| 摘要 |
PROBLEM TO BE SOLVED: To provide a synthesizing system for the rotor inlet temperature of a turbine and its method of synthesizing capable of evaluating the rotor inlet temperature in a gas passage of the turbine engine during operation accurately on the real time basis. SOLUTION: The method of synthesizing the rotor inlet temperature of the turbine consists of such processes as sensing the burner fuel flow rate WFGG, the burner inlet pressure PS32, and the compressor discharge temperature T3 of the turbine, calculating the by-proportion unit parameter from the burner fuel flow rate, the burner inlet pressure, and the compressor discharge temperature, and calculating the synthetic rotor inlet temperature from the by-proportion unit parameter. COPYRIGHT: (C)2005,JPO&NCIPI
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