Piston sealing ring assemblies
The present disclosure provides a sealing ring assembly having a first ring and a second ring, configured to seal a high-pressure region from a lower pressure region of a piston and cylinder device. Accordingly, the sealing ring assembly includes a high-pressure boundary and a low-pressure boundary. Each ring may be segmented, and the first and second rings interface along a surface. Along the surface at the interface, a groove open to the lower pressure region aids in pressure locking the sealing ring assembly. A pocket in the second ring allows for high pressure gas to aid in balancing radial forces on the sealing ring assembly. As the sealing ring wears, the first and second rings remain engaged with one another.
1. A sealing ring assembly, comprising:
a first ring comprising an extension extending axially rearwards, wherein the extension comprises a radially outward surface;
a second ring comprising an inner radial surface configured to interface with the radially outward surface of the extension, wherein the second ring comprises at least two second ring segments, wherein the at least two second ring segments are arranged such that respective ends of the at least two second ring segments form at least one interface between each other; and
a groove extending circumferentially along at least one of the radially outward surface of the extension and the inner radial surface of the second ring.
2. The sealing ring assembly of claim 1 , wherein the groove is configured to be open to a low-pressure boundary of the sealing ring assembly.
3. The sealing ring assembly of claim 1 , wherein the second ring comprises a pocket that extends azimuthally in an outermost radial surface of the second ring, and wherein the pocket is configured to receive gas from a high-pressure boundary of the sealing ring assembly.
4. The sealing ring assembly of claim 3 , wherein the second ring further comprises an orifice that is configured to allow gas to flow from the high-pressure boundary to the pocket.
5. The sealing ring assembly of claim 1 , wherein the sealing ring assembly is configured to be arranged in a ring groove of a piston, wherein the piston comprises an anti-rotation relief, and wherein the sealing ring assembly comprises an anti-rotation tab that engages with the anti-rotation relief to prevent substantial azimuthal movement of the sealing ring assembly.
6. The sealing ring assembly of claim 1 , wherein the first ring comprises an outermost radial surface, and wherein the radially outward surface of the extension is radially inward of the outermost radial surface.
7. The sealing ring assembly of claim 1 , wherein at least one of the first ring and the second ring is comprised of a self-lubricating material.
8. The sealing ring assembly of claim 1 , wherein the sealing ring assembly is configured for operation without liquid lubricant.
9. The sealing ring assembly of claim 1 , wherein the first ring comprises at least two first ring segments, wherein the at least two first ring segments are arranged such that respective ends of the at least two first ring segments form at least one interface between each other.
10. A piston assembly comprising:
a piston comprising a ring groove; and
a sealing ring assembly arranged in the ring groove, the sealing ring assembly comprising:
a first ring comprising an extension extending axially rearwards, wherein the extension comprises a radially outward surface,
a second ring comprising an inner radial surface configured to interface with the radially outward surface of the extension, wherein the second ring comprises at least two second ring segments, wherein the at least two second ring segments are arranged such that respective ends of the at least two second ring segments form at least one interface between each other, and
a groove extending azimuthally along at least one of the radially outer surface of the extension and the inner radial surface of the second ring.
11. The piston assembly of claim 10 , wherein the groove is configured to be open to a low-pressure boundary of the sealing ring assembly.
12. The piston assembly of claim 10 , wherein the second ring comprises a pocket that extends azimuthally in an outermost radial surface of the second ring, and wherein the pocket is configured to receive gas from a high-pressure boundary of the sealing ring assembly.
13. The piston assembly of claim 12 , wherein the second ring further comprises an orifice that is configured to allow gas to flow from a high-pressure boundary to the pocket.
14. The piston assembly of claim 10 , wherein the piston comprises an anti-rotation relief, and wherein the second ring comprises an anti-rotation tab that engages with the anti-rotation relief to prevent substantial azimuthal movement of the sealing ring assembly.
15. The piston assembly of claim 10 , wherein the first ring comprises an outermost radial surface, and wherein the radially outward surface of the extension is radially inward of the outermost radial surface.
16. The piston assembly of claim 10 , wherein at least one of the first ring and the second ring is comprised of a self-lubricating material.
17. The piston assembly of claim 10 , wherein the sealing ring assembly is configured for oil-less operation.
18. The piston assembly of claim 10 , wherein the first ring comprises at least two first ring segments, wherein the at least two first ring segments are arranged such that respective ends of the at least two first ring segments form at least one interface between each other.
19. The piston assembly of claim 10 , wherein the piston is an open-faced piston.
20. A device comprising:
a cylinder comprising a bore;
a piston comprising a ring groove, wherein the piston is configured to travel within the bore along an axis of the bore; and
a sealing ring assembly arranged in the ring groove, the sealing ring assembly comprising:
a first ring comprising an extension extending axially rearwards, wherein the extension comprises a radially outward surface,
a second ring comprising an inner radial surface configured to interface with the radially outward surface of the extension, wherein the second ring comprises a pocket that extends azimuthally in an outermost radial surface of the second ring, and wherein the pocket is configured to receive gas from a high-pressure region in the bore, and
a groove extending azimuthally along at least one of the radially outer surface of the extension and the inner radial surface of the second ring.
21. The device of claim 20 , wherein the sealing ring assembly is configured to seal between the bore and the piston, and wherein the sealing ring assembly is configured to seal a high-pressure region in the bore from a low-pressure region in the bore.
22. The device of claim 20 , wherein the groove is configured to be open to a low-pressure region.
23. The device of claim 20 , wherein the second ring further comprises an orifice that is configured to allow gas to flow from the high-pressure region to the pocket.
24. The device of claim 20 , wherein the piston comprises an anti-rotation relief, and wherein the second ring comprises an anti-rotation tab that engages with the anti-rotation relief to prevent substantial azimuthal movement of the sealing ring assembly.
25. The device of claim 20 , wherein the first ring comprises an outermost radial surface, and wherein the radially outward surface of the extension is radially inward of the outermost radial surface.
26. The device of claim 20 , wherein at least one of the first ring and the second ring is comprised of a self-lubricating material.
27. The device of claim 20 , wherein the sealing ring assembly is configured for operation without liquid lubricant.