PISTON RING

Abstract

A piston ring, and in particular a compression piston ring, has a running face, upper and lower flank regions, an inner circumferential surface and a joint, wherein at least the running face is provided with at least one wear-resistant PVD or CVD layer, wherein the PVD or CVD layer extends at a predefinable layer thickness across a circumferential length of more than 95%, but less than 100% of the piston ring, and defined circumferential sections are designed in a layer-free manner in the region of the joint.

Claims

1. A piston ring comprising a running face, upper and lower flanks, an inner circumferential surface and a joint constituted of free ends of the piston ring and a space therebetween, at least the running face being provided with at least one wear-resistant PVD or CVD layer, wherein the at least one PVD or CVD layer extends as a layer of predetermined thickness across a region constituting a circumferential length of more than 95% but less than 100% of a circumferential length of the piston ring as measured from one of the free ends to the other of the free ends of the piston ring.

2. The piston ring according to claim 1, wherein the at least one wear-resistant PVD or CVD layer is a TaC layer.

3. The piston ring according to claim 1, wherein the predetermined thickness of the at least one PVD or CVD layer is 5 to 30 m.

4. The piston ring according to claim 1, wherein a base body of the piston ring is configured so that radial wall thickness of the piston ring is same in the region provided with the PVD or CVD layer and the regions not provided with the PVD or CVD layer.

5. The piston ring according to claim 1, wherein roughness of the regions provided with the PVD or CVD layer is different from roughness of regions not provided with the PVD or CVD layer.

6. A method for producing a piston ring according to claim 1, comprising providing a piston ring base body having the joint and made of gray cast iron or steel as a base material, the base body having a lesser wall thickness at said regions contiguous with the free ends than at the rest of circumferential length of the piston ring providing a region comprising at least the entire running face of the piston ring, up to the joint with at least one PVD or CVD layer, and removing the at least one PVD or CVD layer down to the base material of the piston ring at said regions contiguous with the free ends.

7. The method according to claim 6, wherein the at least one PVD or CVD layer is a TaC layer.

8. The method according to claim 6, wherein the removing of the at least one PVD or CVD layer is by grinding.

9. The method according to claim 6, wherein the base body is configured so that radial wall thickness of the piston ring is the same in the region provided with the PVD or CVD layer as in the regions not provided with the PVD or CVD layer.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0012] The subject matter of the invention is shown in the drawing based on an exemplary embodiment and is described as follows. In the drawings:

[0013] FIG. 1 shows a top view onto a fully machined piston ring; and

[0014] FIGS. 2 and 3 show different sections through the piston ring according to FIG. 1.

DETAILED DESCRIPTION OF THE INVENTION

[0015] FIG. 1 shows a piston ring designed 1 as a compression piston ring, comprising a running face 2, an inner circumferential surface 3, and upper and lower flank regions 4, 5. In the region of the running face 2, the piston ring 1 is provided with a wear-resistant layer 6, which in the present example is designed as a TaC layer and, in the present example, is to have a layer thickness of 15 m. The base material of the piston ring 1 is to be made of gray cast iron in the present example.

[0016] The piston ring 1 is furthermore provided with a joint 7. In the finished state, the piston ring 1 is provided, on both sides of the joint 7, with a non-coated circumferential section 8, 9 across a predefinable circumferential length I. This measure ensures that combustion gases passing through in the region of the joint 7 cannot reach the region of the TaC layer 6 directly. In this way, spalling of the layer is at least reduced, if not entirely suppressed, in the region of the joint 7.

[0017] In the fully machined state, the piston ring 1 has a radial wall thickness a, which is the same both in the coated region and in the non-coated circumferential section I. However, different roughness levels of the two regions are provided.

[0018] FIG. 2 shows a section A-A through the coating-free circumferential section 9 of the piston ring 1. In addition to the running face 2, the upper flank surface 4 and the lower flank surface 5 are apparent.

[0019] FIG. 3 shows a section B-B through a coated region of the piston ring 1. The running face 2, the upper flank surface 4 and the lower flank surface 5 are apparent here as well. In addition, the TaC layer 6 is indicated.