DE602006007862D1 - Verfahren zur herstellung eines rtm-verbundteils und mit diesem verfahren hergestellte verbundpleuelstange - Google Patents

Verfahren zur herstellung eines rtm-verbundteils und mit diesem verfahren hergestellte verbundpleuelstange

Info

Publication number
DE602006007862D1
DE602006007862D1 DE602006007862T DE602006007862T DE602006007862D1 DE 602006007862 D1 DE602006007862 D1 DE 602006007862D1 DE 602006007862 T DE602006007862 T DE 602006007862T DE 602006007862 T DE602006007862 T DE 602006007862T DE 602006007862 D1 DE602006007862 D1 DE 602006007862D1
Authority
DE
Germany
Prior art keywords
manufacturing
bar arranged
compound bar
rtm composite
rtm
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.)
Active
Application number
DE602006007862T
Other languages
English (en)
Inventor
Frederick Cavaliere
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
EADS CCR
Original Assignee
EADS CCR
European Aeronautic Defence and Space Company EADS France
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 EADS CCR, European Aeronautic Defence and Space Company EADS France filed Critical EADS CCR
Publication of DE602006007862D1 publication Critical patent/DE602006007862D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B29C70/865Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
    • 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
    • B29C70/88Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/887Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced locally reinforced, e.g. by fillers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C7/00Connecting-rods or like links pivoted at both ends; Construction of connecting-rod heads
    • F16C7/02Constructions of connecting-rods with constant length
    • F16C7/026Constructions of connecting-rods with constant length made of fibre reinforced resin
    • 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
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/0809Fabrics
    • 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
    • B29K2105/06Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B29K2105/10Cords, strands or rovings, e.g. oriented cords, strands or rovings
    • B29K2105/101Oriented
    • 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
    • B29K2105/24Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/243Partially cured
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/29Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
    • Y10T428/2913Rod, strand, filament or fiber
    • Y10T428/2933Coated or with bond, impregnation or core
    • Y10T428/2935Discontinuous or tubular or cellular core
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/21Elements
    • Y10T74/2142Pitmans and connecting rods
DE602006007862T 2005-09-12 2006-09-12 Verfahren zur herstellung eines rtm-verbundteils und mit diesem verfahren hergestellte verbundpleuelstange Active DE602006007862D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0552745A FR2890591B1 (fr) 2005-09-12 2005-09-12 Procede de fabrication d'une piece composite rtm et piece composite obtenue selon ce procede
PCT/FR2006/002102 WO2007031649A1 (fr) 2005-09-12 2006-09-12 Procede de fabrication d’une piece composite rtm et bielle composite obtenue selon ce procede

Publications (1)

Publication Number Publication Date
DE602006007862D1 true DE602006007862D1 (de) 2009-08-27

Family

ID=36555443

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006007862T Active DE602006007862D1 (de) 2005-09-12 2006-09-12 Verfahren zur herstellung eines rtm-verbundteils und mit diesem verfahren hergestellte verbundpleuelstange

Country Status (9)

Country Link
US (1) US20090148700A1 (de)
EP (1) EP1924426B1 (de)
JP (1) JP2009507689A (de)
CN (1) CN101287587B (de)
CA (1) CA2622213C (de)
DE (1) DE602006007862D1 (de)
ES (1) ES2329938T3 (de)
FR (1) FR2890591B1 (de)
WO (1) WO2007031649A1 (de)

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FR2932410B1 (fr) 2008-06-11 2010-05-28 Aircelle Sa Procede de fabrication d'une piece a corps creux en materiau composite
EP2266788A1 (de) * 2009-06-26 2010-12-29 Bd Invent S.A. Herstellungsverfahren von Verbund-Pleuelstangen und nach diesem Verfahren erhaltene Pleuelstangen
FR2953160A1 (fr) * 2009-11-30 2011-06-03 Messier Dowty Sa Procede de fabrication d'une bielle en materiau composite integrant une chape renforcee
US8753465B2 (en) 2010-01-22 2014-06-17 Messier-Bugatti-Dowty Method for manufacturing composite parts comprising braided fibers
FR2957844B1 (fr) * 2010-03-26 2012-05-18 Messier Dowty Sa Procede de fabrication d'un organe mecanique en materiau composite ayant une tenue mecanique accrue en traction-compression et en flexion
FR2964339B1 (fr) 2010-09-06 2014-01-31 Messier Dowty Sa Procede de fabrication de pieces en materiaux composites, avec revetement tresse
DE102010063094A1 (de) * 2010-12-15 2012-06-21 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines materialhybriden Bauteils
WO2012085299A1 (es) 2010-12-23 2012-06-28 Internacional De Composites, Sa. Metodo para la fabricación de una barra de material compuesto y barra de carga fabricada en material compuesto
DE102011012900A1 (de) 2011-03-03 2012-02-09 Daimler Ag Faserverstärktes Kunststoffverbundbauteil und dessen Herstellung
FR2979884B1 (fr) * 2011-09-13 2014-05-02 Valeo Systemes Thermiques Piece de structure, notamment longeron de face avant de vehicule, et procede de fabrication d'une telle piece
US10457011B2 (en) 2011-11-03 2019-10-29 The Boeing Company Composite columnar structure having co-bonded reinforcement and fabrication method
US8904904B2 (en) 2011-11-03 2014-12-09 The Boeing Company Tubular composite strut having internal stiffening
US9486965B2 (en) 2011-11-03 2016-11-08 The Boeing Company Composite columnar structure having co-bonded reinforcement and fabrication method
US10464656B2 (en) 2011-11-03 2019-11-05 The Boeing Company Tubular composite strut having internal stiffening and method for making the same
DE102013221172A1 (de) * 2013-10-18 2015-04-23 Bayerische Motoren Werke Aktiengesellschaft Verfahren zum Herstellen eines verstärkten Faserverbundbauteils
CN103921453A (zh) * 2013-12-04 2014-07-16 中航复合材料有限责任公司 一种预浸料闭模液压辅助成型工艺方法
US9463588B2 (en) * 2014-02-07 2016-10-11 Todas Santos Surf, Inc. Surf fin including injection molded pre-impregnated composite fiber matrix inserts
JP5959558B2 (ja) * 2014-03-13 2016-08-02 アイシン高丘株式会社 複合構造体及びその製造方法
CN103963315B (zh) * 2014-05-29 2016-05-25 上海飞机制造有限公司 一种复合材料的预浸料/树脂传递模塑共固化工艺方法
CN105587752A (zh) * 2015-12-09 2016-05-18 上海复合材料科技有限公司 复合材料连接杆及其制备方法
FR3053911B1 (fr) * 2016-07-13 2018-08-17 Safran Aircraft Engines Procede d'impregnation de preforme fibreuse utilisant un joint et procede de fabrication d'une matrice renforcee par une preforme fibreuse
IT201700019306A1 (it) * 2017-02-21 2018-08-21 Automobili Lamborghini Spa Procedimento e semilavorato per fabbricare prodotti compositi e prodotti così ottenuti
FR3081761B1 (fr) 2018-06-04 2021-10-22 Skf Aerospace France Procede de fabrication d'une piece en matiere composite
DE102018213321A1 (de) * 2018-08-08 2020-02-13 Zf Friedrichshafen Ag Mehrpunktlenker für ein Fahrwerk eines Kraftfahrzeugs
CN109737134B (zh) * 2019-03-14 2021-03-30 中国商用飞机有限责任公司 破损安全连杆
FR3102085B1 (fr) * 2019-10-22 2022-12-09 Airbus Operations Sas Procede de fabrication d’une piece en materiau composite comportant une premiere puis une deuxieme polymerisation.
CN114633495A (zh) * 2022-03-18 2022-06-17 安徽玄离智能科技股份有限公司 一种用于井下巡检机器人的碳纤维材料的铺贴和固化工艺

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Also Published As

Publication number Publication date
EP1924426B1 (de) 2009-07-15
WO2007031649A1 (fr) 2007-03-22
CA2622213A1 (fr) 2007-03-22
FR2890591B1 (fr) 2012-10-19
CN101287587B (zh) 2010-08-25
ES2329938T3 (es) 2009-12-02
CA2622213C (fr) 2013-11-05
US20090148700A1 (en) 2009-06-11
FR2890591A1 (fr) 2007-03-16
CN101287587A (zh) 2008-10-15
JP2009507689A (ja) 2009-02-26
EP1924426A1 (de) 2008-05-28

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