IP Library Granted Patent US 9,482,178
Granted Patent B2
US 9,482,178 · App. 14/462,924 · Granted Nov 1, 2016

Cylinder liner with an undercut seal trap

Inventor: Christopher Batta (West Lafayette, IN)
Assignee: Caterpillar Inc.
F02F1/004F02F1/163F02F11/005F02F3/00
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Quick Facts
Patent No.
US 9,482,178
App. No.
14/462,924
Granted
Nov 1, 2016
Kind
B2
Abstract

A cylinder liner for an engine includes a cylindrical wall having a radially internal surface and a radially external surface opposite the radially internal surface, the cylindrical wall defining a longitudinal axis therethrough, the radially external surface including a sealing surface and an undercut surface adjacent to the sealing surface, the sealing surface at least partly facing away from the longitudinal axis. The undercut surface includes a first surface and a second surface, the first surface at least partly facing the longitudinal axis, and the second surface at least partly facing away from the longitudinal axis.

Claims (34)

1. A cylinder liner for an engine, the cylinder liner comprising:

a cylindrical wall having a radially internal surface and a radially external surface opposite the radially internal surface, the cylindrical wall defining a longitudinal axis therethrough,

the radially external surface including a sealing surface and an undercut surface adjacent to the sealing surface, the sealing surface at least partly facing away from the longitudinal axis,

the undercut surface including a first surface and a second surface, the first surface at least partly facing the longitudinal axis, and the second surface at least partly facing away from the longitudinal axis, wherein a radial distance from the first surface to the longitudinal axis is less than a radial distance from the sealing surface to the longitudinal axis.

2. The cylinder liner of claim 1 , wherein the first surface at least partly faces a first longitudinal direction, the first longitudinal direction extending along the longitudinal axis in a direction from the undercut surface toward the sealing surface.

3. The cylinder liner of claim 2 , wherein the second surface at least partly faces a second longitudinal direction, the second longitudinal direction being opposite the first longitudinal direction.

4. The cylinder liner of claim 1 , wherein a portion of the first surface faces the second surface.

5. The cylinder liner of claim 4 , wherein a first portion of the second surface faces the first surface.

6. The cylinder liner of claim 5 , wherein a second portion of the second surface does not face the first surface.

7. The cylinder liner of claim 1 , wherein a first frustoconical surface composes at least a portion of the first surface.

8. The cylinder liner of claim 7 , wherein a second frustoconical surface composes at least a portion of the second surface.

9. The cylinder liner of claim 1 , wherein

the radially external surface further includes a radial protrusion disposed adjacent to the sealing surface,

the radial protrusion is disposed opposite the undercut surface with respect to the sealing surface along a direction parallel to the longitudinal axis, and

a radial distance from the radial protrusion to the longitudinal axis is greater than the radial distance from the sealing surface to the longitudinal axis.

10. The cylinder liner of claim 1 , wherein a radial distance from the second surface to the longitudinal axis is less than the radial distance from the sealing surface to the longitudinal axis.

11. A cylinder liner assembly, comprising:

a cylindrical wall having a radially internal surface and a radially external surface opposite the radially internal surface, the cylindrical wall defining a longitudinal axis therethrough,

the radially external surface including a sealing surface and an undercut surface adjacent to the sealing surface, the sealing surface at least partly facing away from the longitudinal axis,

the undercut surface including a first surface and a second surface, the first surface at least partly facing the longitudinal axis, and the second surface at least partly facing away from the longitudinal axis, wherein a radial distance from the first surface to the longitudinal axis is less than a radial distance from the sealing surface to the longitudinal axis; and

a seal disposed on the sealing surface.

12. The cylinder liner assembly of claim 11 , wherein an undercut depth is less than or equal to 90% of an uncompressed thickness of the seal along a radial direction normal to the longitudinal axis.

13. The cylinder liner assembly of claim 12 , wherein the undercut depth is less than or equal to 85% of the uncompressed thickness of the seal along the radial direction normal to the longitudinal axis.

14. The cylinder liner assembly of claim 12 , wherein the undercut depth extends in a radial direction from a radially outermost point on the first surface to a radially innermost point on the undercut surface, the radial direction being normal to the longitudinal axis.

15. The cylinder liner assembly of claim 14 , wherein the radially innermost point on the undercut surface is a tangent point between a line parallel to the longitudinal axis and the undercut surface.

16. An engine, comprising:

a block;

a cylinder liner disposed within the block, a radially external surface of the cylinder liner at least partly facing the block, the cylinder liner defining a longitudinal axis therethrough;

a piston disposed within the cylinder liner and configured for reciprocal sliding engagement with a radially internal surface of the cylinder liner along the longitudinal axis, the radially internal surface being opposite the radially external surface,

the radially external surface of the cylinder liner including a sealing surface and an undercut surface adjacent to the sealing surface, the sealing surface at least partly facing away from the longitudinal axis, and

the undercut surface including a first surface and a second surface, the first surface at least partly facing the longitudinal axis, and the second surface at least partly facing away from the longitudinal axis, wherein a radial distance from the first surface to the longitudinal axis is less than a radial distance from the sealing surface to the longitudinal axis; and

a seal disposed in sealing engagement with the sealing surface and the block.

17. The engine of claim 16 , wherein an undercut depth is less than or equal to 90% of an uncompressed thickness of the seal along a radial direction normal to the longitudinal axis.

18. The engine of claim 17 , wherein the undercut depth extends in a radial direction from a radially outermost point on the undercut surface to a radially innermost point on the undercut surface, the radial direction being normal to the longitudinal axis.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 19, 2014
From: BATTA, CHRISTOPHER
To: CATERPILLAR INC.
Reel/Frame 033562/0903 →
Continuity (1)
Related Publication 20160053707A1 · Feb 25, 2016