The invention provides a composite vector power omni-directional aircraft which comprises an aircraft body, an undercarriage, electronic equipment and a plurality of composite tilting rotor sets, the undercarriage, the electronic equipment and the composite tilting rotor sets are mounted on the aircraft body, and each composite tilting rotor set comprises an annular rolling tilting structure, a steering wheel, a steering engine, a steering engine seat, a bearing, a bearing seat, a pitching tilting mechanism, a tilting shaft, a carbon tube and a tube clamp. One end of the annular rolling and tilting structure is coaxially matched with the steering engine through the steering wheel, the other end of the annular rolling and tilting structure is of a protruding hollow shaft structure, the hollow shaft structure penetrates through a bearing in the bearing seat and is coaxially matched with the bearing, and the steering engine drives the annular rolling and tilting structure to rotate around the hollow shaft. The control logic is simple, meanwhile, the situation that the rotors incline to generate confrontation acting force is avoided, the rotors provide lift force for the aircraft as sufficiently as possible, the problems of power counteracting and power redundancy are solved fundamentally, energy loss is reduced, and the endurance time is prolonged.
本发明提供了一种复合矢量动力全向飞行器,包括机身以及安装在机身上的起落架、电子设备、若干复合式倾转旋翼组,所述复合式倾转旋翼组包括环形滚转倾转结构、舵盘、舵机、舵机座、轴承、轴承座、俯仰倾转机构、倾转轴、碳管和管夹,所述环形滚转倾转结构一端通过所述舵盘与舵机同轴配合,另一端为突出的空心轴结构,空心轴结构穿过轴承座内轴承,与轴承同轴配合,舵机驱动使环形滚转倾转结构绕空心轴旋转。本发明操控逻辑简洁,同时避免了旋翼倾斜互相产生对抗作用力,使旋翼尽可能充分地为飞行器提供升力,从根本上解决了动力抵消和动力冗余的问题,降低了能量损耗,延长了续航时间。
Composite vector power omnidirectional aircraft and control method thereof
复合矢量动力全向飞行器及其控制方法
2025-03-25
Patent
Electronic Resource
Chinese
IPC: | B64U |
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