发明名称 Shower system for aircraft
摘要 A shower unit for an aircraft comprises: a shower head, and controls to manually control the water output. A shower enclosure defines a receiving cavity to receive the user. The shower enclosure supports the shower head and the controls for the user to shower in the receiving cavity. The shower enclosure comprises 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. The shower unit is adapted to be positioned in the aircraft such that the passageway communicates between two separate zones of the aircraft.
申请公布号 US8931737(B2) 申请公布日期 2015.01.13
申请号 US200813122502 申请日期 2008.10.02
申请人 Bombardier Inc. 发明人 Savignac Stephane;Boies Jean-Francois;Malek Bruce
分类号 B64D11/00;B64D11/02;A47K3/28 主分类号 B64D11/00
代理机构 Thomas, Karceski & Karmilovich, PC 代理人 Thomas, Karceski & Karmilovich, PC
主权项 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.
地址 Dorval, Quebec CA