The invention relates to the technical field of aircrafts, and discloses an aircraft and a multi-rotor flying platform thereof. The multi-rotor flying platform comprises at least one pair of machine arms, wherein the at least one pair of machine arms are symmetrically arranged around a central axis, and a plurality of vertical power devices are arranged in each machine arm; the main wings are symmetrically arranged around the central axis and are connected with at least one pair of arms; the canards and the central avionics cabin are respectively connected with the pair of arms close to the central axis, and the canards and the central avionics cabin form an integrally formed closed structure with the pair of arms. According to the invention, the canards, the arms and the central avionics cabin form an integrally formed closed structure, so that the rigidity of the mounting structure of the motors on the arms is obviously improved.
本申请涉及飞行器技术领域,公开了一种飞行器及其多旋翼飞行平台。本申请多旋翼飞行平台包括至少一对机臂,至少一对机臂绕一中心轴线对称布置且各机臂内设有多个垂起动力装置;主机翼,主机翼绕中心轴线对称布置且连接至少一对机臂;鸭翼和中央航电舱,鸭翼和中央航电舱分别连接靠近中心轴线的一对机臂并与一对机臂组成一体成型闭合型结构。本申请通过将鸭翼、机臂和中央航电舱组成一体成型闭合型结构,使机臂上电机的安装结构刚度明显提升。
Aircraft and multi-rotor flying platform thereof
飞行器及其多旋翼飞行平台
2024-06-04
Patent
Electronic Resource
Chinese
IPC: | B64U |