The invention discloses a tilting multi-rotor unmanned aerial vehicle and a tilting transition method, and belongs to the technical field of unmanned aerial vehicles. The tilting multi-rotor unmanned aerial vehicle comprises a fuselage, wings are symmetrically arranged on the two sides of the fuselage, wingtip small wings with rudders are arranged at the tail ends of the wings, and front tilting mechanisms symmetrically arranged relative to the fuselage are arranged at the front end of the fuselage; rear tilting mechanisms which are symmetrically arranged relative to the fuselage are arranged at the rear end of the fuselage, and a propeller is arranged in the middle of the rear end of the fuselage; the front tilting mechanism comprises a front propeller, the front propeller is connected with the fuselage through a tilting power structure, the rear tilting mechanism comprises a rear propeller, and the rear propeller is connected with the fuselage through a tilting power structure. According to the tilting multi-rotor unmanned aerial vehicle and the tilting transition method, the fuselage layout is matched with the front tilting mechanism and the rear tilting mechanism, the flight stability is improved, and higher air maneuverability is achieved.
本发明公开了一种倾转多旋翼无人机及倾转过渡方法,属于无人机技术领域,其中倾转多旋翼无人机包括机身,机身的两侧对称设置有机翼,机翼的末端设置有带有方向舵的翼尖小翼,机身上前端设置有关于机身对称设置的前倾转机构,机身上后端设置有关于机身对称设置的后倾转机构,机身上后端的中间设置有推进桨;前倾转机构包括前螺旋桨,前螺旋桨通过倾转动力结构与机身连接,后倾转机构包括后螺旋桨,后螺旋桨通过倾转动力结构与机身连接。本发明采用上述一种倾转多旋翼无人机及倾转过渡方法,通过机身布局配合前倾转机构、后倾转机构,提高飞行稳定性,具有更强的空中机动性。
Tilting multi-rotor unmanned aerial vehicle and tilting transition method
一种倾转多旋翼无人机及倾转过渡方法
2024-12-17
Patent
Electronic Resource
Chinese
European Patent Office | 2020
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