The invention discloses a flapping rotor device with an ascending shaft wing vertically operating and a descending shaft wing horizontally operating, which comprises a support assembly, a rotating assembly, a driving assembly, a rotor assembly and a transmission assembly, and is characterized in that the supporting assembly, the rotating assembly, the driving assembly, the rotor assembly and the transmission assembly are in linkage fit, an autorotation spindle in the flapping rotor device can revolve under the driving of a revolution spindle, and meanwhile, autorotation is kept under the driving of a second driving motor. According to the flapping rotor device, in the descending revolution process of the autorotation spindle, the rotation surface of the rotor assembly is always kept parallel to the horizontal plane under the driving of the second driving motor, so that vertically upward lifting force is continuously provided for an aircraft; and in the ascending revolution process of the autorotation spindle, the second driving motor drives the rotor assembly to keep the rotating surface of the rotor assembly perpendicular to the axis of the rotating arm all the time, so that resistance is not generated or small resistance is generated, counteracting of lift force in the revolution process of the rotor wing assembly is avoided, and continuous and stable lift force is provided for the aircraft.
本发明公开了一种上行轴翼垂直运转下行水平运转的扑旋翼装置,包括:支撑组件,转动组件,驱动组件,旋翼组件和传动组件,通过支撑组件、转动组件、驱动组件、旋翼组件和传动组件的联动配合,能够实现该扑旋翼装置中自转主轴在公转主轴的带动下进行公转,且同时在第二驱动电机的驱动下保持自转。该扑旋翼装置中自转主轴下行公转过程中,由第二驱动电机驱动始终保持旋翼组件的旋转面与水平面平行,进而为飞行器持续提供竖直向上的升力,自转主轴上行公转过程中,由第二驱动电机驱动保持旋翼组件的旋转面始终与转臂轴线垂直,进而不产生阻力或产生较小的阻力,避免了旋翼组件公转过程中升力的抵消,为飞行器提供了持续稳定的升力。
Flapping rotor device with ascending shaft wing vertically operating and descending shaft wing horizontally operating
一种上行轴翼垂直运转下行水平运转的扑旋翼装置
2021-03-05
Patent
Electronic Resource
Chinese
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