GAS TURBINE SYSTEM

摘要

A gas turbine system is provided to reduce the entire length of system by arranging the rotational blade and the stationary blade in the radial direction of the rotation axis. A gas turbine system comprises a rotation axis(10), a cylindrical body(20) integrally formed in the rotation axis, a premixing chamber(30) arranged in one side of the body, a combustion chamber(40) in which the mixed air generated in the premixing chamber is inhaled and ignited and combustion gas of high temperature is generated, a fuel supply unit(50) arranged inside the body and supplying the fuel to the premixing chamber, a compressor(60) arranged in one side of the body and compressing the air inhaled by the rotation of the rotation axis, an air channel(65) connected to the compressor so that the compacted air flows into the premixing chamber, an ignition chamber(70) igniting the mixed air in the premixing chamber, a combustion gas channel(80) which is connected to the combustion chamber and arranged in one side of the body and extended to the outside of the body, and a turbine(90) equipped inside the combustion gas channel.