IP Library Granted Patent US 11,274,571
Granted Patent B2
US 11,274,571 · App. 16/994,293 · Granted Mar 15, 2022

Seal runner with passive heat transfer augmentation features

Inventors: Michael Campo (Hartford, CT); Timothy Castaldo (West Hartford, CT)
Assignee: Raytheon Technologies Corporation
F01D25/183F01D25/20F05D2240/55F05D2260/98
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Quick Facts
Patent No.
US 11,274,571
App. No.
16/994,293
Granted
Mar 15, 2022
Kind
B2
Abstract

Oil slinger systems include a seal runner comprising an annular radial member having a radius (R) and an outer axially extending member having an axial length (L), wherein a proximal surface of the outer axially extending member comprising a plurality of helical grooves. Methods of radial convective cooling include pumping a cooling liquid through the oil slinger system and convectively cooling the oil slinger.

Claims (31)

1. An oil slinger system comprising:

a seal runner comprising an annular radial member and an outer axially extending member, a proximal surface of the outer axially extending member comprising a plurality of helical grooves.

2. The oil slinger system according to claim 1 , further comprising an inner axially extending member comprising:

a lower oil passage configured to receive a lubricating oil; and

a radial oil passage configured to permit the lubricating oil to pass from the lower oil passage and through the inner axially extending member to an inner face of the annular radial member.

3. The oil slinger system according to claim 2 , wherein the annular radial member comprises a radius (R) and the outer axially extending member comprises an axial length (L).

4. The oil slinger system according to claim 3 , wherein the annular radial member is disposed at a first angle with respect to the outer axially extending member, and the annular radial member is disposed at a second angle with respect to the inner axially extending member.

5. The oil slinger system according to claim 4 , wherein the second angle is between about 75 degrees and about 90 degrees.

6. The oil slinger system according to claim 5 , wherein the second angle is 90 degrees.

7. The oil slinger system according to claim 1 , wherein the proximal surface of the outer axially extending member comprises a plurality of helical ridges.

8. The oil slinger system according to claim 7 , wherein a first helical ridge, of the plurality of helical ridges, comprises a first width and a first helical groove, of the plurality of helical grooves, comprises a second width which is greater than the first width.

9. The oil slinger system according to claim 1 , further comprising a cooling liquid.

10. The oil slinger system according to claim 9 , wherein the plurality of helical grooves direct the cooling liquid along the proximal surface of the outer axially extending member in a helical cooling liquid flow direction.

11. The oil slinger system according to claim 1 , wherein the outer axially extending member is disposed at an angle with respect to a central axis of the seal runner.

12. The oil slinger system according to claim 11 , wherein the angle is between 0.1 and 3 degrees.

13. The oil slinger system according to claim 12 , wherein the angle is between 1 and 2 degrees.

14. The oil slinger system according to claim 1 , wherein the seal runner comprises at least one of steel, titanium, and alloys thereof.

15. A seal runner, comprising:

an annular radial member; and

an outer axially extending member,

wherein a proximal surface of the outer axially extending member comprising a plurality of helical grooves.

16. The seal runner according to claim 15 , wherein the outer axially extending member is disposed at an angle of between 0.1 and 3 degrees with respect to a central axis of the seal runner.

17. The seal runner according to claim 15 , further comprising a plurality of helical ridges disposed on the proximal surface of the outer axially extending member.

18. The seal runner according to claim 17 , wherein a width of a first helical ridge of the plurality of helical ridges is less than one fourth of a width of a first helical groove of the plurality of helical grooves.

19. A method of axial convective cooling comprising:

pumping a cooling liquid through an oil slinger system; and

convectively cooling the oil slinger system, wherein the oil slinger system comprises:

a seal runner comprising an annular radial member and an outer axially extending member, a proximal surface of the outer axially extending member comprising a plurality of helical grooves, wherein the plurality of helical grooves direct the cooling liquid along the proximal surface of the outer axially extending member in a helical cooling liquid flow direction.

20. The method of claim 19 , wherein the seal runner further comprises an inner axially extending member, comprising:

a lower oil passage configured to receive a lubricating oil; and

a radial oil passage configured to permit the lubricating oil to pass from the lower oil passage and through the inner axially extending member to a proximal surface of the outer axially extending member.

Assignments (2)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 14, 2020
From: CAMPO, MICHAEL; CASTALDO, TIMOTHY
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 053504/0382 →
Continuity (1)
Related Publication 20220049623A1 · Feb 17, 2022
Cited By (3)
US 12,203,412 US 12,428,970 US 12,473,841