BRPI0819353A2 - Cobre-junta de topo transversal bem como processo para união de duas seções de fuselagem cfk especialmente enroladas para provisão de uma célula de fuselagem. - Google Patents

Cobre-junta de topo transversal bem como processo para união de duas seções de fuselagem cfk especialmente enroladas para provisão de uma célula de fuselagem.

Info

Publication number
BRPI0819353A2
BRPI0819353A2 BRPI0819353A BRPI0819353A2 BR PI0819353 A2 BRPI0819353 A2 BR PI0819353A2 BR PI0819353 A BRPI0819353 A BR PI0819353A BR PI0819353 A2 BRPI0819353 A2 BR PI0819353A2
Authority
BR
Brazil
Prior art keywords
fuselage
fuselage sections
well
joining
sections
Prior art date
Application number
Other languages
English (en)
Inventor
Andreas Stephan
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 BRPI0819353A2 publication Critical patent/BRPI0819353A2/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
    • 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
    • B64C2001/0072—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
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Automatic Assembly (AREA)
  • Unwinding Of Filamentary Materials (AREA)
  • Secondary Cells (AREA)
  • Connection Of Batteries Or Terminals (AREA)
  • Butt Welding And Welding Of Specific Article (AREA)
BRPI0819353 2007-10-31 2008-10-30 Cobre-junta de topo transversal bem como processo para união de duas seções de fuselagem cfk especialmente enroladas para provisão de uma célula de fuselagem. BRPI0819353A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US98404207P 2007-10-31 2007-10-31
DE102007052098A DE102007052098A1 (de) 2007-10-31 2007-10-31 Querstoßlasche zur Schaffung einer Rumpfzelle sowie Verfahren zum Verbinden von zwei insbesondere gewickelten CFK-Rumpfsektionen
PCT/EP2008/009176 WO2009056319A1 (de) 2007-10-31 2008-10-30 Querstosslasche, sowie verfahren, zum verbinden von zwei insbesondere gewickelten cfk-rumpfsektionen zur schaffung einer rumpfzelle

Publications (1)

Publication Number Publication Date
BRPI0819353A2 true BRPI0819353A2 (pt) 2015-04-22

Family

ID=40530424

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0819353 BRPI0819353A2 (pt) 2007-10-31 2008-10-30 Cobre-junta de topo transversal bem como processo para união de duas seções de fuselagem cfk especialmente enroladas para provisão de uma célula de fuselagem.

Country Status (10)

Country Link
US (1) US8783610B2 (pt)
EP (1) EP2209710B1 (pt)
JP (1) JP5166543B2 (pt)
CN (1) CN101842285B (pt)
AT (1) ATE544669T1 (pt)
BR (1) BRPI0819353A2 (pt)
CA (1) CA2704764A1 (pt)
DE (1) DE102007052098A1 (pt)
RU (1) RU2010121981A (pt)
WO (1) WO2009056319A1 (pt)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2385906B1 (es) 2009-09-30 2013-06-17 Airbus Operations, S.L. Disposición de unión circunferencial de elementos estructurales con un elemento de acoplamiento realizado en material compuesto.
US8985514B2 (en) * 2012-06-20 2015-03-24 The Boeing Company Composite structural panels and aircraft fuselages
DE102015106761A1 (de) * 2015-04-30 2016-11-03 Airbus Operations Gmbh Montage von Strukturelementen in der Luftfahrt
DE102016210079A1 (de) * 2016-06-08 2017-12-14 Airbus Operations Gmbh Verfahren zum Herstellen eines Rumpfabschnitts
DE102016216527B4 (de) 2016-09-01 2020-08-20 Premium Aerotec Gmbh Spantvorrichtung und Anordnung

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR808710A (fr) 1935-12-19 1937-02-13 Fuselage en métal pour avions
FR1462186A (fr) 1964-12-16 1966-04-15 Cie Generale D Aeronautique Dispositif d'assemblage de pièces soumises à des efforts
US4793727A (en) * 1987-05-21 1988-12-27 United Technologies Corporation Two-step composite joint
US4839771A (en) * 1987-12-04 1989-06-13 The Boeing Company Apparatus for providing a lightning protective vehicle surface
US4920449A (en) * 1988-01-19 1990-04-24 The Boeing Company Conductive bonding of composite structures
US4888451A (en) * 1988-11-29 1989-12-19 United Technologies Corporation Electrical continuity means for composite joints
US5429326A (en) * 1992-07-09 1995-07-04 Structural Laminates Company Spliced laminate for aircraft fuselage
US5862975A (en) * 1996-03-20 1999-01-26 The Boeing Company Composite/metal structural joint with welded Z-pins
US6042055A (en) 1997-12-19 2000-03-28 Boeing North American, Inc. Structural joint to accomodate large thermally-induced displacements
US6327132B1 (en) * 1998-06-10 2001-12-04 Aerospatiale Matra Spark resistant structure, in particular for aircraft
DE19844035C1 (de) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung
US7554785B2 (en) * 2004-03-23 2009-06-30 The Boeing Company Lightning damage protection for composite aircraft
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US9302427B2 (en) * 2005-03-31 2016-04-05 The Boeing Company Aeropspace structure including composite beam chord clamped between reinforcement plates
US7721495B2 (en) * 2005-03-31 2010-05-25 The Boeing Company Composite structural members and methods for forming the same
NL2000100C2 (nl) * 2006-06-13 2007-12-14 Gtm Consulting B V Laminaat uit metaalplaten en kunststof.
FR2910874B1 (fr) * 2007-01-02 2009-02-13 Airbus France Sas Lisses assemblees au niveau d'une jonction circonferentielle d'un fuselage d'avion.
FR2915458B1 (fr) * 2007-04-25 2010-01-01 Airbus France Assemblage de panneaux de fuselage d'un avion
US8016230B2 (en) * 2007-05-11 2011-09-13 The Boeing Company Fastner-free primary structural joint for sandwich panels

Also Published As

Publication number Publication date
RU2010121981A (ru) 2011-12-10
CN101842285A (zh) 2010-09-22
ATE544669T1 (de) 2012-02-15
WO2009056319A4 (de) 2009-07-23
CN101842285B (zh) 2013-06-19
CA2704764A1 (en) 2009-05-07
WO2009056319A1 (de) 2009-05-07
EP2209710B1 (de) 2012-02-08
JP5166543B2 (ja) 2013-03-21
JP2011500449A (ja) 2011-01-06
US8783610B2 (en) 2014-07-22
DE102007052098A1 (de) 2009-05-14
US20100237194A1 (en) 2010-09-23
EP2209710A1 (de) 2010-07-28

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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 7A 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 2343 DE 01-12-2015 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.