Rotor inlet temperature control for turbo machine

Details Rotor inlet temperature control for turbo machine Rotor inlet temperature control for turbo machine

G - Physics

06

F

G06F 17/00 (2006.01) F01D 25/00 (2006.01) F02C 7/00 (2006.01) F02C 7/057 (2006.01) F02C 9/00 (2006.01) F02C 9/26 (2006.01) F02C 9/28 (2006.01) F02C 9/48 (2006.01) F02D 28/00 (2006.01) F02K 1/16 (2006.01)

Patent

CA 2468559

A method of synthesizing rotor inlet temperature in a turbine comprising the steps of determining a burner fuel flow (WFGG), a burner inlet pressure (PS32), and a compressor discharge temperature (T3) of a turbine, calculating a ratio unit parameter from the burner fuel flow, the burner inlet pressure, and the compressor discharge temperature, and calculating a synthesized rotor inlet temperature from the ratio unit parameter.

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