The invention relates to the technical field of aircrafts, in particular to an aircraft rotor motor bracket, comprising: an assembly cavity comprising a bottom wall and a side wall on one side, the assembly cavity being used for sleeving an aircraft rotor support arm; a through hole is formed in the bottom wall of the assembly cavity; the motor mounting surface intersects with the bottom wall of the assembly cavity and is connected with the bottom wall of the assembly cavity, and a motor mounting position is preset on the motor mounting surface; the electronic speed controller mounting surface is intersected and connected with the bottom wall of the assembling cavity, and an electronic speed controller mounting position is preset on the electronic speed controller mounting surface; and the motor mounting surface and the electronic speed controller mounting surface are oppositely arranged and are positioned on two sides of the through hole. The device is ingenious in design and novel in structure, can provide installation space for a rotor motor, an electronic speed controller and other equipment at the same time, is stably connected with a rotor support arm of an aircraft, and has very remarkable popularization significance.
本发明涉及飞行器技术领域,具体涉及一种飞行器旋翼电机支架,包括:装配腔,包括一侧的底壁与侧壁,所述装配腔用于与飞行器旋翼支臂进行套接;所述装配腔的底壁上设置有通孔;电机安装面,相交于所述装配腔的底壁连接且其上预设有电机安装位;电调安装面,相交于所述装配腔的底壁连接且其上预设有电调安装位;所述电机安装面与所述电调安装面相对设置且二者位于所述通孔的两侧。本发明设计巧妙,结构新颖,可同时为旋翼电机和电调及其它设备提供安装空间,而且与飞行器旋翼支臂连接稳定,具有十分显著的推广意义。
Aircraft rotor motor support
一种飞行器旋翼电机支架
2022-06-10
Patent
Electronic Resource
Chinese
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