IP Library Granted Patent US 12,372,099
Granted Patent B2
US 12,372,099 · App. 16/845,743 · Granted Jul 29, 2025

Seal assembly for compressor

Inventor: Vishnu M. Sishtla (Manlius, NY)
Assignee: Carrier Corporation
F04D29/162F04D17/122F05B2240/515F05B2240/57F05B2260/507F16J15/445
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Quick Facts
Patent No.
US 12,372,099
App. No.
16/845,743
Granted
Jul 29, 2025
Kind
B2
Abstract

A seal assembly for a compressor includes at least one impeller. At least one seal land is associated with the impeller including a plurality of radially stepped surfaces. A seal is associated with each of at least one seal lands. The seal includes a plurality of radially stepped projections corresponding to the plurality of radially stepped surfaces on at least one seal land. At least one actuator is configured to move at least one seal land relative to the seal.

Claims (37)

1. A seal assembly for a compressor comprising:

an impeller; and

at least one seal assembly associated with the impeller, the at least one seal assembly including:

a seal land fixed relative to the impeller and having a plurality of radially stepped surfaces;

a seal associated with the seal land, wherein the seal includes a plurality of radially stepped projections corresponding to the plurality of radially stepped surfaces on the seal land; and

an actuator configured to create movement between the seal land and the seal, wherein the actuator is configured to move the seal between a first axial position and a second different axial position in response to a signal from a controller.

2. The assembly of claim 1 , wherein the plurality of radially stepped projections include distal ends with an increasing radially dimension in a first axial direction and adjacent ones of the plurality of radially stepped projections are separated by a trough and the plurality of radially stepped surfaces axially spaced from each other relative to a rotational axis of the impeller.

3. The assembly of claim 2 , wherein the plurality of radially stepped surfaces include an increasing radial dimension in the first axial direction.

4. The assembly of claim 3 , wherein the first axial direction is an axially aft direction.

5. The assembly of claim 1 , wherein the plurality of radially stepped surfaces include three radially stepped surfaces and the plurality of radially stepped projections include three radially stepped projections and the actuator includes an actuator arm in engagement with the seal and moveable between an extended position and a retracted position.

6. A compressor assembly comprising:

at least one impeller;

a shaft in driving engagement with the at least one impeller;

at least one electromagnetic bearing supporting the shaft; and

at least one seal assembly associated with the at least one impeller, the at least one seal assembly includes:

a seal land attached to and configured to rotate with the at least one impeller and the seal land includes a plurality of radially stepped surfaces;

a seal associated with the seal land, wherein the seal includes a plurality of radially stepped projections corresponding to the plurality of radially stepped surface on the seal land; and

an actuator configured to create movement between the seal land and the seal, wherein the actuator is configured to move the seal between a first axial position and a second different axial position in response to a signal from a controller.

7. The assembly of claim 6 , wherein the at least one electromagnetic bearing includes at least one radial support electromagnetic bearing system and at least one axial thrust electromagnetic bearing system and the at least one electromagnetic bearing is located axially between the at least one impeller and an electric motor driving the shaft.

8. The assembly of claim 6 , wherein the plurality of radially stepped projections include distal ends with an increasing radially dimension in a first axial direction and the actuator includes an actuator arm in engagement with the seal and moveable between an extended position and a retracted position.

9. The assembly of claim 8 , wherein the plurality of radially stepped surfaces include an increasing radial dimension in the first axial direction and adjacent ones of the plurality of radially stepped projections are separated by a trough.

10. The assembly of claim 6 , wherein the at least one impeller includes a first stage impeller and a second stage impeller and the at least one seal assembly includes a first seal assembly associated with the first stage impeller and a second and third seal assembly associated with the second stage impeller.

11. The assembly of claim 10 , wherein the first seal assembly is located on an axially upstream side of the first stage impeller, the second seal assembly is located on an axially upstream side of the second stage impeller, and the third seal assembly is located on an axially downstream side of the second stage impeller.

12. A method of operating a compressor comprising:

supporting a shaft in the compressor with at least one electromagnetic bearing;

determining a desired seal clearance of a seal assembly between a seal and a seal land based on an operating condition of the compressor; and

increasing the seal clearance based on the operating condition by creating axial movement between the seal land attached to an impeller and a seal moveable relative to a housing assembly, wherein an actuator creates the axial movement of the seal to move the seal between a first axial position and a second different axial position in response to a signal from a controller.

13. The method of claim 12 , wherein the operating condition includes at least one of a start-up or a shut-down condition for the compressor to increase seal clearance and the actuator includes an actuator arm in engagement with the seal and moveable between an extended position and a retracted position.

14. The method of claim 13 , wherein the at least one electromagnetic bearing includes at least one radial support electromagnetic bearing system and at least one axial thrust electromagnetic bearing system and the at least one electromagnetic bearing is located axially between the impeller and an electric motor driving the shaft.

15. The assembly of claim 11 , wherein the at least one seal assembly includes an O-ring in engagement with a radially outer side of the seal and a radially inner surface on a housing assembly of the compressor.

16. The assembly of claim 1 , wherein the at least one seal assembly includes a first seal assembly located adjacent an axially upstream edge of the impeller and a second seal assembly located adjacent an axially downstream edge of the impeller.

17. The assembly of claim 1 , including an O-ring in engagement with a radially outer side of the seal and a radially inner surface of a housing assembly of the compressor.

18. The method of claim 12 , wherein the seal assembly includes:

the seal land fixed relative to the impeller and having a plurality of radially stepped surfaces;

the seal associated with the seal land and including a plurality of radially stepped projections corresponding to the plurality of radially stepped surfaces on the seal land;

an O-ring engaging the seal and a housing assembly of the compressor; and

an actuator configured to move the seal relative to the seal land.

Continuity (2)
Provisional Application 62843773 · May 6, 2019
Related Publication 20200355194A1 · Nov 12, 2020
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