The invention discloses a container type eVTOL rotorcraft and an eVTOL rotorcraft cluster. The container type eVTOL rotorcraft comprises a rotor system and a cargo hold system, in the rotor wing system, at least two lift short wings are symmetrically arranged along the course of the rotor wing body, and the end part of each lift short wing is connected with a lift rotor wing through a supporting rod; at least two tension short wings are symmetrically arranged along the course of the rotor wing body, and a tension rotor wing is arranged at the front edge or the rear edge of each tension short wing; the rotor wing system is used for providing lift force for the aircraft by the lift force short wings, the lift force rotor wings and the pull force short wings together in the forward flight process, and providing pull force by the pull force rotor wings; in the vertical take-off and landing process, the lift rotors provide lift force for the aircraft; the cargo hold system is connected to the bottom of the rotorcraft body, executes air transportation through the rotor system and is separated from the rotorcraft body after arriving at a destination. According to the technical scheme, the problems that an eVTOL aircraft of an existing structure is high in technical difficulty in implementing transition conversion, and potential safety hazards exist in the transition conversion process are solved.
本发明公开一种集装箱式eVTOL旋翼飞行器及eVTOL旋翼飞行器集群,包括:旋翼系统和货舱系统;旋翼系统中,沿旋翼机体的航向对称设置有至少2个升力短翼,每个升力短翼的端部通过支撑杆连接1个升力旋翼;沿旋翼机体的航向对称设置有至少2个拉力短翼,每个拉力短翼的前缘或后缘设置有拉力旋翼;旋翼系统用于在前飞过程中由升力短翼、升力旋翼和拉力短翼共同向飞行器提供升力,由拉力旋翼提供拉力;在垂直起降过程中由升力旋翼向飞行器提供升力;货舱系统连接于旋翼机体的底部,通过旋翼系统执行空中运输,在达目的地后与旋翼机体分离。本发明技术方案解决了现有构型的eVTOL飞行器实施过渡转换的技术难度较高,且过渡转换过程中存在安全隐患的问题。
Container type eVTOL rotorcraft and eVTOL rotorcraft cluster
一种集装箱式eVTOL旋翼飞行器及eVTOL旋翼飞行器集群
2024-01-12
Patent
Electronic Resource
Chinese
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