DE69603551T2 - Verfahren und System zur Herstellung einer Armierung für ein Verbundmaterialteil - Google Patents

Verfahren und System zur Herstellung einer Armierung für ein Verbundmaterialteil

Info

Publication number
DE69603551T2
DE69603551T2 DE69603551T DE69603551T DE69603551T2 DE 69603551 T2 DE69603551 T2 DE 69603551T2 DE 69603551 T DE69603551 T DE 69603551T DE 69603551 T DE69603551 T DE 69603551T DE 69603551 T2 DE69603551 T2 DE 69603551T2
Authority
DE
Germany
Prior art keywords
reinforcement
producing
composite material
material part
composite
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 - Fee Related
Application number
DE69603551T
Other languages
English (en)
Other versions
DE69603551D1 (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 DE69603551D1 publication Critical patent/DE69603551D1/de
Publication of DE69603551T2 publication Critical patent/DE69603551T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • D04H18/00—Needling machines
    • D04H18/02—Needling machines with needles
    • 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
    • D04H3/002—Inorganic yarns or filaments
    • 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
    • D04H3/002—Inorganic yarns or filaments
    • D04H3/004—Glass yarns or filaments
    • 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
    • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/04—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in rectilinear paths, e.g. crossing at right 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
    • D04H3/02—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments
    • D04H3/05—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of yarns or filaments in another pattern, e.g. zig-zag, sinusoidal
    • 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
    • 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
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K1/00—Printed circuits
    • H05K1/02—Details
    • H05K1/03—Use of materials for the substrate
    • H05K1/0313—Organic insulating material
    • H05K1/0353—Organic insulating material consisting of two or more materials, e.g. two or more polymers, polymer + filler, + reinforcement
    • H05K1/0366—Organic insulating material consisting of two or more materials, e.g. two or more polymers, polymer + filler, + reinforcement reinforced, e.g. by fibres, fabrics

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Inorganic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforcement Elements For Buildings (AREA)
  • Reinforced Plastic Materials (AREA)
DE69603551T 1995-07-17 1996-06-28 Verfahren und System zur Herstellung einer Armierung für ein Verbundmaterialteil Expired - Fee Related DE69603551T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9508595A FR2736941B1 (fr) 1995-07-17 1995-07-17 Procede et systeme pour la realisation d'une armature pour une piece de matiere composite

Publications (2)

Publication Number Publication Date
DE69603551D1 DE69603551D1 (de) 1999-09-09
DE69603551T2 true DE69603551T2 (de) 1999-12-23

Family

ID=9481031

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69603551T Expired - Fee Related DE69603551T2 (de) 1995-07-17 1996-06-28 Verfahren und System zur Herstellung einer Armierung für ein Verbundmaterialteil

Country Status (7)

Country Link
US (1) US5914002A (de)
EP (1) EP0754795B1 (de)
JP (1) JPH0929740A (de)
CA (1) CA2181399A1 (de)
DE (1) DE69603551T2 (de)
ES (1) ES2135189T3 (de)
FR (1) FR2736941B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004060674A1 (de) * 2004-12-15 2006-07-06 Eurocopter Deutschland Gmbh Verfahren und eine Vorrichtung zur Herstellung eines flächigen Faser-Vorformlings
DE10250826B4 (de) * 2002-10-31 2008-05-29 Airbus Deutschland Gmbh Verfahren zur Herstellung eines dreidimensionalen Preforms

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19726831C5 (de) * 1997-06-24 2005-02-17 Liba Maschinenfabrik Gmbh Multiaxial-Maschine mit Portalaufbau
DE19728385C2 (de) * 1997-07-03 2001-02-22 Titv Greiz Verfahren zur Gewinnung eines aus Fäden bestehenden Flächen- und Körpergebildes
WO2001038625A2 (fr) * 1999-11-24 2001-05-31 Snecma Moteurs Procede de fabrication d'un bol en materiau composite thermostructural, bol tel qu'obtenu par le procede, et utilisation du bol comme support de creuset
DE10252671C1 (de) * 2002-11-11 2003-12-04 Mayer Malimo Textilmaschf Verfahren zur Herstellung von faserverstärkten, dreidimensionalen Kunststoffteilen
US7434491B1 (en) * 2003-01-10 2008-10-14 Motoman, Inc. Flexible tooling interface for headstock/tailstock positioner
US7099725B2 (en) * 2003-12-02 2006-08-29 The Boeing Company Alternate ply representation for composite design and manufacturing
US7464621B2 (en) * 2004-11-09 2008-12-16 Steeda Autosports, Inc. Longitudinally displaced shifter
FR2909920B1 (fr) * 2006-12-15 2009-03-20 Snecma Propulsion Solide Sa Procede de realisation d'un ensemble carter-divergent
FR2940172B1 (fr) * 2008-12-18 2011-01-21 Snecma Procede de fabrication d'une aube de turbomachine
DE102010044721A1 (de) * 2010-09-08 2012-03-08 Daimler Ag Verfahren und Vorrichtung zum Herstellen eines Faserhalbzeugs
DE102011109698B4 (de) * 2011-08-06 2016-02-11 Daimler Ag Verfahren zum Herstellen eines harzimprägnierten Faserhalbzeugs

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2110590B (en) * 1981-05-29 1985-09-04 Fumio Usui Method and apparatus for manufacturing hollow article
US5117348A (en) * 1986-03-28 1992-05-26 The Ingersoll Milling Machine Company Method for alignment of a representative surface to an actual surface for a tape laying machine
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
US5637175A (en) * 1988-10-05 1997-06-10 Helisys Corporation Apparatus for forming an integral object from laminations
US5239457A (en) * 1990-07-16 1993-08-24 Cincinnati Milacron Inc. Redirect roller control for fiber placement machine
GB2249050A (en) * 1990-10-05 1992-04-29 Tech Textiles Ltd Reinforcing fabric for plastics
FR2718758B1 (fr) * 1994-04-18 1996-06-14 Aerospatiale Procédé et machine pour la réalisation d'une armature pour une pièce de matière composite.

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10250826B4 (de) * 2002-10-31 2008-05-29 Airbus Deutschland Gmbh Verfahren zur Herstellung eines dreidimensionalen Preforms
DE102004060674A1 (de) * 2004-12-15 2006-07-06 Eurocopter Deutschland Gmbh Verfahren und eine Vorrichtung zur Herstellung eines flächigen Faser-Vorformlings
DE102004060674B4 (de) * 2004-12-15 2010-02-11 Eurocopter Deutschland Gmbh Verfahren und eine Vorrichtung zur Herstellung eines flächigen Faser-Vorformlings

Also Published As

Publication number Publication date
EP0754795A1 (de) 1997-01-22
US5914002A (en) 1999-06-22
EP0754795B1 (de) 1999-08-04
CA2181399A1 (fr) 1997-01-18
FR2736941A1 (fr) 1997-01-24
DE69603551D1 (de) 1999-09-09
ES2135189T3 (es) 1999-10-16
JPH0929740A (ja) 1997-02-04
FR2736941B1 (fr) 1997-09-12

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee