BRPI1012150A2 - método de fabricar um fuselagem de aeronave e uma fuselagem de aeronave - Google Patents

método de fabricar um fuselagem de aeronave e uma fuselagem de aeronave

Info

Publication number
BRPI1012150A2
BRPI1012150A2 BRPI1012150A BRPI1012150A BRPI1012150A2 BR PI1012150 A2 BRPI1012150 A2 BR PI1012150A2 BR PI1012150 A BRPI1012150 A BR PI1012150A BR PI1012150 A BRPI1012150 A BR PI1012150A BR PI1012150 A2 BRPI1012150 A2 BR PI1012150A2
Authority
BR
Brazil
Prior art keywords
aircraft fuselage
manufacturing
fuselage
aircraft
Prior art date
Application number
BRPI1012150A
Other languages
English (en)
Inventor
Eugen Gorr
Rolf Bense
Original Assignee
Airbus Operations Gmbh
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 Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI1012150A2 publication Critical patent/BRPI1012150A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • 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
    • B64C1/061—Frames
    • 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
    • B64C1/069—Joining arrangements therefor
    • 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
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Automatic Assembly (AREA)
  • Connection Of Plates (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
BRPI1012150A 2009-05-12 2010-05-10 método de fabricar um fuselagem de aeronave e uma fuselagem de aeronave BRPI1012150A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US17730609P 2009-05-12 2009-05-12
DE102009021369A DE102009021369A1 (de) 2009-05-12 2009-05-12 Verfahren zur Herstellung eines Flugzeugrumpfes und Flugzeugrumpf
PCT/EP2010/056362 WO2010130687A2 (de) 2009-05-12 2010-05-10 Verfahren zur herstellung eines flugzeugrumpfes und flugzeugrumpf

Publications (1)

Publication Number Publication Date
BRPI1012150A2 true BRPI1012150A2 (pt) 2016-03-29

Family

ID=42979150

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1012150A BRPI1012150A2 (pt) 2009-05-12 2010-05-10 método de fabricar um fuselagem de aeronave e uma fuselagem de aeronave

Country Status (9)

Country Link
US (1) US9359090B2 (pt)
EP (1) EP2429894B1 (pt)
JP (1) JP2012526695A (pt)
CN (1) CN102712356B (pt)
BR (1) BRPI1012150A2 (pt)
CA (1) CA2761654A1 (pt)
DE (1) DE102009021369A1 (pt)
RU (1) RU2011150272A (pt)
WO (1) WO2010130687A2 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009021369A1 (de) 2009-05-12 2010-11-18 Airbus Operations Gmbh Verfahren zur Herstellung eines Flugzeugrumpfes und Flugzeugrumpf
FR2984274B1 (fr) * 2011-12-15 2014-06-27 Airbus Operations Sas Poutre securisee, en particulier cadre fort de fuselage, ainsi que fuselage d'aeronef equipe de tels cadres
CN102765472B (zh) * 2012-07-31 2015-03-11 江西洪都航空工业集团有限责任公司 一种飞机机身模块化连接装置
EP2738085A1 (en) * 2012-11-30 2014-06-04 Airbus Operations GmbH Aircraft fuselage structure and method
EP2759467B1 (en) * 2013-01-24 2016-10-19 Airbus Operations GmbH Aircraft frame and method of mounting two fuselage segments
DE102013102812B4 (de) * 2013-03-19 2017-01-26 Airbus Operations Gmbh Rumpfstruktur für ein Verkehrsmittel, Verkehrsmittel und Verfahren zum Herstellen einer Rumpfstruktur für ein Verkehrsmittel
US8894011B1 (en) * 2014-02-14 2014-11-25 The Boeing Company Aircraft fuselage constructed of aircraft fuselage sections screwed together
US9555587B2 (en) * 2014-08-13 2017-01-31 The Boeing Company Composite layup tools for aircraft fuselage barrels, methods of assembling the layup tools, and aircraft fuselage barrel sections formed utilizing the layup tools
US9981367B2 (en) * 2015-07-07 2018-05-29 The Boeing Company Exterior indexing process and tooling
EP4129817A1 (en) 2021-08-06 2023-02-08 Airbus Operations GmbH Method for joining structural profiles

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR510388A (fr) 1920-02-20 1920-12-03 Marcel Feierstein Procédé de construction et d'assemblage d'un fuselage métallique pour avions de tous modèles
DE727196C (de) 1934-12-23 1942-10-28 Messerschmitt A G Metallener Flugzeugrumpf
GB524721A (en) * 1938-02-05 1940-08-13 Amiot F Improvements in and relating to "stressed skin" fuselages or nacelles for aircraft
DE952595C (de) 1952-02-15 1956-11-15 Lionel Charles Heal Herstellung von Hohlkoerper mit unter Zugvorspannung stehender gekruemmter Haut und Herstellung von Beplankungen und Beplankungsteilen mit vorbestimmter Hautspannung
JPH0414598U (pt) 1990-05-30 1992-02-05
US5297760A (en) * 1992-08-21 1994-03-29 Mcdonnell Douglas Corporation Aircraft skin lap splice
US5266137A (en) * 1992-11-10 1993-11-30 Hollingsworth Ritch D Rigid segmented mandrel with inflatable support
DE19615716A1 (de) * 1996-04-22 1997-10-23 Bodenseewerk Geraetetech Rohrverbindung, insbesondere zum Verbinden zweier rohrförmiger Rumpfteile eines Flugkörpers
DE19735452C2 (de) * 1997-08-16 1999-07-22 Bodenseewerk Geraetetech Rohrverbindung, insbesondere zum Verbinden zweier rohrförmiger Rumpfteile eines Flugkörpers
JP4444033B2 (ja) * 2004-08-10 2010-03-31 三菱重工業株式会社 航空機の機体の製造方法
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
CN100506646C (zh) 2006-05-30 2009-07-01 空中客车德国有限公司 在飞机的两个机身段之间准备连接的方法
FR2915458B1 (fr) * 2007-04-25 2010-01-01 Airbus France Assemblage de panneaux de fuselage d'un avion
DE102007028918A1 (de) 2007-06-22 2009-01-02 Airbus Deutschland Gmbh Verfahren zur Herstellung einer Rumpfzelle eines Flugzeugs sowie Vorrichtung
WO2009068107A1 (en) 2007-11-29 2009-06-04 Airbus France Sas Method of preparing the connection between two fuselage sections of an aircraft
DE102008010197B4 (de) * 2008-02-20 2012-03-22 Airbus Operations Gmbh Verfahren zum Verbinden von zwei Rumpfsektionen unter Schaffung eines Querstoßes sowie Querstoßverbindung
DE102008043490A1 (de) * 2008-11-05 2010-05-12 Airbus Deutschland Gmbh Vorrichtung zur temporären Lagefixierung von zwei zusammen zu fügenden Rumpfsektionen
DE102009021369A1 (de) 2009-05-12 2010-11-18 Airbus Operations Gmbh Verfahren zur Herstellung eines Flugzeugrumpfes und Flugzeugrumpf

Also Published As

Publication number Publication date
CN102712356B (zh) 2015-07-15
US9359090B2 (en) 2016-06-07
WO2010130687A2 (de) 2010-11-18
RU2011150272A (ru) 2013-06-20
DE102009021369A1 (de) 2010-11-18
WO2010130687A3 (de) 2011-05-26
EP2429894A2 (de) 2012-03-21
CA2761654A1 (en) 2010-11-18
JP2012526695A (ja) 2012-11-01
CN102712356A (zh) 2012-10-03
EP2429894B1 (de) 2016-11-23
US20120132750A1 (en) 2012-05-31

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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 AS 4A, 5A E 6A ANUIDADES.

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.