FR2953754B1 - Outillage pour la fabrication d'un panneau en materiau composite, en particulier d'un fuselage d'aeronef - Google Patents

Outillage pour la fabrication d'un panneau en materiau composite, en particulier d'un fuselage d'aeronef Download PDF

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Publication number
FR2953754B1
FR2953754B1 FR0906076A FR0906076A FR2953754B1 FR 2953754 B1 FR2953754 B1 FR 2953754B1 FR 0906076 A FR0906076 A FR 0906076A FR 0906076 A FR0906076 A FR 0906076A FR 2953754 B1 FR2953754 B1 FR 2953754B1
Authority
FR
France
Prior art keywords
tooling
panel
manufacturing
composite material
aircraft fuselage
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
FR0906076A
Other languages
English (en)
Other versions
FR2953754A1 (fr
Inventor
Cedric Meyer
Jocelyn Gaudin
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 Operations SAS
Original Assignee
Airbus Operations SAS
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 filed Critical Airbus Operations SAS
Priority to FR0906076A priority Critical patent/FR2953754B1/fr
Priority to US12/968,579 priority patent/US8869402B2/en
Priority to CA2724935A priority patent/CA2724935C/fr
Publication of FR2953754A1 publication Critical patent/FR2953754A1/fr
Application granted granted Critical
Publication of FR2953754B1 publication Critical patent/FR2953754B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B29C33/76—Cores
    • 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
    • B29C33/30—Mounting, exchanging or centering
    • B29C33/306—Exchangeable mould parts, e.g. cassette moulds, mould 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
    • B29C70/28—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
    • 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
    • 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
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y10T29/49622—Vehicular structural member making
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49764—Method of mechanical manufacture with testing or indicating
    • Y10T29/49771—Quantitative measuring or gauging
    • 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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
FR0906076A 2009-12-16 2009-12-16 Outillage pour la fabrication d'un panneau en materiau composite, en particulier d'un fuselage d'aeronef Active FR2953754B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR0906076A FR2953754B1 (fr) 2009-12-16 2009-12-16 Outillage pour la fabrication d'un panneau en materiau composite, en particulier d'un fuselage d'aeronef
US12/968,579 US8869402B2 (en) 2009-12-16 2010-12-15 Methods for manufacturing a tool equipment including a plurality of removable modules and for molding a fuselage panel
CA2724935A CA2724935C (fr) 2009-12-16 2010-12-15 Outillage pour la fabrication d'un panneau en materiau composite, en particulier d'un fuselage d'aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0906076A FR2953754B1 (fr) 2009-12-16 2009-12-16 Outillage pour la fabrication d'un panneau en materiau composite, en particulier d'un fuselage d'aeronef
FR0906076 2009-12-16

Publications (2)

Publication Number Publication Date
FR2953754A1 FR2953754A1 (fr) 2011-06-17
FR2953754B1 true FR2953754B1 (fr) 2018-03-02

Family

ID=42341461

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0906076A Active FR2953754B1 (fr) 2009-12-16 2009-12-16 Outillage pour la fabrication d'un panneau en materiau composite, en particulier d'un fuselage d'aeronef

Country Status (3)

Country Link
US (1) US8869402B2 (fr)
CA (1) CA2724935C (fr)
FR (1) FR2953754B1 (fr)

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US8955206B2 (en) * 2011-07-12 2015-02-17 The Boeing Company Method and apparatus for creating a layup of reinforcing fibers
FR2979574B1 (fr) * 2011-09-07 2016-12-09 Airbus Operations Sas Procede de fabrication d'une structure comprenant une peau et des raidisseurs
DE102012223810A1 (de) * 2012-12-19 2014-06-26 Sgl Carbon Se Variable Formvorrichtung zur Herstellung einer Halbschale für ein Rotorblatt für eine Windenergieanlage
US10899045B2 (en) * 2013-03-12 2021-01-26 U.S.A. As Represented By The Administrator Of The National Aeronautics And Space Administration High pressure soft lithography for micro-topographical patterning of molded polymers and composites
WO2015004257A1 (fr) * 2013-07-12 2015-01-15 Lm Wp Patent Holding A/S Procédé et outils pour la fabrication d'une pale de turbine éolienne et pale fabriquée
GB201417695D0 (en) 2014-10-07 2014-11-19 Rolls Royce Plc Tooling production method
GB2535193A (en) * 2015-02-12 2016-08-17 Zodiac Seats Uk Ltd Tool for curing a composite component
US11167508B2 (en) 2019-07-30 2021-11-09 Spirit Aerosystems, Inc. System and method for fabricating and curing large composite structures
CN111016223A (zh) * 2019-11-08 2020-04-17 北京宇航系统工程研究所 一种用于无内衬复合材料贮箱制造的可拆卸组合式工装

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US4363617A (en) * 1981-07-17 1982-12-14 Hirsekorn Franklin D Vacuum mold for plastics
US5242523A (en) * 1992-05-14 1993-09-07 The Boeing Company Caul and method for bonding and curing intricate composite structures
US5393479A (en) * 1993-05-27 1995-02-28 Hoover Universal, Inc. Method for shaping a trim cover fabric for a vehicle seat
NO309417B1 (no) * 1997-04-04 2001-01-29 John Cheetham Apparat og fremgangsmåte for preging av et mönster
US7228611B2 (en) * 2003-11-18 2007-06-12 The Boeing Company Method of transferring large uncured composite laminates
US7503368B2 (en) * 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7410352B2 (en) * 2005-04-13 2008-08-12 The Boeing Company Multi-ring system for fuselage barrel formation
ITTO20060463A1 (it) * 2006-06-23 2007-12-24 Alenia Aeronautica Spa Apparecchiatura e procedimento per la fabbricazione di un tronco di fusoliera
GB0614087D0 (en) * 2006-07-14 2006-08-23 Airbus Uk Ltd Composite manufacturing method
GB0616121D0 (en) * 2006-08-14 2006-09-20 Airbus Uk Ltd Moulding tool and method of manufacturing a part
EP2062814B1 (fr) * 2006-08-31 2013-07-10 Airbus Operations S.L. Procédé et outil de fabrication de composants tubulaires pour fuselages aéronautiques
WO2008092971A1 (fr) * 2007-01-30 2008-08-07 Airbus España, S.L. Structure de matière composée pour le fuselage d'un aéronef et son procédé de fabrication
US8256714B2 (en) * 2007-03-07 2012-09-04 Jie Zhao Modularized airplane structures and methods
FR2927013B1 (fr) * 2008-01-31 2010-02-19 Airbus France Dispositif pour la fabrication d'une piece en materiau composite comprenant des toles de lissage a jonctions glissantes et procede de fabrication de toles de lissage a jonctions glissantes
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
GB0810870D0 (en) * 2008-06-13 2008-07-23 Advanced Composite Components Tooling
FR2936496B1 (fr) * 2008-09-30 2010-09-24 Airbus France Procede de fabrication d'un troncon de fuselage d'aeronef en materiau composite
DE102009019434B4 (de) * 2009-04-29 2016-01-07 Airbus Operations Gmbh Flugzeugtür und Verfahren zur Herstellung einer derartigen Flugzeugtür

Also Published As

Publication number Publication date
US8869402B2 (en) 2014-10-28
US20120023727A1 (en) 2012-02-02
CA2724935A1 (fr) 2011-06-16
FR2953754A1 (fr) 2011-06-17
CA2724935C (fr) 2017-12-12

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