| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas turbine for reducing the loss of an air flow in an accessory portion of an air system, simplifying the system and saving space for equipment. SOLUTION: This gas turbine comprises a combustion air system for supplying compressed air from a compressor 1 to a combustor 2 and a cooling air system for supplying the compressed air to a high temperature portion of the gas turbine, the compressed air generated by the compressor being used as combustion air and cooling air. The compressed air a1 from the compressor is controlled to be at preset temperature and pressure via a heat exchanger 4 and a boosting compressor 7 and the controlled compressed air is parted and supplied into an atomized air system and a cooling air system.
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