发明名称 Thrust reverser for turbofan engine - has sliding sleeve which blocks fan outlet and exposes cascade of reversing blades
摘要 <p>A thrust reverser for a turbo-fan engine is provided with a sleeve (28) which normally forms part of the fan outlet duct. When reverse thrust is required the sleeve is pushed rearwards by means of a jack and shuts off the duct outlet. An annulus (37) in the sleeve (28) houses a number of rings which form a cascade of blades (34). These blades are exposed to the air flow by the rearward movement of the sleeve (28). The air from the fan is then deflected by the cascade of blades and consequently exerts a reverse thrust on the aircraft.</p>
申请公布号 FR2349738(A1) 申请公布日期 1977.11.25
申请号 FR19770012163 申请日期 1977.04.22
申请人 GENERAL ELECTRIC CY 发明人 AUGUSTUS MASON HELMINTOLLER
分类号 F02K3/04;B64D33/00;F02K1/72;(IPC1-7):02K1/20;02K3/04 主分类号 F02K3/04
代理机构 代理人
主权项
地址
您可能感兴趣的专利