The invention discloses an adjustable undercarriage and an unmanned aerial vehicle, the undercarriage comprises a left supporting leg and a right supporting leg, the supporting legs comprise an upper supporting leg and a lower supporting leg, the included angle between the upper supporting leg and the lower supporting leg is adjusted through an angle adjusting device, and the length of the upper supporting leg and/or the length of the lower supporting leg are/is adjustable. The landing gear with the structure is provided with the angle adjusting mechanism and the telescopic structure, so that the angle and the length of the support can be adjusted, the landing gear is simple in structure and convenient to adjust, and the weight of the support is basically not increased. By adjusting the angle and the length, the requirements of most unmanned aerial vehicles and loading equipment can be met, and the adaptability of the undercarriage is greatly improved.
本发明公开了一种可调节的起落架及无人机,该起落架包括左右两根支腿,所述支腿包括上支腿和下支腿,所述上支腿和下支腿之间通过角度调节装置来调节夹角,并且所述上支腿和/或下支腿的长度可调节。具有上述结构的起落架,设置有角度调节机构和伸缩结构,使得支架的角度和长度均可以调节,其结构简单,调节方便,基本上不会增加支架的重量。通过角度和长度的调节,可以适应绝大部分无人机及装载设备的需要,大大提高了起落架的适应性。
Adjustable undercarriage and unmanned aerial vehicle
一种可调节的起落架及无人机
2022-06-07
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Rigidity and height adjustable unmanned aerial vehicle undercarriage
Europäisches Patentamt | 2023
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