Rotor inlet temperature control for turbo machine

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

2005-08-23

2005-08-23

Gartenberg, Ehud (Department: 3746)

Power plants

Combustion products used as motive fluid

Process

C060S039281

Reexamination Certificate

active

06931857

ABSTRACT:
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.

REFERENCES:
patent: 6393355 (2002-05-01), Muramatsu
patent: 6708496 (2004-03-01), Gadde et al.
patent: 2004/0011053 (2004-01-01), Murakami et al.
patent: 2004/0055273 (2004-03-01), Hirayama et al.

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