发明名称 Sealed oil dampened roller bearing
摘要 The ball or roller bearing for aircraft gas turbines has squeeze film (54) lubrication. A first channel system (58, 60, 61) feeds oil into the film and then on to the balls (36) or rollers from the oil chamber (46) side. A second channel system (64, 70, 72) recirculates oil so that it does not leak into the air chamber (48).
申请公布号 EP1375941(A1) 申请公布日期 2004.01.02
申请号 EP20030291198 申请日期 2003.05.21
申请人 SNECMA MOTEURS 发明人 DUSSERRE-TELMON, GUY;PLONA, DANIEL
分类号 F16C19/06;F16C19/26;F16C19/36;F16C27/04;F16C33/66 主分类号 F16C19/06
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