Gas turbine, method of controlling air supply and computer program product for controlling air supply
View Patent ↗The present invention provides a gas turbine capable of reducing energy consumption while suppressing a so-called cat back phenomenon. The gas turbine includes a combustor-accommodating chamber casing for accommodating therein a combustor which burns fuel and air compressed by a compressor to generate combustion gas and which injects the combustion gas to a turbine. The gas turbine also includes a first air supply passage and a second air supply passage on an upper portion of the combustor-accommodating chamber casing in the vertical direction. The first air supply passage discharges air toward the compressor in the combustor-accommodating chamber casing. The second air supply passage discharges air in a direction different from that of the first air supply passage.
1. A method of controlling air supply for supplying air into a combustor-accommodating chamber which accommodates a combustor therein after operation of a gas turbine is stopped, the method comprising:
obtaining temperature of an upper portion of the combustor-accommodating chamber in a vertical direction and temperature of a lower portion of the combustor-accommodating chamber in the vertical direction;
obtaining a difference between the temperature of the upper portion of the combustor-accommodating chamber in the vertical direction and the temperature of the lower portion of the combustor-accommodating chamber in the vertical direction;
adjusting an amount of air to be discharged into the combustor-accommodating chamber such that the difference between the temperature of the upper portion of the combustor-accommodating chamber in the vertical direction and the temperature of the lower portion of the combustor-accommodating chamber in the vertical direction falls within a predetermined range; and
discharging air into the combustor-accommodating chamber with the adjusted flow rate.
2. The method of controlling air supply according to claim 1 , wherein air is discharged to the combustor-accommodating chamber after the engine revolution number of the gas turbine becomes smaller than a predetermined revolution number.