The take-off and landing device is provided with a take-off and landing platform, a clamping mechanism is arranged at the lower end of the unmanned aerial vehicle, the take-off and landing platform comprises a vehicle arm contact ring arranged on the upper portion and a guide groove formed in the lower portion, the vehicle arm contact ring is annular and used for supporting vehicle arms of the unmanned aerial vehicle, and the guide groove is formed in the lower portion of the unmanned aerial vehicle. The guiding groove is located in the center of the arm contact ring and used for bearing the clamping mechanism, so that the unmanned aerial vehicle cannot topple over after landing, the guiding groove comprises a guiding ring, and the guiding ring can make contact with the clamping mechanism and guide the clamping mechanism to enter the center of the guiding groove. According to the take-off and landing device of the multi-rotor unmanned aerial vehicle, the problem that when the multi-rotor unmanned aerial vehicle with a clamping mechanism lands, a lifting platform cannot provide stable support, and the unmanned aerial vehicle is difficult to land is solved.
本发明公开了一种多旋翼无人机的起降装置,具有起降平台,在所述无人机下端设置有夹持机构,所述起降平台包括设置在上部的机臂接触环和设置在下部的引导凹槽,其中,所述机臂接触环呈环形,用于支撑旋翼无人机的机臂,所述引导凹槽位于机臂接触环中央位置,用于承接夹持机构,使得无人机降落后不会倾倒,所述引导凹槽包括引导环,所述引导环能够与夹持机构接触,引导夹持机构进入引导凹槽中央位置。本发明公开的多旋翼无人机的起降装置解决了具有夹持机构的多旋翼无人机在降落时,升降平台将无法提供稳定支撑,造成无人机降落困难的问题。
Take-off and landing device of multi-rotor unmanned aerial vehicle
一种多旋翼无人机的起降装置
2024-02-20
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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