IP Library Granted Patent US 11,125,094
Granted Patent B2
US 11,125,094 · App. 16/372,775 · Granted Sep 21, 2021

Extended pilot ring seal arrangement for installation damage prevention

Inventors: Jonathan Logan Miller (Ware, MA); Michael M. Davis (North Granby, CT)
Assignee: Raytheon Technologies Corporation
F01D11/003F05D2240/55
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,125,094
App. No.
16/372,775
Granted
Sep 21, 2021
Kind
B2
Abstract

A seal assembly includes a first and second seats. The first seat includes an axial portion extending circumferentially around a center axis and extending axially from a first end to a second end. A radial portion extends circumferentially around the axial portion and extends radially from the axial portion between the first end and the second end. A cavity is formed in the radial portion and extends circumferentially around the axial portion. A second seat includes a radial segment extending circumferentially around the center axis and extending radially from an inner surface to an outer surface of the radial segment. An axial segment extends circumferentially around the first end of the first seat, and extends axially from the radially segment to a distal end. The axial segment includes a tapered outer surface that tapers radially inward toward the distal end. The distal end is received in the cavity.

Claims (44)

1. A seal assembly comprises:

a first seat comprising:

an annular portion extending circumferentially around a center axis and extending axially from a first end to a second end;

a radial portion extending circumferentially around the annular portion and extending radially from the annular portion, wherein the radial portion is positioned axially on the annular portion between the first end and the second end; and

a cavity extending axially into the radial portion at a base of the radial portion and extending circumferentially around the center axis; and

a second seat comprising:

a radial segment extending circumferentially around the center axis and extending radially from an inner surface to an outer surface of the radial segment; and

an axial segment extending circumferentially around the first end of the first seat, and extending axially from the radial segment to a distal end, wherein at least a portion of an outer surface of the axial segment tapers radially inward toward the distal end, and wherein the distal end is received in the cavity of the first seat.

2. The assembly of claim 1 , further comprising:

a first seal ring extending circumferentially around the axial segment of the second seat and positioned axially between the radial portion of the first seat and the radial segment of the second seat; and

a second seal ring extending circumferentially around the axial segment of the second seat and positioned axially between the first seal ring and the radial portion of the first seat.

3. The assembly of claim 2 , wherein the first seal ring and the second seal ring each comprise carbon.

4. The assembly of claim 2 , further comprising:

a spring between the first seal ring and the second seal ring, wherein the spring is configured to bias the first seal ring against the radial segment of the second seat and bias the second seal ring against the radial portion of the first seat.

5. The assembly of claim 1 , wherein the first end of the annular portion of the first seat contacts the radial segment of the second seat.

6. The assembly of claim 1 , wherein the distal end does not contact the radial portion of the first seat.

7. The assembly of claim 1 , wherein the first seat further comprises:

a shelf formed on the radial portion radially outward of the cavity and on an opposite side of the radial portion from the cavity.

8. The assembly of claim 1 , wherein the distal end of the axial segment is tapered.

9. A seal assembly comprises:

a first seat comprising:

an axial portion extending circumferentially around a center axis and extending axially from a first end to a second end;

a radial portion extending circumferentially around the axial portion and extending radially from the axial portion between the first end and the second end; and

a cavity formed in the radial portion and extending circumferentially around the axial portion; and

a second seat comprising:

a radial segment extending circumferentially around the center axis and extending radially from an inner surface to an outer surface of the radial segment; and

an axial segment extending circumferentially around the first end of the first seat, and extending axially from the radial segment to a distal end, wherein the axial segment comprises a tapered outer surface that tapers radially inward toward the distal end, and wherein the distal end is received in the cavity of the first seat.

10. The assembly of claim 9 , further comprising:

a first seal ring extending circumferentially around the axial segment of the second seat and positioned axially between the radial portion of the first seat and the radial segment of the second seat; and

a second seal ring extending circumferentially around the axial segment of the second seat and positioned axially between the first seal ring and the radial portion of the first seat.

11. The assembly of claim 10 , wherein the first seal ring and the second seal ring each comprise carbon.

12. The assembly of claim 10 , wherein the second seal ring extends circumferentially around a portion of the tapered outer surface of the axial segment.

13. The assembly of claim 10 , further comprising:

a spring between the first seal ring and the second seal ring, wherein the spring is configured to bias the first seal ring against the radial segment of the second seat and bias the second seal ring against the radial portion of the first seat.

14. The assembly of claim 9 , wherein the first end of the axial portion of the first seat contacts the radial segment of the second seat.

15. The assembly of claim 9 , wherein the distal end does not contact the radial portion of the first seat.

16. The assembly of claim 9 , wherein the first seat further comprises:

a shelf formed on the radial portion radially outward of the cavity and on an opposite side of the radial portion from the cavity, and

wherein the shelf extends circumferentially around the center axis on the radial portion.

17. The assembly of claim 9 , wherein the distal end of the axial segment is tapered.

18. The assembly of claim 9 , wherein the distal end of the axial segment is not tapered.

19. The assembly of claim 9 , wherein the second seat further comprises:

a ridge extending radially inward of the axial segment and contacting the axial portion of the first seat, and

wherein the ridge extends circumferentially around the center axis.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE SPELLING ON THE ADDRESS 10 FARM SPRINGD ROAD FARMINGTONCONNECTICUT 06032 PREVIOUSLY RECORDED ON REEL 057190 FRAME 0719. ASSIGNOR(S) HEREBY CONFIRMS THE CORRECT SPELLING OF THE ADDRESS 10 FARM SPRINGS ROAD FARMINGTON CONNECTICUT 06032. Recorded Aug 19, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057226/0390 →
CHANGE OF NAME Recorded Aug 16, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057190/0719 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 2, 2019
From: MILLER, JONATHAN LOGAN; DAVIS, MICHAEL M.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 048766/0713 →
Cited By (1)
US 12,228,043