Panel for a vehicle

Aeronautics and astronautics – Aircraft structure – Details

Reexamination Certificate

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Details

C244S131000, C296S211000, C296S214000, C403S341000, C403S335000, C403S375000

Reexamination Certificate

active

07059568

ABSTRACT:
The invention relates to a device for fastening an in-fill panel element to a plane panel element of a covering for an aircraft, the in-fill panel element and the panel element being releasably interconnected at longitudinal sides facing each other, a transverse pin being arranged at least in the end portion of a longitudinal side so that a hook element arranged in the corresponding end portion of the other longitudinal side is able to clampingly engage with a hook opening, in such a manner that a covering surface of the in-fill panel element is arranged so as to be even with a covering surface of the panel element.

REFERENCES:
patent: 4425001 (1984-01-01), Mauri
patent: 4457249 (1984-07-01), Disen
patent: 6550852 (2003-04-01), Patz et al.
patent: 2002/0089185 (2002-07-01), Hessling et al.
patent: 4445249 (1996-03-01), None
patent: 197 30 269 (1999-01-01), None
patent: 199 00 267 (2000-07-01), None
patent: 1 215 082 (2001-12-01), None
patent: WO 00/40436 (2000-07-01), None

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