The invention discloses a cross-medium water-air amphibious unmanned aircraft and a control system, the cross-medium water-air amphibious unmanned aircraft comprises an aircraft, wing storage grooves are formed in the two sides of the aircraft, wings are arranged at one ends of the wing storage grooves, the nose of the aircraft is connected with propellers, and the propellers are connected with the aircraft. The propeller is composed of a second motor, a second rotating shaft, a second gear disc, a first rotating shaft, a second synchronizing wheel, a third rotating shaft, a first synchronizing wheel, a belt, a third gear disc, a propeller mounting frame and two propeller plates. According to the aircraft, part of the wings are folded in the aircraft body, so that the underwater wet surface area of the aircraft is effectively reduced; meanwhile, the wings outside the fuselage can serve as fin stabilizers underwater, so that the stability of the aircraft is improved, and the resistance of underwater navigation is reduced; the aircraft adopts a foldable air wing design, and air wing blades are converged at a position attached to a nose in a water entry stage, so that the damage of water entry impact to the structure is reduced, and the underwater resistance is reduced.
本发明公开了一种跨介质水空两栖无人航行器以及控制系统,包括航行器,所述航行器的两侧均设有机翼收纳槽,所述机翼收纳槽的一端设有机翼,所述航行器的机头连接有螺旋桨,所述螺旋桨由第二电机、第二转动轴、第二齿轮盘、第一转动轴、第二同步轮、第三转动轴、第一同步轮、皮带、第三齿轮盘、螺旋桨安装架和两个螺旋桨板构成。本航行器将部分机翼折叠在机身内部,有效减小了航行器水下湿表面积;同时,机身外部的机翼可以在水下充当减摇鳍效果,增加了航行器稳定性并且减少了水下航行的阻力;航行器采用可折叠空翼设计,在入水阶段将空翼桨叶收敛在贴合机头的位置,从而减轻入水抨击对结构的破坏和减小水下阻力。
Cross-medium water-air amphibious unmanned vehicle and control system
一种跨介质水空两栖无人航行器以及控制系统
02.04.2024
Patent
Elektronische Ressource
Chinesisch
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