| 摘要 |
The present invention relates to a turbine engine, wherein compressor rotor blades and turbine rotor blades set around the interior circular surface of a hollow revolving shaft while compressor stator blades and turbine stator blades are set around the exterior circular surface of an inner engine case inside the hollow revolving shaft. By using the present invention, the configuration of the turbine engine can be compact, and the volume can be substantially reduced. Besides, the stiffness of the rotor blades can be increased, and efficiency of the compressor, the burner, the turbine, and the whole engine can be increased.
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