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FR3000470B1 - Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe - Google Patents

Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe

Info

Publication number
FR3000470B1
FR3000470B1 FR1262947A FR1262947A FR3000470B1 FR 3000470 B1 FR3000470 B1 FR 3000470B1 FR 1262947 A FR1262947 A FR 1262947A FR 1262947 A FR1262947 A FR 1262947A FR 3000470 B1 FR3000470 B1 FR 3000470B1
Authority
FR
France
Prior art keywords
aircraft
adhesive
self
manufacturing
same
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
FR1262947A
Other languages
English (en)
Other versions
FR3000470A1 (fr
Inventor
Patrick Lieven
Romain Delahaye
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 FR1262947A priority Critical patent/FR3000470B1/fr
Priority to US14/140,513 priority patent/US9446834B2/en
Priority to DE102013114976.6A priority patent/DE102013114976A1/de
Publication of FR3000470A1 publication Critical patent/FR3000470A1/fr
Application granted granted Critical
Publication of FR3000470B1 publication Critical patent/FR3000470B1/fr
Expired - Fee Related 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
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • 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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/068—Fuselage sections
    • 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
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • 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
    • Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
FR1262947A 2012-12-28 2012-12-28 Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe Expired - Fee Related FR3000470B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1262947A FR3000470B1 (fr) 2012-12-28 2012-12-28 Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe
US14/140,513 US9446834B2 (en) 2012-12-28 2013-12-25 Self-stiffened skin for aircraft fuselage including stringers with a closed section and associated manufacturing method
DE102013114976.6A DE102013114976A1 (de) 2012-12-28 2013-12-30 Selbstversteifende Haut für einen Luftfahrzeugrumpf enthaltend Stringer mit einem geschlossenen Abschnitt und zugeordnetes Herstellungsverfahren

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1262947A FR3000470B1 (fr) 2012-12-28 2012-12-28 Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe

Publications (2)

Publication Number Publication Date
FR3000470A1 FR3000470A1 (fr) 2014-07-04
FR3000470B1 true FR3000470B1 (fr) 2015-12-25

Family

ID=47989202

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1262947A Expired - Fee Related FR3000470B1 (fr) 2012-12-28 2012-12-28 Peau auto-raidie pour fuselage d'aeronef comprenant des lisses a section fermee et procede de fabrication associe

Country Status (3)

Country Link
US (1) US9446834B2 (fr)
DE (1) DE102013114976A1 (fr)
FR (1) FR3000470B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2985232A1 (fr) 2014-08-13 2016-02-17 Airbus Operations GmbH Procédé d'assemblage d'un fuselage d'aéronef
US20200135305A1 (en) * 2018-10-24 2020-04-30 Conéctate Soluciones Y Aplicaciones Sl Procedure for unified global registry and universal identification of products of biological origin for medicinal purposes
CN110277254B (zh) * 2019-07-19 2024-01-30 深圳市沅鸿机械有限公司 一种可提高效率的整体替换甩干篮的含浸机
CN113650196B (zh) * 2021-07-27 2023-04-14 中航西安飞机工业集团股份有限公司 一种t型湿长桁成型模具精确定位装置及使用方法

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2845151A (en) * 1955-10-04 1958-07-29 Boeing Co Tube skin joint structure
US2945655A (en) * 1956-01-20 1960-07-19 Boeing Co Double skin airfoil structure
US4749155A (en) * 1985-09-30 1988-06-07 The Boeing Company Method of making wing box cover panel
DE4329744C1 (de) * 1993-09-03 1994-09-08 Deutsche Forsch Luft Raumfahrt Flügel mit Flügelschalen aus Faserverbundwerkstoffen, insbesondere CFK, für Luftfahrzeuge
FR2766407B1 (fr) * 1997-07-22 1999-10-15 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
DE19845863B4 (de) * 1998-10-05 2005-05-19 Deutsches Zentrum für Luft- und Raumfahrt e.V. Strukturelement mit großen unidirektionalen Steifigkeiten
US6231710B1 (en) * 1999-06-04 2001-05-15 The United States Of America As Represented By The Secretary Of The Air Force Method of making composite chambercore sandwich-type structure with inherent acoustic attenuation
US7197852B2 (en) * 2002-09-20 2007-04-03 The Boeing Company Internally stiffened composite panels and methods for their manufacture
US7459048B2 (en) 2006-01-31 2008-12-02 The Boeing Company One-piece inner shell for full barrel composite fuselage
US7871040B2 (en) * 2006-11-10 2011-01-18 The Boeing Company Composite aircraft structures with hat stiffeners
CN103249542A (zh) * 2010-07-13 2013-08-14 里尔喷射机公司 复合结构及其形成方法
GB201020189D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd An aircraft structure
US8616500B2 (en) * 2011-03-04 2013-12-31 The Boeing Company Diamond shaped window for composite and/or metallic airframe

Also Published As

Publication number Publication date
DE102013114976A1 (de) 2014-07-03
US20140186559A1 (en) 2014-07-03
US9446834B2 (en) 2016-09-20
FR3000470A1 (fr) 2014-07-04

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