The invention belongs to the technical field of overall design of vertical take-off and landing aircrafts, and particularly relates to a power layout structure of a single-blade rotor type vertical take-off and landing fixed-wing aircraft. A main body of the power layout structure is a rotor wing with only one blade, one side of a rotor wing rotating shaft is provided with a load cabin used for loading and weight balancing, the other side of the rotor wing rotating shaft is provided with a fixed-distance rotor wing blade, and the rotor wing blade can swing; driving propellers used for driving the rotors to rotate or generating level flight thrust are arranged on the rotor blades. Wherein the single-blade rotor wings are main components for generating lift force during vertical take-off and landing (a rotor wing mode) and cruise flight (a fixed wing mode). The single-blade rotor system provided by the invention can be used as a power system for the vertical take-off and landing aircraft, the power layout can give consideration to the cruising level flight efficiency and the vertical take-off and landing hovering efficiency, and static balance and dynamic balance can be realized in a steady hovering state.
本发明属于垂直起降飞行器总体设计技术领域,具体涉及一种单叶旋翼式垂直起降固定翼飞行器动力布局结构。所述动力布局结构的主体为仅有一片桨叶的旋翼,旋翼转轴的一侧为用于装载及配重的载荷舱,另一侧为定距旋翼桨叶,旋翼桨叶可挥舞;旋翼桨叶上有用于驱动旋翼旋转或产生平飞推力的驱动螺旋桨。其中,单叶旋翼为垂直起降(旋翼模式)及巡航飞行(固定翼模式)时产生升力的主要部件。本发明所提出的单叶旋翼系统可用于垂直起降飞行器作为动力系统,该动力布局可以兼顾巡航平飞效率和垂直起降悬停效率,且可在稳态悬停状态下实现静平衡、动平衡。
Power layout structure of single-blade rotor type vertical take-off and landing fixed-wing aircraft
一种单叶旋翼式垂直起降固定翼飞行器动力布局结构
2023-09-05
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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