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BRPI0817758A2 - Estrutura de fuselagem para fuselagem de aeronave de material compósito, e, aeronave - Google Patents

Estrutura de fuselagem para fuselagem de aeronave de material compósito, e, aeronave

Info

Publication number
BRPI0817758A2
BRPI0817758A2 BRPI0817758A BRPI0817758A2 BR PI0817758 A2 BRPI0817758 A2 BR PI0817758A2 BR PI0817758 A BRPI0817758 A BR PI0817758A BR PI0817758 A2 BRPI0817758 A2 BR PI0817758A2
Authority
BR
Brazil
Prior art keywords
aircraft
fuselage
composite material
fuselage structure
airframe
Prior art date
Application number
Other languages
English (en)
Inventor
Guillaume Gallant
Laurent Giuseppin
Damien Aguera
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
Publication of BRPI0817758A2 publication Critical patent/BRPI0817758A2/pt

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Laminated Bodies (AREA)
  • Tires In General (AREA)
  • Moulding By Coating Moulds (AREA)
  • Reinforced Plastic Materials (AREA)
BRPI0817758 2007-10-08 2008-09-29 Estrutura de fuselagem para fuselagem de aeronave de material compósito, e, aeronave BRPI0817758A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0758132A FR2921898B1 (fr) 2007-10-08 2007-10-08 Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage
PCT/EP2008/063018 WO2009047158A1 (fr) 2007-10-08 2008-09-29 Structure de fuselage pour fuselage d'aeronef en materiau composite et aeronef equipe d'une telle structure de fuselage.

Publications (1)

Publication Number Publication Date
BRPI0817758A2 true BRPI0817758A2 (pt) 2015-03-24

Family

ID=39473966

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0817758 BRPI0817758A2 (pt) 2007-10-08 2008-09-29 Estrutura de fuselagem para fuselagem de aeronave de material compósito, e, aeronave

Country Status (10)

Country Link
US (1) US8550399B2 (pt)
EP (1) EP2197739B1 (pt)
JP (1) JP5462174B2 (pt)
CN (1) CN101821161B (pt)
AT (1) ATE510766T1 (pt)
BR (1) BRPI0817758A2 (pt)
CA (1) CA2701690A1 (pt)
FR (1) FR2921898B1 (pt)
RU (1) RU2473452C2 (pt)
WO (1) WO2009047158A1 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2952905B1 (fr) * 2009-11-20 2012-06-01 Airbus Operations Sas Dispositif d'attache de moyens raidisseurs a un element de cadre, et structure comportant un tel dispositif d'attache
JP5808111B2 (ja) * 2011-02-04 2015-11-10 三菱重工業株式会社 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体
FR2984845B1 (fr) * 2011-12-21 2014-07-11 Airbus Operations Sas Element de structure de fuselage d'aeronef anti deversement
RU2595354C1 (ru) * 2015-05-21 2016-08-27 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Корпус гиперзвукового летательного аппарата и способ его изготовления
CN107434031A (zh) 2016-05-25 2017-12-05 空中客车简化股份公司 飞行器翼体的结构部件和包括该结构部件的飞行器
RU2694638C2 (ru) * 2017-11-09 2019-07-16 Акционерное общество Научно-производственное объединение "Опытно-конструкторское бюро имени М.П. Симонова" Кессон фюзеляжа
RU202616U1 (ru) * 2020-11-02 2021-03-01 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" Фюзеляж летательного аппарата из ферменного заполнителя

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2489779A1 (fr) * 1980-09-09 1982-03-12 Aerospatiale Structure de fuselage pour aeronef resistant aux ruptures longitudinales du revetement exterieur
US4502092A (en) * 1982-09-30 1985-02-26 The Boeing Company Integral lightning protection system for composite aircraft skins
FR2693976B1 (fr) * 1992-07-22 1994-09-30 Eurocopter France Structure de fuselage pour hélicoptère.
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
JP4318381B2 (ja) * 2000-04-27 2009-08-19 本田技研工業株式会社 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体
EP1336469A1 (en) * 2002-02-19 2003-08-20 Alenia Aeronautica S.P.A. Methods of manufacturing a stiffening element for an aircraft skin panel and a skin panel provided with the stiffening element
DE102004001078B8 (de) * 2004-01-05 2013-06-13 Airbus Operations Gmbh Flugzeugrumpf
DE102004001049B4 (de) * 2004-01-05 2009-12-10 Airbus Deutschland Gmbh Isolierpaket-Anordnung zur Innenisolierung eines Flugzeugrumpfes
RU2270135C2 (ru) * 2004-03-04 2006-02-20 Карклин Андрей Михайлович Фюзеляж летательного аппарата
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
FR2894869B1 (fr) 2005-12-20 2009-10-09 Airbus France Sas Procede de fabrication d'un fuselage d'aeronef en materiau composite
US7277266B1 (en) * 2006-03-29 2007-10-02 The Boeing Company Lightning protection system for composite structure

Also Published As

Publication number Publication date
RU2473452C2 (ru) 2013-01-27
EP2197739B1 (fr) 2011-05-25
WO2009047158A1 (fr) 2009-04-16
US8550399B2 (en) 2013-10-08
CA2701690A1 (fr) 2009-04-16
ATE510766T1 (de) 2011-06-15
JP5462174B2 (ja) 2014-04-02
FR2921898A1 (fr) 2009-04-10
RU2010117200A (ru) 2011-11-20
CN101821161A (zh) 2010-09-01
JP2010540348A (ja) 2010-12-24
FR2921898B1 (fr) 2009-12-11
US20100264273A1 (en) 2010-10-21
EP2197739A1 (fr) 2010-06-23
CN101821161B (zh) 2013-02-13

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 8A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2385 DE 20-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.