AIRCRAFT ENGINE STARTER/GENERATOR
    1.
    发明申请
    AIRCRAFT ENGINE STARTER/GENERATOR 有权
    飞机发动机起动器/发电机

    公开(公告)号:US20130207395A1

    公开(公告)日:2013-08-15

    申请号:US13371657

    申请日:2012-02-13

    IPC分类号: H02K23/52 H02K9/19

    摘要: An assembly for a gas turbine engine includes a S/G having a rotatable shaft, a main machine, a PMG, and an exciter wherein at least one of the main machine, PMG, and exciter includes a rotor mounted to the shaft and having multiple rotor poles, a stator having multiple stator poles and at least one of the rotor poles and stator poles being formed by a core with a post and wire wound about the post to form a winding, with the winding having at least one end turn, and a layer to increase cooling capabilities of a portion of at least one of the stator and the rotor.

    摘要翻译: 用于燃气涡轮发动机的组件包括具有可旋转轴的S / G,主机,PMG和励磁机,其中主机PMG和励磁机中的至少一个包括安装到轴上并具有多个 转子极,具有多个定子极的定子,以及转子极和定子极中的至少一个由具有缠绕在柱上的柱和线的芯形成,以形成绕组,绕组具有至少一个端部转弯,以及 提高定子和转子中的至少一个的一部分的冷却能力的层。