IP Library Granted Patent US 12,624,643
Granted Patent B2
US 12,624,643 · App. 18/942,835 · Granted May 12, 2026

Rotary machine seal having a wear protection assembly with an abradable covering

Inventors: Narendra Anand Hardikar (Bengaluru, IN); Scott Alan Schimmels (Miamisburg, OH)
Assignee: General Electric Company
F01D11/001F16J15/3284F05D2220/32
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Quick Facts
Patent No.
US 12,624,643
App. No.
18/942,835
Granted
May 12, 2026
Kind
B2
Abstract

A seal assembly for rotary machines having a wear protection assembly with an abradable covering. The wear protection assembly has one or more wear protection features that enable in-operation opening of the seal assembly by increasing a clearance between a seal rotor and a seal slider of the seal assembly. In particular, the wear protection assembly is configured to open the seal assembly and increase the clearance of the seal rotor and the seal slider during slider air-bearing wear conditions, slider counterbore wear conditions, rotor air-bearing wear conditions, or extreme vibration wear conditions. Under such or similar wear conditions (or under conditions preceding or leading up to a wear condition), the wear protection assembly yields a pressure gradient and/or a fluid flow that oppose the forces acting to decrease the clearance between the seal rotor and the seal slider.

Claims (35)

1 . A rotary machine, comprising:

a stator;

a rotor configured to rotate with respect to the stator, the rotor being arranged with the stator at a rotor-stator interface; and

a seal assembly at the rotor-stator interface, the seal assembly comprising:

a seal cavity defined by a seal rotor and a seal slider of a seal stator, the seal rotor defining a rotor face, the seal slider defining a slider face and an air bearing wall, wherein the seal slider comprises a high-pressure aspiration conduit;

at least one non-contacting seal interface; and

a wear protection assembly comprising an abradable covering positioned over an opening of the high-pressure aspiration conduit;

wherein, during operation of the rotary machine, and upon the seal rotor and the seal stator of the rotary machine making contact with each other at the rotor-stator interface such that the seal cavity of the seal assembly is at least partially closed, allowing a portion of the seal rotor to abrade the abradable covering to expose the opening, thereby allowing airflow to pressurize a trench cavity defined by the at least partially closed seal cavity and the slider face of the seal slider, wherein the pressurized trench cavity is configured to at least partially reopen the seal cavity,

wherein the opening of the high-pressure aspiration conduit is defined by the slider face of the seal slider, and wherein the high-pressure aspiration conduit is integral with the seal slider,

wherein the wear protection assembly further comprises an opening cover arranged between the opening of the high-pressure aspiration conduit and the abradable covering.

2 . The rotary machine of claim 1 , wherein the seal assembly is configured as at least one of an aspirating face seal, a fluid bearing, a gas bearing, or a film riding seal.

3 . The rotary machine of claim 1 , wherein the opening cover and the opening of the high-pressure aspiration conduit form an air pocket therebetween.

4 . The rotary machine of claim 1 , wherein the wear protection assembly further comprises a weld structure securing the opening cover on the slider face over the opening.

5 . The rotary machine of claim 1 , wherein the opening is at an outlet of a secondary airflow channel of the high-pressure aspiration conduit, the secondary airflow channel being in fluid communication with a primary airflow channel of the high-pressure aspiration conduit.

6 . The rotary machine of claim 1 , wherein the portion of the seal rotor is a primary tooth of the seal rotor.

7 . The rotary machine of claim 1 , wherein the abradable covering has a thickness less than a thickness of the air bearing wall of the seal slider.

8 . A rotary machine, comprising:

a stator;

a rotor configured to rotate with respect to the stator, the rotor being arranged with the stator at a rotor-stator interface; and

a seal assembly at the rotor-stator interface, the seal assembly comprising:

a seal cavity defined by a seal rotor and a seal slider of a seal stator, the seal rotor defining a rotor face, the seal slider defining a slider face and an air bearing wall, wherein the seal slider comprises a high-pressure aspiration conduit;

at least one non-contacting seal interface; and

a wear protection assembly comprising an abradable covering positioned over an opening of at least one hole extending partially through a thickness of the rotor face such that a seal-side of the at least one hole is covered during non-contacting conditions,

wherein, during operation of the rotary machine, and upon the seal rotor and the seal stator making contact with each other at the rotor-stator interface such that the seal cavity is at least partially closed, allowing a portion of the seal slider to abrade the abradable covering to expose the opening, thereby allowing airflow to enter the at least one hole to pressurize a trench cavity defined by the at least partially closed seal cavity and the slider face of the seal cavity, wherein the pressurized trench cavity is configured to at least partially reopen the seal cavity,

wherein the wear protection assembly further comprises an opening cover arranged between the opening of the at least one hole and the abradable covering.

9 . The rotary machine of claim 8 , wherein the seal assembly is configured as at least one of an aspirating face seal, a fluid bearing, a gas bearing, or a film riding seal.

10 . The rotary machine of claim 8 , wherein the opening cover and the opening of the at least one hole form an air pocket therebetween.

11 . The rotary machine of claim 8 , wherein the wear protection assembly further comprises a weld structure securing the opening cover on the slider face over the opening.

12 . The rotary machine of claim 8 , wherein the abradable covering has a thickness less than a thickness of the air bearing wall of the seal slider.

13 . A rotary machine, comprising:

a stator;

a rotor configured to rotate with respect to the stator; and

a member coupled to or formed integrally with the stator or the rotor, the member defining a high-pressure aspiration conduit and comprising a wear surface, the member including an abradable covering positioned over an opening of the high-pressure aspiration conduit, the abradable covering configured to wear during an operation of the stator and the rotor to allow a high pressure airflow through the opening,

wherein the member further comprises an opening cover arranged between the opening of the high-pressure aspiration conduit and the abradable covering.

14 . The rotary machine of claim 13 , wherein the abradable covering comprises successive layers of abradable material.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 11, 2024
From: HARDIKAR, NARENDRA ANAND; SCHIMMELS, SCOTT ALAN
To: GENERAL ELECTRIC COMPANY
Reel/Frame 069196/0868 →
Continuity (2)
Division 17979113 · Nov 2, 2022
Related Publication 20250067192A1 · Feb 27, 2025
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