Patent ID: 8931737
Filing Date: 2015-01-13
Classification: B64D

Abstract:
1. A shower unit for an aircraft, comprising: at least one shower head adapted to output water from a water source; at least one control to manually control the water output by the at least one shower head; and a shower enclosure defining a receiving cavity adapted to receive the user, the shower enclosure supporting the at least one shower head and the at least one control for the user to shower in the receiving cavity, the shower enclosure comprising a first door on a first side of the shower enclosure, and a second door on a second side of the shower enclosure to define a passageway through the shower enclosure; wherein the shower unit is adapted to be positioned in the aircraft such that the passageway communicates between two separate zones of the aircraft; and wherein the first door is a sliding door sliding into the receiving cavity toward an opened position, and the second door is a hinged door pivoting into the receiving cavity toward an opened position, to define the passageway.