发明名称 |
Method of operating a gas turbine engine |
摘要 |
The present invention provides a method of maintaining fan airflow at 100% for throttle transients from 100% military power to 30% thereof by increasing exhaust nozzle area as the fuel flow the engine decreases until the exhaust nozzle reaches its fully open position. Subsequent reductions in fuel flow produce a commensurate reduction fan airflow.
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申请公布号 |
US6000215(A) |
申请公布日期 |
1999.12.14 |
申请号 |
US19970996792 |
申请日期 |
1997.12.23 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
ROBERTS, JR., WILLIAM C. |
分类号 |
F02C9/28;F02C9/50;F02K1/17;(IPC1-7):F02K1/17;F02K3/02 |
主分类号 |
F02C9/28 |
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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