Gap covering device

Details Gap covering device Gap covering device

B - Operations, Transporting

64

C

B64C 1/00 (2006.01) B64C 1/06 (2006.01) B64C 1/12 (2006.01)

Patent

CA 2684629

A gap covering device (10) for covering a gap (16) between two mutually adjacent first aircraft interior components (12, 14) comprises a visible portion (18) as well as a retaining portion (20) connected to the visible portion (18) and extending opposite the visible portion (18). A receiving structure is fastened to an inner surface of the visible portion (18) and/or of the retaining portion (20) and has a receiving contour adapted to an edge contour of the first aircraft interior components (12, 14).

Cette invention concerne un dispositif (10) de recouvrement d'interstice conçu pour recouvrir un interstice (16) entre deux premiers éléments intérieurs d'aéronef adjacents (12, 14), lequel dispositif comprend une partie visible (18) et une partie de retenue (20) connectée à la partie visible (18) et s'étendant à l'opposé de la partie visible (18). Une structure réceptrice est reliée à une surface interne de la partie visible (18) et/ou de la partie de retenue (20) et elle présente un contour de réception conçu pour recevoir un contour périphérique des composants intérieurs (12,14) d'aéronef.

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