WO2005062747A3 - Method of inserting z-axis reinforcing fibers into a composite laminate - Google Patents

Method of inserting z-axis reinforcing fibers into a composite laminate Download PDF

Info

Publication number
WO2005062747A3
WO2005062747A3 PCT/US2004/034620 US2004034620W WO2005062747A3 WO 2005062747 A3 WO2005062747 A3 WO 2005062747A3 US 2004034620 W US2004034620 W US 2004034620W WO 2005062747 A3 WO2005062747 A3 WO 2005062747A3
Authority
WO
WIPO (PCT)
Prior art keywords
composite laminate
reinforcing fibers
axis reinforcing
fiber
deposition
Prior art date
Application number
PCT/US2004/034620
Other languages
French (fr)
Other versions
WO2005062747A2 (en
Inventor
David W Johnson
Scott A Garrett
James M Hook
Stephen G Moyers
Original Assignee
Ebert Composites Corp
David W Johnson
Scott A Garrett
James M Hook
Stephen G Moyers
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 Ebert Composites Corp, David W Johnson, Scott A Garrett, James M Hook, Stephen G Moyers filed Critical Ebert Composites Corp
Priority to AU2004308244A priority Critical patent/AU2004308244B2/en
Priority to JP2006539524A priority patent/JP2007511391A/en
Priority to EP04820910A priority patent/EP1682333A4/en
Priority to CA002545181A priority patent/CA2545181A1/en
Publication of WO2005062747A2 publication Critical patent/WO2005062747A2/en
Publication of WO2005062747A3 publication Critical patent/WO2005062747A3/en

Links

Classifications

    • 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
    • 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
    • B29C31/00Handling, e.g. feeding of the material to be shaped, storage of plastics material before moulding; Automation, i.e. automated handling lines in plastics processing plants, e.g. using manipulators or robots
    • B29C31/04Feeding of the material to be moulded, e.g. into a mould cavity
    • B29C31/08Feeding of the material to be moulded, e.g. into a mould cavity of preforms to be moulded, e.g. tablets, fibre reinforced preforms, extruded ribbons, tubes or profiles; Manipulating means specially adapted for feeding preforms, e.g. supports conveyors
    • 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
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/086Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
    • 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
    • B29C70/06Fibrous reinforcements only
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • 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
    • B29C70/50Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/521Pultrusion, i.e. forming and compressing by continuously pulling through a die and impregnating the reinforcement before the die
    • 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
    • B32B21/00Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
    • B32B21/04Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board comprising wood as the main or only constituent of a layer, which is next to another layer of the same or of a different 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
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form
    • B32B3/10Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar form; Layered products having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • 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
    • B32B5/02Layered 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 structural features of a fibrous or filamentary layer
    • 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
    • B32B5/02Layered 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 structural features of a fibrous or filamentary layer
    • B32B5/08Layered 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 structural features of a fibrous or filamentary layer the fibres or filaments of a layer being of different substances, e.g. conjugate fibres, mixture of different fibres
    • 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
    • B32B5/22Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • 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
    • B32B5/22Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed
    • B32B5/24Layered 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 the presence of two or more layers which are next to each other and are fibrous, filamentary, formed of particles or foamed one layer being a fibrous or filamentary layer
    • EFIXED CONSTRUCTIONS
    • E01CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01CCONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
    • E01C9/00Special pavings; Pavings for special parts of roads or airfields
    • E01C9/08Temporary pavings
    • E01C9/086Temporary pavings made of concrete, wood, bitumen, rubber or synthetic material or a combination thereof
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/02Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials
    • E04C2/26Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups
    • E04C2/284Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating
    • E04C2/296Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by specified materials composed of materials covered by two or more of groups E04C2/04, E04C2/08, E04C2/10 or of materials covered by one of these groups with a material not specified in one of the groups at least one of the materials being insulating composed of insulating material and non-metallic or unspecified sheet-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
    • B29K2105/04Condition, form or state of moulded material or of the material to be shaped cellular or porous
    • 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
    • B32B2250/00Layers arrangement
    • B32B2250/033 layers
    • 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
    • B32B2250/00Layers arrangement
    • B32B2250/40Symmetrical or sandwich layers, e.g. ABA, ABCBA, ABCCBA
    • 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
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/02Synthetic macromolecular fibres
    • B32B2262/0261Polyamide fibres
    • B32B2262/0269Aromatic polyamide fibres
    • 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
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/101Glass fibres
    • 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
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/106Carbon fibres, e.g. graphite fibres
    • 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
    • B32B2305/00Condition, form or state of the layers or laminate
    • B32B2305/02Cellular or porous
    • B32B2305/024Honeycomb

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Structural Engineering (AREA)
  • Civil Engineering (AREA)
  • Robotics (AREA)
  • Textile Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wood Science & Technology (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Nonwoven Fabrics (AREA)

Abstract

A method of inserting a z-x/y direction reinforcing fiber into a composite laminate to provide z-x/y reinforcement therein is disclosed wherein fibers (7) are deposited into x-y composite material (30) in the z-x/y direction wherein the fiber deposition material is offset at an angle during the deposition process including the fiber placement tube 16 and the pathway deposition probe (35).
PCT/US2004/034620 2003-11-10 2004-10-20 Method of inserting z-axis reinforcing fibers into a composite laminate WO2005062747A2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AU2004308244A AU2004308244B2 (en) 2003-11-10 2004-10-20 Method of inserting z-axis reinforcing fibers into a composite laminate
JP2006539524A JP2007511391A (en) 2003-11-10 2004-10-20 Method for inserting Z-axis reinforcing fiber into composite laminate
EP04820910A EP1682333A4 (en) 2003-11-10 2004-10-20 Method of inserting z-axis reinforcing fibers into a composite laminate
CA002545181A CA2545181A1 (en) 2003-11-10 2004-10-20 Method of inserting z-axis reinforcing fibers into a composite laminate

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/705,047 2003-11-10
US10/705,047 US7105071B2 (en) 2001-04-06 2003-11-10 Method of inserting z-axis reinforcing fibers into a composite laminate

Publications (2)

Publication Number Publication Date
WO2005062747A2 WO2005062747A2 (en) 2005-07-14
WO2005062747A3 true WO2005062747A3 (en) 2005-08-11

Family

ID=34738959

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2004/034620 WO2005062747A2 (en) 2003-11-10 2004-10-20 Method of inserting z-axis reinforcing fibers into a composite laminate

Country Status (6)

Country Link
US (3) US7105071B2 (en)
EP (1) EP1682333A4 (en)
JP (1) JP2007511391A (en)
AU (1) AU2004308244B2 (en)
CA (1) CA2545181A1 (en)
WO (1) WO2005062747A2 (en)

Families Citing this family (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7785693B2 (en) * 2001-04-06 2010-08-31 Ebert Composites Corporation Composite laminate structure
US6676785B2 (en) * 2001-04-06 2004-01-13 Ebert Composites Corporation Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate
US7105071B2 (en) * 2001-04-06 2006-09-12 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
EP1596024A1 (en) 2004-05-11 2005-11-16 Groep Stevens International, Naamloze Vennootschap Reinforced sandwich panel
DE102005024408A1 (en) * 2005-05-27 2006-11-30 Airbus Deutschland Gmbh Producing fiber reinforced foam materials for aircraft involves engaging through hole from first surface to engage at least one fiber bundle and pulling bundle(s) into through hole in foam material
US7811666B2 (en) 2005-07-01 2010-10-12 Carolyn Dry Multiple function, self-repairing composites with special adhesives
DE102005035681A1 (en) * 2005-07-27 2007-02-08 Röhm Gmbh Manufacturing process for reinforcing core materials for core composites and core composite structures
DE102006042920A1 (en) * 2005-11-30 2007-05-31 Thomas Gmbh + Co. Technik + Innovation Kg Producing a reinforced plastic profile by pultrusion comprises using reinforcements comprising a series of yarn or thread stitches, loops or woven linkages
GB0713239D0 (en) * 2007-07-07 2007-08-15 Trw Ltd Electriv motor control
US9782951B2 (en) * 2007-07-18 2017-10-10 The Boeing Company Composite structure having ceramic truss core and method for making the same
US8512853B2 (en) 2007-07-31 2013-08-20 The Boeing Company Composite structure having reinforced core
US8431214B2 (en) * 2007-07-31 2013-04-30 The Boeing Company Composite structure having reinforced core and method of making same
US20090058180A1 (en) * 2007-08-29 2009-03-05 Compositech, Inc. Reinforced Composite Rim
DE102007055684A1 (en) * 2007-11-21 2009-06-10 Airbus Deutschland Gmbh Device for producing a reinforced foam material
US8455085B2 (en) * 2008-01-25 2013-06-04 The Boeing Company Metal/composite joint with selective interlaminar reinforcement
US8747098B1 (en) 2008-03-24 2014-06-10 Ebert Composites Corporation Thermoplastic pultrusion die system and method
US8123510B1 (en) * 2008-03-24 2012-02-28 Ebert Composite Corporation Thermoplastic pultrusion die system and method
DE102008001826B3 (en) * 2008-05-16 2009-09-17 Airbus Deutschland Gmbh Method for manufacturing reinforcement of recess for circularly fabric sandwich, involves braiding annular fabric core with fabric traces, and feed through is generated in fabric core before or after braiding
US8852473B1 (en) 2008-09-23 2014-10-07 Wright Materials Research Co. Reinforced polymer composite foams and method of manufacture
DE102008043314B4 (en) * 2008-10-30 2010-12-09 Airbus Deutschland Gmbh Method and device for reinforcing a substrate or a textile of a core structure of a component, for example an aircraft or spacecraft
US8293353B2 (en) 2008-11-25 2012-10-23 Milliken & Company Energy absorbing panel
US20100196652A1 (en) * 2009-02-03 2010-08-05 Demien Jacquinet Quasi-isotropic sandwich structures
MX2012014176A (en) 2010-06-11 2013-05-28 Ticona Llc Inc Structural member formed from a solid lineal profile.
CA2801081A1 (en) 2010-06-22 2011-12-29 Ticona Llc Thermoplastic prepreg containing continuous and long fibers
CN102947078B (en) 2010-06-22 2015-07-08 提克纳有限责任公司 Method for forming reinforced pultruded profiles
WO2011163357A2 (en) 2010-06-22 2011-12-29 Ticona Llc Reinforced hollow profiles
DE102010052737B3 (en) * 2010-11-26 2012-04-19 Daimler Ag Modular manufacturing apparatus for integral semi-finished fiber products and process for the production of continuous fiber composite components from integral fiber composite semi-finished products with a hollow body structure
FR2975335B1 (en) * 2011-05-20 2013-05-17 Coriolis Composites Attn Olivier Bouroullec FIBER APPLICATION MACHINE WITH FLEXIBLE FIBER DELIVERY TUBES WITH FLEXIBLE BLADES
GB201117467D0 (en) * 2011-10-11 2011-11-23 Rolls Royce Plc A method of providing through-thickness reinforcement of a laminated material
WO2013114386A1 (en) * 2011-12-13 2013-08-08 Aravamudan, Gosakan 3d fiber composite
US9248958B2 (en) 2011-12-27 2016-02-02 Advanced Composite Structures, Llc Air cargo container
US20130330496A1 (en) * 2012-06-06 2013-12-12 General Electric Company Composite structure with low density core and composite stitching reinforcement
US9149997B2 (en) 2012-09-14 2015-10-06 United Technologies Composite flange from braided preform
US8776698B2 (en) 2012-10-08 2014-07-15 Advanced Composite Structures, Llc Composite air cargo pallet
US9249530B2 (en) 2013-05-30 2016-02-02 General Electric Company Fiber preform architecture for composite articles and method of fabrication
US9735466B2 (en) * 2013-07-18 2017-08-15 Ebert Composites Corporation Advanced composite radome and method of manufacturing
US20190293052A1 (en) * 2013-07-18 2019-09-26 Ebert Composites Corporation Advanced composite nacelle
US9150072B2 (en) 2013-11-14 2015-10-06 Hendrickson Usa, L.L.C. Heavy-duty vehicle axle/suspension system with composite beam
DE102014014961A1 (en) * 2014-10-14 2016-04-14 Airbus Defence and Space GmbH Device and method
FR3029834B1 (en) * 2014-12-10 2019-06-07 Doyen Entreprises PROCESS FOR INSERTING AND PLACING INDIVIDUAL YARNS THROUGH A PANEL
US10131113B2 (en) 2015-05-13 2018-11-20 Honeywell International Inc. Multilayered carbon-carbon composite
US10302163B2 (en) 2015-05-13 2019-05-28 Honeywell International Inc. Carbon-carbon composite component with antioxidant coating
US9944526B2 (en) * 2015-05-13 2018-04-17 Honeywell International Inc. Carbon fiber preforms
GB201510247D0 (en) 2015-06-12 2015-07-29 Rolls Royce Plc Method of manufacturing a composite component
GB2539249A (en) * 2015-06-12 2016-12-14 Composite Tech And Applications Ltd Method of manufacturing a composite component
US10035305B2 (en) 2015-06-30 2018-07-31 Honeywell International Inc. Method of making carbon fiber preforms
US10022890B2 (en) 2015-09-15 2018-07-17 Honeywell International Inc. In situ carbonization of a resin to form a carbon-carbon composite
US10773881B2 (en) * 2015-10-05 2020-09-15 Advanced Composite Structures, Llc Air cargo container and curtain for the same
FR3043010B1 (en) 2015-10-28 2017-10-27 Coriolis Composites FIBER APPLICATION MACHINE WITH PARTICULAR CUTTING SYSTEMS
US10300631B2 (en) 2015-11-30 2019-05-28 Honeywell International Inc. Carbon fiber preforms
US10519965B2 (en) 2016-01-15 2019-12-31 General Electric Company Method and system for fiber reinforced composite panels
DE102016000703B4 (en) * 2016-01-18 2019-10-02 Audi Ag Method and device for producing a fiber-reinforced plastic composite profile with integrated load introduction elements
FR3048373B1 (en) 2016-03-07 2018-05-18 Coriolis Group PROCESS FOR MAKING PREFORMS WITH APPLICATION OF A BINDER ON DRY FIBER AND CORRESPONDING MACHINE
US10590945B2 (en) 2016-08-10 2020-03-17 United Technologies Corporation Fiber composite material and preform and fan blade made therefrom
CN109500934A (en) * 2016-08-19 2019-03-22 苏州毕诺佳医药技术有限公司 A kind of intelligent extrusion system of medical consolidated floor processing
FR3056438B1 (en) 2016-09-27 2019-11-01 Coriolis Group METHOD FOR PRODUCING COMPOSITE MATERIAL PARTS BY IMPREGNATING A PARTICULAR PREFORM
US10532539B2 (en) * 2017-01-12 2020-01-14 Ford Global Technologies, Llc Thermal and mechanical shock resistant laminated metal plate assembly
US11851270B2 (en) 2017-10-10 2023-12-26 Advanced Composite Structures, Llc Latch for air cargo container doors
FR3076248A1 (en) * 2017-12-30 2019-07-05 Latecoere ASSEMBLY OF THERMOPLASTIC MATERIAL PARTS AND METHOD OF ASSEMBLING SUCH PARTS THERMOPLASTIC RIVET
KR102038095B1 (en) * 2019-02-20 2019-10-29 국방과학연구소 Carbon composite material reinforced with z-axis fiber and method of preparing the same
GB201903192D0 (en) * 2019-03-09 2019-04-24 Rolls Royce Plc A method and apparatus for inserting a reinforcing rod into a laminated material
US11572162B2 (en) * 2019-05-29 2023-02-07 Lockheed Martin Corporation Securing assembly for a rotor blade
US20200407149A1 (en) 2019-06-28 2020-12-31 Advanced Composite Structures, Llc Thermally Insulated Air Cargo Container
US11279080B2 (en) * 2019-12-06 2022-03-22 Honeywell Federal Manufacturing & Technologies, Llc Additive manufacturing method and assembly
CA3177703A1 (en) * 2020-05-02 2021-11-11 Terry MCQUARRIE System and method of manufacturing a composite core for an electrical transmission cable

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3837985A (en) * 1972-02-24 1974-09-24 Whittaker Corp Multi-directional reinforced composite and method of making the same
US5466506A (en) * 1992-10-27 1995-11-14 Foster-Miller, Inc. Translaminar reinforcement system for Z-direction reinforcement of a fiber matrix structure
US20020153084A1 (en) * 2001-04-06 2002-10-24 Johnson David W. Method of inserting z-axis reinforcing fibers into a composite laminate

Family Cites Families (111)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2762739A (en) 1953-11-19 1956-09-11 Alexander C H Weiss Fiber-reinforced structural panel and method of making same
US2954001A (en) 1957-05-03 1960-09-27 Luxenburg Julius Automatic eyelet attachment
FR1315844A (en) 1961-12-12 1963-01-25 Rhodiaceta Method and apparatus for sewing fabrics based on thermoplastic threads
US3328218A (en) 1962-04-09 1967-06-27 Noyes Howard Process of making a structural element
FR1359354A (en) 1963-03-15 1964-04-24 Rhodiaceta Apparatus for sewing flat elements based on thermoplastic threads
US3761345A (en) 1969-04-03 1973-09-25 R Smith Nonwoven structure for reinforcing resinous material
NL7008333A (en) 1969-06-30 1971-12-13
US3647606A (en) 1969-11-21 1972-03-07 Union Carbide Corp Semirigid multilayer thermal insulation and method of making same
US3870580A (en) 1971-02-25 1975-03-11 Jack T Belcher Method of manufacturing of a fiber reinforced structure and method of manufacture
FR2129931B1 (en) 1971-03-22 1973-12-28 Vidal Benjamin
US4218276A (en) 1972-03-31 1980-08-19 Avco Corporation Method for making 3-D structures
US3948194A (en) 1973-07-23 1976-04-06 Heinz Gunold Sewing machine accessory apparatus
US3993523A (en) 1975-03-10 1976-11-23 Booz Allen & Hamilton, Inc. Method and apparatus for adhesively joining a plurality of superimposed material layers by a needling operation
FR2315562A1 (en) 1975-06-26 1977-01-21 Commissariat Energie Atomique METHOD AND DEVICES FOR MANUFACTURING BODIES OR PARTS FROM THREE-DIMENSIONAL FABRICS
DE2544165C3 (en) 1975-10-03 1978-08-10 Pfaff Industriemaschinen Gmbh, 6750 Kaiserslautern Equipment on sewing machines for prepunching the sewing material
US4032383A (en) 1975-11-04 1977-06-28 Mcdonnell Douglas Corporation Fiber insertion device for continuous 3d foaming machine and method
FR2355936A1 (en) 1976-02-03 1978-01-20 Commissariat Energie Atomique PROCESS FOR MANUFACTURING PARTS IN THREE-DIMENSIONAL FABRICS
US4256790A (en) 1978-01-19 1981-03-17 Rockwell International Corporation Reinforced composite structure and method of fabrication thereof
US4206895A (en) 1978-03-30 1980-06-10 Olez Nejat A Loop-tension joint
US4196251A (en) 1979-04-16 1980-04-01 International Harvester Company Rigidized resinous foam core sandwich structure
US4291081A (en) 1979-07-26 1981-09-22 Northrop Corporation Laced composite structure
US4299871A (en) 1979-09-04 1981-11-10 Grumman Aerospace Corporation Stitch bond fastening of composite structures
US4506611A (en) 1979-10-22 1985-03-26 Hitco Three-dimensional thick fabrics and methods and apparatus for making same
US4331091A (en) 1979-10-22 1982-05-25 Hitco Three-dimensional thick fabrics and method and apparatus for making same
US4350728A (en) * 1980-10-02 1982-09-21 The United States Of America As Represented By The Secretary Of The Navy Cross reinforcement in a graphite-epoxy laminate
US4335176A (en) 1980-11-24 1982-06-15 Ppg Industries, Inc. Bonded needled fiber glass thermoplastic reinforced mats
IL66104A0 (en) 1981-07-27 1982-09-30 Tesch G H Preparation of fiber reinforced flat bodies containing a hardenable binder
US4498941A (en) 1981-08-05 1985-02-12 Goldsworthy Engineering, Inc. Method for producing fiber reinforced sheet structures
JPS5898077U (en) 1981-12-24 1983-07-04 株式会社井上ジャパックス研究所 sewing machine equipment
US4503788A (en) * 1982-09-24 1985-03-12 Grumman Aerospace Corporation Translaminar stitching apparatus for composite airframe part assembly
US4495231A (en) 1982-09-29 1985-01-22 Avco Corporation Fiber composite
DE3246803A1 (en) 1982-12-17 1984-06-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München METHOD FOR PRODUCING COMPONENTS FROM LAYERS OF FIBER REINFORCED PLASTIC
JPS60129246A (en) * 1983-12-15 1985-07-10 Nitto Electric Ind Co Ltd Manufacture of three-dimensional fiber-reinforced expanded material
FR2565262B1 (en) 1984-05-29 1986-09-26 Europ Propulsion METHOD FOR MANUFACTURING A MULTI-DIRECTIONAL FIBROUS TEXTURE AND DEVICE FOR CARRYING OUT THIS METHOD
US4571355A (en) 1984-11-28 1986-02-18 The Boeing Company Fiber reinforced resin composites formed of basic ply blankets
DE3508252A1 (en) 1985-03-08 1986-09-11 Johann 2212 Brunsbüttel Götz METHOD FOR PULLING LIGHT FIBER FIBERS THROUGH TEXTILES AND A DEVICE FOR CARRYING OUT THE METHOD
GB8602003D0 (en) 1986-01-28 1986-03-05 Lawton P G Carbonisable fibre assembly
US4761871A (en) 1986-11-21 1988-08-09 Phillips Petroleum Company Method of joining two thermoplastic articles
FR2612950B1 (en) 1987-03-25 1989-06-09 Aerospatiale METHOD FOR MANUFACTURING THREE-DIMENSION WOVEN COMPOSITE REINFORCING ELEMENTS, MACHINE FOR IMPLEMENTING SAME AND PRODUCT OBTAINED
US4752513A (en) 1987-04-09 1988-06-21 Ppg Industries, Inc. Reinforcements for pultruding resin reinforced products and novel pultruded products
GB2205374B (en) 1987-05-19 1991-03-27 Rockwell International Corp Composite fasteners & method for fastening structural components therewith
JPH01110944A (en) * 1987-10-26 1989-04-27 Toyota Motor Corp Frp structure
GB2284031B (en) 1987-11-27 1995-11-08 Gen Electric Composite fastener
US4808461A (en) 1987-12-14 1989-02-28 Foster-Miller, Inc. Composite structure reinforcement
US4913937A (en) 1988-02-17 1990-04-03 Xerkon Inc. Composite articles using meltable resin holding threads
US4963408A (en) 1988-06-13 1990-10-16 Mono-Lite Corporation Structural unitary composite laminate structure and method for making same
GB8822520D0 (en) 1988-09-26 1988-11-02 Tech Textiles Ltd Process for continuously forming reinforced plastics articles
GB8822521D0 (en) 1988-09-26 1988-11-02 Tech Textiles Ltd Method of producing formable composite material
US4952513A (en) * 1988-10-24 1990-08-28 Crystal Diagnostics, Inc. Assays for qualitative and quantitative detection of organic and inorganic analytes of diverse chemical classes via the selective formation and growth of light scattering crystals
FR2658841B1 (en) 1990-02-26 1993-06-11 Aerospatiale METHOD AND DEVICE FOR PRODUCING REINFORCING ELEMENTS COMPOSED OF RESISTANT FIBERS.
US5186776A (en) 1990-05-07 1993-02-16 Foster-Miller, Inc. Composite laminate translaminar reinforcement apparatus and method
GB9014770D0 (en) * 1990-07-03 1990-08-22 Short Brothers Plc Manufacture of a composite material
JPH06503517A (en) 1990-08-16 1994-04-21 オムニグラス リミテッド Drawing method involving transverse fibers
US5778806A (en) 1990-12-26 1998-07-14 Ralph's Industrial Sewing Machine Company Sewing and material removal assembly
US5286320A (en) 1991-11-18 1994-02-15 Owens-Corning Fiberglas Technology Inc. Method for making a pultruded panel
FR2686627B1 (en) 1992-01-24 1995-06-16 Aerospatiale METHOD FOR STITCHING A FIBROUS PIECE, FIBROUS PIECE THUS OBTAINED AND FIBER-MATRIX COMPOSITE PIECE OBTAINED FROM SAID FIBROUS PIECE.
FR2687173B1 (en) 1992-02-11 1995-09-08 Aerospatiale PROCESS FOR THE PRODUCTION OF A FIBER REINFORCEMENT FOR A COMPOSITE MATERIAL, AND A COMPOSITE PIECE COMPRISING SUCH A REINFORCEMENT.
DE4203988A1 (en) 1992-02-12 1993-08-19 Will E C H Gmbh & Co METHOD AND DEVICE FOR BINDING PAPER LAYERS
US5327621A (en) 1992-03-23 1994-07-12 Kabushiki Kaisha Toyoda Jidoshokki Seisakusho Method of producing fabric reinforcing matrix for composites
US5834082A (en) 1992-05-04 1998-11-10 Webcore Technologies, Inc. Reinforced foam cores and method and apparatus of production
US5589243A (en) 1992-05-04 1996-12-31 Webcore Technologies, Inc. Reinforced foam cores and method and apparatus of production
GB9212697D0 (en) 1992-06-15 1992-07-29 Short Brothers Plc Composite structure manufacture
US5445861A (en) 1992-09-04 1995-08-29 The Boeing Company Lightweight honeycomb panel structure
US6106646A (en) 1992-09-14 2000-08-22 General Electric Company Method for joining composite materials
US5445860A (en) 1992-12-29 1995-08-29 Gff Holding Company Tufted product having an improved backing
JP2622656B2 (en) * 1993-01-29 1997-06-18 サカセ・アドテック株式会社 Method and apparatus for binding laminated sheets
US5364681A (en) 1993-02-05 1994-11-15 Gencorp Inc. Acoustic lamina wall covering
DE69431909T2 (en) 1993-04-30 2003-11-06 Foster Miller Inc A REINFORCED CONNECTING ELEMENT OF COMPOSITE STRUCTURES AND METHOD FOR CONNECTING COMPONENT PARTS
CA2138775C (en) 1993-05-04 2000-03-14 Glenn A. Freitas Truss reinforced foam core sandwich structure
DE4342575A1 (en) 1993-10-12 1995-04-13 Textilma Ag Textile insert for the production of a fiber composite material and fiber composite material
GB9406537D0 (en) 1994-03-31 1994-05-25 British Aerospace Blind stitching apparatus and composite material manufacturing methods
FR2718758B1 (en) 1994-04-18 1996-06-14 Aerospatiale Method and machine for producing a frame for a piece of composite material.
FR2718757B1 (en) 1994-04-18 1996-06-14 Aerospatiale Method and machine for producing a plate-shaped reinforcement for a piece of composite material.
JPH07308927A (en) * 1994-05-18 1995-11-28 Sekisui Chem Co Ltd Fiber-reinforced resin foam molded body and its manufacture
US5470649A (en) 1994-06-24 1995-11-28 The United States Of America As Represented By The Adminstrator Of The National Aeronautics And Space Administration Composite with through the thickness reinforcement
US6090465A (en) 1994-08-29 2000-07-18 Spectrum Solutions, Ltd. Reinforced composite structure
JP3584065B2 (en) 1994-09-12 2004-11-04 住友化学工業株式会社 Manufacturing apparatus and manufacturing method for long fiber reinforced resin structure
JPH0899366A (en) * 1994-09-30 1996-04-16 Sekisui Chem Co Ltd Manufacture of fiber reinforced resin formed body
US5549771A (en) 1994-12-23 1996-08-27 Brooker; David A. Fabrication of body containing lengths of fiber embedded therein
US5873973A (en) 1995-04-13 1999-02-23 Northrop Grumman Corporation Method for single filament transverse reinforcement in composite prepreg material
AU3411395A (en) 1995-08-21 1997-03-12 Foster-Miller Inc. System for inserting elements in composite structure
FR2740068B1 (en) 1995-10-20 1998-01-09 Aerospatiale PART OF REINFORCED LOW DENSITY THERMAL PROTECTION MATERIAL AND PROCESS FOR OBTAINING SAME
US6027798A (en) 1995-11-01 2000-02-22 The Boeing Company Pin-reinforced sandwich structure
US5885020A (en) * 1995-11-15 1999-03-23 Spartan Felt Company, Inc. Marker pen having improved fibrous nib
US5868886A (en) 1995-12-22 1999-02-09 Alston; Mark S. Z-pin reinforced bonded composite repairs
US6151439A (en) * 1995-12-29 2000-11-21 Ani-Motion, Inc. Apparatus and method for implanting optical fibers in fabric panels and the like
US5789061A (en) 1996-02-13 1998-08-04 Foster-Miller, Inc. Stiffener reinforced assembly and method of manufacturing same
US5862975A (en) 1996-03-20 1999-01-26 The Boeing Company Composite/metal structural joint with welded Z-pins
US5876652A (en) 1996-04-05 1999-03-02 The Boeing Company Method for improving pulloff strength in pin-reinforced sandwich structure
US5832594A (en) 1996-05-31 1998-11-10 The Boeing Company Tooling for inserting Z-pins
US5876540A (en) 1996-05-31 1999-03-02 The Boeing Company Joining composites using Z-pinned precured strips
US5980665A (en) 1996-05-31 1999-11-09 The Boeing Company Z-pin reinforced bonds for connecting composite structures
US5916469A (en) 1996-06-06 1999-06-29 The Boeing Company Susceptor integration into reinforced thermoplastic composites
FR2752640B1 (en) * 1996-08-21 1998-11-06 Jolly Andre Jean METHOD FOR MANUFACTURING A SANDWICH PANEL WITH HIGH RESILIENCE CONDUCTIVE CORES AND PANEL OBTAINED
US6187411B1 (en) * 1996-10-04 2001-02-13 The Boeing Company Stitch-reinforced sandwich panel and method of making same
US6139942A (en) * 1997-02-06 2000-10-31 Cytec Technology, Inc. Resin composition, a fiber reinforced material having a partially impregnated resin and composites made therefrom
US6051089A (en) 1997-02-07 2000-04-18 Mcdonnell Douglas Corporation Reinforcing member for composite workpieces and associated methods
US5941185A (en) 1997-08-25 1999-08-24 Selbach Machinery L.L.C. Optical filament insertion apparatus
US6151089A (en) * 1998-01-20 2000-11-21 Sony Corporation Reflection type display with light waveguide with inclined and planar surface sections
US6190602B1 (en) * 1998-03-13 2001-02-20 Aztex, Inc. Method of manufacturing a perforated laminate
FR2779749B1 (en) * 1998-06-10 2000-08-11 Aerospatiale FIBROUS REINFORCEMENT FOR A PART OF COMPOSITE MATERIAL, AS WELL AS METHOD AND DEVICE FOR ITS IMPLEMENTATION
US6128998A (en) * 1998-06-12 2000-10-10 Foster Miller, Inc. Continuous intersecting braided composite structure and method of making same
US6291049B1 (en) * 1998-10-20 2001-09-18 Aztex, Inc. Sandwich structure and method of making same
US6196145B1 (en) * 1998-11-17 2001-03-06 Albany International Techniweave, Inc. Yarn insertion mechanism
AU2459101A (en) * 1999-12-28 2001-07-09 Webcore Technologies, Inc. Fiber reinforced composite cores and panels
JP2001246686A (en) * 2000-03-07 2001-09-11 Toyota Autom Loom Works Ltd Composite material structure
US20020014302A1 (en) * 2000-07-13 2002-02-07 Kazak Composites, Incorporated Method for incorporating rigid elements into the core of composite structural members in a pultrusion process
US6467149B2 (en) * 2000-12-07 2002-10-22 The Goodyear Tire & Rubber Company Apparatus for injecting materials into a composite
US7105071B2 (en) * 2001-04-06 2006-09-12 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
US6676785B2 (en) * 2001-04-06 2004-01-13 Ebert Composites Corporation Method of clinching the top and bottom ends of Z-axis fibers into the respective top and bottom surfaces of a composite laminate
DE10205965A1 (en) * 2002-02-14 2003-09-04 Daimler Chrysler Ag Construction element made of fiber-reinforced plastic

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3837985A (en) * 1972-02-24 1974-09-24 Whittaker Corp Multi-directional reinforced composite and method of making the same
US5466506A (en) * 1992-10-27 1995-11-14 Foster-Miller, Inc. Translaminar reinforcement system for Z-direction reinforcement of a fiber matrix structure
US20020153084A1 (en) * 2001-04-06 2002-10-24 Johnson David W. Method of inserting z-axis reinforcing fibers into a composite laminate
WO2003011576A1 (en) * 2001-08-02 2003-02-13 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate

Also Published As

Publication number Publication date
JP2007511391A (en) 2007-05-10
AU2004308244B2 (en) 2010-07-01
EP1682333A2 (en) 2006-07-26
US20070029024A1 (en) 2007-02-08
US8002919B2 (en) 2011-08-23
US7105071B2 (en) 2006-09-12
US7387147B2 (en) 2008-06-17
WO2005062747A2 (en) 2005-07-14
EP1682333A4 (en) 2009-10-21
CA2545181A1 (en) 2005-07-14
US20050006023A1 (en) 2005-01-13
AU2004308244A1 (en) 2005-07-14
US20090071594A1 (en) 2009-03-19

Similar Documents

Publication Publication Date Title
WO2005062747A3 (en) Method of inserting z-axis reinforcing fibers into a composite laminate
WO2004041528A3 (en) Method and apparatus for z-direction reinforcement of composite laminates
PL362738A1 (en) Method for reducing impurities in cellulose fibers for manufacture of fiber reinforced cement composite materials
AU2402900A (en) Process of forming fiber reinforced composite articles using an insitu cured resin infusion port
AU2002241047A1 (en) Method and device for making a composite sheet with multiaxial fibrous reinforcement
ATE416905T1 (en) METHOD FOR INTRODUCING Z-AXIS ORIENTED REINFORCEMENT FIBERS INTO A COMPOSITE LAMINATE
WO2000002959A3 (en) New and useful improvements in fiber-reinforced composite materials structures and methods of making same
HUP0201825A2 (en) Method for producing fiber reinforced materials
WO2002002300A3 (en) Method for composite material repair
GB9917854D0 (en) A process for producing bodies made of fibre-reinforced composites
PL368181A1 (en) A liner for reinforcing a pipe and method of making the same
DE69420527D1 (en) Method for changing the electrical charge of a preform for optical fibers by means of plasma and optical fiber, produced from a preform with changed charge by this method
ATE423804T1 (en) FIBER COMPOSITE MATERIAL AND METHOD FOR THE PRODUCTION THEREOF
IL174077A0 (en) A reinforcing device and a bifacial reinforcing unit for earthworks and a method for the production of a reinforced earthwork
CA2012032A1 (en) Process for joining elements in the manufacture of thermostructural composite material parts
EP1071072A3 (en) Acoustic liner and method of making an acoustic liner
CA2377744A1 (en) Pultruded part and method of preparing a reinforcement mat for the part
WO2000026452A8 (en) Fiber reinforced cementitious materials with improved toughness and ductility
GB0327044D0 (en) A method of manufacturing a fibre reinforced metal matrix composite article and a cassette for use therein
AU2003207456A1 (en) Controlled placement of a reinforcing web within a fibrous absorbent
NO20014582D0 (en) Reinforcing element and method of producing reinforcing element
IL132381A (en) Method of upgrading existing nylon fibers and use of same for reinforcement of cementitious composites
AU5569299A (en) A wiremesh reinforcement-plastic composite pipe component and method for making the same
AU2001257229A1 (en) Method of forming repair material for conduit interface area and for repairing anon-linear conduit with a fiber repair material
NZ500855A (en) A method of securing a composite reinforcement layer to a structural element

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BW BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE EG ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NA NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): BW GH GM KE LS MW MZ NA SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 2545181

Country of ref document: CA

Ref document number: 2004308244

Country of ref document: AU

WWE Wipo information: entry into national phase

Ref document number: 2006539524

Country of ref document: JP

WWE Wipo information: entry into national phase

Ref document number: PA/a/2006/005241

Country of ref document: MX

Ref document number: 2004820910

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2004308244

Country of ref document: AU

Date of ref document: 20041020

Kind code of ref document: A

WWP Wipo information: published in national office

Ref document number: 2004308244

Country of ref document: AU

WWP Wipo information: published in national office

Ref document number: 2004820910

Country of ref document: EP