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The present invention provides a method and apparatus for balancing the pressure across a front bearing in a compressor housing. The present invention may protect the bearing from lubricant migration by eliminating pressure differentials across the bearing. When a blower or fan is running, the beari

The present invention provides a method and apparatus for balancing the pressure across a front bearing in a compressor housing. The present invention may protect the bearing from lubricant migration by eliminating pressure differentials across the bearing. When a blower or fan is running, the bearing experiences the same pressure differential that is across the blower. Unless this pressure is balanced, lubricant may migrate from the bearing very quickly. The present invention may provide a pressure balance and sealing across the front bearing of a blower or fan. A plurality of grooves on the face of a compressor impeller and a plurality of grooves on a compressor shaft surface restrict the gas flow to balance pressure across a bearing. Alternatively, a labyrinth seal may cooperate with a plurality of grooves on the face of a compressor impeller to balance pressure across the bearing.

대표청구항 ▼

1. An apparatus for balancing a pressure differential across a bearing, comprising:an impeller for producing a high pressure in a fluid, said impeller being mounted on a shaft;the impeller having an upstream side and a downstream side;a bearing housing on the downstream side of the impeller;the bear

1. An apparatus for balancing a pressure differential across a bearing, comprising:an impeller for producing a high pressure in a fluid, said impeller being mounted on a shaft;the impeller having an upstream side and a downstream side;a bearing housing on the downstream side of the impeller;the bearing housing having an upstream side and a downstream side; anda plurality of annular grooves on the downstream side of the impeller;the plurality of annular grooves concentrically situated in relation to the shaft to control a flow of the high pressure fluid across the downstream side of the impeller.2. The apparatus of claim 1, wherein the shaft has a plurality of grooves on the shaft surface, the grooves being axially situated in relation to the shaft to control a flow of the high pressure fluid in a downstream direction.3. The apparatus of claim 1, wherein a labyrinth seal is situated on the downstream side of the bearing housing with a seal gap that controls flow of the high pressure fluid in a downstream direction.4. An apparatus for balancing a pressure differential across a bearing, comprising:an impeller on a shaft;the impeller having an upstream side and a downstream side;a bearing housing on the downstream side of the impeller;a plurality of annular grooves on the downstream side of the impeller;the plurality of annular grooves concentrically situated in relation to the shaft;the shaft having a cylindrical outer surface; anda plurality of grooves on the shaft;a fluid channel housing situated downstream from the bearing housing; anda fluid channel traveling through the fluid channel housing.5. The apparatus of claim 4, wherein a base of the fluid channel housing is situated just above the outer surface of the shaft.6. The apparatus of claim 4 wherein the plurality of grooves on the shaft are axially situated in relation to the shaft.7. The apparatus of claim 6 wherein the plurality of grooves on the shaft comprises three grooves.8. The apparatus of claim 6 wherein the plurality of annular grooves on the downstream side of the impeller comprises three grooves.9. An apparatus for balancing a pressure differential across a bearing, comprising:an impeller on a shaft;the impeller having an upstream side and a downstream side;a bearing housing on the downstream side of the impeller;a plurality of annular grooves on the downstream side of the impeller;the plurality of annular grooves concentrically situated in relation to the shaft; anda labyrinth seal situated downstream from the bearing housing;the labyrinth seal being positioned around the shaft with a seal gap adjacent the shaft, the gap being sufficient in size to permit flow of pressure balancing fluid therethrough.10. The apparatus of claim 9, wherein the labyrinth seal includes a plurality of discs.11. The apparatus of claim 9, wherein the plurality of annular grooves on the downstream side of the impeller comprises three grooves.12. The apparatus of claim 9, wherein the shaft comprises aluminum.13. The apparatus of claim 9, wherein the impeller comprises aluminum.14. An apparatus for balancing a pressure differential across a bearing, comprising:an impeller on a shaft;the impeller having an upstream side and a downstream side;a bearing housing on the downstream side of the impeller;a plurality of annular grooves on the downstream side of the impeller;the plurality of annular grooves concentrically situated in relation to the shaft; anda labyrinth seal situated downstream from the bearing housing;the labyrinth seal including a plurality of discsa fluid channel housing situated downstream from the bearing housing; anda fluid channel traveling through the fluid channel housing.15. The apparatus of claim 14, wherein a base of the fluid channel housing is situated just above the outer surface of the shaft.16. The apparatus of claim 14 wherein the labyrinth seal is positioned around the shaft with a seal gap adjacent the shaft, the gap being sufficient in size to permit flow of pressure balancing fluid therethrough.17. The apparatus of claim 16 wherein the labyrinth seal includes a plurality of discs.18. The apparatus of claim 16 wherein the plurality of annular grooves on the downstream side of the impeller comprises three grooves.19. The apparatus of claim 16 wherein the shaft comprises aluminum.20. The apparatus of claim 16 wherein the impeller comprises aluminum.21. A die cast aluminum compressor housing, comprising:an impeller on a shaft; the shaft within a bore in a compressor housing;the impeller having an upstream side and a downstream side;a bearing housing on the downstream side of the impeller;a plurality of annular grooves on the downstream side of the impeller;the plurality of annular grooves concentrically situated in relation to the shaft;the shaft having a cylindrical outer surface;a plurality of grooves on the cylindrical outer surface of the shaft;a fluid channel housing situated downstream from the bearing housing; anda fluid channel traveling through the fluid channel housing.22. The apparatus of claim 21, wherein a base of the fluid channel housing is situated just above the outer surface of the shaft.23. The die cast aluminum compressor housing of claim 21, wherein the plurality of annular grooves on the downstream side of the impeller comprises three grooves.24. The die cast aluminum compressor housing of claim 21, wherein the shaft comprises aluminum.25. The apparatus of claim 21, wherein the plurality of grooves on the cylindrical outer surface of the shaft comprises three grooves.26. A method of balancing pressure within a compressor housing, comprising:providing annular grooves on an impeller on a downstream side of the impeller to produce aerodynamic resistance to a flow of a compressed gas;rotating the impeller with a shaft;positioning a bearing housing around the outer circumference of the shaft and downstream from the impeller; anddirecting the aerodynamically resisted flow of the compressed gas to a downstream side of the bearing housing thereby counteracting a pressure differential across the bearing housing.27. The method of claim 26, which includes the further step of providing the shaft with a plurality of grooves.28. A method of balancing pressure within a compressor housing, comprising:providing annular grooves on an impeller;using a shaft to rotate the impeller;positioning a bearing housing around the outer circumference of the shaft and downstream from the impeller;positioning a labyrinth seal downstream from the bearing housing with a seal gap relative to the shaft; anddirecting the aerodynamically resisted flow of the compressed gas to a downstream side of the bearing housing and through the seal gap thereby counteracting a pressure differential across the bearing housing.29. The method of claim 28, wherein the plurality of annular grooves are on the downstream side of the impeller.30. The method of claim 28, wherein the labyrinth seal comprises a plurality of discs.31. The method of claim 30, wherein the plurality of discs comprises four discs.32. A method of compressing a gas without causing bearing lubricant leak, comprising:flowing a compressed gas into a compressor housing;applying aerodynamic resistance to the compressed gas; anddirecting the compressed gas around a bearing to expose an upstream and a downstream side of the bearing to the compressed gas to preclude flow of the compressed gas through the bearing.