Fuselage structure including an integrated fuselage stanchion

Details Fuselage structure including an integrated fuselage stanchion Fuselage structure including an integrated fuselage stanchion

2011-01-04

2011-01-04

Michener, Joshua J (Department: 3644)

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

C244S119000

Reexamination Certificate

active

07861970

ABSTRACT:
A fuselage structure for an aircraft or similar vehicle may include an upper fuselage portion and a lower fuselage portion. A floor may be disposed between the upper fuselage portion and the lower fuselage portion. At least one unitized stanchion may be disposed between the floor and the lower fuselage portion. The at least one unitized stanchion may form the only structural support between the floor and the lower fuselage portion without any vertical beams.

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UK Intellectual Property Office, Combined Search and Examination Report under Sections 17 and 18(3), for United Kingdom Patent Application No. GB0721312.7, dated Feb. 13, 2008.

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