The invention discloses a scissor wing unmanned aerial vehicle, and relates to the technical field of aircrafts, the scissor wing unmanned aerial vehicle mainly comprises a fuselage main body, a left front wing, a left rear wing, a right front wing and a right rear wing, the wings are respectively provided with a tiltable ducted fan, the left front wing and the left rear wing as well as the right front wing and the right rear wing can be closed or unfolded, only one set of power system is adopted in the scissor wing unmanned aerial vehicle, the unmanned aerial vehicle can have the operation advantages of a fixed wing unmanned aerial vehicle and a rotor unmanned aerial vehicle at the same time, wing structures which can be separated like scissors are utilized, a power system capable of tilting is matched, wings are unfolded in the take-off and landing stages to take off and land vertically, the wings are closed in the navigation stage to fly at a high speed, and through conversion between the fixed wing and the rotor, the unmanned aerial vehicle can take off and land vertically. A corresponding wing form is used in a specific stage, and the nuclear load capacity, the cruising ability and the flexibility are comprehensively improved.
本发明公开了一种剪刀翼无人机,设计飞行器技术领域,主要包括有机身主体以及左前翼、左后翼、右前翼和右后翼,机翼上分别设置可倾转的涵道风扇,左前翼和左后翼以及右前翼和右后翼能够闭合或展开,其仅采用一套动力系统,能同时具备固定翼和旋翼无人机的运作优点,利用类似“剪刀”一样可以分开的机翼结构,配合可以倾转的动力系统,在起飞和降落阶段展开机翼垂直起降,在航行阶段闭合机翼高速飞行,通过在固定翼和旋翼间的转换,特定阶段使用对应机翼形式,综合提升了核载能力、续航能力以及灵活性。
Scissor wing unmanned aerial vehicle
剪刀翼无人机
25.04.2025
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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