CA2349122C - Composant de coque de fuselage d'aeronef resistant a la propagation des fissures - Google Patents

Composant de coque de fuselage d'aeronef resistant a la propagation des fissures Download PDF

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Publication number
CA2349122C
CA2349122C CA002349122A CA2349122A CA2349122C CA 2349122 C CA2349122 C CA 2349122C CA 002349122 A CA002349122 A CA 002349122A CA 2349122 A CA2349122 A CA 2349122A CA 2349122 C CA2349122 C CA 2349122C
Authority
CA
Canada
Prior art keywords
profile member
web
stiffening
profile
stiffening profile
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
CA002349122A
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English (en)
Other versions
CA2349122A1 (fr
Inventor
Hans-Juergen Schmidt
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
Priority claimed from DE10031510A external-priority patent/DE10031510A1/de
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of CA2349122A1 publication Critical patent/CA2349122A1/fr
Application granted granted Critical
Publication of CA2349122C publication Critical patent/CA2349122C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Pressure Welding/Diffusion-Bonding (AREA)
  • Laminated Bodies (AREA)
CA002349122A 2000-06-28 2001-05-30 Composant de coque de fuselage d'aeronef resistant a la propagation des fissures Expired - Fee Related CA2349122C (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE10031510.0 2000-06-28
DE10031510A DE10031510A1 (de) 2000-06-28 2000-06-28 Strukturbauteil für ein Flugzeug
US09/727,830 2000-11-30
US09/727,830 US6595467B2 (en) 2000-06-28 2000-11-30 Aircraft fuselage shell component with crack propagation resistance

Publications (2)

Publication Number Publication Date
CA2349122A1 CA2349122A1 (fr) 2001-12-28
CA2349122C true CA2349122C (fr) 2008-04-15

Family

ID=26006220

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002349122A Expired - Fee Related CA2349122C (fr) 2000-06-28 2001-05-30 Composant de coque de fuselage d'aeronef resistant a la propagation des fissures

Country Status (1)

Country Link
CA (1) CA2349122C (fr)

Also Published As

Publication number Publication date
CA2349122A1 (fr) 2001-12-28

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Effective date: 20150601