The invention relates to the technical field of aircrafts, in particular to a self-rotor aircraft with vehicle wings separated from multi-shaft tilting rotors, which comprises an aircraft bracket, self-rotors, a trolley, a cross rod, side rotors, a propeller, an empennage, a rudder, an empennage connecting plate and an empennage frame push rod assembly, the aircraft support is of an inverted-U-shaped structure and installed at the upper end of the trolley, the upper end of the aircraft support is provided with the self-rotor, the outer walls of the left end and the right end of the aircraft support are fixedly connected with the transverse rods, one end of each transverse rod is provided with the side rotor, and the rear end of the trolley is provided with the propeller. The empennages are installed in the empennage frame push rod assembly, rudders are installed in the empennages, and an empennage connecting plate is fixedly connected between every two adjacent empennages. The trolley can be rapidly transported at different places, in addition, through the empennage frame push rod assembly and the sliding groove locking structure, the empennage can be automatically recycled, and an aircraft can be rapidly separated from and fix the trolley.
本发明涉及飞行器技术领域,尤其涉及一种车翼分离多轴倾转旋翼的自旋翼飞行器,包括有飞行器支架、自旋翼、小车、横杆、侧旋翼、螺旋桨、尾翼、方向舵、尾翼连接板和尾翼架推杆组件;飞行器支架为倒U型结构且安装于小车的上端,飞行器支架的上端安装有自旋翼,飞行器支架的左右两端外壁固定连接有横杆,横杆的一端安装有侧旋翼,小车的后端安装有螺旋桨,尾翼架推杆组件安装于小车的左右两端,尾翼安装于尾翼架推杆组件内,尾翼内安装有方向舵,相邻两块尾翼之间固定连接有尾翼连接板;本发明可以在不同地点快速运输小车,此外,通过尾翼架推杆组件和滑槽锁定结构,不仅能够自动回收尾翼,还可以使得飞行器快速分离与固定小车。
Self-rotor aircraft with separated wings and multi-shaft tilting rotors
一种车翼分离多轴倾转旋翼的自旋翼飞行器
2024-12-31
Patent
Electronic Resource
Chinese
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