发明名称 INTEGRATED AIRCRAFT GALLEY SYSTEM
摘要 An integrated aircraft galley structure includes a service module having a plurality of galley inserts including at least one oven and at least one refrigeration unit. The service module is formed with a plurality of bays sized to receive the plurality of galley inserts, along with a human machine interface for controlling all of the galley inserts. The service module further includes a plurality of galley insert modules for controlling each galley insert, and an insert power and control unit for each galley insert for controlling power to said insert. The entire system is controlled by a galley power and control unit for controlling each of the insert galley power and control units, and an AC distribution unit for distributing power to the insert power and control units.
申请公布号 US2015232183(A1) 申请公布日期 2015.08.20
申请号 US201514701365 申请日期 2015.04.30
申请人 B/E Aerospace, Inc. 发明人 Godecker William J.;West Grand J.;Thayer Ralph B.
分类号 B64D11/04;B64D11/00;B64D13/08 主分类号 B64D11/04
代理机构 代理人
主权项 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; anda galley power and control unit for controlling each of the insert galley power and control units; anda cooling panel behind the service module including a shield for limiting heat dissemination beyond the cooling panel.
地址 Wellington FL US