Patent ID: 9387932
Filing Date: 2016-07-12
CPC Classification: B32B,B64D,Y10T

Claim Text:
1. A panel insert system for use on-board an aircraft, comprising: (a) an aircraft galley receiving surface comprising at least four edges, with a continuous channel positioned along at least three of the edges of the receiving surface, leaving at least one receiving surface edge without a channel for insertion and removal of a single panel insert, (b) a plurality of panel inserts comprising panels displaying a portion of a visual scene, each panel in the plurality of panel inserts comprising edges that slide into and fit with respect to the continuous channel, and (c) at least one trim edge having a length similar to at least one portion of the continuous channel, such that once the single panel insert has been selected and inserted into the continuous channel, the trim edge is located along an edge of the single selected panel insert and secures the panel insert in place, completing the continuous channel and preventing edges of the panel insert from being exposed, wherein the portions of a visual scene of each panel insert in the plurality of panel inserts collectively form a visual effect across a plurality of aircraft galley components.