发明名称 Auxiliary power take off valve for turbo jet engine - has an under cut throttle valve to allow an air flow in the closed position
摘要 <p>The variable power take off valve is an independent unit fitted by a flange to the compressor and contains a throttle flap turned by a shaft. The throttle flap is undercut so that a gap is formed in the completely closed position. A venturi is provided above the throttle plate and forms the large opening area by completely open throttle valve position. The throttle valve actuator works with a combination of air propulsion pressure and atmospheric pressure. Compressor air enters the chamber via the aperture below the throttle valve and the calibrated jet to press against a plate which is subjected to atmospheric pressure. Air for the auxiliaries can only be tapped off according to its availability.</p>
申请公布号 IT1022325(B) 申请公布日期 1978.03.20
申请号 IT19740027722 申请日期 1974.09.26
申请人 UNITED AIRCRAFT CORPORATION 发明人
分类号 F02K;(IPC1-7):02K/ 主分类号 F02K
代理机构 代理人
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