The invention relates to the field of unmanned aerial vehicles, in particular to a vertical fixed wing variable airfoil profile structure and a transformation method thereof.The vertical fixed wing variable airfoil profile structure comprises a fuselage, a fixed wing assembly, a folding assembly and a rotor assembly, the fuselage comprises a main body, a balance plate located at the head of the fuselage and a tail plate located at the tail of the fuselage, and the fixed wing assembly comprises two fixed wing plates; the rotor assemblies are uniformly distributed on each fixed wing plate; the method is used for solving the problem of insufficient application flexibility caused by slow response, convenience and complexity of a vertical fixed-wing unmanned aerial vehicle switching mode. The fixed wing plate is quickly switched back and forth through the variable wing type structure, so that the fixed wing unmanned aerial vehicle has the effects of high-speed flight and stable flight of a fixed wing unmanned aerial vehicle and spot hovering of a rotor unmanned aerial vehicle; convenient, fast and stable switching is achieved through the folding assembly, the flight mode switching response time is shortened, and the application scene of the unmanned aerial vehicle is more flexible.
本发明涉及无人机领域,更具体地,涉及一种垂起固定翼可变翼型结构及其变换方法,包括机身、固定翼组件、折叠组件和旋翼组件,所述机身包括主体、位于其头部的平衡板和位于其尾部的尾板,所述固定翼组件包括两个固定翼板,所述旋翼组件均匀分布于每个固定翼板上;用于解决垂起固定翼无人机切换模式响应迟缓、便捷复杂,导致应用灵活性不足问题;通过可变翼型结构实现固定翼板的快速来回切换,使其兼具固定翼无人机高速飞行、稳定飞行以及旋翼无人机定点悬停的效果;通过折叠组件实现便捷、快速、稳定切换,缩短飞行模式切换响应时间,使无人机的应用场景更灵活。
Vertical fixed wing variable airfoil profile structure and transformation method thereof
一种垂起固定翼可变翼型结构及其变换方法
15.11.2024
Patent
Elektronische Ressource
Chinesisch
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