Reduced leakage balance piston seal

Patent metadata

Field	Value
Publication number	US-9279324-B2
Application number	US-201213675368-A
Country	US
Kind code	B2
Filing date	Nov 13, 2012
Priority date	Dec 7, 2011
Publication date	Mar 8, 2016
Grant date	Mar 8, 2016

Abstract

Balance piston assembly, apparatus, and methods are provided. The assembly includes a balance piston coupled to a rotatable shaft and configured to rotate therewith, the balance piston including a first shelf and a second shelf, the first and second shelves being axially-overlapping and radially-offset. The assembly also includes a seal including a first sealing surface configured to seal with the first shelf and a second sealing surface configured to seal with the second shelf.

First claim

We claim:

1. A balance piston assembly, comprising:
a balance piston coupled to a rotatable shaft and configured to rotate therewith, the balance piston including a first shelf and a second shelf, the first and second shelves being axially-overlapping and radially-offset; and
a seal including a first sealing surface configured to seal with the first shelf and a second sealing surface configured to seal with the second shelf,
wherein the seal further includes a third sealing surface disposed radially between the first and second sealing surfaces, and
wherein the first shelf of the balance piston includes a radially-outer surface configured to seal with the first sealing surface and a radially-inner surface configured to seal with the third sealing surface.

2. The balance piston of claim 1 , wherein the seal has a substantially J-shape.

3. The balance piston assembly of claim 1 , wherein the first shelf includes a plurality of teeth configured to seal with the first sealing surface.

4. The balance piston assembly of claim 1 , wherein the seal and the balance piston define a continuous flowpath between the first, second, and third sealing surfaces.

5. The balance piston assembly of claim 1 , wherein at least one of the radially-outer surface and the radially-inner surface includes a plurality of teeth.

6. The balance piston assembly of claim 1 , wherein at least one of the first and second sealing surfaces provides at least part of a damper seal, a honeycomb seal, a hole pattern seal, a labyrinth seal, or a combination thereof.

7. The balance piston assembly of claim 1 , wherein the seal extends axially away from the balance piston and engages a header to at least partially define a cavity therebetween.

8. The balance piston assembly of claim 7 , wherein the seal defines a gas flow port extending therethrough, the gas flow port being configured to fluidly connect an area positioned between the first and second sealing surfaces and the balance piston with a conduit fluidly communicating with the cavity.

9. The balance piston assembly of claim 1 , wherein the seal is segmented into first and second radially-offset, axially-overlapping annular sections, the first section including the first sealing surface and the second section including the second sealing surface.

10. An apparatus for sealing and balancing axial thrust, comprising:
a balance piston coupled to a rotatable shaft and including first and second radially-offset, parallel shelves and first and second axial sides, the first axial side configured to communicate with a higher-pressure area and the second axial side configured to communicate with a lower-pressure area; and
a seal including first and second axially-overlapping, radially-offset sealing surfaces, the first sealing surface sealing with the first shelf of the balance piston and the second sealing surface sealing with the second shelf to reduce migration of gas from the higher-pressure area to the lower-pressure area,
wherein the first shelf includes a radially-outer surface and a radially-inner surface, and the seal includes a third sealing surface disposed radially between the first and second sealing surfaces, the first sealing surface of the seal configured to seal with the radially-outer surface of the first shelf, and the third sealing surface of the seal configured to seal with the radially-inner surface of the first shelf.

11. The apparatus of claim 10 , wherein at least one of the first, second, and third sealing surfaces includes teeth for a labyrinth-type seal, holes for a hole-pattern-type seal, or a combination thereof.

12. The apparatus of claim 10 , wherein the seal is horizontally split, axially split, or both.

13. The apparatus of claim 10 , wherein the seal defines a gas flow port extending therethrough to fluidly communicate an area between the seal and the balance piston with a conduit defined outside of the area.

14. The apparatus of claim 13 , wherein the seal extends away from the balance piston and engages a header and defines a cavity at least partially therewith, the conduit extending from the cavity and the cavity fluidly communicating with the area via the gas flow port.

15. A method for balancing thrust forces along a shaft, comprising:
coupling a seal having first, second, and third radially-offset, axially-overlapping sealing surfaces with a balance piston having first and second shelves, wherein the first and third sealing surfaces align with opposing radial sides of the first shelf, and the second sealing surface aligns with the second shelf, and wherein the balance piston is configured to rotate with the shaft; and
referencing an outboard side of the balance piston to a reduced pressure as compared to a pressure applied to the inboard side of the balance piston.

16. The method of claim 15 , further comprising:
injecting gas into a first cavity defined on an outboard side of the balance piston;
directing the gas past the second and third sealing surfaces and into an area defined between the balance piston and the seal; and
directing process gas past the first sealing surface and into the area.

17. The method of claim 16 , further comprising venting gas from the area to a second cavity defined on the outboard side of the balance piston.

Assignees

• Clute Stephen G
• Kuzdzal Mark J
• Grosso Glenn R
• Peer David J
• Dresser Rand Co

Inventors

• Clute Stephen G
• Kuzdzal Mark J
• Grosso Glenn R
• Peer David J

Classifications

• F01D3/04 Primary

  axial thrust being compensated by thrust-balancing dummy piston or the like · CPC title

• F01D11/025

  Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations · CPC title

• F01D11/02

  by non-contact sealings, e.g. of labyrinth type (for sealing space between rotor blade tips and stator F01D11/08) · CPC title

• F04D29/2266

  for sealing or thrust balance (F04D29/04 and F04D29/16 take precedence) · CPC title

• F01D11/04

  using sealing fluid, e.g. steam · CPC title