The invention provides a solar unmanned aerial vehicle with foldable wings, and relates to the technical field of solar unmanned aerial vehicles, the solar unmanned aerial vehicle comprises a fuselage, middle wings are arranged on the two sides of the fuselage, folding wings are rotationally connected to the two ends, away from the fuselage, of the middle wings respectively, and solar panels are arranged on the upper surfaces of the folding wings and the middle wings; the folding wings extend in the wingspan direction of the middle wing when unfolded, and the upper surfaces of the folding wings are located above the upper surface of the middle wing when the folding wings are folded; the folding driving mechanism is arranged at the rotating joint of the middle wing and the folding wing, and the folding driving mechanism can drive the folding wing to rotate relative to the middle wing; the front propellers are arranged on the front side of the fuselage and the front sides of the outer ends of the middle wings, and the rear propellers are arranged on the rear sides of the outer ends of the folding wings; the problems that in the prior art, a solar unmanned aerial vehicle has high requirements for take-off and landing sites and is poor in transportation and storage performance are solved.
本发明提供一种可折叠机翼太阳能无人机,涉及太阳能无人机技术领域,包括:机身,机身的两侧设置有中间机翼,中间机翼远离机身的两端分别转动连接有折叠翼,折叠翼和中间机翼的上表面设置有太阳能板,折叠翼展开时沿中间机翼的翼展方向延伸,折叠翼折叠时折叠翼的上表面处于中间机翼的上表面的上方;折叠驱动机构,折叠驱动机构设置在中间机翼与折叠翼的转动连接处,折叠驱动机构能够驱动折叠翼相对于中间机翼转动;前螺旋桨和后螺旋桨,前螺旋桨设置在机身前侧和中间机翼的外端前侧,后螺旋桨设置在折叠翼的外端后侧;解决现有技术中太阳能无人机对起降场地要求较高和运输收纳性差的问题。
Solar unmanned aerial vehicle with foldable wings
一种可折叠机翼太阳能无人机
2025-04-08
Patent
Electronic Resource
Chinese
IPC: | B64U |