Self-aligning sealing assembly for a rotating shaft

• US 6,145,844 A
• Filed: 05/13/1998
• Issued: 11/14/2000
• Est. Priority Date: 05/13/1998
• Status: Expired due to Term

• Current Assignee: Dresser-Rand Company (Siemens AG)
• Original Assignee: Dresser-Rand Company (Siemens AG)
• Inventors: Waggott, John
• Primary Examiner(s): Knight, Anthony
• Assistant Examiner(s): Beres, John L.
• Application Number:
  US09/078,092
• Time in Patent Office: 916 Days
• Field of Search: 277/411, 277/412, 277/413, 277/416, 277/421, 277/422, 277/580, 277/581, 415/174.5
• US Class Current: 277/412
• CPC Class Codes: F01D 11/025 Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
• CPC Class Codes: F16J 15/442 segmented
• CPC Class Codes: F16J 15/445 with means for adjusting the clearance

Abstract

A self-aligning, sealing assembly in accordance with the present invention includes a sealing apparatus and at least one preloading device. The sealing assembly is mounted in machinery which has a rotating shaft and a stationary member with an inner surface which is spaced from and surrounds a shaft. A slot is located in and extends around the inner surface of the stationary member. The slot has an upstream surface, a downstream surface, and an outer surface. The sealing apparatus is adjustably disposed in the slot and has an inner surface, an outer surface, an upstream surface and a downstream surface. Labyrinth seal teeth extend radially inward from the inner surface of the sealing apparatus. Each tooth is radially spaced from the shaft to form a non-contact seal. A space between the outer surface of the ring and the inner surface of the slot is designed to accommodate radial movement of the ring resulting from radial movement of the shaft. The preloading device has first and second ends, with the first end abutting the upstream surface of the slot and the second end abutting an opposing surface of the sealing apparatus. The preloading device ensures sufficient frictional forces between the ring and the slot to support the weight of the sealing apparatus when an insufficient pressure difference exists.

Claims

1. A sealing structure for a shaft, the shaft extending along and rotating about a central axis, a stationary member having an inner surface which is spaced from and surrounds the shaft, and a slot located in and extending around the inner surface of the member, the slot having an outer surface, an upstream surface, and a downstream surface, the structure comprising:

a sealing apparatus being disposed in the slot, the sealing apparatus having an inner surface, an outer surface, an upstream surface and a downstream surface;

a space between the outer surface of the sealing apparatus and the outer surface of the slot to accommodate radial movement of the sealing apparatus, the space extending all around the outer surface of the sealing apparatus; and

one or more preloading devices, each of the preloading devices applying a force in a substantially axial direction between the upstream surface and the downstream surface of the slot to support the weight of the sealing apparatus.

2. The sealing structure according to claim 1 further comprising one or more labyrinth seal teeth which extend radially inward from the inner surface of the sealing apparatus each of the teeth being radially spaced from the shaft to form a non-contact seal.

3. The sealing structure according to claim 2 further comprising at least one broad bearing surface which extends radially inward from the inner surface of the sealing apparatus, the bearing surface being radially spaced from the shaft and having an axial width larger than any of the labyrinth seal teeth.

4. The sealing structure according to claim 1 further comprising a protrusion extending from the downstream surface of the sealing apparatus or the downstream surface of the slot.

5. The sealing structure according to claim 1 wherein each of the preloading device comprises a spring located in a hole in the sealing apparatus, the spring having a first and second end with the first end of the spring abutting the upstream surface of the slot through an opening in the sealing apparatus and the second end abutting the opposing surface of the sealing apparatus.

6. The sealing structure according to claim 1 wherein the force exerted by the preloading devices is about five times the weight of the sealing apparatus.

7. The sealing structure according to claim 1 wherein the sealing apparatus is split in half and is held together by at least one securing and aligning device.

8. The sealing structure according to claim 7 wherein the securing and aligning device comprises:

an opening extending between each end of each of the halves of the sealing apparatus, one end of each opening being threaded;

a bushing located in each opening to align the halves of the sealing apparatus; and

a screw mountable in each opening, the screw extending through the bushing and having threads for engaging with the threads in the opening to secure the halves of the sealing apparatus together.

19. The sealing structure as set forth in claim 1 wherein the upstream surface of the slot extends in a direction substantially along a plane which intersects with the central axis.

20. The sealing structure as set forth in claim 1 wherein the sealing apparatus comprises one piece which moves within the slot.

9. A turbine with a self-aligning sealing assembly, the turbine comprising:

a shaft which extends along and rotates about a central axis;

a housing which surrounds at least a portion of the shaft;

at least one pressure boundary penetrated by the shaft, the pressure boundary having an inner surface which is spaced from and surrounds the shaft;

a slot located in and extending around the circumference of the inner surface of the pressure boundary, the slot having an outer surface, an upstream surface, and a downstream surface;

a sealing apparatus being disposed in the slot, the sealing apparatus having an inner surface, an outer surface, an upstream surface and a downstream surface;

one or more labyrinth seal teeth which extend radially inward from the inner surface of the sealing apparatus, each of the teeth spaced from the shaft to form a plurality of non-contact seals;

space between the outer surface of the sealing apparatus and the outer surface of the slot to accommodate radial movement of the sealing apparatus, the space extending all around the outer surface of the sealing apparatus; and

one or more preloading devices, each of the preloading devices applying a force in a substantially axial direction between the upstream surface and the downstream surface of the slot to support the weight of the sealing apparatus.

10. The turbine according to claim 9 further comprising at least one broad bearing surface which extends radially inward from the inner surface of the sealing apparatus, the broad bearing surface being radially spaced from the shaft and having an axial width sufficient to reduce abrasion when the rotating shaft contacts it.

11. The turbine according to claim 10 wherein the preloading device comprises a spring located in a hole in the sealing apparatus, the spring having a first and second end, with end of the spring abutting the upstream surface of the slot through an opening the first in the sealing apparatus and the second end abutting the opposing surface of the sealing apparatus.

12. The turbine according to claim 9 further comprising a protrusion extending from the downstream surface of the sealing apparatus or the downstream surface of the slot.

13. The turbine according to claim 9 wherein the force exerted by the preloading devices is about five times the weight of the sealing apparatus.

14. The turbine according to claim 10 wherein the sealing apparatus is split in half and is held together by at least one securing and aligning device.

15. The turbine according to claim 14 wherein the securing and aligning device comprises:

an opening extending between each end of each of the halves of the sealing apparatus, one end of each opening being threaded;

a bushing located in each opening to align the halves of the sealing apparatus; and

a screw mountable in each opening, the screw extending through the bushing and having threads for engaging with the threads in the opening to secure the halves of the sealing apparatus together.

21. The turbine as set forth in claim 9 wherein the upstream surface of the slot extend in a direction substantially along a plane which intersects with the central axis.

22. The turbine as set forth in claim 9 wherein the sealing apparatus comprises one piece which moves within the slot.

16. A turbine with a sealing structure, the turbine comprising:

a shaft which extends along and rotates about a central axis;

a housing which surrounds at least a portion of the shaft;

at least one pressure boundary penetrated by the shaft, the pressure boundary having an inner surface which surrounds the shaft;

a slot located in and extending around the circumference of the inner surface of the pressure boundary, the slot having an outer surface, an upstream surface, and a downstream surface;

a non-contact sealing member disposed in the slot, the non-contact sealing member having an inner surface, an outer surface, an upstream surface and a downstream surface;

one or more labyrinth seal teeth which extend radially inward from the inner surface of the non-contact sealing member each of the teeth spaced from the shaft to form a plurality of non-contact seals;

at least one broad bearing surface which extends radially inward from the inner surface of the sealing member, the broad bearing surface being radially spaced from the shaft and having an axial width larger than any of the labyrinth seal teeth;

a space between the outer surface of the non-contact sealing member and the outer surface of the slot to accommodate radial movement of the non-contact sealing member resulting from radial movement of the shaft, the space extending all around the outer surface of the sealing apparatus; and

one or more preloading devices applying a force in a substantially axial direction between the upstream surface and the downstream surface of the slot to support the weight of the sealing member.

17. The turbine according to claim 16 wherein each of the preloading devices comprise a spring located in a hole in the sealing apparatus, the spring having a first and second end, with the first end of the spring abutting the upstream surface of the slot through an opening in the sealing apparatus and the second end abutting the opposing surface of the non-contact sealing member.

18. The turbine according to claim 17 wherein the force exerted by the preloading devices is about five times the weight of the non-contact sealing member.

23. The turbine as set forth in claim 16 wherein the upstream surface of the slot extends in a direction substantially along a plane which intersects with the central axis.

24. The turbine as set forth in claim 16 wherein the sealing apparatus comprises one piece which moves within the slot.