OVERHEATING PREVENTING GAS TURBINE SYSTEM

摘要

A gas turbine system preventing overheating is provided to discharge air by extending an air passage to an air discharge port. A gas turbine system includes a rotational shaft(10), a body(20), a fixing chamber(30), a combustion chamber(40), a fuel supplying unit(50), a compressor(60), an air passage(65), a plurality of separators, an ignition part(70), a combustion gas passage(80), a turbine(90), and a cold air passage(100). The mixing chamber is provided at one side of the body. Fuel is introduced into the mixing chamber. An air compressed by the compressor is introduced into the mixing chamber through the air passage. The combustion chamber rotates with the rotational shaft.