm
US2854696A (en) * 1949-11-30 1958-10-07 Kreibaum Otto Method for the production of molded articles
US2701893A (en) * 1951-08-06 1955-02-15 Joseph Lincoln Mfg Company Inc Apparatus for making hat covers
US3018210A (en) * 1955-05-09 1962-01-23 Gentex Corp Ballistic helmet and method of making same
US2951780A (en) * 1955-10-19 1960-09-06 Gen Am Transport Methods of making decorative glass fiber reinforced resin bodies
US2845699A (en) * 1955-12-13 1958-08-05 Lee L Woodard Sons Method of making contoured dished articles
US3000429A (en) * 1956-06-22 1961-09-19 Studebaker Packard Corp Machine for prestressing and molding reinforced plastic members
US3214319A (en) * 1959-03-17 1965-10-26 Robert N Williams Hollow plastic structure method and apparatus for the same
US3097125A (en) * 1960-02-02 1963-07-09 Plastic Age Sales Inc Method of fabricating a glass fiber reinforced plastic luminaire globe
US3205110A (en) * 1960-07-08 1965-09-07 Lonza Electric & Chem Works Method for producing shaped multilayer bodies
US3122787A (en) * 1960-11-18 1964-03-03 Owens Illinois Glass Co Apparatus and method for molding cellular articles
US3208104A (en) * 1961-01-28 1965-09-28 Ornapress A G Ornamentation of plastic articles
US3224658A (en) * 1963-08-12 1965-12-21 Kelsey Hayes Co Cold pressure welding apparatus
US3348549A (en) * 1964-07-06 1967-10-24 Du Pont Brassiere pad and process
US4025597A (en) * 1975-03-14 1977-05-24 Sawamoto Sangyo Kabushiki Kaisha Method of making brassiere cup
US4562026A (en) * 1984-03-15 1985-12-31 Motorola, Inc. Compression molding against an insert
US4708900A (en) * 1984-04-30 1987-11-24 Henkel Kommanditgesellschaft Auf Aktien Fibrous perfume carrier for artificial flowers and a process for its manufacture
EP0324714A2 (en) * 1988-01-12 1989-07-19 Textec Textil Engineering Und Consulting Gmbh Flat textile material
EP0324714A3 (en) * 1988-01-12 1992-03-18 Textec Textil Engineering Und Consulting Gmbh Flat textile material
EP0433857A2 (en) * 1989-12-12 1991-06-26 The Dow Chemical Company Reaction injection molding apparatus for forming fibre-reinforced molded article
EP0433857A3 (en) * 1989-12-12 1991-09-04 The Dow Chemical Company Reaction injection molding apparatus for forming fibre-resin forced molded article
WO1996009927A1 (en) * 1994-09-27 1996-04-04 Empe-Werke Ernst Pelz Gmbh & Co. Kg Method of manufacturing a moulding for use in particular as interior trim, etc., in motor vehicles
DE19922799B4 (en) * 1999-05-18 2014-06-12 Bayerische Motoren Werke Aktiengesellschaft Process for producing a plastic molding
US6803005B2 (en) * 2001-11-14 2004-10-12 Mjd Innovations, Llc Method for making multi-layer, personnel-protective helmet shell
US6671889B2 (en) 2001-11-14 2004-01-06 Michael R. Dennis Multi-layer, personnel-protective helmet shell with spray-fabricated inner and outer structural layers
DE102007046734A1 (en) * 2007-09-28 2009-04-02 Bayerische Motoren Werke Aktiengesellschaft Method for manufacturing fiber-reinforced plastic component, involves inserting one or multiple fiber mats into cavity of multipart forming tool, shaping fiber mats by forming tool, and evacuating forming tool
US8454876B2 (en) 2007-12-06 2013-06-04 Airbus Operations Gmbh Method for manufacturing an FC parison out of a laminate with at least two prepreg layers as well as a manufacturing device for such a method
US20100263789A1 (en) * 2007-12-06 2010-10-21 Airbus Operations Gmbh method for manufacturing an fc parison out of a laminate with at least two prepreg layers as well as a manufacturing device for such a method
WO2009071331A2 (en) 2007-12-06 2009-06-11 Airbus Deutschland Gmbh Method for the production of a fiber-reinforced composite preform from a laminate, having at least two prepreg layers, and production device for such a method
DE102007058727A1 (en) * 2007-12-06 2009-06-10 Airbus Deutschland Gmbh A method of making a FVW preform from a laminate having at least two prepreg layers and a manufacturing apparatus for such a method
US20120090768A1 (en) * 2009-04-14 2012-04-19 Airbus Operations Gmbh Apparatus and method for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material
US10668671B2 (en) 2009-04-14 2020-06-02 Airbus Operations Gmbh Apparatus and method for draping knitted fiber fabrics for curved profiled structural parts of fiber composite material
US20140103585A1 (en) * 2012-10-12 2014-04-17 The Boeing Company Method and Apparatus for Forming Fuselage Stringers
US9162396B2 (en) * 2012-10-12 2015-10-20 The Boeing Company Method for forming fuselage stringers
US20160023409A1 (en) * 2012-10-12 2016-01-28 The Boeing Company Apparatus for Forming Fuselage Stringers
US10654229B2 (en) * 2012-10-12 2020-05-19 The Boeing Company Apparatus for forming fuselage stringers
US20220361623A1 (en) * 2021-05-12 2022-11-17 Galvion Incorporated System for forming a deep drawn helmet and method therefor
US11832677B2 (en) * 2021-05-12 2023-12-05 Galvion Incorporated System for forming a deep drawn helmet

Similar Documents

Publication Publication Date Title
US2378642A (en) Process of making fiber-body articles
US3850723A (en) Method of making a stampable reinforced sheet
US3947207A (en) Apparatus for preforming brassiere pads
US3664909A (en) Needled resin fibrous article
US3713962A (en) Composite mat structure
US5667857A (en) Toe puff for safety shoe
US4131664A (en) Method of making a multiple-density fibrous acoustical panel
US2763105A (en) Burnishing wheel
US4061817A (en) Luggage shells and process for the manufacture thereof
GB1342147A (en) Polyester resin sheets and their use in the manufacture of shaped articles
US4296168A (en) Padding sheet formed of a mixture of fibers bonded at their intersections
US20050140059A1 (en) Method and device for producing nonwoven moulded bodies
US4013750A (en) Method for making brassiere pad preforms
US5658511A (en) Method of manufacturing molded articles
US4025597A (en) Method of making brassiere cup
US2349365A (en) Flexible abrasive article
US3366291A (en) Hat making method
US2728701A (en) Friction element and method of making same
US2121496A (en) Fiber bodies and method of producing same
GB1348896A (en) Manufacturing porous bodies of resin-bonded fibrous material
US2672176A (en) Die apparatus for making laminated panels
DE102010004530A1 (en) Method for producing a reinforcement matrix for a plastic part, comprises arranging two semi-finished product consists of a fibrous material partially overlapped, and connecting together in the overlap region to the reinforcing matrix
US1945414A (en) Method of producing segmental rims
GB903143A (en) Cushioning material and method of producing the same
CN109203627A (en) The manufacturing method of resin composite plates