The invention discloses a fairing, an aircraft and an aircraft heat-dissipation method. The fairing comprises an air inlet and a flow guide structure, wherein the flow guide structure is used for guiding air entering from the air inlet; during assembly, the fairing is fixedly installed in front of blades of the aircraft and rotates along with the blades when the blades rotate, so that air enters from the air inlet and is exhausted by the flow guide structure in an accelerated mode, and therefore the mobility of air in the fairing is improved, and heat dissipation is conducted on a motor behindthe blades. The fairing comprises the air inlet and the flow guide structure; during assembly, the fairing is mounted in front of blades of the aircraft and rotates along with the blades; the air inlet can enable air to enter the fairing, and the flow guide structure can enable the entering air to be exhausted in an accelerated mode, so that the fluidity of the air in the fairing is improved, theeffect of dissipating heat of the motor behind the blades is achieved, the heat dissipation problem of the motor is solved, the service life of the motor is prolonged, and the flight safety performance of the aircraft is also enhanced.

    本发明公开了一种整流罩、一种飞行器和一种飞行器散热方法。该整流罩包括进风口和导流结构,导流结构用于疏导从进风口进入的空气;装配时,整流罩固定安装在飞行器的桨叶前方,并在桨叶转动时随桨叶一起转动,使空气从进风口进入,并被导流结构加速排出,以增加整流罩内的气体流动性从而为桨叶后方的电机散热。由于本申请整流罩包括进风口和导流结构,装配时安装在飞行器的桨叶前方并随桨叶一起转动,进风口可以使空气进入整流罩,而导流结构可以使进入的空气加速排出,从而增加整流罩内的气体流动性,达到为桨叶后方的电机散热的效果,因此解决了电机的散热问题,提高了电机的使用寿命,也增强了飞行器飞行的安全性能。


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    Titel :

    Fairing, aircraft and aircraft heat-dissipation method


    Weitere Titelangaben:

    一种整流罩、一种飞行器和一种飞行器散热方法


    Beteiligte:
    ZHENG LIKUN (Autor:in)

    Erscheinungsdatum :

    2020-05-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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