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Summary:The invention discloses an eccentric sliding vane type gas turbine, and relates to the technical field of gas turbines. The eccentric sliding vane type gas turbine comprises a load, a gas compressionchamber, a combustion chamber, a power chamber and a main shaft. The main shaft is sequentially connected through the load, a main shaft rotor of the gas compression chamber, a main shaft rotor of thecombustion chamber and a main shaft rotor of the power chamber in a penetrating manner. The eccentric sliding vane type gas turbine is used for solving the problems that in the prior art, gas turbines and turbine engines are complex in structure, large in manufacture difficulty, high in machining cost and large in mass, need to be started through external force and are not convenient to operate or maintain. The eccentric sliding vane type gas turbine which is simple in structure, mature in manufacture technology and wide in rotating speed range, does not need to be started through external force and can be applied to
Bibliography:Application Number: CN201910336501