Fuselage structure

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Reexamination Certificate

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Details

C244S131000

Reexamination Certificate

active

07850117

ABSTRACT:
A fuselage structure comprises a plurality of elements that in longitudinal direction are interconnected by weld joints; a plurality of circumferential ribs that are connected to the plurality of elements and that extend so as to be substantially perpendicular in relation to the longitudinal direction of the elements; and a plurality of clips that are arranged between the elements and the ribs such that said clips do not cover the respective weld joints.

REFERENCES:
patent: 5518208 (1996-05-01), Roseburg
patent: 5649888 (1997-07-01), Micale et al.
patent: 6328261 (2001-12-01), Wollaston et al.
patent: 6684593 (2004-02-01), Brenneis et al.
patent: 2006/0065643 (2006-03-01), Hackius et al.
patent: 2317366 (2001-03-01), None
patent: 100 07 995 (2002-03-01), None
patent: 199 41 924 (2004-07-01), None
patent: 103 32 003 (2004-12-01), None
patent: 10 2004 035 170 (2005-08-01), None

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