DE602007012844D1 - Verfahren zur herstellung versteifter platten aus verbundwerkstoff - Google Patents

Verfahren zur herstellung versteifter platten aus verbundwerkstoff

Info

Publication number
DE602007012844D1
DE602007012844D1 DE602007012844T DE602007012844T DE602007012844D1 DE 602007012844 D1 DE602007012844 D1 DE 602007012844D1 DE 602007012844 T DE602007012844 T DE 602007012844T DE 602007012844 T DE602007012844 T DE 602007012844T DE 602007012844 D1 DE602007012844 D1 DE 602007012844D1
Authority
DE
Germany
Prior art keywords
composite
fibres
plates
stiffener
cured
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
DE602007012844T
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
Original Assignee
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 European Aeronautic Defence and Space Company EADS France filed Critical European Aeronautic Defence and Space Company EADS France
Publication of DE602007012844D1 publication Critical patent/DE602007012844D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
    • B29C33/3821—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process composed of particles enclosed in a bag
    • 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
    • B29C33/00—Moulds or cores; Details thereof or accessories therefor
    • B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
    • B29C33/50—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
    • B29C33/505—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping 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
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
DE602007012844T 2006-03-20 2007-03-20 Verfahren zur herstellung versteifter platten aus verbundwerkstoff Active DE602007012844D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0650957A FR2898539B1 (fr) 2006-03-20 2006-03-20 Procede de realisation de panneaux raidis en materiau composite et panneaux ainsi realises
PCT/EP2007/052622 WO2007107553A1 (fr) 2006-03-20 2007-03-20 Procede de realisation de panneaux raidis en materiau composites et panneaux ainsi realises

Publications (1)

Publication Number Publication Date
DE602007012844D1 true DE602007012844D1 (de) 2011-04-14

Family

ID=37507713

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007012844T Active DE602007012844D1 (de) 2006-03-20 2007-03-20 Verfahren zur herstellung versteifter platten aus verbundwerkstoff

Country Status (10)

Country Link
US (1) US20090309264A1 (de)
EP (1) EP2004390B1 (de)
CN (1) CN101448631A (de)
AT (1) ATE500052T1 (de)
CA (1) CA2649621A1 (de)
DE (1) DE602007012844D1 (de)
ES (1) ES2360832T3 (de)
FR (1) FR2898539B1 (de)
RU (1) RU2426646C2 (de)
WO (1) WO2007107553A1 (de)

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US8601694B2 (en) † 2008-06-13 2013-12-10 The Boeing Company Method for forming and installing stringers
DE102006031336B4 (de) 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt
DE102006031335B4 (de) 2006-07-06 2011-01-27 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031334A1 (de) 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031325B4 (de) 2006-07-06 2010-07-01 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
FR2924375B1 (fr) * 2007-11-30 2013-05-10 Eads Europ Aeronautic Defence Procede de realisation d'un noyau de moulage et noyau de moulage pour la fabrication d'une piece complexe en materiau compositie
EP2067596B1 (de) 2007-12-06 2010-10-20 Saab Ab Verfahren und Vorrichtung zur Herstellung eines Gegenstandes mit einem leeren Raum
FR2928577B1 (fr) * 2008-03-14 2011-11-25 Airbus France Procede de realisation d'un raidisseur evide en forme de omega et noyau pour la realisation d'un raidisseur evide en forme de omega
JP5416554B2 (ja) * 2009-11-06 2014-02-12 川崎重工業株式会社 複合材料構造物製造用治具
DE102010008711A1 (de) * 2010-02-19 2011-08-25 GKN Aerospace Services Limited, Isle of Wight Verfahren und Anordnung zur Herstellung eines einstückigen Hohlprofilbauteils mit Faserverbundwerkstoff
GB2485183A (en) * 2010-11-04 2012-05-09 Rolls Royce Plc Generating residual stress in hollow body during cure to deflect composite body on relaxation
GB201020152D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress
FR2995279B1 (fr) * 2012-09-10 2017-05-26 European Aeronautic Defence & Space Co Eads France Panneau raidi
US8986484B2 (en) * 2012-10-10 2015-03-24 The Boeing Company Shape-distorting tooling system and method for curing composite parts
FR2998545B1 (fr) * 2012-11-23 2016-10-28 Airbus Operations Sas Nacelle d'aeronef comprenant une liaison renforcee entre une entree d'air et une motorisation
CN104057648A (zh) * 2013-03-18 2014-09-24 空客(北京)工程技术中心有限公司 混合夹层结构、加强件及其加工方法
CN103195446A (zh) * 2013-04-19 2013-07-10 山东科技大学 软岩巷道底臌让压缓冲装置及其施工方法
US9205634B2 (en) * 2013-05-16 2015-12-08 The Boeing Company Composite structure and method
US20160214331A1 (en) * 2013-10-04 2016-07-28 United Technologies Corporation Flexible resin transfer molding tool
EP2865516B1 (de) 2013-10-28 2016-03-09 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Oberflächeversteifte Verbundplatte und Verfahren zu deren Herstellung
DE102014215965A1 (de) * 2014-08-12 2016-02-18 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines faserverstärkten Kunststoffbauteils
DE102015122211A1 (de) * 2015-06-26 2016-12-29 Grob Aircraft Ag Werkzeug
TWI613065B (zh) * 2015-12-08 2018-02-01 National Chung Shan Institute Of Science And Technology Armaments Bureau 一種樑肋與蒙皮一體成形之模具結構及其製作方法
US20170232688A1 (en) * 2016-02-15 2017-08-17 General Electric Company Incorporation Of Jamming Technologies In Tooling For Composites Processing
CN106273539A (zh) * 2016-08-29 2017-01-04 中航复合材料有限责任公司 一种帽型加筋壁板共固化成型工艺方法
CN106314753A (zh) * 2016-09-23 2017-01-11 江西洪都航空工业集团有限责任公司 一种高强度高刚度轻质整体机体结构
US10899103B2 (en) 2016-11-03 2021-01-26 Anthony A. DUPont Isogrid stiffening elements
US10639855B2 (en) * 2017-02-07 2020-05-05 General Electric Company Applicator systems for applying pressure to a structure
CN106933098B (zh) * 2017-02-24 2019-10-01 上海理工大学 平板型机械结构热变形补偿系统设计方法
US10717239B2 (en) * 2017-09-28 2020-07-21 The Boeing Company Fabrication of gap fillers for composite parts that exhibit varying radii of curvature
CN108639310B (zh) * 2018-06-15 2021-10-15 大连理工大学 一种基于充压变刚度弧形管驱动的可变形板结构
CN109228375B (zh) * 2018-11-01 2023-08-18 成都纵横大鹏无人机科技有限公司 一种蒙皮成型方法
CA3119802C (en) * 2019-03-08 2023-06-27 Ihi Aerospace Co., Ltd. Frp molding system and method
DE102019005910A1 (de) * 2019-08-22 2021-02-25 Siempelkamp Maschinen- Und Anlagenbau Gmbh Verfahren und Vorrichtung zum Erzeugen eines Bauelements
CN110524910A (zh) * 2019-09-09 2019-12-03 山东非金属材料研究所 一种vartm工艺用复合材料模具及其制造方法
US20210308967A1 (en) * 2020-04-07 2021-10-07 Rohr, Inc. Hybrid mandrel for use in tooling methods and the manufacture of thrust reverser cascades and structures susceptible to trapped tooling
DE102020134901A1 (de) * 2020-12-23 2022-06-23 Airbus Operations Gmbh Formkern zur Herstellung eines Bauteils aus Faserverbundmaterial
CN115258128B (zh) * 2022-09-27 2022-12-02 成都市鸿侠科技有限责任公司 用于飞机壁板加工的加固结构

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IT1223923B (it) * 1988-11-22 1990-09-29 Ferrari Engineering Spa Procedimento per la costruzione di elementi monolitici cavi in materiale composito in particolare in fibra di carbonio
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US5387098A (en) * 1992-04-23 1995-02-07 The Boeing Company Flexible reusable mandrels
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GB2292332B (en) * 1994-04-22 1999-04-28 Alan Roger Harper Moulding process and apparatus therefor
US5968445A (en) * 1998-01-05 1999-10-19 The Boeing Company Method and apparatus for curing large composite panels
US6458309B1 (en) * 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
US7559332B2 (en) * 2002-07-02 2009-07-14 Toyota Motor Sales U.S.A., Inc. Media removal apparatus and methods of removing media
US7293737B2 (en) * 2004-04-20 2007-11-13 The Boeing Company Co-cured stringers and associated mandrel and fabrication method

Also Published As

Publication number Publication date
CN101448631A (zh) 2009-06-03
RU2008141301A (ru) 2010-04-27
EP2004390A1 (de) 2008-12-24
EP2004390B1 (de) 2011-03-02
FR2898539B1 (fr) 2008-05-23
RU2426646C2 (ru) 2011-08-20
WO2007107553A1 (fr) 2007-09-27
ATE500052T1 (de) 2011-03-15
US20090309264A1 (en) 2009-12-17
CA2649621A1 (fr) 2007-09-27
ES2360832T3 (es) 2011-06-09
FR2898539A1 (fr) 2007-09-21

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