IP Library Granted Patent US 10,107,121
Granted Patent B2
US 10,107,121 · App. 13/705,259 · Granted Oct 23, 2018

Carbon seal assembly

Inventor: Ivor John Roberts (Rockwood, CA)
Assignee: PRATT & WHITNEY CANADA CORP.
F01D11/00F02C7/28F16J15/3444F05D2240/55F05D2300/224
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Quick Facts
Patent No.
US 10,107,121
App. No.
13/705,259
Granted
Oct 23, 2018
Kind
B2
Abstract

A carbon seal assembly comprises an annular member adapted to be secured to a structure. An annular seal runner is sealingly mounted to a shaft to rotate therewith, with the seal runner being made of a material complementary to that of the annular member for magnetic attraction therebetween. An annular carbon seal element is mounted to the annular seal runner to rotate therewith and positioned in a gap between the annular member and the annular seal runner, the annular carbon seal element having an annular wear surface abutting against a face of the annular member. A cross-sectional area of the annular carbon seal element increases as the axial dimension of the annular seal runner decreases for at least a part of the seal.

Claims (28)

1. A carbon seal assembly comprising:

an annular member adapted to be secured to a structure;

an annular seal runner adapted to be sealingly mounted to a shaft to rotate therewith, with the seal runner being made of a material complementary to that of the annular member for magnetic attraction therebetween; and

an annular carbon seal element mounted to the annular seal runner to rotate therewith and positioned in a gap between the annular member and the annular seal runner, the annular carbon seal element having a leading sectional shape portion and a trailing sectional shape portion, with the leading sectional shape portion projecting axially beyond the annular seal runner and defining an annular wear surface abutting against, and in contact with, a face of the annular member when the annular carbon seal element rotates, an area of the annular wear surface increasing as the axial dimension of the annular carbon seal element decreases when worn for at least a part of the leading sectional shape portion of the seal.

2. The carbon seal assembly according to claim 1 , wherein the entirety of the sectional shape of the annular carbon seal element has an increasing cross-sectional thickness along the axial direction of the annular carbon seal element from the annular wear surface toward the annular seal runner.

3. The carbon seal assembly according to claim 1 , wherein the leading sectional shape portion has a trapezoid shape with an outer side and an inner side being oblique relative to the axial direction.

4. The carbon seal assembly according to claim 1 , wherein the trailing sectional shape portion has a trapezoid shape with an outer side parallel to the axial direction, and an inner side being oblique relative to the axial direction.

5. The carbon seal assembly according to claim 4 , wherein the outer side of the trailing sectional shape portion is in abutment with a counterbore surface of the annular seal runner.

6. The carbon seal assembly according to claim 1 , wherein the sectional shape of the annular carbon seal element is a five-sided polygonal shape.

7. The carbon seal assembly according to claim 1 , wherein the annular carbon seal element is made of hard matter carbon.

8. The carbon seal assembly according to claim 1 , wherein the annular member is made of a magnetic material, and wherein the annular seal runner is made of a metallic material attracted to the magnetic material.

9. The carbon seal assembly according to claim 1 , further comprising at least one resilient annular seal between the annular seal runner and the shaft.

10. An engine comprising:

a structure;

a shaft operatingly mounted to the structure to rotate relative to the structure;

a carbon seal assembly comprising:

an annular member secured to the structure;

an annular seal runner sealingly mounted to the shaft to rotate therewith, with the seal runner being made of a material complementary to that of the annular member for magnetic attraction therebetween; and

an annular carbon seal element mounted to the annular seal runner to rotate therewith and positioned in a gap between the annular member and the annular seal runner, the annular carbon seal element having a leading sectional shape portion and a trailing sectional shape portion, with the leading sectional shape portion projecting axially beyond the annular seal runner and defining an annular wear surface abutting against, and in contact with, a face of the annular member when the annular carbon seal element rotates, an area of the annular wear surface increasing as the axial dimension of the annular carbon seal element decreases when worn for at least a part of the leading sectional shape portion of the seal.

11. The engine according to claim 10 , wherein the entirety of the sectional shape of the annular carbon seal element has an increasing cross-sectional thickness along the axial direction of the annular carbon seal element from the annular wear surface toward the annular seal runner.

12. The engine according to claim 10 , wherein the leading sectional shape portion has a trapezoid shape with an outer side and an inner side being oblique relative to the axial direction.

13. The engine according to claim 10 , wherein the trailing sectional shape portion has a trapezoid shape with an outer side parallel to the axial direction, and an inner side being oblique relative to the axial direction.

14. The engine according to claim 13 , wherein the outer side of the trailing sectional shape portion is in abutment with a counterbore surface of the annular seal runner.

15. The engine according to claim 10 , wherein the sectional shape of the annular carbon seal element is a five-sided polygonal shape.

16. The engine according to claim 10 , wherein the annular carbon seal element is made of hard matter carbon.

17. The engine according to claim 10 , wherein the annular member is made of a magnetic material, and wherein the annular seal runner is made of a metallic material attracted to the magnetic material.

18. The engine according to claim 10 , further comprising at least one resilient annular seal between the annular seal runner and the shaft.

19. The carbon seal assembly according to claim 9 , wherein the at least one resilient annular seal has a sectional shape greater than the annular carbon seal element.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2012
From: ROBERTS, IVOR JOHN
To: PRATT & WHITNEY CANADA CORP.
Reel/Frame 029416/0227 →
Continuity (1)
Related Publication 20140154053A1 · Jun 5, 2014