发明名称 |
Method of monitoring gas turbine engine operation |
摘要 |
A system, method and apparatus for monitoring the performance of a gas turbine engine. A counter value Indicative of the comparison between the engine condition and the threshold condition is adjusted. The aircraft operator is warned of an impending maintenance condition based on the counter value and determines an appropriate course of action.
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申请公布号 |
US7487029(B2) |
申请公布日期 |
2009.02.03 |
申请号 |
US20040850436 |
申请日期 |
2004.05.21 |
申请人 |
PRATT & WHITNEY CANADA |
发明人 |
FEENEY MARK EDWARD;LESLIE KEITH JOHN;SYED YUSUF RAZL;HARTROPP SIMON JOHN |
分类号 |
G06F19/00;F01D19/00;F01D19/02;F02C9/00;F02C9/28;F02D28/00;G01M15/00;G06G7/70;G07C5/08 |
主分类号 |
G06F19/00 |
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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