The invention discloses an electric engine for a hybrid electric aircraft and the aircraft. The electric engine comprises an engine shell, and a rotating mechanism is arranged in the engine shell; the rotating mechanism comprises a radial magnetic suspension assembly and a rotor assembly; the radial magnetic suspension assembly is used for generating magnetic force to the rotor assembly, so that the rotor assembly is stabilized at a preset radial position; or, the rotor assembly is stabilized at a preset radial position, and the rotor assembly is driven to rotate; the rotor assembly comprises a rotating shaft, and pneumatic thrust bearings are installed at the two ends of the rotating shaft. The circuit structure of the shaftless turbine electric engine can be simplified, and the weight of the whole engine is reduced.
本发明公开了一种用于混纯电动飞行器的电发动机及飞行器,该电发动机包括发动机壳体,在所述发动机壳体内设有旋转机构;所述旋转机构包括径向磁悬浮组件和转子组件;所述径向磁悬浮组件用于对所述转子组件产生磁力,以使所述转子组件稳定在预定的径向位置;或者,使所述转子组件稳定在预定的径向位置,并驱动所述转子组件转动;所述转子组件包括旋转轴,所述旋转轴的两端均安装有气动止推轴承。本发明能够简化无轴涡轮电发动机电路结构,减小整个发动机的重量。
Electric engine for hybrid electric aircraft and aircraft
一种用于混纯电动飞行器的电发动机及飞行器
2023-03-31
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |