FR2832668B1 - Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede - Google Patents

Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede

Info

Publication number
FR2832668B1
FR2832668B1 FR0115264A FR0115264A FR2832668B1 FR 2832668 B1 FR2832668 B1 FR 2832668B1 FR 0115264 A FR0115264 A FR 0115264A FR 0115264 A FR0115264 A FR 0115264A FR 2832668 B1 FR2832668 B1 FR 2832668B1
Authority
FR
France
Prior art keywords
portions
composite material
lay
layer
aircraft
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.)
Expired - Fee Related
Application number
FR0115264A
Other languages
English (en)
Other versions
FR2832668A1 (fr
Inventor
Franck Bequet
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 FR0115264A priority Critical patent/FR2832668B1/fr
Priority to CA2411744A priority patent/CA2411744C/fr
Priority to US10/304,654 priority patent/US6908526B2/en
Publication of FR2832668A1 publication Critical patent/FR2832668A1/fr
Application granted granted Critical
Publication of FR2832668B1 publication Critical patent/FR2832668B1/fr
Priority to US11/147,011 priority patent/US7874517B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • B29C70/30—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
    • 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
    • B29L2031/3085—Wings
    • 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

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
FR0115264A 2001-11-26 2001-11-26 Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede Expired - Fee Related FR2832668B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR0115264A FR2832668B1 (fr) 2001-11-26 2001-11-26 Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede
CA2411744A CA2411744C (fr) 2001-11-26 2002-11-13 Procede de fabrication d'un materiau composite et d'une aile d'avion, et element de stabilisation ainsi obtenu
US10/304,654 US6908526B2 (en) 2001-11-26 2002-11-25 Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process
US11/147,011 US7874517B2 (en) 2001-11-26 2005-06-07 Process for making a composite material assembly and aircraft wing and stabilizing element obtained by this process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0115264A FR2832668B1 (fr) 2001-11-26 2001-11-26 Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede

Publications (2)

Publication Number Publication Date
FR2832668A1 FR2832668A1 (fr) 2003-05-30
FR2832668B1 true FR2832668B1 (fr) 2004-02-13

Family

ID=8869787

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0115264A Expired - Fee Related FR2832668B1 (fr) 2001-11-26 2001-11-26 Procede de fabrication d'un ensemble en materiau composite et voilure et element stabilisateur d'aeronef obtenus par ce procede

Country Status (3)

Country Link
US (2) US6908526B2 (fr)
CA (1) CA2411744C (fr)
FR (1) FR2832668B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7837148B2 (en) * 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
EP1918193A1 (fr) * 2006-10-31 2008-05-07 Airbus Espana, S.L. Revêtement composite intégré pour surfaces de levage d'aéronef
US7851040B2 (en) * 2007-10-24 2010-12-14 Embraer - Empresa Brasileira De Aeronautica S.A. Methods for making composite material components especially useful for aircraft, and composite material components thereof
GB201103122D0 (en) 2011-02-23 2011-04-06 Airbus Uk Ltd Composite structure
GB201103125D0 (en) 2011-02-23 2011-04-06 Airbus Uk Ltd Composite structure
EP2700574B1 (fr) * 2012-08-22 2016-08-17 Airbus Operations GmbH Réduction de charge passive pour caisson central à fibres renforcées d'un avion ayant une structure de coque rigide

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3687795A (en) * 1970-01-28 1972-08-29 Robert A Elkin Tubular laminate
US4601770A (en) * 1980-09-11 1986-07-22 Ameron, Inc. Fiber reinforced plastic pipe tee
DE3103710C2 (de) * 1981-02-04 1983-03-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Rotor in Schalenbauweise"
US4437616A (en) * 1981-09-08 1984-03-20 Ameron, Inc. Winding fiber reinforced pipe fittings
US4741943A (en) * 1985-12-30 1988-05-03 The Boeing Company Aerodynamic structures of composite construction
DE4335221C1 (de) * 1993-10-15 1995-03-16 Deutsche Forsch Luft Raumfahrt Rotorblatt für Windkraftanlagen
GB9816938D0 (en) * 1998-08-05 1998-09-30 British Aerospace An aircraft fin and rudder
US6190484B1 (en) * 1999-02-19 2001-02-20 Kari Appa Monolithic composite wing manufacturing process

Also Published As

Publication number Publication date
US7874517B2 (en) 2011-01-25
CA2411744C (fr) 2010-08-24
FR2832668A1 (fr) 2003-05-30
US6908526B2 (en) 2005-06-21
US20030098116A1 (en) 2003-05-29
CA2411744A1 (fr) 2003-05-26
US20060076102A1 (en) 2006-04-13

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

ST Notification of lapse

Effective date: 20120731