Patent ID: 9511864
Filing Date: 2016-12-06
CPC Classification: A63H,B64D,Y10T

Claim Text:
1. In combination, an aircraft having an interior cabin including at least one structural wall or door panel, and an aircraft trim component covering the structural panel, the trim component being characterized by a selected softness and selected structural dimensions, shape, configuration and rigidity suitable for conforming to the structural panel, the trim component comprising a layer of a soft resilient foam, the foam comprising a polyvinylidene fluoride closed cell foam, a cover attached to and extending over a front side of said foam layer, and attachment means at a rear side of said foam layer for releasably attaching the trim component to the structural panel in covering relation thereto, the attachment means comprising a first fastener device including a protuberance projecting from one of the structural panel and the trim component and a female connector portion on the other of the structural panel and the trim component in mating releasable engagement with one another and a second fastener device releasably adhering the trim component to the structural panel at a location closely adjacent to the first fastener device, the attachment means providing secure attachment of the trim component to the structural panel and permitting releasable detachment of the trim component from the structural panel without damage thereto.