Back to results
US 5,489,190 AGranted
Dynamic oil scavenge system
AssigneeAlliedSignal Inc.
InventorJohn D. Sullivan
Life of this patent
Estimating the term…
Abstract
An oil scavenge assembly for small gas turbine engine. The assembly includes a rolling element bearing, for supporting a rotating shaft, slip fit within a bearing liner. The bearing liner has a plurality of helical grooves along its surface. A plurality of circumferentially spaced scoops extend inward from the liner and direct the oil expelled from the bearing into the helical grooves.
Claims1
In a gas turbine engine having:
- a centrifugal compressor having a hub portion extending from a compressor shaft to define an open ended annular channel;
- a gearbox casing circumscribing and radially spaced from a rotating turbine shaft concentric about the axial centerline of said engine, said casing having an axial end portion extending into said annular channel;
- a gear shaft disposed between said casing and said turbine shaft and drivingly coupled to said turbine shaft and said compressor shaft;
- a rolling element bearing disposed adjacent said annular channel and mounted to said gear shaft and having a first axial end receiving a lubricant and a second axial end expelling said lubricant, said bearing including an inner race mounted to said gear shaft, an outer race concentric with said inner race, and a plurality of rolling elements mounted therebetween;
- an annular bearing liner disposed between said casing and said outer race and having a plurality of axially extending, helical grooves along its outer surface;
- and
- a plurality of circumferentially spaced apart. scoops integral with said liner and extending radially inward adjacent said second axial end of said bearing, said scoops defining a plurality of radial passageways each of which curves into one of said helical grooves.
4 more elements
Dependencies are inferred from the claim text.