The invention discloses a hydrogen kinetic energy engine fuel endurance device. The device comprises a composite wing unmanned aerial vehicle. A hydrogen storage mechanism is arranged at a lower end of the composite wing unmanned aerial vehicle, a gas cylinder switching mechanism is arranged on one side of the hydrogen storage mechanism, and a gas cylinder fixing mechanism is arranged on one sideof the hydrogen storage mechanism. The device has the following beneficial effects that a plurality of hydrogen cylinders can be separated under the action of the hydrogen storage mechanism; and the unmanned aerial vehicle is prevented from being greatly threatened by leakage or burst of the hydrogen cylinder, safety of a fuel is effectively improved, the hydrogen cylinder can provide stable energy for an engine under the action of the gas cylinder switching mechanism, a phenomenon of gas supply interruption is effectively prevented, and stable flight of the unmanned aerial vehicle is guaranteed.

    本发明公开了一种氢动能发动机燃料续航装置,包括复合翼无人机,所述复合翼无人机下端设有氢气储存机构,所述氢气储存机构一侧设有气瓶切换机构,氢气储存机构一侧设有气瓶固定机构。本发明的有益效果是,通过氢气储存机构的作用可以将多个氢气瓶隔离开,防止因氢气瓶泄漏或爆裂而对无人机造成较大的威胁,有效提高燃料的安全性,通过气瓶切换机构的作用可以使氢气瓶为发动机提供稳定的能源,有效防止供气中断现象的发生,保证无人机的稳定飞行。


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    Title :

    Hydrogen kinetic energy engine fuel endurance device


    Additional title:

    一种氢动能发动机燃料续航装置


    Contributors:
    LI JIE (author)

    Publication date :

    2020-09-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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