| 发明名称 |
Gas turbine engine having controllable inlet guide vanes |
| 摘要 |
An inlet guide vane assembly includes an active control feedback system and a plurality of inlet guide vanes. The inlet guide vanes are variable between a plurality of positions. Each of the plurality of inlet guide vanes is positioned in response to an output of the activate control feedback system.
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| 申请公布号 |
US8348600(B2) |
申请公布日期 |
2013.01.08 |
| 申请号 |
US20080127104 |
申请日期 |
2008.05.27 |
| 申请人 |
UNITED TECHNOLOGIES CORPORATION;NORRIS JAMES W.;BANKS ANTON G. |
发明人 |
NORRIS JAMES W.;BANKS ANTON G. |
| 分类号 |
F01D9/04 |
主分类号 |
F01D9/04 |
| 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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