发明名称 GASKYLD ROTOR FOR TURBOGENERATOR
摘要 A gas-cooled rotor assembly for use with a turbogenerator type device, wherein a coil side is positioned within a winding slot formed in the rotor core, such that a pair of cooling channels extend between opposite sides of the coil side and adjacent wall portions of the winding slot. Positioning devices of insulating material are positioned adjacent to radially inner-most and outer-most end portions of the coil side, with the positioning devices electrically insulating the coil side from confronting surface portions of the slot walls, while at the same time transmitting tangential forces therebetween.
申请公布号 SE409268(B) 申请公布日期 1979.08.06
申请号 SE19770013540 申请日期 1977.11.30
申请人 * ASEA AB 发明人 K * DAHL MADSEN
分类号 H02K9/08;H02K3/24;H02K3/48;(IPC1-7):02K3/48 主分类号 H02K9/08
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