WO2009098088A3 - Verfahren zur herstellung eines fvw-bauteils, fvw-bauteil sowie ein fvw-rumpfteil eines flugzeugs - Google Patents

Verfahren zur herstellung eines fvw-bauteils, fvw-bauteil sowie ein fvw-rumpfteil eines flugzeugs Download PDF

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Publication number
WO2009098088A3
WO2009098088A3 PCT/EP2009/000891 EP2009000891W WO2009098088A3 WO 2009098088 A3 WO2009098088 A3 WO 2009098088A3 EP 2009000891 W EP2009000891 W EP 2009000891W WO 2009098088 A3 WO2009098088 A3 WO 2009098088A3
Authority
WO
WIPO (PCT)
Prior art keywords
component
fibre composite
preg
skinning
composite component
Prior art date
Application number
PCT/EP2009/000891
Other languages
English (en)
French (fr)
Other versions
WO2009098088A2 (de
Inventor
Wolfgang Kastner
Thomas Grauerholz
Original Assignee
Airbus Operations Gmbh
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 Operations Gmbh filed Critical Airbus Operations Gmbh
Priority to US12/866,375 priority Critical patent/US8398910B2/en
Priority to EP09708885A priority patent/EP2254788A2/de
Priority to JP2010545414A priority patent/JP2011510866A/ja
Priority to BRPI0908375A priority patent/BRPI0908375A2/pt
Priority to CN200980104568.5A priority patent/CN101939217B/zh
Priority to CA2714175A priority patent/CA2714175C/en
Publication of WO2009098088A2 publication Critical patent/WO2009098088A2/de
Publication of WO2009098088A3 publication Critical patent/WO2009098088A3/de

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
    • B29C70/88—Shaping 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
    • B29C70/887—Shaping 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
    • 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
    • B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • 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
    • B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • 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
    • B29L2031/724—Doors
    • 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
    • B29L2031/778—Windows
    • 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
    • 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.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24521—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness with component conforming to contour of nonplanar surface

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

Verfahren zur Herstellung eines FVW-Bauteils (1) mit einem Beplankungsfeld (2) und einem Primärbauteil (8) zur Verstärkung des FVW-Bauteils (1), mit den Schritten: Aufbringen eines Prepreg-Halbzeugs (4) auf eine Werkzeugform zur Ausbildung des Beplankungsfelds (2), wobei in dem Prepreg-Halbzeug (4) Fasern entsprechend eines angenommenen Kraftflussverlaufs in dem Beplankungsfeld (2) des herzustellenden Bauteils (1) bereichsweise krummlinig verlaufen; Härten des Prepreg-Halbzeugs (4); Aufbringen von Lagen eines Textil-Halbzeugs (10) auf das gehärtete Prepreg-Halbzeug (4) zur Ausbildung des Primärbauteils (8); Tränken des Textil-Halbzeugs (10) mit Matrixmaterial und Härten der Baugruppe aus vorgehärtetem Prepreg-Halbzeug (4) und Textil-Halbzeug (10); FVW-Bauteil mit zumindest einem Trägerbauteil und einem mit diesem verbundenen Hautabschnitt mit einer Ausnehmung sowie ein FVW-Rumpfteil eines Flugzeugs mit einem Schalenteil mit zumindest einer Ausnehmung und mit einem als Rahmenteil gebildeten Trägerbauteil.
PCT/EP2009/000891 2008-02-08 2009-02-09 Verfahren zur herstellung eines fvw-bauteils, fvw-bauteil sowie ein fvw-rumpfteil eines flugzeugs WO2009098088A2 (de)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US12/866,375 US8398910B2 (en) 2008-02-08 2009-02-09 Method for manufacturing a fibre-composite component, fibre-composite component and fibre-composite fuselage component of an aircraft
EP09708885A EP2254788A2 (de) 2008-02-08 2009-02-09 Verfahren zur herstellung eines fvw-bauteils, fvw-bauteil sowie ein fvw-rumpfteil eines flugzeugs
JP2010545414A JP2011510866A (ja) 2008-02-08 2009-02-09 ファイバ複合材料構成部品を製造するための方法、ファイバ複合材料構成部品、および航空機のファイバ複合材料機体構成部品
BRPI0908375A BRPI0908375A2 (pt) 2008-02-08 2009-02-09 processo para a fabricação de componente de fvw, componente de fvw, bem como, parte de fuselagem de fvw de avião
CN200980104568.5A CN101939217B (zh) 2008-02-08 2009-02-09 用于制造纤维复合材料构件的方法、纤维复合材料构件以及飞机的纤维复合材料机身部件
CA2714175A CA2714175C (en) 2008-02-08 2009-02-09 Method for manufacturing a fibre-composite component, fibre-composite component and fibre-composite fuselage component of an aircraft

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US2716808P 2008-02-08 2008-02-08
US61/027,168 2008-02-08
DE102008008386.0 2008-02-09
DE102008008386A DE102008008386A1 (de) 2008-02-09 2008-02-09 Verfahren zur Herstellung eines FVW-Bauteils

Publications (2)

Publication Number Publication Date
WO2009098088A2 WO2009098088A2 (de) 2009-08-13
WO2009098088A3 true WO2009098088A3 (de) 2010-01-14

Family

ID=40847339

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/000891 WO2009098088A2 (de) 2008-02-08 2009-02-09 Verfahren zur herstellung eines fvw-bauteils, fvw-bauteil sowie ein fvw-rumpfteil eines flugzeugs

Country Status (9)

Country Link
US (1) US8398910B2 (de)
EP (1) EP2254788A2 (de)
JP (1) JP2011510866A (de)
CN (1) CN101939217B (de)
BR (1) BRPI0908375A2 (de)
CA (1) CA2714175C (de)
DE (1) DE102008008386A1 (de)
RU (1) RU2010136997A (de)
WO (1) WO2009098088A2 (de)

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ES2338084B1 (es) * 2008-10-30 2011-03-14 Airbus Operations, S.L. Metodo de fabricacion de un panel de geometria compleja en material compuesto preimpregnado.
US9108718B2 (en) * 2009-10-08 2015-08-18 Mitsubishi Heavy Industries, Ltd. Composite-material structure and aircraft main wing and aircraft fuselage provided with the same
DE102009056533B4 (de) * 2009-12-03 2015-02-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugzeugrumpfbauteil
DE102010014265B4 (de) * 2010-04-08 2013-01-31 Deutsches Zentrum für Luft- und Raumfahrt e.V. Türrahmenanordnung mit einer Tür für einen Rumpf insbesondere für Luft- oder Raumfahrzeuge
ES2400768B1 (es) * 2010-06-30 2014-02-12 Airbus Operations, S.L. Estructura interna de aeronave en material compuesto.
CA2815966C (en) * 2011-02-04 2017-09-19 Mitsubishi Heavy Industries, Ltd. Composite material structure, and aircraft wing and fuselage provided therewith
US8616500B2 (en) * 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe
US9243407B2 (en) * 2013-04-25 2016-01-26 Sikorsky Aircraft Corporation Structure repair with polymer matrix composites
CN103324782B (zh) * 2013-05-29 2016-01-20 北京航空航天大学 一种复合材料受压蒙皮稳定性及承载能力的不确定性优化方法
DE102013215332A1 (de) * 2013-08-05 2015-02-05 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines Faserverbundbauteils mittels einer Trägerschicht
EP2843020A1 (de) * 2013-08-29 2015-03-04 Airbus Operations S.L. Laminat zur Verbindung von Teilen, und Verfahren und System zum Verbinden von Teilen
DE112014005199T5 (de) * 2013-12-16 2016-08-04 Borgwarner Inc. Verbund-Spannarm oder -Führung für Steuerantriebsanwendungen
JP6309324B2 (ja) * 2014-03-28 2018-04-11 三菱重工業株式会社 複合材構造体、これを備えた航空機翼および航空機胴体、並びに複合材構造体の製造方法
FR3027273B1 (fr) * 2014-10-17 2018-04-27 Arianegroup Sas Architecture de paroi de face de voiture telle qu'une voiture de train en composite sandwich
US10195817B2 (en) * 2015-01-02 2019-02-05 The Boeing Company Skin-stringer design for composite wings
DE102016115418B4 (de) 2016-08-19 2023-12-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Versteifungsstruktur zur Versteifung von Flächengebilden sowie Herstellungsverfahren hierzu
US10179438B2 (en) 2016-09-23 2019-01-15 Bell Helicopter Textron Inc. Method and assembly for manufacturing door skin and wall with doorway
DE102017107524A1 (de) * 2017-04-07 2018-10-11 Airbus Operations Gmbh Verfahren und Formwerkzeug zur Herstellung eines profilversteiften Schalenbauteils
US11370181B2 (en) * 2017-10-18 2022-06-28 General Electric Company Methods for manufacturing composite components
DE102017126052A1 (de) * 2017-11-08 2019-05-09 Airbus Operations Gmbh Versteifungsanordnung für eine Öffnung in einer Flugzeugstruktur
DE102017222983A1 (de) * 2017-12-18 2019-06-19 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines Faserverbundbauteils
DE102020105602A1 (de) 2020-03-03 2021-09-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zum Herstellen eines flächigen Strukturbauteils aus einem Faser-Kunststoff-Verbund
CN113844078B (zh) * 2021-07-20 2023-07-28 航天材料及工艺研究所 一种超轻质多特征无蒙皮骨架式复合材料壳体制备方法
EP4166307A1 (de) * 2021-10-14 2023-04-19 Airbus Defence and Space GmbH Faserverbundstruktur und verfahren zur herstellung einer faserverbundstruktur

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US20070218795A1 (en) * 2000-07-28 2007-09-20 David Taggart Process and equipment for manufacture of advanced composite structures
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Also Published As

Publication number Publication date
CN101939217A (zh) 2011-01-05
DE102008008386A1 (de) 2009-08-13
CN101939217B (zh) 2014-10-08
RU2010136997A (ru) 2012-03-20
EP2254788A2 (de) 2010-12-01
US20110024562A1 (en) 2011-02-03
BRPI0908375A2 (pt) 2019-02-26
US8398910B2 (en) 2013-03-19
CA2714175A1 (en) 2009-08-13
CA2714175C (en) 2016-06-21
JP2011510866A (ja) 2011-04-07
WO2009098088A2 (de) 2009-08-13

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