发明名称 Rotor of a turbogenerator with direct gas cooling
摘要 The rotor (4) has a flow grid (30a,30b) positioned within the flow channel (30) provided by the annular gap between the inner edge of a rotor cap plate (22) and a rotor shaft (28). The flow grid has at least 2 stages, provided by an initial delay grid (30b), with a pressure generation characteristic and a delay grid (30a) with a deflection characteristic, adjacent the rotor winding head (29).
申请公布号 EP0849859(A1) 申请公布日期 1998.06.24
申请号 EP19970810949 申请日期 1997.12.05
申请人 ASEA BROWN BOVERI AG 发明人 STEFAN, ERNOE
分类号 H02K9/08;F04D29/16;F04D29/54;H02K1/32 主分类号 H02K9/08
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