发明名称 Strahlablenkvorrichtung
摘要 1,182,568. Deflecting propulsive jets. SOC NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. 3 May, 1968 [18 May, 1967], No. 21048/68. Heading B7G. A jet issuing from the outlet 1 of a jet propulsion engine (e.g. a rocket engine) is deflected by a transversely injected auxiliary jet (e.g. as at 2) supplied by a compressed gas generator 3 separate from the engine, there being an outlet branch 7 leading to a variable area nozzle 8, the variation in which is controlled by a regulator (e.g. a movable plug 9) which regulates the gas pressure in the generator. The flow of compressed gas for the auxiliary jet may be controlled by a valve 5 operated by a jack 6. The nozzle plug 9 may be moved in response to the combustion chamber pressure, detected at 16 by a servovalve 14 supplying oil under pressure to a piston 11 in a cylinder 10. The servovalve 14 and piston 11 and cylinder 10 may be replaced by electrical control and a solenoid.
申请公布号 DE1756360(A1) 申请公布日期 1970.03.12
申请号 DE19681756360 申请日期 1968.05.13
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION 发明人 JEAN COLOMBANI,DON PIERRE LOUIS;GONTIER ERNST,ADOLPHE OTTON
分类号 F02K1/00;F02K1/28;F02K9/82 主分类号 F02K1/00
代理机构 代理人
主权项
地址