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.
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
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