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 |
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分类号 |
F02K;(IPC1-7):02K/ |
主分类号 |
F02K |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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