Cargo floor, system, and method

Aeronautics and astronautics – Aircraft structure – Load accommodation

Reexamination Certificate

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Reexamination Certificate

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07954760

ABSTRACT:
Embodiments provide a cargo floor, a system, and a method adapted to be made integral with or complementary of the aircraft fuselage. Cargo floor members may be adapted to be coupled with a flat fuselage bottom inner skin of an aircraft fuselage to serve as the main orthotropic stiffeners to the flat fuselage bottom inner skin such that a portion of the in service loading experienced by the aircraft are shared by a combination of the fuselage and the cargo floor.

REFERENCES:
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patent: 3612316 (1971-10-01), Baldwin et al.
patent: 4674712 (1987-06-01), Whitener et al.
patent: 5014935 (1991-05-01), Dalbera
patent: 6219983 (2001-04-01), Gråkjaar Jensen et al.
patent: 6427945 (2002-08-01), Bansemir
patent: 6517028 (2003-02-01), Huber
patent: 6834833 (2004-12-01), Sankrithi
patent: 7261257 (2007-08-01), Helou, Jr.
patent: 2001/0010345 (2001-08-01), Clifford
patent: 2002/0005150 (2002-01-01), Taylor et al.

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