ATE427211T1 - Verfahren zur herstellung eines gabelkopfs an einem aus verbundwerkstoff hergestellten strukturelement, insbesondere einer verbindungsstange - Google Patents

Verfahren zur herstellung eines gabelkopfs an einem aus verbundwerkstoff hergestellten strukturelement, insbesondere einer verbindungsstange

Info

Publication number
ATE427211T1
ATE427211T1 AT06831104T AT06831104T ATE427211T1 AT E427211 T1 ATE427211 T1 AT E427211T1 AT 06831104 T AT06831104 T AT 06831104T AT 06831104 T AT06831104 T AT 06831104T AT E427211 T1 ATE427211 T1 AT E427211T1
Authority
AT
Austria
Prior art keywords
plies
fibers
separating
producing
connecting rod
Prior art date
Application number
AT06831104T
Other languages
English (en)
Inventor
Patrick Dunleavy
Original Assignee
Messier Dowty Sa
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 Messier Dowty Sa filed Critical Messier Dowty Sa
Application granted granted Critical
Publication of ATE427211T1 publication Critical patent/ATE427211T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00—Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/02—Constructions of connecting-rods with constant length
    • F16C7/026—Constructions of connecting-rods with constant length made of fibre reinforced resin
    • 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
    • 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 [3D] 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
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/304—In-plane lamination by juxtaposing or interleaving of plies, e.g. scarf joining
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00—Woven fabrics not otherwise provided for
    • D03D25/005—Three-dimensional woven fabrics
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/06—Rods, e.g. connecting rods, rails, stakes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2220/00—Shaping
    • F16C2220/28—Shaping by winding impregnated fibres
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24777—Edge feature

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)
  • Forging (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Joining Of Building Structures In Genera (AREA)
AT06831104T 2005-11-23 2006-11-10 Verfahren zur herstellung eines gabelkopfs an einem aus verbundwerkstoff hergestellten strukturelement, insbesondere einer verbindungsstange ATE427211T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0511846A FR2893532B1 (fr) 2005-11-23 2005-11-23 Procede de fabrication d'une chape sur un element structural en materiau composite, notamment une bielle

Publications (1)

Publication Number Publication Date
ATE427211T1 true ATE427211T1 (de) 2009-04-15

Family

ID=36570444

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06831104T ATE427211T1 (de) 2005-11-23 2006-11-10 Verfahren zur herstellung eines gabelkopfs an einem aus verbundwerkstoff hergestellten strukturelement, insbesondere einer verbindungsstange

Country Status (13)

Country Link
US (1) US7601288B2 (de)
EP (1) EP1951506B1 (de)
JP (1) JP4705174B2 (de)
CN (1) CN101316694B (de)
AT (1) ATE427211T1 (de)
BR (1) BRPI0618903A2 (de)
CA (1) CA2630715C (de)
DE (1) DE602006006090D1 (de)
ES (1) ES2323901T3 (de)
FR (1) FR2893532B1 (de)
PL (1) PL1951506T3 (de)
RU (1) RU2383438C1 (de)
WO (1) WO2007060305A1 (de)

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* Cited by examiner, † Cited by third party
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FR2907475B1 (fr) * 2006-10-18 2008-12-05 Messier Dowty Sa Sa Tissu composite 3d
FR2907800B1 (fr) * 2006-10-27 2009-03-20 Airbus France Sas Tissage tridimensionnel surfacique
AT505512B1 (de) * 2007-07-03 2009-09-15 Teufelberger Gmbh Anordnung zum verbinden eines länglichen elements mit einer weiteren komponente
FR2932408B1 (fr) * 2008-06-11 2010-05-28 Aircelle Sa Preforme destinee a former une piece mecanique structurante creuse
FR2932409B1 (fr) 2008-06-13 2013-04-12 Messier Dowty Sa Procede de fabrication d'une piece structurale en materiau composite a matrice organique, piece obtenue.
FR2944469A1 (fr) * 2009-04-16 2010-10-22 Messier Dowty Sa Procede de fabrication d'une bielle en materiau composite ayant des extremites renforcees
FR2945847B1 (fr) * 2009-05-20 2011-12-02 Messier Dowty Sa Procede de fabrication d'une bielle en materiau composite et bielle obtenue par la mise en oeuvre dudit procede.
FR2953160A1 (fr) * 2009-11-30 2011-06-03 Messier Dowty Sa Procede de fabrication d'une bielle en materiau composite integrant une chape renforcee
FR2953443B1 (fr) 2009-12-08 2013-08-23 Messier Dowty Sa Procede de fabrication d'une bielle en materiau composite comprenant une surepaisseur localisee
BR112012016701A2 (pt) * 2010-01-22 2018-06-05 Messier Bugatti Domty "método para fabricação de partes compostas compreendendo fibras trançadas"
FR2964340B1 (fr) * 2010-09-06 2012-08-24 Messier Dowty Sa Procede de fabrication de pieces composites comportant des fibres tressees
FR2955525B1 (fr) * 2010-01-22 2012-02-17 Messier Dowty Sa Procede de fabrication d'une bielle en materiau composite comportant des zones de renforcement.
FR2960818B1 (fr) * 2010-06-04 2012-07-20 Snecma Structure fibreuse formant une bride et une contre-bride
ES2695040T3 (es) * 2010-12-23 2018-12-28 Internacional De Composites, Sa. Método para la producción de una barra a partir de un material compuesto y una barra de carga
FR2969666B1 (fr) * 2010-12-24 2013-02-01 Messier Dowty Sa Procede de tressage de fibres renforcantes a variation d'inclinaison des fibres tressees
DE102011006792B4 (de) * 2011-04-05 2017-07-27 Airbus Operations Gmbh Verfahren zum Herstellen und Verbinden von faserverstärkten Bauteilen sowie Luft- oder Raumfahrzeug
FR2978696B1 (fr) * 2011-08-01 2013-08-23 Messier Bugatti Dowty Bielle en materiau composite ayant une tenue mecanique augmentee
US9212437B2 (en) * 2011-11-02 2015-12-15 GM Global Technology Operations LLC One-piece fiber reinforcement for a reinforced polymer combining aligned and random fiber layers
FR2991228B1 (fr) 2012-05-29 2015-03-06 Airbus Operations Sas Procede et dispositif de realisation d'un panneau composite auto-raidi
CN102899778A (zh) * 2012-11-13 2013-01-30 天津工业大学 一种整体环形三维织物及其织造方法
DE102013213653A1 (de) * 2013-07-12 2015-01-15 Bayerische Motoren Werke Aktiengesellschaft Kraftfahrzeug
US9259858B2 (en) * 2013-10-18 2016-02-16 Green Dynamics Corporation Laminate stitching method for improved fiber logistics and placement precision
US9897122B2 (en) 2015-05-22 2018-02-20 Goodrich Corporation Attachment of composite lug to composite structural tube
GB201514579D0 (en) 2015-08-17 2015-09-30 Invibio Device Component Mfg Ltd A device
JP6790967B2 (ja) * 2017-03-31 2020-11-25 株式会社豊田自動織機 繊維構造体及び繊維強化複合材
JP6700615B2 (ja) * 2017-03-31 2020-05-27 株式会社豊田自動織機 繊維構造体及び繊維強化複合材
FR3065182B1 (fr) * 2017-04-13 2019-06-21 Safran Procede de fabrication d'une piece en materiau composite comportant un corps prolonge par une extremite de fixation renforcee
JP6614225B2 (ja) * 2017-10-31 2019-12-04 トヨタ自動車株式会社 タンクの製造方法およびタンク
EP3859066B1 (de) * 2020-02-03 2024-01-24 STÄUBLI BAYREUTH GmbH Webverfahren und schussfadenwähler zur durchführung solch eines verfahrens

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GB1319235A (en) * 1969-07-18 1973-06-06 Dowty Rotol Ltd Devices of fibrous-reinforced plastics material
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SU721308A1 (ru) * 1978-08-07 1980-03-15 Физико-технический институт АН Белорусской ССР Способ изготовлени многослойных изделий
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
US4571355A (en) * 1984-11-28 1986-02-18 The Boeing Company Fiber reinforced resin composites formed of basic ply blankets
DE3726340A1 (de) * 1987-08-07 1989-02-16 Sachs Systemtechnik Gmbh Verfahren zur herstellung einer zug-druck-strebe mit krafteinleitungsaugen
US5279892A (en) * 1992-06-26 1994-01-18 General Electric Company Composite airfoil with woven insert
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.
FR2718802B1 (fr) * 1994-04-18 1996-06-14 Aerospatiale Bielle en matière composite et procédé pour sa fabrication.
US6036904A (en) * 1994-04-18 2000-03-14 Aerospatiale Societe Nationale Industrielle Method of manufacturing a connecting rod made from composite material
FR2759096B1 (fr) * 1997-02-04 1999-02-26 Snecma Texture multicouche liee pour materiaux composites structuraux

Also Published As

Publication number Publication date
CN101316694A (zh) 2008-12-03
JP2009516607A (ja) 2009-04-23
PL1951506T3 (pl) 2009-08-31
WO2007060305A1 (fr) 2007-05-31
BRPI0618903A2 (pt) 2013-01-08
ES2323901T3 (es) 2009-07-27
DE602006006090D1 (de) 2009-05-14
RU2008125097A (ru) 2009-12-27
CA2630715C (fr) 2010-06-15
EP1951506B1 (de) 2009-04-01
EP1951506A1 (de) 2008-08-06
JP4705174B2 (ja) 2011-06-22
CA2630715A1 (fr) 2007-05-31
FR2893532A1 (fr) 2007-05-25
US7601288B2 (en) 2009-10-13
CN101316694B (zh) 2012-08-22
RU2383438C1 (ru) 2010-03-10
US20090223588A1 (en) 2009-09-10
FR2893532B1 (fr) 2008-02-15

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