BR112012001721A2 - processo de fabricação de uma peça aeronave, peça de aeronave, aeronave e instalação para a fabricação de uma peça de aeronave - Google Patents

processo de fabricação de uma peça aeronave, peça de aeronave, aeronave e instalação para a fabricação de uma peça de aeronave

Info

Publication number
BR112012001721A2
BR112012001721A2 BR112012001721A BR112012001721A BR112012001721A2 BR 112012001721 A2 BR112012001721 A2 BR 112012001721A2 BR 112012001721 A BR112012001721 A BR 112012001721A BR 112012001721 A BR112012001721 A BR 112012001721A BR 112012001721 A2 BR112012001721 A2 BR 112012001721A2
Authority
BR
Brazil
Prior art keywords
aircraft
aircraft part
manufacturing
installation
manufacturing process
Prior art date
Application number
BR112012001721A
Other languages
English (en)
Inventor
Benoît Hochart
Philippe Blot
Stéphane Bechtel
Original Assignee
Airbus Operations Sas
Eads Europ Aeronautic Defence
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 Sas, Eads Europ Aeronautic Defence filed Critical Airbus Operations Sas
Publication of BR112012001721A2 publication Critical patent/BR112012001721A2/pt

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
    • B29C70/28—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
    • B29C70/443—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 and impregnating by vacuum or injection
    • 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
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546—Measures for feeding or distributing the matrix material in the reinforcing structure
    • 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
    • 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
BR112012001721A 2009-07-28 2010-07-16 processo de fabricação de uma peça aeronave, peça de aeronave, aeronave e instalação para a fabricação de uma peça de aeronave BR112012001721A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0955290A FR2948600B1 (fr) 2009-07-28 2009-07-28 Procede de fabrication d'une piece d'aeronef par infusion de resine
PCT/FR2010/051498 WO2011015747A1 (fr) 2009-07-28 2010-07-16 Procede de fabrication d'une piece d'aeronef par infusion de resine

Publications (1)

Publication Number Publication Date
BR112012001721A2 true BR112012001721A2 (pt) 2016-04-12

Family

ID=41820354

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012001721A BR112012001721A2 (pt) 2009-07-28 2010-07-16 processo de fabricação de uma peça aeronave, peça de aeronave, aeronave e instalação para a fabricação de uma peça de aeronave

Country Status (9)

Country Link
US (1) US9272470B2 (pt)
EP (1) EP2459363B1 (pt)
JP (1) JP5762406B2 (pt)
CN (1) CN102656006B (pt)
BR (1) BR112012001721A2 (pt)
CA (1) CA2769560C (pt)
FR (1) FR2948600B1 (pt)
RU (1) RU2531811C2 (pt)
WO (1) WO2011015747A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2995556B1 (fr) 2012-09-17 2014-10-10 Eads Europ Aeronautic Defence Dispositif d'infusion d'une piece composite et procede associe
DK2799215T3 (en) * 2013-05-02 2019-01-14 Siemens Ag Perforated vacuum membrane for fiber reinforced laminates
EP2843020A1 (en) * 2013-08-29 2015-03-04 Airbus Operations S.L. Laminate for joining parts, and method and system for joining parts
CN103909659B (zh) * 2014-04-03 2016-03-30 中航复合材料有限责任公司 一种树脂膜渗透成型树脂基复合材料的方法
EP3489001A1 (en) * 2017-11-22 2019-05-29 Afros S.P.A. Apparatus for fine and controlled adjustment of an injection molding process and related industrial process
JP7202258B2 (ja) * 2018-09-03 2023-01-11 株式会社Subaru 樹脂含浸測定システム

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5770155A (en) * 1995-11-21 1998-06-23 United Technologies Corporation Composite structure resin cure monitoring apparatus using an optical fiber grating sensor
US6048488A (en) * 1997-04-04 2000-04-11 The United States Of America As Represented By The Secretary Of The Army One-step resin transfer molding of multifunctional composites consisting of multiple resins
DE19912723C1 (de) * 1999-03-20 2000-11-09 Dlr Ev Verfahren und Vorrichtung zur Bestimmung der Durchtränkung von Faserhalbzeugen
DE10013409C1 (de) * 2000-03-17 2000-11-23 Daimler Chrysler Ag Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens
US7081218B2 (en) * 2001-08-07 2006-07-25 Toray Industries, Inc. Method for producing upsized FRP member
DE10228649A1 (de) * 2002-06-26 2004-01-22 Bakelite Ag Verfahren zur Herstellung eines faserverstärkten Produktes auf Epoxidharzbasis
EP2644365B1 (en) 2002-10-09 2019-03-27 Toray Industries, Inc. Method of RTM molding
JP2004309332A (ja) 2003-04-08 2004-11-04 R & D Inst Of Metals & Composites For Future Industries Ｒｔｍ成形における樹脂先端検出センサ
CA2434447A1 (fr) * 2003-06-27 2004-12-27 Eduardo Ruiz Fabrication des composites par un procede d'injection flexible au moyen d'un moule a double chambre ou a chambres multiples
JP4803028B2 (ja) * 2004-03-30 2011-10-26 東レ株式会社 プリフォーム、ｆｒｐおよびそれらの製造方法
DK176135B1 (da) * 2004-11-30 2006-09-18 Lm Glasfiber As Vakuuminfusion ved hjælp af semipermeabel membran
US7332049B2 (en) * 2004-12-22 2008-02-19 General Electric Company Method for fabricating reinforced composite materials
DE102006031336B4 (de) * 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt
US7850897B2 (en) * 2007-03-14 2010-12-14 Spectrum Aeronautical, Llc Method and device for manufacturing a unitary caul sheet
FR2921295A1 (fr) 2007-09-24 2009-03-27 Airbus France Sas Dispositif pour la fabrication d'une piece en materiau composite integrant un systeme de drainage

Also Published As

Publication number Publication date
EP2459363B1 (fr) 2014-03-05
CA2769560A1 (fr) 2011-02-10
JP2013500180A (ja) 2013-01-07
US20120126060A1 (en) 2012-05-24
RU2012107001A (ru) 2013-09-10
FR2948600A1 (fr) 2011-02-04
JP5762406B2 (ja) 2015-08-12
CN102656006A (zh) 2012-09-05
FR2948600B1 (fr) 2011-10-07
EP2459363A1 (fr) 2012-06-06
RU2531811C2 (ru) 2014-10-27
CN102656006B (zh) 2016-05-18
CA2769560C (fr) 2018-07-31
WO2011015747A1 (fr) 2011-02-10
US9272470B2 (en) 2016-03-01

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B11E Dismissal acc. art. 34 of ipl - requirements for examination incomplete
B11T Dismissal of application maintained [chapter 11.20 patent gazette]