基本信息:
- 专利标题： 一种多余度电机绕组分单元结构
- 专利标题（英）：Disclosed is a multi-redundancy motor winding subunit structure
- 申请号：CN201821428081.5 申请日：2018-08-31
- 公开(公告)号：CN208890509U 公开(公告)日：2019-05-21
- 发明人： 赵炜 , 崔涛 , 酒晨霄 , 马聪 , 郭建军 , 杨维 , 陈卫东 , 樊晋
- 申请人： 中国航空工业集团公司西安飞行自动控制研究所
- 申请人地址： 陕西省西安市雁塔区锦业路129号
- 专利权人： 中国航空工业集团公司西安飞行自动控制研究所
- 当前专利权人： 中国航空工业集团公司西安飞行自动控制研究所
- 当前专利权人地址： 陕西省西安市雁塔区锦业路129号
- 代理机构： 中国航空专利中心
- 代理人： 高霖
- 主分类号： H02K3/50
- IPC分类号： H02K3/50
The utility model relates to a redundant motor winding subunit structure, which comprises an iron core (1) and windings (2), and is characterized in that a plurality of coils are sequentially and tightly connected through outgoing lines to form a winding (2), the windings (2) are sequentially and uniformly distributed and fixed on the inner cylindrical surface of the iron core (1), and two ends ofeach winding (2) extend out of the end surface of the iron core (1). According to the structure, combination of single redundancy, double redundancy, four redundancy and the like can be achieved through different connection modes among the windings according to design requirements, the manufacturing problem of the multi-redundancy windings of the toothless iron core (1) can be solved, and the manufacturing and assembling difficulty of the multi-redundancy windings is simplified through the thought of the sub-unit windings.