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
Dates
2017-01-19—Published
2012-11-22—Filed