An engine for an aircraft is presented that includes a rotor, an electric motor that drives the rotor in rotation, and an ECU that controls the electric motor, where rotation of the rotor provides a primary airflow that induces thrust of the engine, and where the ECU is located within a volume defined by the primary airflow.
提出了一种用于飞行器的发动机,其包括转子、驱使转子旋转的电动机和控制电动机的ECU,其中转子的旋转提供引起发动机的推力的主气流,并且其中ECU位于由主气流限定的体积内。
Aircraft engine
飞行器发动机
30.08.2022
Patent
Elektronische Ressource
Chinesisch
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