CPC F02C 6/08 (2013.01) [F02C 7/04 (2013.01); F01D 15/10 (2013.01); F02C 1/04 (2013.01); F02C 3/04 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2240/35 (2013.01)] | 11 Claims |
1. A gas turbine system used for a moving body comprising a thrust generator configured to generate thrust from electric power, the gas turbine system comprising:
a compressor that compresses external air to generate compressed air;
a combustor that burns the compressed air generated by the compressor together with fuel to generate a combustion gas;
a turbine driven by the combustion gas generated by the combustor;
a generator that is coupled to the turbine to generate the electric power by driving of the turbine and supplies the electric power to the thrust generator;
a turbocharger that guides external air to the compressor;
an exhaust unit that guides a combustion gas that passed through the turbine to outside,
a bypass unit that guides a part of the combustion gas guided to the exhaust unit to the turbocharger,
wherein the turbocharger is directly rotated by the part of the combustion gas guided by the bypass unit, the part of the combustion gas being supplied to the turbocharger through a bypass channel into which the part of the combustion gas flows.
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