DE102006060360B8 - Fuselage section to form a fuselage cell of an aircraft - Google Patents

Fuselage section to form a fuselage cell of an aircraft Download PDF

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Publication number
DE102006060360B8
DE102006060360B8 DE102006060360A DE102006060360A DE102006060360B8 DE 102006060360 B8 DE102006060360 B8 DE 102006060360B8 DE 102006060360 A DE102006060360 A DE 102006060360A DE 102006060360 A DE102006060360 A DE 102006060360A DE 102006060360 B8 DE102006060360 B8 DE 102006060360B8
Authority
DE
Germany
Prior art keywords
fuselage
aircraft
cell
section
fuselage section
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
DE102006060360A
Other languages
German (de)
Other versions
DE102006060360A1 (en
DE102006060360B4 (en
Inventor
Andreas Stephan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
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
Priority to DE102006060360A priority Critical patent/DE102006060360B8/en
Publication of DE102006060360A1 publication Critical patent/DE102006060360A1/en
Application granted granted Critical
Publication of DE102006060360B4 publication Critical patent/DE102006060360B4/en
Publication of DE102006060360B8 publication Critical patent/DE102006060360B8/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Connection Of Plates (AREA)
DE102006060360A 2006-12-20 2006-12-20 Fuselage section to form a fuselage cell of an aircraft Expired - Fee Related DE102006060360B8 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE102006060360A DE102006060360B8 (en) 2006-12-20 2006-12-20 Fuselage section to form a fuselage cell of an aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006060360A DE102006060360B8 (en) 2006-12-20 2006-12-20 Fuselage section to form a fuselage cell of an aircraft

Publications (3)

Publication Number Publication Date
DE102006060360A1 DE102006060360A1 (en) 2008-06-26
DE102006060360B4 DE102006060360B4 (en) 2010-02-04
DE102006060360B8 true DE102006060360B8 (en) 2010-09-30

Family

ID=39431468

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102006060360A Expired - Fee Related DE102006060360B8 (en) 2006-12-20 2006-12-20 Fuselage section to form a fuselage cell of an aircraft

Country Status (1)

Country Link
DE (1) DE102006060360B8 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008041173A1 (en) * 2008-08-12 2010-03-04 Airbus Deutschland Gmbh Fuselage section with integral pressure bulkhead and hull shell with such a fuselage section
DE102008041172B9 (en) * 2008-08-12 2014-03-13 Airbus Operations Gmbh Aircraft with a fuselage structure with welded skin panels
DE102015106761A1 (en) 2015-04-30 2016-11-03 Airbus Operations Gmbh Assembly of structural elements in aviation

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19615716A1 (en) * 1996-04-22 1997-10-23 Bodenseewerk Geraetetech Pipe connection, in particular for connecting two tubular fuselage parts of a missile
DE19929471C1 (en) * 1999-06-26 2001-01-18 Eads Airbus Gmbh Method and device for producing a three-dimensional large component
US20080105785A1 (en) * 2006-11-02 2008-05-08 Griess Kenneth H Optimized fuselage structure

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19615716A1 (en) * 1996-04-22 1997-10-23 Bodenseewerk Geraetetech Pipe connection, in particular for connecting two tubular fuselage parts of a missile
DE19929471C1 (en) * 1999-06-26 2001-01-18 Eads Airbus Gmbh Method and device for producing a three-dimensional large component
US20080105785A1 (en) * 2006-11-02 2008-05-08 Griess Kenneth H Optimized fuselage structure

Also Published As

Publication number Publication date
DE102006060360A1 (en) 2008-06-26
DE102006060360B4 (en) 2010-02-04

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Legal Events

Date Code Title Description
OP8 Request for examination as to paragraph 44 patent law
8364 No opposition during term of opposition
8396 Reprint of erroneous front page
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE

R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee