The invention relates to a vertical take-off and landing combination aircraft and a vertical take-off and landing method of a fixed-wing aircraft, the vertical take-off and landing combination aircraft comprises the fixed-wing aircraft and a rotor aircraft, the rotor aircraft comprises a center machine box, a plurality of rotor arms and a plurality of side wing arm frames, and motor mounting shells are arranged at the ends, away from the center machine box, of the rotor arms; a rotating motor with an output shaft arranged downwards is mounted in the motor mounting shell, the output shaft of the rotating motor is connected with a propeller, a reconstruction device is arranged on the upper surface of the side wing arm frame, a camera is further arranged on the upper surface of the side wing arm frame, and a power source and a control module are arranged in the center machine box; a plurality of wings are arranged on the fixed-wing aircraft, a butt joint device is arranged on the lower surface of each wing, and the butt joint devices are used for butt joint and fixation of the reconstruction device and have an automatic locking function after butt joint is completed. The device has the following predictable technical effects that butt joint and separation of the fixed-wing aircraft are facilitated, and stable and efficient vertical take-off and landing of the fixed-wing aircraft are assisted.
本申请涉及一种垂直起降组合体飞行器及固定翼飞行器的垂直起降方法,该垂直起降组合体飞行器包括固定翼飞行器与旋翼飞行器,旋翼飞行器包括中心机盒、多根旋翼臂和多根侧翼臂架,旋翼臂远离中心机盒的端部设置有电机安装壳,电机安装壳内安装有输出轴朝下布置的旋转电机,旋转电机的输出轴连接有螺旋桨,侧翼臂架的上表面设置有重构装置,侧翼臂架的上表面还设置有摄像头,中心机盒内设置有动力源和控制模块;固定翼飞行器上设置有多个机翼,机翼的下表面设置对接装置,对接装置供重构装置对接固定且对接完成后具备自动锁定功能。本申请具有以下可预期的技术效果:方便于固定翼飞行器对接及分离,辅助固定翼飞行器稳定且高效的垂直起降。
Vertical take-off and landing combination aircraft and vertical take-off and landing method of fixed-wing aircraft
垂直起降组合体飞行器及固定翼飞行器的垂直起降方法
2022-03-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |