DE69510491D1 - Verfahren und Vorrichtung zur Herstellung einer Verstärkungsplatte für einen Teil Verbundmaterial - Google Patents

Verfahren und Vorrichtung zur Herstellung einer Verstärkungsplatte für einen Teil Verbundmaterial

Info

Publication number
DE69510491D1
DE69510491D1 DE69510491T DE69510491T DE69510491D1 DE 69510491 D1 DE69510491 D1 DE 69510491D1 DE 69510491 T DE69510491 T DE 69510491T DE 69510491 T DE69510491 T DE 69510491T DE 69510491 D1 DE69510491 D1 DE 69510491D1
Authority
DE
Germany
Prior art keywords
producing
composite material
reinforcing plate
reinforcing
plate
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
DE69510491T
Other languages
English (en)
Other versions
DE69510491T2 (de
Inventor
Georges Cahuzac
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of DE69510491D1 publication Critical patent/DE69510491D1/de
Publication of DE69510491T2 publication Critical patent/DE69510491T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24—Fibrous 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • B29C70/228—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure the structure being stacked in parallel layers with fibres of adjacent layers crossing at substantial angles
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
    • D04H3/115—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by applying or inserting filamentary binding elements
    • D—TEXTILES; PAPER
    • D05—SEWING; EMBROIDERING; TUFTING
    • D05B—SEWING
    • D05B23/00—Sewing apparatus or machines not otherwise provided for
    • D—TEXTILES; PAPER
    • D05—SEWING; EMBROIDERING; TUFTING
    • D05B—SEWING
    • D05B31/00—Workpiece holders or hold-downs in machines for sewing leather
    • D—TEXTILES; PAPER
    • D05—SEWING; EMBROIDERING; TUFTING
    • D05B—SEWING
    • D05B29/00—Pressers; Presser feet
    • D05B29/06—Presser feet
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00—Industrial
    • D10B2505/02—Reinforcing materials; Prepregs

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Treatment Of Fiber Materials (AREA)
  • Reinforced Plastic Materials (AREA)
DE69510491T 1994-04-18 1995-04-03 Verfahren und Vorrichtung zur Herstellung einer Verstärkungsplatte für einen Teil Verbundmaterial Expired - Lifetime DE69510491T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9404582A FR2718757B1 (fr) 1994-04-18 1994-04-18 Procédé et machine pour la réalisation d'une armature en forme de plaque pour une pièce de matière composite.

Publications (2)

Publication Number Publication Date
DE69510491D1 true DE69510491D1 (de) 1999-08-05
DE69510491T2 DE69510491T2 (de) 1999-11-25

Family

ID=9462198

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69510491T Expired - Lifetime DE69510491T2 (de) 1994-04-18 1995-04-03 Verfahren und Vorrichtung zur Herstellung einer Verstärkungsplatte für einen Teil Verbundmaterial

Country Status (6)

Country Link
US (1) US5759321A (de)
EP (1) EP0678610B1 (de)
JP (1) JPH07290451A (de)
CA (1) CA2147037C (de)
DE (1) DE69510491T2 (de)
FR (1) FR2718757B1 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6051089A (en) * 1997-02-07 2000-04-18 Mcdonnell Douglas Corporation Reinforcing member for composite workpieces and associated methods
ES2160282T3 (es) * 1997-06-10 2001-11-01 Trevira Gmbh Un metodo y una planta para la produccion de un producto tridimensional reforzado con fibra.
DE10005202B4 (de) * 2000-02-03 2007-03-01 Institut Für Verbundwerkstoffe Gmbh Verfahren und Vorrichtung zur kontinuierlichen bauteil- und prozessorientierten Herstellung von Verstärkungsstruktur-Halbzeugen für Faser-Kunststoff-Verbundwerkstoffe
FR2819804B1 (fr) * 2001-01-24 2003-04-25 Eads Launch Vehicles Procede de fabrication d'une piece en carbone/carbone
US6645333B2 (en) 2001-04-06 2003-11-11 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into 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
US7056576B2 (en) * 2001-04-06 2006-06-06 Ebert Composites, Inc. 3D fiber elements with high moment of inertia characteristics in composite sandwich laminates
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
US7731046B2 (en) * 2001-04-06 2010-06-08 Ebert Composites Corporation Composite sandwich panel and method of making same
US20050025948A1 (en) * 2001-04-06 2005-02-03 Johnson David W. Composite laminate reinforced with curvilinear 3-D fiber and method of making the same
US20040005435A1 (en) * 2001-09-08 2004-01-08 Gangarao Hota V.S. 3-Dimensionally (3-d) stitched fabrics
FR2832738B1 (fr) * 2001-11-27 2004-02-13 Eads Launch Vehicles Dispositif de tramage pour la realisation d'armatures textiles epaisses et armatures ainsi obtenues
FR2835854B1 (fr) * 2002-02-14 2005-12-30 Jean Dessinges Preformes fibreuses et leur procede de fabrication
FR2836690B1 (fr) * 2002-03-04 2004-08-27 Eads Launch Vehicles Procede pour la realisation d'une piece monolithique composite thermostructurale a double paroi et piece obtenue
US20050118448A1 (en) * 2002-12-05 2005-06-02 Olin Corporation, A Corporation Of The Commonwealth Of Virginia Laser ablation resistant copper foil
IL163135A (en) * 2004-07-21 2010-02-17 Yair Eilam Sewing machine for stitching with a composite thread
FR2909920B1 (fr) * 2006-12-15 2009-03-20 Snecma Propulsion Solide Sa Procede de realisation d'un ensemble carter-divergent
ITMI20080971A1 (it) * 2008-05-26 2009-11-27 Nat Style Ltd Dispositivo e procedimento di produzione in continuo di un tessuto tridimensionale per la produzione di pannelli.
KR101319361B1 (ko) * 2009-07-16 2013-10-16 시노마 사이언스 앤드 테크놀러지 엘티디. 통합형 다층 직물의 형성 방법 및 그 장치
US9115584B2 (en) 2012-04-24 2015-08-25 General Electric Company Resistive band for turbomachine blade
US11701845B2 (en) * 2019-09-17 2023-07-18 Nike, Inc. Method for forming a composite sole structure component

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3322868A (en) * 1963-07-02 1967-05-30 Douglas Aircraft Co Inc Three dimensional reinforced structure
US3955602A (en) * 1967-10-16 1976-05-11 Avco Corporation Apparatus for fabricating three-dimensional fabric material
US3425884A (en) * 1967-11-06 1969-02-04 Crompton & Knowles Corp Method of making an open mesh,rigid,glass fiber reinforced resin structure
US4038440A (en) * 1972-01-24 1977-07-26 Avco Corporation Three dimensional fabric material
US4218276A (en) * 1972-03-31 1980-08-19 Avco Corporation Method for making 3-D structures
FR2355936A1 (fr) * 1976-02-03 1978-01-20 Commissariat Energie Atomique Procede de fabrication de pieces en tissus tri-dimensionnels
FR2395340A1 (fr) * 1977-06-20 1979-01-19 Aerospatiale Procede et machine de tissage tridimensionnel pour la realisation d'armatures tissees de revolutions creuses
FR2427198A1 (fr) * 1978-06-02 1979-12-28 Europ Propulsion Texture tridimensionnelle presentant une direction privilegiee
US4288267A (en) * 1980-01-21 1981-09-08 Mcclean Anderson, Inc. Preliminary and end winding method and apparatus
FR2531459A1 (fr) * 1982-08-09 1984-02-10 Aerospatiale Procede et machine de realisation de pieces complexes par tissage multidirectionnel
US4503788A (en) * 1982-09-24 1985-03-12 Grumman Aerospace Corporation Translaminar stitching apparatus for composite airframe part assembly
FR2565262B1 (fr) * 1984-05-29 1986-09-26 Europ Propulsion Procede de fabrication d'une texture fibreuse multidirectionnelle et dispositif destine a la mise en oeuvre du procede
FR2612950B1 (fr) * 1987-03-25 1989-06-09 Aerospatiale Procede de fabrication d'elements d'armature composites tisses en trois dimensions, machine pour sa mise en oeuvre et produit obtenu
DE3712013A1 (de) * 1987-04-09 1988-10-27 Vorwerk Co Interholding Verfahren und vorrichtung zur herstellung von textilbloecken unbegrenzter dicke
EP0484391B1 (de) * 1989-07-25 1995-09-20 Dunlop Limited Herstellung von kohlefaser-halbfabrikaten
US5158027A (en) * 1991-12-19 1992-10-27 Tapistron International, Inc. Presser foot for hollow needle tufting apparatus
FR2686627B1 (fr) * 1992-01-24 1995-06-16 Aerospatiale Procede pour le piquage d'une piece fibreuse, piece fibreuse ainsi obtenue et piece composite fibres-matrice obtenue a partir de ladite piece fibreuse.
FR2687173B1 (fr) * 1992-02-11 1995-09-08 Aerospatiale Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature.
FR2705610B1 (fr) * 1993-05-26 1995-08-11 Aerospatiale Procédé de fabrication de bielle en matériau composite monobloc par mise en place de fibres pré-imprégnées sur un mandrin extractible et bielle ainsi obtenue.
US5468329A (en) * 1994-03-01 1995-11-21 Advanced Composites, Inc. Universal pin strip and ring for filament winding

Also Published As

Publication number Publication date
FR2718757A1 (fr) 1995-10-20
US5759321A (en) 1998-06-02
DE69510491T2 (de) 1999-11-25
JPH07290451A (ja) 1995-11-07
CA2147037A1 (fr) 1995-10-19
CA2147037C (fr) 2005-07-12
EP0678610A1 (de) 1995-10-25
FR2718757B1 (fr) 1996-06-14
EP0678610B1 (de) 1999-06-30

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Legal Events

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