High-pressure seal for a liquid jet cutting system

1. A seal assembly for use with a liquid jet cutting system, comprising:

an annular seal having—

a longitudinal axis;

a first end portion;

a second end portion opposite the first end portion along the longitudinal axis, the second end portion having—

a first annular face facing away from the first end portion of the annular seal;

a first tapered portion extending from the first annular face away from the longitudinal axis and toward the first end portion of the annular seal; and

a first transition between the first annular face and the first tapered portion; and

a radially-inner surface configured to seal an outer surface of a plunger of the liquid jet cutting system;

an annular backup ring coaxial with the annular seal along the longitudinal axis of the annular seal, the annular backup ring having—

a first end portion having—

a second annular face facing the first annular face of the annular seal;

a second tapered portion extending from the second annular face away from the longitudinal axis and away from the annular seal; and

a second transition between the second annular face and the second tapered portion; and

a second end portion opposite the first end portion of the annular backup ring along the longitudinal axis,

wherein the annular backup ring does not overlap the annular seal in a direction parallel to the longitudinal axis of the annular seal; and

an annular hoop ring coaxial with the annular seal along the longitudinal axis of the annular seal and positioned between the annular seal and the annular backup ring, the annular hoop ring having a—

a first tapered surface configured to engage the first tapered portion of the second end portion of the annular seal;

a second tapered surface configured to engage the second tapered portion of the first end portion of the annular backup ring; and

a radially-inner apex between the first tapered surface and the second tapered surface and configured to be positioned adjacent the first transition and the second transition;

wherein an angle between the second tapered surface and the longitudinal axis of the annular hoop ring, when measured in a plane on which the longitudinal axis of the annular seal lies, is between 50 degrees and 80 degrees.

2. The seal assembly of claim 1 wherein the seal assembly is configured for use with a water jet cutting system.

3. The seal assembly of claim 1 wherein the annular hoop ring comprises an aluminum bronze alloy.

4. The seal assembly of claim 1 wherein the annular hoop ring has a substantially triangular cross-section on a cut-plane on which the longitudinal axis of the annular seal lies.

5. The seal assembly of claim 1 wherein a radial thickness of the annular hoop ring, when measured perpendicular to the longitudinal axis of the annular seal, is between ⅓ and ⅔ of a radial distance between an outer surface of the plunger and an inner surface of a cylinder surrounding the annular hoop ring.

6. The seal assembly of claim 5 wherein the radial thickness of the annular hoop ring, when measured perpendicular to the longitudinal axis of the annular seal, is ½ of the radial distance between the outer surface of the plunger and the inner surface of the cylinder surrounding the annular hoop ring.

7. The seal assembly of claim 1 wherein the first annular face is configured to contact the second annular face when axial force is applied to the seal assembly.

8. The seal assembly of claim 1 wherein the second end portion of the annular seal is a mirror image of the first end portion of the annular backup ring across a plane perpendicular to the longitudinal axis of the annular seal.

9. The seal assembly of claim 1 wherein a radially-outermost edge of the first annular face and a radially-outermost edge of the second annular face are both located at the radially-inner apex when axial force is applied to the seal assembly.

10. The seal assembly of claim 1 wherein an angle between the first tapered portion and the second tapered portion, when measured in a plane on which the longitudinal axis of the annular seal lies, is between 58 degrees and 64 degrees.

11. The seal assembly of claim 1 , further comprising a gasket positioned between the annular seal and a cylinder surrounding the annular seal, wherein the gasket is configured to inhibit or prevent fluid passage between the annular seal and the cylinder.

12. The seal assembly of claim 1 wherein the annular hoop ring has a substantially isosceles triangular cross-section on cut-plane on which the longitudinal axis of the annular seal lies.

13. The seal assembly of claim 1 wherein the annular hoop ring is configured to contact the annular seal and the annular backup ring only along the first tapered surface and the second tapered surface, respectively.

14. The seal assembly of claim 1 wherein—

the annular seal further includes an outer surface configured to face a cylinder of the liquid jet cutting system and defines a radial clearance between the radially-inner surface of the annular seal and the outer surface;

the annular hoop ring has a radial thickness; and

the radial thickness of the annular hoop ring is between 33% to 66% of the radial clearance defined by the annular seal.

15. The seal assembly of claim 14 wherein the radial thickness of the annular hoop ring is between 40% to 60% of the radial clearance defined by the annular seal.

16. The seal assembly of claim 14 wherein the radial thickness of the annular hoop ring is between 45% to 55% of the radial clearance defined by the annular seal.