The invention discloses an unmanned aerial vehicle parachute device, a parachute control system and a landing method thereof, which can collect the electric quantity and flight state data of an unmanned aerial vehicle in real time in the flight process of the unmanned aerial vehicle, and calculate whether the unmanned aerial vehicle needs to land or not in real time through the electric quantity and the flight state data. Once the electric quantity of the unmanned aerial vehicle is insufficient or the flying state of the unmanned aerial vehicle has potential danger, the unmanned aerial vehicle parachute device is controlled to be opened and released through the control module, and the unmanned aerial vehicle is rapidly landed in time; and meanwhile, centrifugal force is provided through rotation of a rotating disc in the unmanned aerial vehicle parachute device, high-pressure gas is output to the parachute cover through a high-pressure gas cylinder, the parachute cover is opened through cooperation of a parachute cover opening framework, then it is guaranteed that the folded parachute can be rapidly and completely unfolded, and then safe landing of the unmanned aerial vehicle is guaranteed.

    本发明公开了一种无人机降落伞装置、降落伞控制系统及其降落方法,本发明能够在无人机飞行过程中实时采集无人机的电量以及飞行状态数据,并通过电量与飞行状态数据实时解算是否需要对无人机进行降落作业,一旦无人机的电量不足或者无人机的飞行状态存在潜在危险,即通过控制模块控制无人机降落伞装置开启释放,及时迅速对无人机进行降落作业;同时通过无人机降落伞装置中的转动盘的转动提供离心力,通过高压气瓶向伞面输出高压气体,通过伞面撑开骨架配合将伞面撑开,进而保证折叠的降落伞能够迅速且完整的展开,进而保证无人机的安全降落。


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    Title :

    Unmanned aerial vehicle parachute device, parachute control system and landing method thereof


    Additional title:

    一种无人机降落伞装置、降落伞控制系统及其降落方法


    Contributors:
    CHEN BO (author) / YANG JING (author) / GU BINGLING (author) / TIAN LIN (author) / ZHANG FEI (author)

    Publication date :

    2024-11-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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