发明名称 AIRCRAFT GALLEY CONFIGURATION
摘要 An aircraft galley configuration (10) extending along a longitudinal axis of a fuselage of an aircraft and on one side of the aircraft includes a forward end (12) of the galley (10) closest to the front of the aircraft and a rear end (14) of the galley (10) on an opposite longitudinal end of the galley (10) and closest to a passenger section of the aircraft, and a plurality of galley modules (20, 22, 24, 26) disposed in the galley (10) between the forward (12) and rear ends (14) of the galley. The galley modules comprise a storage module (20), a heating module (22), a preparation module (24), and a service module (26). The storage module (20) is disposed at the forward end (12) of the galley (10) and the service module (26) is disposed at the rear end (14) of the galley (10), An efficient work flow in the direction of the passenger section is created by the galley configuration (10).
申请公布号 EP3134318(A2) 申请公布日期 2017.03.01
申请号 EP20150736859 申请日期 2015.04.22
申请人 Bombardier Inc.;SHORT BROTHERS PLC 发明人 MIRON, Bruno;TREMBLAY, Michel;LADD, Gradyn;TREMBLAY, Benjamin
分类号 B64D11/04 主分类号 B64D11/04
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