The present invention forms a circular hole for accommodating an exhaust turbine, a power transmission differential chamber, and a power integrated device in the center of a small circular fuselage of an electric motor type, and an axial cylinder is a satellite type around the centrifugal hole. The hybrid engine (HYBRIDENGINE) combines the volumetric pressure "energy cycle" of the two-cycle "piston engine" and the "speed energy cycle" of the conventional "radial exhaust turbine". The overall thermal efficiency is greatly improved from 30-40% to 50-60%, and the exhaust air is also reduced, relatively low quality oil can be used, and the fuel cost is also greatly reduced. have. And the present invention has a variety of uses, such as automobile helicopters, ships, farm equipment.
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