ATE525281T1 - Strukturelement für einen flugzeugrumpf - Google Patents

Strukturelement für einen flugzeugrumpf

Info

Publication number
ATE525281T1
ATE525281T1 AT08736584T AT08736584T ATE525281T1 AT E525281 T1 ATE525281 T1 AT E525281T1 AT 08736584 T AT08736584 T AT 08736584T AT 08736584 T AT08736584 T AT 08736584T AT E525281 T1 ATE525281 T1 AT E525281T1
Authority
AT
Austria
Prior art keywords
structural element
aircraft fuselage
aircraft
stringers
fuse
Prior art date
Application number
AT08736584T
Other languages
English (en)
Inventor
Claus-Peter Gross
Cord Haack
Dirk Humfeldt
Oliver Thomaschewski
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
Application granted granted Critical
Publication of ATE525281T1 publication Critical patent/ATE525281T1/de

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
    • B64C1/064—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
    • B64C1/40—Sound or heat insulation, e.g. using insulation blankets
    • 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)
  • Body Structure For Vehicles (AREA)
  • Mutual Connection Of Rods And Tubes (AREA)
  • Tires In General (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Gasket Seals (AREA)
AT08736584T 2007-04-26 2008-04-25 Strukturelement für einen flugzeugrumpf ATE525281T1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US91409707P 2007-04-26 2007-04-26
DE102007019821A DE102007019821B4 (de) 2007-04-26 2007-04-26 Strukturelement eines Flugzeugrumpfs
PCT/EP2008/055084 WO2008132171A2 (en) 2007-04-26 2008-04-25 Structural element of an aircraft fuselage

Publications (1)

Publication Number Publication Date
ATE525281T1 true ATE525281T1 (de) 2011-10-15

Family

ID=39829141

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08736584T ATE525281T1 (de) 2007-04-26 2008-04-25 Strukturelement für einen flugzeugrumpf

Country Status (10)

Country Link
US (1) US8905349B2 (de)
EP (1) EP2137064B1 (de)
JP (1) JP2010524771A (de)
CN (1) CN101674978B (de)
AT (1) ATE525281T1 (de)
BR (1) BRPI0810569A2 (de)
CA (1) CA2682969A1 (de)
DE (1) DE102007019821B4 (de)
RU (1) RU2470830C2 (de)
WO (1) WO2008132171A2 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007032233B4 (de) 2007-07-11 2014-07-10 Airbus Operations Gmbh Installationssystem für ein Flugzeug
DE102007032235B4 (de) * 2007-07-11 2015-05-07 Airbus Operations Gmbh Leichtes Schienensystem zur Krafteinleitung großer Lasten in eine Struktur
DE102007052672B4 (de) * 2007-11-05 2016-12-01 Airbus Operations Gmbh Rumpfzellenstruktur eines Flugzeugs zur vereinfachten Verlegung und Befestigung von Haltern zur Befestigung von Leitungen
DE102008020789A1 (de) 2008-04-25 2009-11-05 Airbus Deutschland Gmbh Befestigungssystem sowie Verfahren zum Befestigen eines Elementes einer Flugzeuginnenausstattung
DE102009029120B4 (de) 2009-09-02 2011-12-08 Airbus Operations Gmbh Anordnung, insbesondere im Luft- und Raumfahrtbereich
EP2655194B1 (de) * 2010-12-23 2017-05-17 Airbus Operations GmbH Flugzeugsystemhalterung und methode zum zusammenbauen von systemkomponenten
FR2976916B1 (fr) * 2011-06-27 2013-07-26 Airbus Operations Sas Dispositif et procede d'assemblage de deux troncons de fuselage d'aeronef
DE102012001797A1 (de) * 2012-01-30 2013-08-01 Airbus Operations Gmbh System und Verfahren zur Montage von Flugzeugsystemkomponenten in der Crown Area eines Flugzeugs
DE102012009312A1 (de) * 2012-05-10 2013-11-14 Airbus Operations Gmbh Rumpfaufbau
EP3266705B1 (de) * 2016-07-05 2019-06-26 Airbus Operations GmbH Innenraumkomponententrägersystem und verfahren zur montage eines flugzeuginnenraumkomponententrägersystems
DE102018210507A1 (de) * 2018-06-27 2020-01-02 Airbus Operations Gmbh Montagesystem für eine automatisierte Innenmontage eines Flugzeugrumpfes
CN111055995A (zh) * 2019-12-31 2020-04-24 南京儒一航空机械装备有限公司 一种不易变形的主梁梁体及其加工工艺
EP4378837B1 (de) * 2022-11-30 2025-06-11 Airbus Operations GmbH Installationssystem und verfahren zur installation einer selbsttragenden fachwerkstruktur

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US5931415A (en) * 1997-05-09 1999-08-03 The Boeing Company Plug-type overwing emergency exit door assembly
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US6648273B2 (en) 2001-10-30 2003-11-18 The Boeing Company Light weight and high strength fuselage
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JP4354463B2 (ja) 2006-02-28 2009-10-28 三菱重工業株式会社 複合材を用いた構造部材の成形方法及び複合材料を用いた構造部材

Also Published As

Publication number Publication date
CN101674978B (zh) 2015-04-29
EP2137064B1 (de) 2011-09-21
CA2682969A1 (en) 2008-11-06
DE102007019821A1 (de) 2008-11-13
WO2008132171A2 (en) 2008-11-06
WO2008132171A3 (en) 2009-01-15
RU2470830C2 (ru) 2012-12-27
CN101674978A (zh) 2010-03-17
BRPI0810569A2 (pt) 2017-05-09
US8905349B2 (en) 2014-12-09
RU2009136665A (ru) 2011-04-20
WO2008132171A4 (en) 2009-02-26
DE102007019821B4 (de) 2012-11-22
EP2137064A2 (de) 2009-12-30
JP2010524771A (ja) 2010-07-22
US20100243805A1 (en) 2010-09-30

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