The invention relates to a helicopter and a tail assembly thereof. The tail assembly comprises a tail pipe, a tail motor installed on the tail pipe, a rotating blade installed on the tail motor and acontroller used for controlling the tail motor, wherein a first heat dissipation hole is formed in the tail pipe side of the tail motor, and an air outlet is formed in the blade side; the tail pipe isa hollow pipe, a controller is arranged in the tail pipe, and a second heat dissipation hole corresponding to the first heat dissipation hole in position is formed in the side wall of the tail pipe so that gas in the tail pipe and the tail motor can be exhausted through the air outlet. Thus, the heat generated by the controller can be discharged into the air through the tail pipe and the tail motor, and the heat generated when the tail motor works can be discharged in time, namely, the heat cannot be concentrated in the tail motor and is dissipated into the air. And through the arrangement ofthe second heat dissipation hole, the first heat dissipation hole and the air outlet, heat generated when the controller and the tail motor work can be effectively reduced, so that the service life of the controller and the tail motor is prolonged, and potential safety hazards are avoided.

    本公开涉及一种直升机及其机尾总成,其中,机尾总成包括尾管、安装在尾管上的尾电机、安装在尾电机上的旋转叶片以及用于控制尾电机的控制器,尾电机的尾管侧开设有第一散热孔,叶片侧开设有出风口;尾管为中空管,控制器设置在尾管中,尾管的侧壁开设有与第一散热孔位置对应的第二散热孔,以使尾管以及尾电机内的气体经由出风口排出。这样,控制器产生的热量可以经由尾管和尾电机排出到空气中,尾电机工作时产生的热量能够及时排出,即,使得热量不会集中在尾电机的内部,而是散发到空气中。通过第二散热孔、第一散热孔以及出风口的设置,可以有效减小控制器、尾电机工作时的热量,从而提高控制器和尾电机的使用寿命,避免产生安全隐患。


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    Titel :

    Helicopter and tail assembly thereof


    Weitere Titelangaben:

    直升机及其机尾总成


    Beteiligte:
    ZHANG SHUO (Autor:in) / GU WEICHUN (Autor:in) / SONG DALEI (Autor:in) / SU WENBO (Autor:in)

    Erscheinungsdatum :

    08.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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