发明名称 Method for performing gas turbine performance diagnostics
摘要 <p>A method of performing diagnostics on a system comprises receiving a plurality of measurement parameters, each corresponding to one of a plurality of parameters at a time k, forming a deviation vector from the plurality of measurement parameters, calculating an initial deviation vector from an initial fault vector, calculating a multiple fault isolation deviation vector using the initial deviation vector and the deviation vector, determining if an event is in progress using the multiple fault isolation deviation vector, performing statistical data validity to set a present inhibit flag and a past inhibit flag, and performing module performance analysis according to the present inhibit flag and the past inhibit flag.</p>
申请公布号 EP1418481(B1) 申请公布日期 2005.12.28
申请号 EP20030256918 申请日期 2003.10.31
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 VOLPONI, ALLAN J.;DEPOLD, HANS R.
分类号 F01D25/00;F02C9/00;F02C9/28;F02C9/44;G05B23/02;(IPC1-7):G05B23/02 主分类号 F01D25/00
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