F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 9/48 (2006.01) F01D 17/16 (2006.01) F02C 7/228 (2006.01) F02C 9/18 (2006.01) F02C 9/22 (2006.01) F02C 9/26 (2006.01) F02C 9/28 (2006.01) F02C 9/50 (2006.01) F02C 9/52 (2006.01) F23R 3/26 (2006.01) F23N 5/16 (2006.01)
Patent
CA 2398522
In a gas turbine control apparatus, a frequency analyzing section frequency-analyzes at least one of pressure oscillation in combustors of a gas turbine and acceleration oscillation of each of the combustors and outputs a first frequency analysis result as the result of frequency analysis for a plurality of predetermined frequency bands. A control unit controls at least one of a first fuel flow rate of fuel and a first air flow rate of air based on the first frequency analysis result for the plurality of frequency bands. The fuel and the air are supplied to the gas turbine.
Nomura Masumi
Toyama Kozo
G. Ronald Bell & Associates
Mitsubishi Heavy Industries Ltd.
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