ENGINE LAYOUTS AND ASSOCIATED COMPARTMENTALIZATION OF A SYSTEM FOR A HYBRID ELECTRIC PROPULSION SYSTEM FOR AEROSPACE APPLICATION

摘要

A power plant a for an aircraft having a hybrid-electric propulsion system including a nacelle body including therein an electric motor directly connected to a gearbox for driving a propeller, wherein the gearbox is connected directly to a heat motor for driving the propeller, and at least one heat exchanger for cooling the electric motor or the heat motor.