The invention discloses an unmanned aerial vehicle and an unmanned aerial vehicle escape method, relates to the field of unmanned aerial vehicles, and aims to optimize the performance of the unmannedaerial vehicle. The unmanned aerial vehicle comprises a vehicle body, a seat, a parachute, an ejection device and a control device. The seat is detachably mounted on the vehicle body; the parachute ismounted on the seat; the ejection device is mounted between the vehicle body and the seat, and the ejection device is configured to eject the seat that has been separated from the vehicle body; and the control device is electrically connected with the ejection device so as to control an ejection angle of the ejection device. According to the technical scheme, the unmanned aerial vehicle is provided with the ejection device and the control device, after the manned multi-rotor unmanned aerial vehicle breaks down, the control device calculates the ejection angle of the seat, and then the ejection device is controlled to eject the seat according to the ejection angle obtained through calculation so that a possibility that a driver and passengers escape smoothly is increased.

    本发明公开了一种无人机以及无人机逃生方法,涉及无人机领域,用以优化无人机的性能。无人机包括机身、座椅、降落伞、弹射装置以及控制装置。座椅可拆卸地安装于机身;降落伞安装于座椅;弹射装置安装于机身和座椅之间,弹射装置被构造为将已经与机身分离的座椅弹射出去。控制装置与弹射装置电连接,以控制弹射装置的弹射角度。上述技术方案提供的无人机,配备有弹射装置和控制装置,在载人多旋翼无人机出现故障后,控制装置计算出座椅的弹射角度,然后按照计算得到的弹射角度,控制弹射装置弹射座椅,以增加驾乘人员顺利逃生的可能性。


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    Titel :

    Unmanned aerial vehicle and unmanned aerial vehicle escape method


    Weitere Titelangaben:

    无人机以及无人机逃生方法


    Beteiligte:
    QIE XINYUE (Autor:in)

    Erscheinungsdatum :

    2020-10-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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