| 摘要 |
A gas turbine engine for highly efficient fuel consumption includes as elements a rotor, a stator and a spindle. The rotor includes a system of passageways, a combustion chamber, and a plurality of exhaust ports. The system of passageways comprises a plurality of axial passageways and radial passageways configured to receive a precombustion air-fuel mixture and transport the precombustion air-fuel mixture to the combustion chamber. The exhaust ports provide fluid communication of postcombustion gas between the combustion chamber and the exterior of the rotor.
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