| 发明名称 |
PROTECTING OPERATING MARGIN OF A GAS TURBINE ENGINE |
| 摘要 |
<p>A method of protecting operating margin of the gas turbine engine includes calculating an aerodynamic distortion of air entering an inlet of a gas turbine engine that has a compressor section with variable vanes that are movable subject to a control parameter. The control parameter is selectively modified in response to the aerodynamic distortion.</p> |
| 申请公布号 |
WO2014031199(A3) |
申请公布日期 |
2014.05.15 |
| 申请号 |
WO2013US42559 |
申请日期 |
2013.05.24 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
PARENTE, WAYNE P. |
| 分类号 |
F02C9/20;F01D17/16;F02K3/00 |
主分类号 |
F02C9/20 |
| 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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