ATE465943T1 - Flugzeugrumpfstruktur und herstellungsverfahren dafür - Google Patents

Flugzeugrumpfstruktur und herstellungsverfahren dafür

Info

Publication number
ATE465943T1
ATE465943T1 AT07729879T AT07729879T ATE465943T1 AT E465943 T1 ATE465943 T1 AT E465943T1 AT 07729879 T AT07729879 T AT 07729879T AT 07729879 T AT07729879 T AT 07729879T AT E465943 T1 ATE465943 T1 AT E465943T1
Authority
AT
Austria
Prior art keywords
shell
lower shell
aircraft
aircraft fuselage
manufacturing
Prior art date
Application number
AT07729879T
Other languages
English (en)
Inventor
Cord Haack
Original Assignee
Airbus 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 Gmbh filed Critical Airbus Gmbh
Application granted granted Critical
Publication of ATE465943T1 publication Critical patent/ATE465943T1/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
    • B64C1/061—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
    • 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
    • B64C2001/0045—Fuselages characterised by special shapes
    • 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
    • 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
    • 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
    • Y10T29/49826—Assembling or joining
    • Y10T29/49947—Assembling or joining by applying separate fastener

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Body Structure For Vehicles (AREA)
AT07729879T 2006-06-06 2007-06-05 Flugzeugrumpfstruktur und herstellungsverfahren dafür ATE465943T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006026170A DE102006026170B4 (de) 2006-06-06 2006-06-06 Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
PCT/EP2007/055494 WO2007141251A2 (en) 2006-06-06 2007-06-05 Aircraft fuselage structure and method for its production

Publications (1)

Publication Number Publication Date
ATE465943T1 true ATE465943T1 (de) 2010-05-15

Family

ID=38720942

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07729879T ATE465943T1 (de) 2006-06-06 2007-06-05 Flugzeugrumpfstruktur und herstellungsverfahren dafür

Country Status (10)

Country Link
US (1) US8651421B2 (de)
EP (1) EP2032430B1 (de)
JP (1) JP2009539672A (de)
CN (1) CN101466592B (de)
AT (1) ATE465943T1 (de)
BR (1) BRPI0712248A2 (de)
CA (1) CA2654045A1 (de)
DE (2) DE102006026170B4 (de)
RU (1) RU2435703C2 (de)
WO (1) WO2007141251A2 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006026170B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026169B4 (de) 2006-06-06 2012-06-21 Airbus Operations Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
DE102006026168A1 (de) * 2006-06-06 2008-01-31 Airbus Deutschland Gmbh Flugzeugrumpfstruktur und Verfahren zu deren Herstellung
FR2934562B1 (fr) * 2008-07-31 2011-04-22 Airbus France Panneau de protection et module de train d'atterissage le comportant.
CN102126549A (zh) * 2010-01-20 2011-07-20 苏章仁 圆形截面飞行载体壳体顺航向非对称分离仿生结构
WO2012021283A1 (en) * 2010-08-13 2012-02-16 Hexcel Corporation Machinable composite material
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
RU2737210C1 (ru) * 2017-10-11 2020-11-26 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Узел крепления металлической конструкции с конструкцией из полимерных композиционных материалов
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Also Published As

Publication number Publication date
WO2007141251A3 (en) 2009-01-22
US8651421B2 (en) 2014-02-18
WO2007141251A2 (en) 2007-12-13
EP2032430B1 (de) 2010-04-28
DE102006026170B4 (de) 2012-06-21
JP2009539672A (ja) 2009-11-19
US20090314891A1 (en) 2009-12-24
RU2008151379A (ru) 2010-07-20
BRPI0712248A2 (pt) 2012-01-17
CA2654045A1 (en) 2007-12-13
DE602007006188D1 (de) 2010-06-10
CN101466592B (zh) 2011-07-06
CN101466592A (zh) 2009-06-24
RU2435703C2 (ru) 2011-12-10
EP2032430A2 (de) 2009-03-11
DE102006026170A1 (de) 2007-12-27

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