The invention relates to a hybrid unmanned aerial vehicle (UAV) with vertical takeoff and landing (VTOL) capability. In particular, the present disclosure relates to a stabilized hybrid fixed angle rotor array UAV having VTOL capabilities of hovering capabilities using rotors and cruising capabilities using fixed wings.
本公开涉及具有垂直起飞和着陆(VTOL)能力的混合无人飞行器(UAV)。具体而言,本公开涉及稳定的混合固定角度旋翼阵列UAV,其具有使用旋翼的悬停能力和使用固定翼的巡航能力的VTOL能力。
Hybrid fixed angle rotor unmanned aerial vehicle with vertical take-off and landing capabilities
具有垂直起飞和着陆能力的混合固定角度旋翼无人驾驶飞行器
2024-02-09
Patent
Electronic Resource
Chinese
IPC: | B64U |
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