The invention discloses an ejection two-rotor mooring unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The system specifically comprises a two-rotor mooring unmanned aerial vehicle which can be powered by the ground and hovers in the air; the launching device is arranged at the bottom of the two-rotor-wing mooring unmanned aerial vehicle and used for launching the two-rotor-wing mooring unmanned aerial vehicle to a specified height; the catapulting bracket is arranged between the two-rotor mooring unmanned aerial vehicle and the launching device and used for bearing the folded mooring unmanned aerial vehicle and limiting the rotors of the folded two-rotor mooring unmanned aerial vehicle from being unfolded, and after the two-rotor mooring unmanned aerial vehicle is launched, the catapulting bracket can be separated from the two-rotor mooring unmanned aerial vehicle. The rotors of the two-rotor mooring unmanned aerial vehicle are prevented from making contact with the inner side wall of the launching device. Friction between the folding rotors of the catapult two-rotor mooring unmanned aerial vehicle and the inner side wall of the launch canister is avoided, and the service life of the catapult two-rotor mooring unmanned aerial vehicle is prolonged.
本发明公开了一种可弹射二旋翼系留无人机,涉及无人机技术领域。具体包括:二旋翼系留无人机,可由地面供电,悬停于空中;发射装置,设于所述二旋翼系留无人机底部,用于将所述二旋翼系留无人机发射至指定高度;以及弹射托架,设于所述二旋翼系留无人机与发射装置之间,用于承托折叠后的系留无人并限制折叠后二旋翼系留无人机的旋翼展开,待二旋翼系留无人机发射后,所述弹射托架可与所述二旋翼系留无人机分离,以避免二旋翼系留无人机的旋翼与发射装置的内侧壁接触。避免弹射二旋翼系留无人机折叠旋翼与发射筒内侧壁之间摩擦,延长弹射二旋翼系留无人机的使用寿命。
Ejectable two-rotor mooring unmanned aerial vehicle
一种可弹射二旋翼系留无人机
2024-10-11
Patent
Electronic Resource
Chinese
IPC: | B64U |
Mooring unmanned aerial vehicle and mooring unmanned aerial vehicle system
European Patent Office | 2022
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