Flow control arrangement
flow control arrangement for controlling the flow of lubricant discharged from a bearing includes a flow control member locatable, in use, adjacent to the bearing. The flow control member defines a generally radially outer edge and is rotatable to direct lubricant discharged onto the flow control member radially outwardly towards the outer edge for ejection therefrom.
1. A flow control arrangement for controlling the flow of lubricant discharged from a bearing, the flow control arrangement comprising:
a flow control member disposed adjacent to the bearing,
the flow control member defining a generally radially outer edge and being rotatable to direct lubricant discharged onto the flow control member radially outwardly towards the outer edge for ejection therefrom, wherein the flow control member includes a generally annular portion and a lip portion extending from an outer edge of the annular portion in a direction towards the bearing to permit ejection of the lubricant.
2. A flow control arrangement according to claim 1 , wherein the flow control member is locatable in use at a position axially spaced from the bearing.
3. A flow control arrangement according to claim 1 , wherein the flow control member includes an orifice to permit the ejection of lubricant from the radially outer edge.
4. A flow control arrangement according to claim 3 , wherein the orifice is arranged to permit the ejection of lubricant from the radially outer edge in a predetermined direction.
5. A flow control arrangement according to claim 3 , wherein the flow control member includes a plurality of said orifices.
6. A flow control arrangement according to claim 1 , wherein the annular portion defines a radial axis, the radial axis being substantially parallel in use to a radial axis of the bearing.
7. A flow control arrangement according to claim 1 , wherein the annular portion defines a radial axis, the radial axis being inclined relative to a radial axis of the bearing such that the annular portion is inclined in use towards the bearing.
8. A flow control arrangement according to claim 1 , wherein the annular portion includes a plurality of said orifices spaced circumferentially around the outer edge thereof to define a circumferential row of orifices.
9. A flow control arrangement according to claim 8 , wherein the annular portion includes a plurality of said circumferential rows of orifices.
10. A flow control arrangement according to claim 9 , wherein said circumferential rows of orifices are spaced radially across the annular portion in proximity to the outer edge thereof.
11. A flow control arrangement according to claim 1 , wherein the lip portion includes a plurality of said orifices spaced circumferentially therearound to define a circumferential row of orifices.
12. A flow control arrangement according to claim 11 , wherein the lip portion includes a plurality of said circumferential rows of orifices.
13. A flow control arrangement according to claim 12 , wherein said circumferential rows of orifices are spaced along the lip portion.
14. A flow control arrangement according to claim 1 , wherein the flow control member is arranged to be mounted in use on a shaft on which the bearing is mounted for rotation by the shaft.
15. A flow control arrangement according to claim 1 , wherein the flow control member is arranged to be mounted in use on an inner ring of the bearing for rotation by the inner ring.
16. A bearing assembly including a bearing mountable in use on a shaft for rotation by the shaft and a flow control arrangement according to claim 1 for controlling the flow of lubricant discharged from the bearing.
17. A gas turbine engine including a flow control arrangement according to claim 1 .