发明名称 Surge detector for gas turbine engines
摘要 Sensed engine inlet temperature is utilized to detect compressor surge whenever its computed temperature rate of change or rise signal exceeds a predetermined value. This signal may be coupled to another engine operating parameter, such as rotor speed, compressor discharge pressure and the like and permutations thereof, to guard against false detection. Engine inlet temperature rate of change or rise is an efficacious surge detection parameter particularly when an afterburner is used inasmuch as the hot gases of the afterburner will have a significant influence on the engine inlet temperature sensor in a reverse flow situation making that signal a positive indication of imminent surge.
申请公布号 US4137710(A) 申请公布日期 1979.02.06
申请号 US19770762763 申请日期 1977.01.26
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 PRETI, EDMOND;RIPY, HOWARD W.
分类号 F02C9/00;F04D27/02;(IPC1-7):F02C7/22 主分类号 F02C9/00
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