发明名称 Bearing for a turbocharger rotor bearing
摘要 The outer ring (6) of the bearing is in one piece and has two tracks (7,7a) for the two rows of rollers (8,8a). The inner ring (9) of one row of rollers extends axially under the second row of rollers and supports the inner rings (10,11). An annular duct (12) on the inner ring (11) is connected to at least one groove (14) leading out of the bearing. Ducts (15,15a) lead from the annular duct to both tracks so as to lubricate the ducts or the rows of rollers. The numbers of ducts and grooves differ.
申请公布号 EP0769630(B1) 申请公布日期 2002.05.02
申请号 EP19960116391 申请日期 1996.10.12
申请人 FAG AIRCRAFT/SUPER PRECISION BEARINGS GMBH 发明人 SEBALD, WILHELM;KREISELMEIER, GERHARD
分类号 F02B39/00;F01M1/06;F02B39/14;F16C19/08;F16C19/18;F16C33/60;F16C33/66 主分类号 F02B39/00
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