The invention relates to the technical field of aircrafts, and particularly discloses a three-rotor vertical take-off and landing aircraft which comprises a rack and wings symmetrically and vertically arranged on the two sides of the rack, a first supporting foot stool and a second supporting foot stool are arranged at the tail end of the rack and below the wings correspondingly, and driving propeller assemblies are arranged above the two wings correspondingly. A balance propeller assembly and a driving assembly are arranged at the tail end of the machine frame, the initial rotating face of the balance propeller assembly is the same as or parallel to the rotating face of the driving propeller assembly, a controller assembly and a plurality of posture and environment sensing assemblies are arranged on the machine frame, and a load hanging rod is connected to the lower portion of the machine frame through a hinge. A load, a control assembly and an energy assembly are arranged at the tail end of the load hanging rod, and the driving assembly, the energy assembly, the control assembly, the posture and environment sensing assembly, the balance propeller assembly and the driving propeller assembly are all connected with the controller assembly. The aircraft can be switched between a multi-rotor-wing flight state and a fixed-wing flight state, and the application range of the aircraft is effectively widened.
本发明涉及飞行器技术领域,具体公开了一种三旋翼垂直起降飞行器,包括机架及对称且垂直设置在机架两侧的机翼,机架尾端和机翼的下方分别设有第一支撑脚架和第二支撑脚架,两个机翼的上方均设置有驱动螺桨组件,机架的尾端设有平衡螺桨组件及驱动组件,平衡螺桨组件的初始旋转面与驱动螺桨组件的旋转面相同或平行,机架上设有控制器组件和多组姿态及环境感知组件,机架的下方通过铰链连接有负载吊杆,负载吊杆的末端设有负载、操控组件和能源组件,驱动组件、能源组件、操控组件、姿态及环境感知组件、平衡螺桨组件和驱动螺桨组件均与控制器组件连接。本发明能够在多旋翼飞行状态和固定翼飞行状态之间进行切换,有效的提高了飞行器的适用范围。
Three-rotor vertical take-off and landing aircraft
一种三旋翼垂直起降飞行器
2024-11-19
Patent
Electronic Resource
Chinese
IPC: | B64U |
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