The invention discloses a foldable wing aircraft with a wing variant structure. The foldable wing aircraft comprises an aircraft body, a left wing, a right wing, a horizontal tail wing, a vertical tail wing and a power device, the wing mounting platform comprises a first supporting rod mounting platform, a second supporting rod mounting platform, an actuator cylinder mounting platform and a connecting rod assembly; an electric push rod is arranged on the actuator cylinder mounting platform, a first actuator cylinder is arranged on the electric push rod, the connecting rod assembly comprises a first connecting rod mounting platform and a second connecting rod mounting platform, and a connecting rod structure is arranged between the first connecting rod mounting platform and the second connecting rod mounting platform; through the folding design of the left wing and the right wing, the space occupied by the wings after the aircraft is folded is small, the wingspans of the left wing and the right wing can be freely expanded and folded, and the lift-drag ratio, the cruising ability and the service life of an engine are increased by increasing the areas of the left wing and the right wing.
本发明公开了一种机翼变体结构的可折叠翼飞行器包括机身、左机翼、右机翼、水平尾翼、垂直尾翼和动力装置,左机翼包括设置在机身上的机翼安装平台,机翼安装平台包括第一支撑杆安装平台、第二支撑杆安装平台、作动筒安装平台和连杆组件;作动筒安装平台上设置有电动推杆,电动推杆上设置有第一作动筒,连杆组件包括第一连杆安装平台和第二连杆安装平台,第一连杆安装平台与第二连杆安装平台之间设置有连杆结构;本发明通过左机翼、右机翼的折叠设计,能够使得飞行器折叠后机翼所占的空间较小,而且左机翼、右机翼的翼展可以自由伸展折叠,通过增加左机翼、右机翼的面积,增加升阻比、续航能力和发动机寿命。
Foldable wing aircraft with wing variant structure
一种机翼变体结构的可折叠翼飞行器
2023-09-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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