Invention Grant
- Patent Title: Structural element of an aircraft fuselage
- Patent Title (中): 飞机机身的结构元件
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Application No.: US12595230Application Date: 2008-04-25
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Publication No.: US08905349B2Publication Date: 2014-12-09
- Inventor: Claus-Peter Gross , Cord Haack , Dirk Humfeldt , Oliver Thomaschewski
- Applicant: Claus-Peter Gross , Cord Haack , Dirk Humfeldt , Oliver Thomaschewski
- Applicant Address: DE Hamburg
- Assignee: AIRBUS Operations GmbH
- Current Assignee: AIRBUS Operations GmbH
- Current Assignee Address: DE Hamburg
- Agency: Fenwick & West LLP
- Priority: DE102007019821 20070426
- International Application: PCT/EP2008/055084 WO 20080425
- International Announcement: WO2008/132171 WO 20081106
- Main IPC: B64C1/06
- IPC: B64C1/06 ; B64C1/40
Abstract:
The structural element of an aircraft fuselage, with stringers running in the longitudinal direction of the aircraft fuselage and ribs running transversely to the stringers in the circumferential direction of the fuselage. According to the invention, at least one of the stringers running in the longitudinal direction of the aircraft fuselage is designed as a fastening rail for elements to be installed in the aircraft fuselage.
Public/Granted literature
- US20100243805A1 Structural Element of an Aircraft Fuselage Public/Granted day:2010-09-30
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