The invention provides a multi-rotor combined type unmanned aerial vehicle. The multi-rotor combined type unmanned aerial vehicle comprises a fuselage; the rotor assemblies are connected to the two longitudinal sides of the fuselage respectively and can provide lift force in the vertical stage and provide thrust in the level flight stage; the wing assemblies are connected to the two longitudinal sides of the fuselage respectively and can provide lift force in the level flight stage; wherein on the same side of the fuselage, each wing assembly is located between every two adjacent rotor wing assemblies, every two adjacent rotor wing assemblies are distributed in the longitudinal direction of the fuselage, one rotor wing assembly is arranged on the upper portion of the fuselage, and the other rotor wing assembly is arranged on the lower portion of the fuselage. According to the arrangement, by means of the mode that the rotor wing assemblies and the wing assemblies are matched, the cruising speed is increased, energy consumption is reduced, the flight range is improved, and by means of the position design of the rotor wing assemblies and the wing assemblies, interference between the rotor wings and the wings can be reduced, and the flight stability is improved.
本申请提供了一种多旋翼复合式无人机,包括:机身;多个旋翼组件,分别连接在所述机身的纵向两侧,并能够在垂起阶段提供升力、在平飞阶段提供推力;多个机翼组件,分别连接在所述机身的纵向两侧,并能够在平飞阶段提供升力;其中,在所述机身的同一侧,所述机翼组件位于相邻的两个所述旋翼组件之间,相邻的两个所述旋翼组件沿所述机身的纵向分布,其中一者设置在所述机身的上部、另一者设置在所述机身的下部。如此设置,通过旋翼组件和机翼组件相配合的形式,有利于提升巡航速度,减少能耗并提升飞行航程,而且通过旋翼组件和机翼组件的位置设计,可以减少旋翼和机翼之间的干扰,提升飞行稳定性。
Multi-rotor combined type unmanned aerial vehicle
一种多旋翼复合式无人机
2025-05-09
Patent
Electronic Resource
Chinese
Multi-rotor unmanned aerial vehicle and multi-rotor unmanned aerial vehicle system
European Patent Office | 2020
|MULTI-ROTOR UNMANNED AERIAL VEHICLE AND MULTI-ROTOR UNMANNED AERIAL VEHICLE SYSTEM
European Patent Office | 2022
|