Patent ID: 9340290
Filing Date: 2016-05-17
CPC Classification: B64D

Claim Text:
1. An integrated aircraft galley structure comprising: a bottom portion including a storage area for serving carts; an upper portion including a second storage area; and a service module between the upper portion and the bottom portion, the service module comprising: a plurality of galley inserts; a plurality of bays formed in the service module and sized to receive the plurality of galley inserts; a plurality of galley insert modules for controlling each galley insert, the galley insert modules being received in the service module in designated slots; an insert power and control unit for each galley insert for controlling power to said insert; and a galley power and control unit for controlling each of the insert galley power and control units; and a cooling panel behind the service module including a shield for limiting heat dissemination beyond the cooling panel.