The invention discloses a novel single-person eVTOL aircraft structure. The novel single-person eVTOL aircraft structure comprises a fuselage and wings symmetrically arranged on the two sides of the front portion of the fuselage. Coaxial contra-rotating propellers are arranged at the front end of the fuselage, 360-degree rotating tilting rotors are symmetrically arranged on the two sides of the rear portion of the fuselage, V-shaped empennages formed by combining empennages symmetrically arranged on the two sides are arranged on the upper portion of the rear end of the fuselage, and vertical empennages are arranged on the lower portion of the rear end of the fuselage and correspond to the middle of the position between the V-shaped empennages. The aircraft has the beneficial effects that 1, the take-off mode and the parking mode of a traditional fixed wing aircraft are changed, the V-shaped empennage and the vertical empennage are used as supports when the aircraft is parked, and the multifunctionality of the aircraft is achieved through a pair of tilting rotors rotating by 360 degrees; 2, the structure is simple, light and easy to maintain, and the manufacturing cost and the maintenance cost are reduced; safety is high, and the system can be widely applied to the field of urban air traffic.
本发明公开一种新型单人eVTOL飞行器结构,包括:机身以及对称设置在机身靠前部分两侧的机翼;机身的前端设置有同轴对转螺旋桨,机身靠后部分的两侧对称设置有360°旋转倾转旋翼,机身的后端上部设有由两侧对称设置的尾翼组合而成的V型尾翼,机身的后端下部且对应V型尾翼之间的中部设有垂直尾翼;本发明的有益效果:1.改变了传统的固定翼飞行器的起飞方式和停靠方式,利用V型尾翼和垂直尾翼作为飞行器停靠时候的支撑,并通过一对360°旋转的倾转旋翼实现飞行器的多功能性;2.结构简单、轻便、易于维护,降低了制造成本和维护成本;3.安全性高,可广泛应用于城市空中交通领域。
Novel single-person eVTOL aircraft structure
一种新型单人eVTOL飞行器结构
2024-09-27
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |