The invention discloses a sudden failure unmanned helicopter landing device and a landing control system, and belongs to the technical field of unmanned helicopter landing control. The sudden failure unmanned helicopter landing device comprises a main clamping assembly and an auxiliary clamping assembly, the main clamping assembly is used for clamping a pair of landing sledge bars at the bottom of an undercarriage in the vertical direction, and the auxiliary clamping assembly is used for clamping two pairs of supporting rods which are fixed to the two landing sledge bars and are symmetrically arranged front and back in the horizontal direction. And after the main clamping assembly clamps the two landing pinch bars, the auxiliary clamping assembly can clamp the two pairs of supporting rods from the front side and the rear side respectively, so that the undercarriage is in a stable posture capable of vertically landing, and a faulted helicopter is centralized and fixed. In addition, the landing control system can drive the landing device to automatically move towards the faulted helicopter, so that the faulted helicopter can be ready to land at any time, and the faulted helicopter can be automatically transferred to a designated place, which is convenient and fast.

    本发明公开了一种突发故障无人直升机降落装置及降落控制系统,属于无人直升机降落控制技术领域;其中,突发故障无人直升机降落装置包括主夹持组件和副夹持组件,主夹持组件用于从竖直方向夹紧起落架底部的一对着陆橇杆,副夹持组件用于从水平方向上夹紧两着陆橇杆上固定的呈前后对称布置的两对支撑杆,且主夹持组件夹住两着陆橇杆后,副夹持组件才能将两对支撑杆分别从前后两侧夹紧,以使得起落架处于能竖直着陆的平稳姿态,对故障直升机进行扶正和固定。此外,本发明的降落控制系统则可以带着降落装置自动地朝故障直升机移动,以便故障直升机随时备降,并自动转运故障直升机至指定地点,方便快捷。


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    Title :

    Sudden failure unmanned helicopter landing device and landing control system


    Additional title:

    一种突发故障无人直升机降落装置及降落控制系统


    Contributors:
    GUO LI (author) / CHEN JUANJUAN (author) / WU YUE (author) / XU YUHANG (author) / CHEN YAJIE (author) / LI RUNZE (author) / YAN HUAIQIANG (author) / PENG HAIRONG (author)

    Publication date :

    2025-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / G01S RADIO DIRECTION-FINDING , Funkpeilung



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