GAS-TURBINE SYSTEM, METHOD OF POWER OF GAS-TURBINE SYSTEM OUTPUT CHANGING, METHOD OF GAS-TURBINE SYSTEM CONTROL RANGE EXPANDING, GAS TURBINE EFFICIENCY INCREASING METHOD AND SYSTEM Russian patent published in 2017 - IPC F02C9/22 

Abstract RU 2608533 C2

FIELD: turbines.

SUBSTANCE: gas turbine system comprises compressor protection subsystem, sleep mode subsystem and control subsystem, which controls compressor subsystem and sleep mode subsystem. At partial loads on turbine system compressor protection subsystem maintains air flow through compressor with air flow rate factor for partial load above minimum flow rate factor, when aeromechanic stresses occur in compressor. Maintaining fuel-air mix components ratio, at which turbine exhaust gas emissions components are kept below predetermined component emissions level during operation at partial loads.

EFFECT: technical result is increasing efficiency in control over gas turbine at low load levels.

37 cl, 12 dwg

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Authors

Freeman Thomas John

Obenhoff Ryan Eric

Klosinski Joseph

Cocca Michael Anthony

Scipio Alston I

Yarnold Mike

Ekanayake Sanji

Warwick Douglas Corbin

Dates

2017-01-19Published

2012-11-22Filed