The oil separator, for the gearing of an aircraft power plant, feeds the oil/air mixture into a rotating unit (1) near the rotating axis (3), where it initially moves outwards. An outer guide wall section (4c) deflects the air flow back towards the rotary axis (3) while the oil passes through passage openings (8) in the guide wall out of the rotating assembly.
申请公布号
DE19704845(A1)
申请公布日期
1998.08.13
申请号
DE19971004845
申请日期
1997.02.08
申请人
BMW ROLLS-ROYCE GMBH, 61440 OBERURSEL, DE
发明人
HASELBAUER, FRANZ, 35516 MUENZENBERG, DE;KOCH, RAFFAEL, 12207 BERLIN, DE