Abstract
The article discusses the synchronization of the operation of a piston and electric engine in an aviation hybrid power plant in a parallel circuit. Diagrams of a parallel and series hybrid power plant based on a piston engine and an electric motor are presented. The features of the parallel circuit hybrid power plant are noted. The power and torque graphs of a piston engine, an electric motor and a hybrid propulsion system with a propeller are analyzed. Conclusions are drawn about the possibility of synchronizing different types of engines as part of a hybrid power plant, taking into account power losses
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