Soft-wing power aircraft

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Soft-wing power aircraft

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ZHANG ANPING

The invention discloses a soft wing power aircraft, which relates to the technical field of aircrafts, and comprises a connecting shaft, power components arranged at the left and right ends of the connecting shaft, a wing component connected to the connecting shaft, a wing mounting component connected to the wing component, and a first connecting node and a second connecting node arranged at the middle section of the connecting shaft, the wing assembly comprises a wing plate fixed to the shaft sleeve, the wing assembly comprises a human body wing assembly connected to the wing plate, a first control rod and a first supporting handle are connected to the lower portion of the first connecting node, and a second control rod and a second supporting handle are connected to the lower portion of the second connecting node. Axle sticking devices are arranged between the first control rod and the connecting shaft and between the second control rod and the wing plate, the first supporting handle and the second supporting handle are each provided with an axle sticking removing handle, and the first supporting handle and the second supporting handle are each provided with an accelerator controller. The device has the advantages of light weight, simple structure, convenience and rapidness in operation, safety and reliability.

本发明公开了一种软翼动力飞行器，涉及飞行器技术领域，包括连接轴，连接轴左右两端设置有动力组件，连接轴上连接有机翼组件，机翼组件连接有翼装组件，连接轴中段设置有第一连接节点和第二连接节点，动力组件包括蜗喷发动机，机翼组件包括固定在轴套上的翼板，翼装组件包括连接在翼板上的人体翼装，第一连接节点下方连接有第一控制杆和第一支撑手柄，第二连接节点下方连接有第二控制杆和第二支撑手柄，第一控制杆和第二控制杆与连接轴和翼板之间均设置有抱轴装置，第一支撑手柄和第二支撑手柄上均设置有解抱轴手把，第一支撑手柄和第二支撑手柄上还均设置有油门控制器。本发明具有重量轻、结构简单、操作方便快捷以及安全可靠的优点。