The invention discloses a landing supporting mechanism and an aircraft, and the landing supporting mechanism comprises a mounting seat, an inner supporting rod, an outer supporting rod, a first elastic part, a second elastic part and a locking mechanism; the mounting base is connected with an aircraft; the front end of the inner supporting rod is rotationally arranged on the mounting seat; one end of the first elastic piece is connected to the inner supporting rod, and the other end of the first elastic piece is located on the installation base and connected to the installation base or the aircraft. The outer supporting rod is rotationally connected to the inner supporting rod; one end of the second elastic piece is arranged on the inner supporting rod, and the other end is arranged on the outer supporting rod; when the outer supporting rod and the inner supporting rod are folded, the rear end of the inner supporting rod faces downwards, the rear end of the outer supporting rod faces upwards, and the first elastic piece and the second elastic piece are both in a compressed state. When the landing supporting mechanism is unfolded, the rear end of the inner supporting rod is unfolded outwards, and the rear end of the outer supporting rod faces downwards. The aircraft comprises the landing supporting mechanisms, and a plurality of sets of landing supporting mechanisms are evenly arranged on the outer side of the aircraft. According to the scheme, the stability and safety of the aircraft during landing can be effectively improved.

    一种着陆支撑机构及飞行器,着陆支撑机构,包括:安装座、内撑杆、外撑杆、第一弹性件、第二弹性件及锁止机构;安装座用于连接飞行器;内撑杆的前端转动设于安装座;第一弹性件的一端连接于内撑杆,第一弹性件的另一端位于安装座,连接于安装座或飞行器;外撑杆转动连接于内撑杆;第二弹性件的一端设于内撑杆,另一端设于外撑杆;外撑杆及内撑杆收拢时,内撑杆的后端朝下,外撑杆的后端朝上,第一弹性件及第二弹性件均呈压缩状态;着陆支撑机构展开时,内撑杆的后端向外展开,外撑杆的后端朝下。飞行器,包括上述的着陆支撑机构,着陆支撑机构在飞行器的外侧均匀设置多组。本方案能有效提高飞行器着陆时的平稳性及安全性。


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    Titel :

    Landing supporting mechanism and aircraft


    Weitere Titelangaben:

    一种着陆支撑机构及飞行器


    Beteiligte:
    YAN MI (Autor:in) / LUO GUANCHEN (Autor:in) / WANG MINGJIE (Autor:in) / SUN RENBIN (Autor:in) / WANG BIN (Autor:in)

    Erscheinungsdatum :

    13.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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