发明名称 Jet propulsion outlets
摘要 An outlet assembly (1) for a ASTOVL aircraft (14) comprises a duct (2) for directing by-pass air to a position forward of the powerplant (46) in order to provide jet efflux for assistance in vertical landing and short take-off. The duct (2) has a curved downstream portion (6) and terminates in a bicuspid portion (7) on which is mounted a nozzle assembly (10). The nozzle assembly (10) can be moved between a vertical landing position in which jet efflux is directed vertically downwards, and an assisted take-off position in which jet efflux is directed at typically 20{ to the horizontal. The nozzle arrangement provides a self-supporting structure for the outlet assembly (1) when in its extended position. A surface (14) of the nozzle (10) forms a closure member for an aperture in the main body portion (8) of the aircraft when in a retracted position.
申请公布号 GB2435637(A) 申请公布日期 2007.09.05
申请号 GB19910026108 申请日期 1991.12.06
申请人 BRITISH AEROSPACE PUBLIC LIMITED COMPANY;BAE SYSTEMS PLC 发明人 JOHN STUART BLAKELEY
分类号 F02K1/00;B64C15/02;B64C29/00 主分类号 F02K1/00
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