The invention relates to a ducted fan structure, an aircraft power system and an aircraft. The ducted fan structure comprises an outer frame, a paddle assembly, a motor and a fixing rod, and the motor is fixedly installed in the outer frame; the paddle assembly is fixedly mounted at the driving end of the motor; the fixing rod is located outside the outer frame, and one end is fixedly connected with the tail end of the motor. The motor has the beneficial effects of simple structure, reasonable design, small size, high rotating speed, high power and long service life.

    本发明涉及一种涵道风扇结构、飞行器动力系统及飞行器,该涵道风扇结构包括外框、桨叶组件、电机及固定杆,电机固定安装在外框内;桨叶组件固定安装在电机的驱动端上;固定杆位于外框外,其一端与电机的末端固定连接。本发明的有益效果是结构简单,设计合理,体积小,电机转速高,功率大,使用寿命长。


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    Title :

    Ducted fan structure, aircraft power system and aircraft


    Additional title:

    一种涵道风扇结构、飞行器动力系统及飞行器


    Contributors:
    CAI XIAODONG (author) / ZHOU GUANGYONG (author) / CHEN SHIXIONG (author) / CAI HAOYU (author)

    Publication date :

    2024-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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