IP Library Granted Patent US 10,125,872
Granted Patent B2
US 10,125,872 · App. 13/586,773 · Granted Nov 13, 2018

Reciprocating seal for high pulsating pressure

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 10,125,872
App. No.
13/586,773
Granted
Nov 13, 2018
Kind
B2
Abstract

Device, system, and method are described directed to seal assemblies with support to reduce seal extrusion under high to very high pressure changes due to repeated piston reciprocating movement. In some examples, concave features are incorporated on the inner and outer edges of support and backup ring elements to support and hug the preceding element and constrain extrusion, as well as utilizing multiple contact points on certain elements in order to reduce friction against the dynamic surface. The seal assemblies described herein can also incorporate bearing surfaces to reduce damage to seal ID due to off-axis floating rod, such as incorporating one or more multi-point contacts to reduce friction.

Claims (43)

1. A seal assembly comprising:

a rigid support ring or a backup ring comprising a terminal end portion along an inside diameter and a terminal end portion along an outside diameter, a concave interface surface, a bore defined by the inside diameter, and a most concave part of the concave interface surface defining a plane orthogonal to an axis passing through the inside diameter;

a seal ring comprising a convex surface on an outer face matching the concave interface surface, a center channel section, an inner flange having a sealing lip, and an outer flange; and said seal ring comprising a recessed section formed at the outer flange at a location proximate an inner surface of a gland against which part of the outside flange of the seal ring seals when the seal assembly is located in the gland;

a spring cavity defined by the center channel section, the inner flange, and the outer flange of the seal ring;

a canted coil spring comprising a plurality of interconnected canted coils located in the spring cavity of the seal ring and being in contact with the inner flange of the seal ring biasing both the inner flange of the seal ring and the outer flange of the seal ring away from one another;

wherein the convex surface of the seal ring is in direct abutting contact with the concave interface surface without mechanical inter-engagement and wherein the terminal end portion along the outside diameter of the rigid support ring or backup ring extends away from the plane defined by the most concave part of the concave interface surface and along a corresponding portion of a first outer edge of the seal ring proximate the outer flange and the recessed section of the outer flange, and the terminal end portion along the inside diameter of the rigid support ring or backup ring extends away from the plane defined by the most concave part of the concave interface surface and along a corresponding portion of a second outer edge of the seal ring proximate the inner flange.

2. The seal assembly according to claim 1 , comprising both the rigid support ring and the backup ring; and wherein the backup ring comprises a support foot, the rigid support ring comprises a support foot, and the seal ring comprises an inside axial lip extension for contacting a dynamic shaft and an outside radial lip extension for contacting a holding bore.

3. The seal assembly of claim 1 , wherein the seal ring is made from a polymer material.

4. The seal assembly of claim 3 , wherein the seal ring is made from a PTFE, a polyethylene, a PTFE composition, or a polyethylene composition.

5. The seal assembly of claim 1 , wherein the rigid support ring is made from a high modulus high temperature polymer material, a ferrous material, or a non-ferrous metal.

6. The seal assembly of claim 1 wherein the backup ring is made from a high modulus high temperature polymer material, a ferrous material, or a non-ferrous metal.

7. The seal assembly of claim 1 , wherein the canted coil spring is a radial canted coil spring.

8. The seal assembly of claim 1 , wherein the rigid support ring has a support foot with multi-point contacts defined by a recessed section between the multi-point contacts, the multi-point contacts providing a barrier surface to guide the shaft.

9. The seal assembly of claim 1 , comprising both the backup ring and the rigid support ring and wherein the backup ring has a concave support surface and is in direct contact with a convex outer surface of the rigid support ring.

10. The seal assembly of claim 1 , further comprising a locking ring in abutting contact with the outer flange of the seal ring and directly urged by the canted coil spring.

11. The seal assembly of claim 10 , further comprising a groove on the rigid support ring or the backup ring having a canted coil spring located therein and wherein the groove comprises two sidewalls and a bottom wall located therebetween.

12. The seal assembly of claim 1 , wherein the outside diameter of the rigid support ring or the backup ring extends radially outside at least a portion of the outer flange of the seal ring.

13. The seal assembly of claim 1 , further comprising a groove on the rigid support ring or the backup ring having a canted coil spring located therein and wherein the groove comprises two sidewalls and a bottom wall located therebetween.

14. The seal assembly of claim 13 , wherein the canted coil spring in the groove is spaced from the seal ring.

15. A method for manufacturing a seal assembly comprising:

providing at least two mating components:

wherein at least one component is a seal ring comprising an inner flange, an outer flange, and a center channel section defining a cavity and at least one component is a rigid support ring or a backup ring, and wherein a recessed section is formed at the outer flange at a location proximate an inner surface of a gland against which part of the outside flange of the seal ring seals when the seal assembly is located in the gland;

the at least one of the rigid support ring or the backup ring comprises a terminal end portion along an inside diameter and a terminal end portion along an outside diameter, a concave interface surface, a bore defined by the inside diameter, and a most concave part of the concave interface surface defining a plane orthogonal to an axis passing through the inside diameter; and

the seal ring comprises a convex surface to accept the concave interface surface; and

placing the seal ring in direct contact with the rigid support ring or the backup ring so that the convex surface on the seal ring directly contacts the concave interface surface on the rigid support ring or the backup ring; and

wherein a canted coil spring comprising a plurality of interconnected canted coils is disposed in the cavity and biasing both the inner flange of the seal ring and the outer flange of the seal ring away from one another and the groove is spaced from the seal ring; and

wherein the convex surface of the seal ring is in direct abutting contact with the concave interface surface without mechanical inter-engagement and wherein the terminal end portion along the outside diameter of the rigid support ring or backup ring extends away from the plane defined by the most concave part of the concave interface surface and along a corresponding portion of a first outer edge of the seal ring proximate the outer flange and the recessed section of the outer flange, and the terminal end portion along the inside diameter of the rigid support ring or backup ring extends away from the plane defined by the most concave part of the concave interface surface and along a corresponding portion of a second outer edge of the seal ring proximate the inner flange.

16. The method for manufacturing of claim 15 , further comprising:

providing both the rigid support ring and the backup ring.

17. The method for manufacturing of claim 15 , wherein the rigid support ring or the backup ring has a groove having an energizer disposed therein to center the rigid support ring or the backup ring when located in a gland.

18. The method for manufacturing of claim 15 , further comprising providing a support foot on the rigid support ring or the backup ring and locating the support foot under the seal ring.

19. A seal assembly comprising:

a rigid support ring or a backup ring comprising a first interface surface, a second interface surface, a terminal end portion along an inside diameter and a terminal end portion along an outside diameter;

a seal ring comprising an interface feature, a center channel section, an inside flange, and an outside flange defining a spring cavity having a canted coil spring located therein biasing the inside flange of the seal ring and the outside flange of the seal ring away from one another, said seal ring further comprising a recessed section formed between the inside flange of the seal ring and a shaft against which a sealing lip of the inside flange of the seal ring seals and a recessed section formed at the outer flange at a location proximate an inner surface of a gland against which part of the outside flange of the seal ring seals;

a support foot on the rigid support ring or backup ring extending into the recessed section, the support foot comprising an inner bearing comprising multi-point contacts defined by a recess;

wherein the interface feature of the seal ring directly contacts the first interface surface of the rigid support ring or the backup ring without mechanical inter-engagement, and wherein the terminal end portion along the outside diameter of the rigid support ring or the backup ring extends along a corresponding portion of the seal ring proximate the outer flange and the recessed section of the outer flange; and

wherein a slant section of the support foot projects into the recessed section of the seal ring to support the inside flange from extrusion by operating seal box pressure.

20. The seal assembly of claim 19 , comprising both the backup ring and the support ring; wherein the second interface surface directly contacts an inner support surface of the backup ring.

21. The seal assembly of claim 19 , further comprising a locking ring in contact with the outer flange and the gland, and directly biased by the canted coil spring.

22. The seal assembly of claim 19 , further comprising a groove on the rigid support ring or the backup ring having at least one of a canted coil spring, a ribbon spring, an elastomer, or a V-spring disposed therein.

23. The seal assembly of claim 22 , wherein the groove comprises two sidewalls and a bottom wall located therebetween.

24. The seal assembly of claim 23 , wherein the groove is located at an outer diameter of the rigid support ring or the backup ring.

25. The seal assembly of claim 24 , further comprising an outer bearing on the rigid support ring or backup ring spaced from an inner bearing, the outer bearing comprising multi-point contacts defined by a recess, and wherein the inner bearing and the outer bearing cooperatively stabilize the seal assembly against the shaft, minimize gaps between the shaft and a bore, and provide a bearing surface to guide the shaft.

Assignments (7)
SECURITY INTEREST Recorded Feb 27, 2025
From: X-MICROWAVE, LLC; TANTALUM PELLET COMPANY, LLC; EVANS CAPACITOR COMPANY, LLC; PACIFIC AEROSPACE & ELECTRONICS, LLC; OHIO ASSOCIATED ENTERPRISES, LLC; FILCONN, LLC; HERMETIC SOLUTIONS GROUP INC.; RUBBERCRAFT CORPORATION OF CALIFORNIA, LTD.; SWIFT TEXTILE METALIZING LLC; RMB PRODUCTS; BAL SEAL ENGINEERING, LLC; KAMATICS CORPORATION; BEI PRECISION SYSTEMS & SPACE COMPANY, INC.; PAKTRON LLC; OHMEGA TECHNOLOGIES, LLC; TICER TECHNOLOGIES, LLC; CUSTOM INTERCONNECTS, LLC; SANDERS INDUSTRIES HOLDINGS, INC.; AKROFIRE, LLC; KAMAN AEROSPACE CORPORATION; KAMAN CORPORATION
To: CITIBANK, N.A., AS COLLATERAL AGENT
Reel/Frame 070344/0430 →
RELEASE OF INTELLECTUAL PROPERTY SECURITY AGREEMENTS (PATENTS) AT REEL 067175/FRAME 0740 Recorded Feb 27, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: KAMAN CORPORATION; KAMAN AEROSPACE CORPORATION; BAL SEAL ENGINEERING, LLC; AIRCRAFT WHEEL AND BRAKE, LLC; KAMATICS CORPORATION
Reel/Frame 070347/0014 →
RELEASE OF SECURITY INTEREST Recorded Apr 23, 2024
From: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
To: KAMATICS CORPORATION; BAL SEAL ENGINEERING, LLC; AIRCRAFT WHEEL AND BRAKE, LLC
Reel/Frame 067200/0800 →
IP SECURITY AGREEMENT Recorded Apr 22, 2024
From: KAMAN CORPORATION; KAMAN AEROSPACE CORPORATION; BAL SEAL ENGINEERING, LLC; AIRCRAFT WHEEL AND BRAKE, LLC; KAMATICS CORPORATION
To: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
Reel/Frame 067175/0740 →
AMENDED AND RESTATED PATENT COLLATERAL SECURITY AND PLEDGE AGREEMENT Recorded Sep 18, 2020
From: KAMATICS CORPORATION; BAL SEAL ENGINEERING, LLC
To: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
Reel/Frame 054304/0388 →
CHANGE OF NAME Recorded Apr 15, 2020
From: BAL SEAL ENGINEERING, INC.
To: BAL SEAL ENGINEERING, LLC
Reel/Frame 052410/0399 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 6, 2012
From: BINDER, MICHAEL; TARIQ, AMIN
To: BAL SEAL ENGINEERING, INC.
Reel/Frame 028911/0280 →