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WO2001092002A3 - Method for consolidation for random carbon fiber orientation and for forming a carbon fiber preform - Google Patents

Method for consolidation for random carbon fiber orientation and for forming a carbon fiber preform Download PDF

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Publication number
WO2001092002A3
WO2001092002A3 PCT/US2001/017983 US0117983W WO0192002A3 WO 2001092002 A3 WO2001092002 A3 WO 2001092002A3 US 0117983 W US0117983 W US 0117983W WO 0192002 A3 WO0192002 A3 WO 0192002A3
Authority
WO
WIPO (PCT)
Prior art keywords
carbon fiber
forming
arrangement
layer
heat
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.)
Ceased
Application number
PCT/US2001/017983
Other languages
French (fr)
Other versions
WO2001092002A2 (en
WO2001092002A9 (en
Inventor
Mark Sloan
Richard D Blackmore
William M Lepola
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.)
IHC REHABILITATION PRODUCTS
Original Assignee
IHC REHABILITATION PRODUCTS
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 IHC REHABILITATION PRODUCTS filed Critical IHC REHABILITATION PRODUCTS
Priority to AU2001284641A priority Critical patent/AU2001284641A1/en
Publication of WO2001092002A2 publication Critical patent/WO2001092002A2/en
Anticipated expiration legal-status Critical
Publication of WO2001092002A3 publication Critical patent/WO2001092002A3/en
Publication of WO2001092002A9 publication Critical patent/WO2001092002A9/en
Ceased legal-status Critical Current

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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
    • B32B5/22Layered 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
    • B32B5/26Layered 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 another layer next to it also being fibrous or filamentary
    • 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
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/443Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
    • 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]
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    • 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
    • B32B5/06Layered 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 characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
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    • D04H1/4242Carbon fibres
    • DTEXTILES; PAPER
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    • B32B2377/00Polyamides

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Reinforced Plastic Materials (AREA)
  • Nonwoven Fabrics (AREA)
  • Laminated Bodies (AREA)

Abstract

The present invention is a method of forming a composite including a carbon fiber layer surrounded by at least a single layer of non-woven fibers both above and below the carbon fiber layer. The layer(s) of carbon fiber and the layers of non-woven fibers are consolidated with a unique needle-punching method. According to another aspect of the invention, the layer(s) of carbon fiber and the layers of non-woven fibers are consolidated with a stitching method. The present invention also provides a method of forming a preform part, comprising a number of steps. First, arrangement of carbon fibers is coated with a binder, which is either a liquid or dry adhesive. Next, the carbon fiber arrangement is placed on a forming surface. The forming surface can be either a curved or generally flat surface. Third, pressure is applied to the carbon fiber arrangement. A vacuum bag or portions of a conventional mold can be used to apply pressure to the arrangement. Lastly, heat is applied to the carbon fiber arrangement to set the binder. Heat can be applied in a number of ways, including applying an electric current to the carbon fibers to resistively heat the carbon fiber arrangement. Once a sufficient quantity of heat has been applied to set the binder, the resulting preform part is allowed to cool and then removed from the forming surface. The preform part is then ready to be injected with resin and used with a mold to form a finished part.
PCT/US2001/017983 2000-06-02 2001-06-01 Method for consolidation for random carbon fiber orientation and for forming a carbon fiber preform Ceased WO2001092002A2 (en)

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AU2001284641A AU2001284641A1 (en) 2000-06-02 2001-06-01 Method for consolidation for random carbon fiber orientation and for forming a carbon fiber preform

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US20943500P 2000-06-02 2000-06-02
US60/209,435 2000-06-02
US21350900P 2000-06-22 2000-06-22
US60/213,509 2000-06-22

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WO2001092002A3 true WO2001092002A3 (en) 2002-12-27
WO2001092002A9 WO2001092002A9 (en) 2004-05-21

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US7993477B2 (en) 2002-11-01 2011-08-09 Bell Helicopter Textron Inc. Method and apparatus for Z-direction fiber insertion of discrete fibers for reinforcement of composite laminates
RU2558904C1 (en) * 2012-08-01 2015-08-10 Тейдзин Лимитед Mat with arbitrary orientation of fibres and moulded product of fibre-reinforced composite material

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ES2690719T3 (en) 2011-04-12 2018-11-22 Fundación Tecnalia Research & Innovation Device for the preparation of preforms of components reinforced with carbon fibers
US20140003923A1 (en) 2012-07-02 2014-01-02 Peter Finnigan Functionally graded composite fan containment case
US9771669B2 (en) 2013-11-08 2017-09-26 Georgia Tech Research Corporation Use, stabilization and carbonization of polyacrylonitrile/carbon composite fibers
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IT201800003741A1 (en) * 2018-03-19 2019-09-19 Freni Brembo Spa METHOD FOR MAKING A FIBROUS PREFORM AND A FIBROUS PREFORM SO OBTAINED
US11571861B2 (en) * 2019-10-25 2023-02-07 Spirit Aerosystems, Inc. System and method for thermoplastic welding using an induced thermal gradient
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US7993477B2 (en) 2002-11-01 2011-08-09 Bell Helicopter Textron Inc. Method and apparatus for Z-direction fiber insertion of discrete fibers for reinforcement of composite laminates
RU2558904C1 (en) * 2012-08-01 2015-08-10 Тейдзин Лимитед Mat with arbitrary orientation of fibres and moulded product of fibre-reinforced composite material
US10738168B2 (en) 2012-08-01 2020-08-11 Teijin Limited Random mat and fiber-reinforced composite material shaped product
US11168186B2 (en) 2012-08-01 2021-11-09 Teijin Limited Random mat and fiber-reinforced composite material shaped product

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WO2001092002A9 (en) 2004-05-21
AU2001284641A1 (en) 2001-12-11

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