Gas turbine system and method of controlling the same

Details Gas turbine system and method of controlling the same Gas turbine system and method of controlling the same

1988-11-30

1990-10-02

Stout, Donald E.

Power plants

Combustion products used as motive fluid

60 3907, 60 3929, F02C 7057

Patent

active

049599542

ABSTRACT:
A gas turbine system having an extraction channel supplying part of the discharged air of a compressor to another installation, and a method of controlling the gas turbine system wherein an inlet guide vane or any other regulator for regulating the flow rate of inlet air is disposed at the inlet of the compressor of a gas turbine engine, and the flow rate of the inlet air of the compressor is controlled in correspondence with the fluctuation of the flow rate of extraction air to provide a gas turbine system and a controlling method therefore which do not adversely affect the efficiency of the gas turbine engine regardless of the fluctuations of the flow rate of the extraction air.

REFERENCES:
patent: 2618431 (1952-11-01), Walker
patent: 2934094 (1960-04-01), Szydlowski
patent: 3080712 (1963-03-01), Wood
patent: 3659417 (1972-05-01), Grieb
patent: 3747355 (1973-07-01), Strub
patent: 3795104 (1974-03-01), McLean
patent: 4149371 (1979-04-01), Spraker et al.
patent: 4182117 (1980-01-01), Exley et al.
patent: 4709546 (1987-12-01), Weiler
patent: 4809497 (1989-03-01), Schuh

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