Patent ID: 9387912
Filing Date: 2016-07-12
CPC Classification: B61D,B63B,B64D,Y10T

Claim Text:
1. A panel insert system comprising: an aircraft galley component door, the aircraft galley component door comprising: a receiving surface and a raised edge bordering the receiving surface, and a plurality of panel inserts, each of the panel inserts displaying a portion of a visual scene, each of the panel inserts configured to be removeably secured to the receiving surface the aircraft galley component door such that a single panel insert is removeably secured to the aircraft galley component door via a plurality of discrete magnets or magnetically responsive surfaces, each of panel inserts having a thickness rendering the panel insert generally flush with the raised edge of the receiving surface when secured, wherein the portions of a visual scene of each of the plurality of panel inserts collectively form a visual effect across a plurality of aircraft galley components.