发明名称 AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM AIR DUCT ARRANGEMENT
摘要 An air duct arrangement (58) for an aircraft (40). The arrangement (58) comprises an environmental control system (ECS) (50). The ECS (50) comprises an air inlet (60) arranged to ingest a low velocity portion of a boundary layer flow adjacent the aircraft fuselage (44), and to deliver a flow of air to an environmental control system air intake (66). The arrangement (58) further comprises an ejector (70) arranged to receive an ECS exhaust (76), and boundary layer air from an aft region of the aircraft (40), and to exhaust air to the ambient airstream at an aft portion of the aircraft (40).
申请公布号 US2016075435(A1) 申请公布日期 2016.03.17
申请号 US201514830143 申请日期 2015.08.19
申请人 ROLLS-ROYCE PLC 发明人 STIEGER Rory D.;RAFFAELLI Lorenzo
分类号 B64D13/08 主分类号 B64D13/08
代理机构 代理人
主权项 1. An air duct arrangement for an aircraft, the arrangement comprising; an environmental control system air inlet arranged to ingest a low velocity portion of a boundary layer flow adjacent an aircraft external surface, and to deliver a flow of air to an environmental control system air intake; and an ejector arranged to receive an environmental control system exhaust and boundary layer air from an aft region of the aircraft, and to exhaust air from an ejector exhaust to the ambient airstream at an aft portion of the aircraft.
地址 London GB