Patent ID: 9193464
Filing Date: 2015-11-24
Classification: B64C,B64D,Y02T

Abstract:
1. An aircraft comprising: an aircraft fuselage containing an aircraft cabin, the aircraft fuselage having a longitudinal length between a front of the aircraft fuselage and a rear of the aircraft fuselage, the aircraft cabin having a longitudinal length between a front of the aircraft cabin and a rear of the aircraft cabin, and the aircraft cabin having a lateral width between laterally opposite first and second outboard sidewalls of the aircraft cabin; a floor surface in the aircraft cabin; a galley in the rear of the aircraft cabin; an aft pressure bulkhead at the rear of the aircraft cabin, the aft pressure bulkhead including a forward wall surface facing toward the aircraft cabin and extending laterally across the rear of the aircraft cabin between the first and second outboard sidewalls of the aircraft cabin, and the forward wall surface having a recessed cavity in the forward wall surface and above the floor surface, the cavity extending rearwardly of the forward wall surface; and, at least a portion of the galley extending into the recessed cavity in the forward wall surface.