Swirl control labyrinth seal

• US 5,190,440 A
• Filed: 03/11/1991
• Issued: 03/02/1993
• Est. Priority Date: 03/11/1991
• Status: Expired due to Fees

• Current Assignee: DRESSER-RAND COMPANY, CORNING, NY, A GENERAL PARTNERSHIP OF NY
• Original Assignee: Dresser-Rand Group Incorporated (Siemens AG)
• Inventors: Maier, Martin D., Osborne, Colin
• Primary Examiner(s): KWON, JOHN
• Application Number:
  US07/667,768
• Time in Patent Office: 722 Days
• Field of Search: 415/170.1, 415/172.1, 415/174.5, 277/53.75, 277/70, 277/3, 277/27
• US Class Current: 415/174.5
• CPC Class Codes: F01D 11/02 by non-contact sealings, e.g. of labyrinth type for sealing space between rotor blade tips and stator F01D11/08
• CPC Class Codes: F04D 29/162 of a centrifugal flow wheel
• CPC Class Codes: F04D 29/667 by influencing the flow pattern, e.g. suppression of turbulence
• CPC Class Codes: F05D 2210/42 Axial inlet and radial outlet
• CPC Class Codes: F16J 15/164 the sealing action depending on movements; pressure difference, temperature or presence of leaking fluid

Abstract

A labyrinth seal which reduces the inlet swirl and circumferential flow of fluid within the sealing cavity of a rotating shaft system in order to eliminate the destabilizing influence of the labyrinth seal, has a plurality of primary flow bypass passageways which extend from the high pressure face of the seal to the space between a first set and a second set of labyrinth teeth. The plurality of primary flow bypass passageways are equally spaced around the circumference of the seal and are preferably inclined such that the fluid is introduced into the seal cavity at a desired orientation. Each of the primary flow bypass passageways can be a passageway which is inclined at an acute angle to the shaft axis or a combination of an axial passageway and a radial passageway. The primary flow bypass passageways can be in the form of a plurality of generally radial passageways which intersect a common annular opening in the high pressure face of the seal. Also, multiple sets of secondary flow bypass passageways can be positioned at predetermined locations downstream from the first set of passages to function in a similar manner. Annular grooves can be provided in the outer surface of the seal to connect each adjacent set of secondary flow bypass passageways which straddle a set of labyrinth teeth.

Claims

1. An apparatus comprising a housing, a rotatable shaft positioned in said housing, a low pressure chamber in said housing for containing a fluid at a low pressure, a high pressure chamber in said housing for containing said fluid at a high pressure, said rotatable shaft constituting a rotatable element, an annular labyrinth seal element positioned coaxially with said rotatable shaft and between a rotatable element and said housing, said annular labyrinth seal element having a plurality of annular teeth facing a radially adjacent surface, said annular labyrinth seal element having a first annular end exposed to said high pressure chamber and a second annular end exposed to said low pressure chamber, said annular teeth being spaced along the longitudinal length of the annular labyrinth seal element between said first and second annular ends, said annular teeth extending radially into sealing relationship with said radially adjacent surface such that a portion of said fluid passes from said high pressure chamber at said first annular end through the annular space between said annular teeth and said radially adjacent surface to said low pressure chamber at said second annular end with the rotation of said rotatable shaft tending to cause a circumferential flow of said portion of said fluid as said portion of said fluid passes through said annular space, a first plurality of flow bypass passageways, each of said first plurality of flow bypass passageways being stationary and extending from a predetermined opening in said high pressure chamber to a respective one of a first plurality of openings located in an annular chamber formed between a predetermined adjacent pair of said annular teeth, said first plurality of openings being spaced at least substantially uniformly about the circumference of said annular chamber, wherein the flow resistance from said high pressure chamber through said first plurality of flow bypass passageways to said annular chamber is substantially less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber, thereby reducing the circumferential flow of said portion of said fluid passing from said high pressure chamber through said annular space to said low pressure chamber.

2. An apparatus in accordance with claim 1, wherein said predetermined opening in said high pressure chamber comprises a second plurality of openings in said first annular end which are spaced at least substantially uniformly in a circular array, corresponding in number to said first plurality of flow bypass passageways, each of said first plurality of flow bypass passageways having a first portion extending at least generally parallel to the longitudinal axis of said rotatable shaft to intersect a respective one of said second plurality of openings and having a second portion extending from a respective one of said first plurality of openings in said annular chamber at least generally outwardly with respect to said rotatable shaft to intersect the associated first portion.

3. An apparatus in accordance with claim 2, wherein said housing has a fluid inlet and a fluid outlet, wherein at least one centrifugal fluid impeller is secured to said rotatable shaft for rotation therewith about the longitudinal axis of said rotatable shaft and for reaction with fluid passing from said fluid inlet to said fluid outlet such that said fluid exists at said low pressure in said low pressure chamber and at said low pressure in said low pressure chamber and at said high pressure in said high pressure chamber, wherein said impeller has an impeller cover secured to said impeller for rotation therewith, wherein each of said impeller and said impeller cover constitutes a rotatable element, wherein said annular labyrinth seal element is secured to said housing, and wherein said radially adjacent surface comprises an annular portion of a circumferentially extending outer surface of one of said impeller and said impeller cover.

4. An apparatus in accordance with claim 2, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface comprises an annular portion of a circumferentially extending outer surface of said rotatable shaft.

5. An apparatus in accordance with claim 2, further comprising an annular rotatable element positioned coaxially on said rotatable shaft for rotation therewith about said longitudinal axis of said rotatable shaft, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface is an annular portion of a circumferentially extending outer surface of said annular rotatable element.

6. An apparatus in accordance with claim 5 wherein said annular rotatable element is a balance piston.

7. An apparatus in accordance with claim 2 wherein said predetermined adjacent pair of said annular teeth includes the one of said annular teeth which is closest to said first annular end.

15. An apparatus in accordance with claim 1, wherein said predetermined opening in said high pressure chamber comprises an annular slot formed in said first annular end and extending at least substantially coaxially with respect to said rotatable shaft, and wherein each of said first plurality of flow bypass passageways extends at least generally outwardly from said annular chamber with respect to said rotatable shaft to intersect said annular slot.

16. An apparatus in accordance with claim 15, wherein said housing has a fluid inlet and a fluid outlet, wherein at least one centrifugal fluid impeller is secured to said rotatable shaft for rotation therewith about the longitudinal axis of said rotatable shaft and for reaction with fluid passing from said fluid inlet to said fluid outlet such that said fluid exists at said low pressure in said low pressure chamber, wherein said impeller has an impeller cover secured to said impeller for rotation therewith, wherein said of said impeller and said impeller cover constitutes a rotatable element, wherein said annular labyrinth seal element is secured to said housing, and wherein said radially adjacent surface comprises an annular portion of a circumferentially extending outer surface of one of said impeller and said impeller cover.

17. An apparatus in accordance with claim 15, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface comprises an annular portion of a circumferentially extending outer surface of said rotatable shaft.

18. An apparatus in accordance with claim 15, further comprising an annular rotatable element positioned coaxially on said rotatable shaft for rotation therewith about said longitudinal axis of said rotatable shaft, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface is an annular portion of a circumferentially extending outer surface of said annular rotatable element.

19. An apparatus in accordance with claim 18 wherein said annular rotatable element is a balance piston.

20. An apparatus in accordance with claim 15 wherein said predetermined adjacent pair of said annular teeth includes the one of said annular teeth which is closest to said first annular end.

28. An apparatus in accordance with claim 1, wherein said predetermined opening in said high pressure chamber comprises an annular groove formed in said first annular end around the circumference of the labyrinth seal element and extending at least substantially coaxially with respect to said rotatable element and wherein each of said flow bypass passageways extends at least generally outwardly from said annular chamber with respect to said rotatable shaft to intersect said annular groove.

29. An apparatus in accordance with claim 28, wherein said housing has a fluid inlet and a fluid outlet, wherein at least one centrifugal fluid impeller is secured to said rotatable shaft for rotation therewith about the longitudinal axis of said rotatable shaft and for reaction with fluid passing from said fluid inlet to said fluid outlet such that said fluid exists at said low pressure in said low pressure chamber, wherein said impeller has an impeller cover secured to said impeller for rotation therewith, wherein each of said impeller and said impeller cover constitutes a rotatable element, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface comprises an annular portion of a circumferentially extending outer surface of one of said impeller and said impeller cover.

30. An apparatus in accordance with claim 28 wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface comprises an annular portion of the circumferentially extending outer surface of said rotatable shaft.

31. An apparatus in accordance with claim 28, further comprising an annular rotatable element positioned coaxially on said rotatable shaft for rotation therewith about said longitudinal axis of said rotatable shaft, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface is an annular portion of a circumferentially extending outer surface of said annular rotatable element.

32. An apparatus in accordance with claim 31 wherein said annular rotatable element is a balance piston.

33. An apparatus in accordance with claim 28 wherein said predetermined adjacent pair of said annular teeth includes the one of said annular teeth which is closest to said first annular end.

43. An apparatus in accordance with claim 1 wherein each of said first plurality of flow bypass passageways is at least substantially a cylindrical bore extending from said first annular end to said annular chamber at an acute angle to the longitudinal axis of said rotatable element.

44. An apparatus in accordance with claim 43, wherein said housing has a fluid inlet and a fluid outlet, wherein at least one centrifugal fluid impeller is secured to said rotatable shaft for rotatable therewith about the longitudinal axis of said rotatable shaft and for reaction with fluid passing from said fluid inlet to said fluid outlet such that said fluid exists at said low pressure in said low pressure chamber and at said high pressure in said high pressure chamber, wherein said impeller has an impeller cover secured to said impeller for rotation therewith, wherein each of said impeller and said impeller cover constitutes a rotatable element, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface comprises an annular portion of a circumferentially extending outer surface of one of said impeller and said impeller cover.

45. An apparatus in accordance with claim 43, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface comprises an annular portion of a circumferentially extending outer surface of said rotatable shaft.

46. An apparatus in accordance with claim 43, further comprising an annular rotatable element positioned coaxially on said rotatable shaft for rotation therewith about said longitudinal axis of said rotatable shaft, wherein said annular labyrinth seal element is secured to said housing, wherein said first plurality of flow bypass passageways are located in said annular labyrinth seal element, and wherein said radially adjacent surface is an annular portion of a circumferentially extending outer surface of said annular rotatable element.

47. An apparatus in accordance with claim 46 wherein said annular rotatable element is a balance piston.

48. An apparatus in accordance with claim 43 wherein said predetermined adjacent pair of said annular teeth includes the one of said annular teeth which is closest to said first annular end.

8. An apparatus comprising a housing, a rotatable shaft positioned in said housing, a low pressure chamber in said housing for containing a fluid at a low pressure, a high pressure chamber in said housing for containing said fluid at a high pressure, said rotatable shaft constituting a rotatable element, an annular labyrinth seal element positioned coaxially with said rotatable shaft and between a rotatable element and said housing, said annular labyrinth seal element having a plurality of annular teeth facing a radially adjacent surface, said annular labyrinth seal element having a first annular end exposed to said high pressure chamber and a second annular end exposed to said low pressure chamber, said annular teeth being spaced along the longitudinal length of said annular labyrinth seal element between said first and second annular ends, said annular teeth extending radially into sealing relationship with said radially adjacent surface such that a portion of said fluid passes from said high pressure chamber at said first annular end through the annular space between said annular teeth and said radially adjacent surface to said low pressure chamber at said second annular end with the rotation of said rotatable shaft tending to cause a circumferential flow of said portion of said fluid as said portion of said fluid passes through said annular space, a first plurality of flow bypass passageways being stationary and extending from a predetermined opening in said high pressure chamber to a respective one of a first plurality of openings located in an annular chamber formed between a predetermined adjacent pair of said annular teeth, said first plurality of openings being spaced at least substantially uniformly about the circumference of said annular chamber, wherein the flow resistance from said high pressure chamber through said first plurality of flow bypass passageways to said annular chamber is substantially less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber, thereby reducing the circumferential flow of said portion of said fluid passing from said high pressure chamber through said annular space to said low pressure chamber, wherein said predetermined opening in said high pressure chamber comprises a second plurality of openings in said first annular end which are spaced at least substantially uniformly in a circular array, corresponding in number to said first plurality of flow bypass passageways, each of said first plurality of flow bypass passageways having a first portion extending at least generally parallel to the longitudinal axis of said rotatable shaft to intersect a respective one of said second plurality of openings and having a second portion extending from a respective one of said first plurality of openings in said annular chamber at least generally outwardly with respect to said rotatable shaft to intersect the associated first portion, wherein said second portion of each of said first plurality of flow bypass passageways is inclined with respect to a reference line at an angle of inclination such that fluid enters said annular chamber from the respective one of said first plurality of flow bypass passageways in a direction opposite to the rotation of said rotatable shaft, said reference line being radial to said rotatable shaft.

9. An apparatus in accordance with claim 8 wherein said angle of inclination is about 60°

.

10. An apparatus in accordance with claim 8 wherein each said second portion extends in a plane which is at least generally perpendicular to the longitudinal axis of said rotatable shaft.

11. An apparatus in accordance with claim 8 wherein the flow resistance from said first annular end through said first plurality of flow bypass passageways to said annular chamber is at least an order of magnitude less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber.

12. An apparatus in accordance with claim 8 wherein said predetermined adjacent pair of said annular teeth includes the one of said annular teeth which is closest to said first annular end.

13. An apparatus in accordance with claim 8 wherein said angle of inclination is in the range of about 0°

to about 90°

.

14. An apparatus in accordance with claim 13 wherein each said second portion extends in a plane which is at least generally perpendicular to the longitudinal axis of said rotatable shaft.

21. An apparatus comprising a housing, a rotatable shaft positioned in said housing, a low pressure chamber in said housing for containing a fluid at a low pressure, a high pressure chamber in said housing for containing said fluid at a high pressure, said rotatable shaft constituting a rotatable element, an annular labyrinth seal element positioned coaxially with said rotatable shaft and between a rotatable element and said housing, said annular labyrinth seal element having a plurality of annular teeth facing a radially adjacent surface, said annular labyrinth seal element having a first annular end exposed to said high pressure chamber and a second annular end exposed to said low pressure chamber, said annular teeth being spaced along the longitudinal length of said annular labyrinth seal element between said first and second annular ends, said annular teeth extending radially into sealing relationship with said radially adjacent surface such that a portion of said fluid passes from said high pressure chamber at said first annular end through the annular space between said annular teeth and said radially adjacent surface to said low pressure chamber at said second annular end with the rotation of said rotatable shaft tending to cause a circumferential flow of said portion of said fluid as said portion of said fluid passes through said annular space, a first plurality of flow bypass passageways, each of said first plurality of flow bypass passageways being stationary and extending from a predetermined opening in said high pressure chamber to a respective one of a first plurality of openings located in an annular chamber formed between a predetermined adjacent pair of said annular teeth, said first plurality of openings being spaced at least substantially uniformly about the circumference of said annular chamber, wherein the flow resistance from said high pressure chamber through said first plurality of flow bypass passageways to said annular chamber is substantially less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber, thereby reducing the circumferential flow of said portion of said fluid passing from said high pressure chamber through said annular space to said low pressure chamber, wherein said predetermined opening in said high pressure chamber comprises an annular slot formed in said first annular end and extending at least substantially coaxially with respect to said rotatable shaft, and wherein each of said first plurality of flow bypass passageways extends at least generally outwardly from said annular chamber with respect to said rotatable shaft to intersect said annular slot, wherein each of said first plurality of flow bypass passageways is inclined with respect to a reference line at an angle of inclination such that fluid enters said annular chamber from the respective one of said first plurality of flow bypass passageways in a direction opposite to the rotation of said rotatable shaft, said reference line being radial to said rotatable shaft.

22. An apparatus in accordance with claim 21 wherein said angle of inclination is about 60°

.

23. An apparatus in accordance with claim 21 wherein the flow resistance from said first annular end through said first plurality of flow bypass passageways to said annular chamber is at least an order of magnitude less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber.

24. An apparatus in accordance with claim 21 wherein said annular slot is oriented generally perpendicular to said first annular end.

25. An apparatus in accordance with claim 21 wherein said predetermined adjacent pair of said annular teeth includes the one of said annular teeth which is closest to said first annular end.

26. An apparatus in accordance with claim 21 wherein said angle of inclination is in the range of about 0°

to about 90°

.

27. An apparatus in accordance with claim 26 wherein each of said first plurality of flow bypass passageways extends in a plane which is at least generally perpendicular to the longitudinal axis of said rotatable shaft.

34. An apparatus comprising a housing, a rotatable shaft positioned in said housing, a low pressure chamber in said housing for containing a fluid at a low pressure, a high pressure chamber in said housing for containing said fluid at a high pressure, said rotatable shaft constituting a rotatable element, an annular labyrinth seal element positioned coaxially with said rotatable shaft and between a rotatable element and said housing, said annular labyrinth seal element having a plurality of annular teeth facing a radially adjacent surface, said annular labyrinth seal element having a first annular end exposed to said high pressure chamber and a second annular end exposed to said low pressure chamber, said annular teeth being spaced along the longitudinal length of said annular labyrinth seal element between said first and second annular ends, said annular teeth extending radially into sealing relationship with said radially adjacent surface such that a portion of said fluid passes from said high pressure chamber at said first annular end through the annular space between said annular teeth and said radially adjacent surface to said low pressure chamber at said second annular end with the rotation of said rotatable shaft tending to cause a circumferential flow of said portion of said fluid as said portion of said fluid passes through said annular space, a first plurality of flow bypass passageways, each of said first plurality of flow bypass passageways being stationary and extending from a predetermined opening in said high pressure chamber to a respective one of a first plurality of openings located in an annular chamber formed between a predetermined adjacent pair of said annular teeth, said first plurality of openings being spaced at least substantially uniformly about the circumference of said annular chamber, wherein the flow resistance from said high pressure chamber through said first plurality of flow bypass passageways to said annular chamber is substantially less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber, thereby reducing the circumferential flow of said portion of said fluid passing from said high pressure chamber through said annular space to said low pressure chamber, wherein said predetermined opening in said high pressure chamber comprises an annular groove formed in said first annular end around the circumference of the labyrinth seal element and extending at least substantially coaxially with respect to said rotatable element and wherein each of said flow bypass passageways extends at least generally outwardly from said annular chamber with respect to said rotatable shaft to intersect said annular groove, wherein each of said first plurality of flow bypass passageways is inclined with respect to a reference line at an angle of inclination such that fluid enters said annular chamber from the respective one of said first plurality of flow bypass passageways in a direction opposite to the rotation of said rotatable shaft, said reference line being radial to said rotatable shaft.

35. An apparatus in accordance with claim 34 wherein said angle of inclination is about 60°

.

36. An apparatus in accordance with claim 34 wherein each of said first plurality of flow bypass passageways extends in a plane which is at least generally perpendicular to the longitudinal axis of said rotatable shaft, wherein said angle of inclination is in the range of about 0°

to about 90°

, and wherein said annular groove is oriented generally perpendicular to said first annular end.

37. An apparatus in accordance with claim 34 wherein each of said first plurality of flow bypass passageways extends in a plane which is at least generally perpendicular to the longitudinal axis of said rotatable shaft.

38. An apparatus in accordance with claim 37 wherein the flow resistance from said first annular end through said first plurality of flow bypass passageways to said annular chamber is at least an order of magnitude less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber.

39. An apparatus in accordance with claim 34 wherein said annular groove is oriented generally perpendicularly to said first annular end.

40. An apparatus in accordance with claim 34 wherein the end of each said flow bypass passageway which communicates with said annular groove is flared to reduce resistance to the flow of fluid therethrough.

41. An apparatus in accordance with claim 34 wherein said angle of inclination is in the range of about 0°

to about 90°

.

42. An apparatus in accordance with claim 41 wherein each of said first plurality of flow bypass passageways extends in a plane which is at least generally perpendicular to the longitudinal axis of said rotatable shaft.

49. An apparatus comprising a housing, a rotatable shaft positioned in said housing, a low pressure chamber in said housing for containing a fluid at a low pressure, a high pressure chamber in said housing for containing said fluid at a high pressure, said rotatable shaft constituting a rotatable element, an annular labyrinth seal element positioned coaxially with said rotatable shaft and between a rotatable element and said housing, said annular labyrinth seal element having a plurality of annular teeth facing a radially adjacent surface, said annular labyrinth seal element having a first annular end exposed to said high pressure chamber and a second annular end exposed to said low pressure chamber, said annular teeth being spaced along the longitudinal length of said annular labyrinth seal element between said first and second annular ends, said annular teeth extending radially into sealing relationship with said radially adjacent surface such that a portion of said fluid passes from said high pressure chamber at said first annular end through the annular space between said annular teeth and said radially adjacent surface to said low pressure chamber at said second annular end with the rotation of said rotatable shaft tending to cause a circumferential flow of said portion of said fluid as said portion of said fluid passes through said annular space, a first plurality of flow bypass passageways, being stationary and extending from a predetermined opening in said high pressure chamber to a respective one of a first plurality of openings located in an annular chamber formed between a predetermined adjacent pair of said annular teeth, said first plurality of openings being spaced at least substantially uniformly about the circumference of said annular chamber, wherein the flow resistance from said high pressure chamber through said first plurality of flow bypass passageways to said annular chamber is substantially less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber, thereby reducing the circumferential flow of said portion of said fluid passing from said high pressure chamber through said annular space to said low pressure chamber, wherein each of said first plurality of flow bypass passageways is at least substantially a cylindrical bore extending from said first annular end to said annular chamber at an acute angle to the longitudinal axis of said rotatable element, wherein each of said first plurality of flow bypass passageways is inclined with respect to a reference line at an angle of inclination such that fluid enters said annular chamber from the respective one of said first plurality of flow bypass passageways in a direction opposite to the rotation of said rotatable shaft, said reference line being radial to said rotatable shaft.

50. An apparatus in accordance with claim 49 wherein said angle of inclination is about 60°

.

51. An apparatus in accordance with claim 49 wherein the flow resistance from said first annular end through said first plurality of flow bypass passageways to said annular chamber is at least an order of magnitude less than the flow resistance through the portion of said annular space from said first annular end to said annular chamber.

52. An apparatus in accordance with claim 49 wherein said angle of inclination is in the range of about 0°

to about 90°

.

53. An apparatus in accordance with claim 52 wherein said acute angle is about 45°

, and wherein said predetermined adjacent pair of said annular teeth includes the one of said annular teeth which is closest to said first annular end.