BRPI0917986A2 - seção de fuselagem possuindo um anteparo de pressão integral formado de material de fibras compostas assim como um casco de fuselagem possuindo uma seção de fuselagem como esta. - Google Patents

seção de fuselagem possuindo um anteparo de pressão integral formado de material de fibras compostas assim como um casco de fuselagem possuindo uma seção de fuselagem como esta.

Info

Publication number
BRPI0917986A2
BRPI0917986A2 BRPI0917986A BRPI0917986A BRPI0917986A2 BR PI0917986 A2 BRPI0917986 A2 BR PI0917986A2 BR PI0917986 A BRPI0917986 A BR PI0917986A BR PI0917986 A BRPI0917986 A BR PI0917986A BR PI0917986 A2 BRPI0917986 A2 BR PI0917986A2
Authority
BR
Brazil
Prior art keywords
fuselage
fuselage section
well
hull
fiber material
Prior art date
Application number
BRPI0917986A
Other languages
English (en)
Inventor
Birgit Willms
Torsten Noebel
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 BRPI0917986A2 publication Critical patent/BRPI0917986A2/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Gasket Seals (AREA)
BRPI0917986A 2008-08-12 2009-07-30 seção de fuselagem possuindo um anteparo de pressão integral formado de material de fibras compostas assim como um casco de fuselagem possuindo uma seção de fuselagem como esta. BRPI0917986A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US18874908P 2008-08-12 2008-08-12
DE102008041173A DE102008041173A1 (de) 2008-08-12 2008-08-12 Rumpfsektion mit integralem Druckschott sowie Rumpfschale mit einer derartigen Rumpfsektion
PCT/EP2009/059836 WO2010018063A1 (de) 2008-08-12 2009-07-30 Rumpfsektion mit einem aus faserverbundwerkstoff ausgebildeten integralem druckschott sowie rumpfschale mit einer derartigen rumpfsektion

Publications (1)

Publication Number Publication Date
BRPI0917986A2 true BRPI0917986A2 (pt) 2015-11-17

Family

ID=41605805

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0917986A BRPI0917986A2 (pt) 2008-08-12 2009-07-30 seção de fuselagem possuindo um anteparo de pressão integral formado de material de fibras compostas assim como um casco de fuselagem possuindo uma seção de fuselagem como esta.

Country Status (9)

Country Link
US (1) US8651422B2 (pt)
EP (1) EP2310261B1 (pt)
JP (1) JP2011530448A (pt)
CN (1) CN102164817B (pt)
BR (1) BRPI0917986A2 (pt)
CA (1) CA2733664A1 (pt)
DE (1) DE102008041173A1 (pt)
RU (1) RU2011103081A (pt)
WO (1) WO2010018063A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008040213B4 (de) * 2008-07-07 2011-08-25 Airbus Operations GmbH, 21129 Verfahren zur Montage eines kalottenförmigen Druckschotts in einer Hecksektion eines Flugzeugs sowie Vorrichtung zur Durchführung des Verfahrens
DE102008041173A1 (de) 2008-08-12 2010-03-04 Airbus Deutschland Gmbh Rumpfsektion mit integralem Druckschott sowie Rumpfschale mit einer derartigen Rumpfsektion
WO2012096696A1 (en) 2011-01-12 2012-07-19 Stanford University Composite laminated structures and methods for manufacturing and using the same
GB201217801D0 (en) * 2012-10-05 2012-11-14 Airbus Operations Ltd An aircraft structure
US10189578B2 (en) * 2013-06-12 2019-01-29 The Boeing Company Self-balancing pressure bulkhead
US20150030805A1 (en) * 2013-07-29 2015-01-29 Compagnie Chomarat Composite bi-angle and thin-ply laminate tapes and methods for manufacturing and using the same
CA2969519A1 (en) * 2014-05-06 2015-11-12 The Patent Well LLC A thin gel gasket and a method of making and using the same
EP3040266B1 (en) * 2014-12-30 2018-04-11 Airbus Operations S.L. Aircraft rear structure
EP3059156B1 (en) * 2015-02-23 2020-04-01 Airbus Operations, S.L. Flat kinked rear pressure bulkhead
CN110465102A (zh) * 2019-07-05 2019-11-19 嘉兴安行信息科技有限公司 一种组装式固定翼无人机手办

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB562301A (en) * 1941-07-29 1944-06-27 Vickers Armstrongs Ltd Improvements in or connected with aircraft
DE3010958A1 (de) 1980-03-21 1981-10-01 Stiebel Eltron Gmbh & Co Kg, 3450 Holzminden Kunststoff-druckbehaelter
DE3923871A1 (de) 1989-02-28 1991-01-31 Dornier Luftfahrt Druckspant
FR2693976B1 (fr) * 1992-07-22 1994-09-30 Eurocopter France Structure de fuselage pour hélicoptère.
US5297760A (en) * 1992-08-21 1994-03-29 Mcdonnell Douglas Corporation Aircraft skin lap splice
DE19503939C1 (de) * 1995-02-07 1996-06-05 Daimler Benz Aerospace Airbus Verfahren und Vorrichtung zum Herstellen eines Druckspants
DE19652172C2 (de) * 1996-12-14 1998-09-17 Daimler Benz Aerospace Airbus Druckspant für einen Flugzeugrumpf
US5908175A (en) * 1997-11-19 1999-06-01 Magnes; Gene One-piece airplane tail-cone with inspection door(s)
US6042055A (en) * 1997-12-19 2000-03-28 Boeing North American, Inc. Structural joint to accomodate large thermally-induced displacements
US7261257B2 (en) * 2004-11-23 2007-08-28 Helou Jr Elie Cargo aircraft
DE102006060360B8 (de) * 2006-12-20 2010-09-30 Airbus Deutschland Gmbh Rumpfsektion zur Bildung einer Rumpfzelle eines Flugzeugs
DE102008041173A1 (de) 2008-08-12 2010-03-04 Airbus Deutschland Gmbh Rumpfsektion mit integralem Druckschott sowie Rumpfschale mit einer derartigen Rumpfsektion

Also Published As

Publication number Publication date
CN102164817B (zh) 2014-09-17
CN102164817A (zh) 2011-08-24
US20110198443A1 (en) 2011-08-18
DE102008041173A1 (de) 2010-03-04
JP2011530448A (ja) 2011-12-22
US8651422B2 (en) 2014-02-18
EP2310261A1 (de) 2011-04-20
EP2310261B1 (de) 2014-04-23
WO2010018063A1 (de) 2010-02-18
RU2011103081A (ru) 2012-09-20
CA2733664A1 (en) 2010-02-18

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Legal Events

Date Code Title Description
B11A Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]