An aircraft galley configuration extending along a longitudinal axis of a fuselage of an aircraft and on one side of the aircraft includes a forward end of the galley closest to the front of the aircraft and a rear end of the galley on an opposite longitudinal end of the galley and closest to a passenger section of the aircraft, and a plurality of galley modules disposed in the galley between the forward and rear ends of the galley. The galley modules comprise a storage module, a heating module, a preparation module, and a service module. The storage module is disposed at the forward end of the galley and the service module is disposed at the rear end of the galley. An efficient work flow in the direction of the passenger section is created by the galley configuration.
AIRCRAFT GALLEY CONFIGURATION
CONFIGURATION D'OFFICE D'AERONEF
2015-10-29
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |