The invention belongs to the field of unmanned aerial vehicles, and relates to a vertical take-off and landing unmanned aerial vehicle with Z-shaped folding wings. The aircraft comprises a tubular fuselage, a main wing, a lift motor support arm, a lift motor, a horizontal propulsion motor and a full-moving empennage, the main wing is mounted above the tubular fuselage, and the main wing sections can be folded towards the center to reduce the projection area; the lift motor support arms are symmetrically mounted on the non-foldable sections of the main wings by taking the tubular fuselage as the center; lifting motors are respectively mounted at the front and rear ends of the lifting motor support arms; the horizontal propelling motor is mounted at the head of the fuselage to generate horizontal propelling force; and the two full-moving empennages are arranged at the tail part of the fuselage in an inverted V shape.
本发明属于无人机领域,涉及一种Z型折叠翼的垂直起降无人飞行器。飞行器包括:管状机身、主翼、升力电机支臂、升力电机、水平推进电机、全动式尾翼;主翼安装在管状机身上方,主翼分段可向中心折叠以减小投影面积;升力电机支臂以管状机身为中心对称安装在主翼的不可折叠段;升力电机支臂前后两端各安装一台升力电机;水平推进电机安装在机身头部,产生水平推进力;全动式尾翼共两片,呈倒V形布局安装在机身尾部。
Vertical take-off and landing unmanned aerial vehicle with Z-shaped folding wings
一种Z型折叠翼的垂直起降无人飞行器
06.12.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
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