发明名称 Hybrid gas turbine engine state variable model
摘要 The present invention relates to a system and a method for developing an engine model. The system broadly comprises a module for generating a state variable model of an engine, which module receives a plurality of inputs to an engine representative of a particular flight condition and generates a set of estimated engine parameters representative of the model. The system further comprises a comparator for comparing the set of estimated engine parameters to a set of measured engine parameters for generating a set of residuals and an artificial neural network module to be trained and to be used in an implementation configuration after training has been completed. The artificial neural network receives the set of residuals and the engine inputs during a training phase and generates a set of estimated residuals representative of the engine condition.
申请公布号 US2003200069(A1) 申请公布日期 2003.10.23
申请号 US20020132108 申请日期 2002.04.23
申请人 VOLPONI ALLAN J. 发明人 VOLPONI ALLAN J.
分类号 F01D25/00;F02C9/28;G05B13/02;G05B17/02;G06F17/50;G06N3/00;(IPC1-7):G06G7/48 主分类号 F01D25/00
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