Coated steel piston ring

Abstract

A piston ring is formed from a steel substrate consisting of the carbon in a range of 0.80-0.95 wt. %, silicon in a range of 0.30-0.55 wt. %, manganese in a range of 0.25-0.5 wt. %, phosphorus in a range of up to 0.04 wt. %, sulfur in a range of up to 0.04 wt. %, chromium in a range of 17-18 wt. %, molybdenum in a range of 0.70-1.25 wt. %, vanadium in a range of 0.05-0.15%, the remainder iron. The ring has been through hardened and tempered so that it has a hardness of 46-54 HRC. A coating is then applied via PVD or other suitable methods onto the ring surface to create the finished piston ring.

Claims

1. A piston ring comprising: a steel substrate consisting of the following components: carbon in a range of 0.80-0.95 wt. % silicon in a range of 0.30-0.55 wt. % manganese in a range of 0.25-0.5 wt. % phosphorus in a range of up to 0.04 wt. % sulfur in a range of up to 0.04 wt. % chromium in a range of 17-18 wt. % molybdenum in a range of 0.70-1.25 wt. % vanadium in a range of 0.05-0.15% the remainder iron, and a coating on the steel substrate, wherein the piston ring has a hardness of 38-42 HRC through an entire thickness of the piston ring after through-hardening and tempering.

2. The piston ring according to claim 1, wherein the coating has been applied by physical vapor deposition.

3. The piston ring according to claim 1, wherein the coating is CrN.

4. A method for forming a piston ring comprising: forming a ring with a steel substrate, the steel consisting of: carbon in a range of 0.80-0.95 wt. % silicon in a range of 0.30-0.55 wt. % manganese in a range of 0.25-0.5wt. % phosphorus in a range of up to 0.04 wt. % sulfur in a range of up to 0.04 wt. % chromium in a range of 17-18 wt. % molybdenum in a range of 0.70-1.25 wt. % vanadium in a range of 0.05-0.15% the remainder iron, and through-hardening the ring by heating the ring above a transformation temperature of the steel, quenching the heated ring and tempering the ring by re-heating the ring to achieve a hardness of 38-42 HRC through an entire thickness of the piston ring; and applying a coating to the ring.

5. The method according to claim 4, wherein the step of applying the coating comprises applying the coating via physical vapor deposition.

6. The method according to claim 5, wherein the coating is formed of CrN.

7. The piston ring according to claim 6, wherein the coating is CrN.

8. The piston ring according to claim 1, wherein the coating is CrN.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Other objects and features of the present invention will become apparent from the following detailed description considered in connection with the accompanying drawings. It is to be understood, however, that the drawings are designed as an illustration only and not as a definition of the limits of the invention.

(2) In the drawings:

(3) FIG. 1A shows a section of a piston ring according to the invention;

(4) FIG. 1B shows a section of a piston ring according to the prior art;

(5) FIG. 2 shows a cross-section of the piston ring according to the invention;

(6) FIG. 3 shows a photograph of the material used in the piston ring according to the invention;

(7) FIGS. 4 and 5 show photographs of comparison materials; and

(8) FIG. 6 shows a graph of common steel compounds comparing the material hardness according to the invention with other materials.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

(9) The piston ring 1 according to the invention as shown in FIGS. 1 and 2 is formed from AISI440B Steel that after rolling and forming has been completed, is through hardened by heating above the transformation stage, rapid quenching and then reheating to a lower temperature to temper the ring and heat shape it on a cam shaped plug. The ring is lapped, and grinding is done on an outer diameter surface, in preparation for coating. The ring is then coated with a coating 2, via PVD or other suitable methods. The coating 2 is located on the outer diameter surface of the ring and offers a running surface for sealing against the cylinder wall (not shown), as is well known in the art.

(10) The material of the piston ring in one form, AISI440B steel, has the following composition (shown as percentages by weight) across two different specifications:

(11) TABLE-US-00001 Elements Specification A Specification B C 0.80-0.95 0.80-0.95 Si 0.50 max 0.30-0.55 Mn 0.25-0.40 0.25-0.50 P 0.040 max 0.040 max S 0.040 max 0.040 max Cr 17.0-18.0 17.0-18.0 Mo 1.00-1.25 0.70-1.15 V 0.08-0.15 0.05-0.10

(12) The AISI440B metal wire, before any heat treatment, has a hardness HR30N of 58-62, an HRC of 38-42, and an HV of 370-420. The material has a tensile strength of 1000-1325 MPa. The lower hardness of the AISI440B metal is typically needed to allow for the coiling and shaping of the wire, before it is case hardened or heat treated, since hardness rating that are higher commonly have cracking issues during the shaping process.

(13) The AISI440B steel composition according to the invention is shown magnified in FIG. 3, after the through-hardening process. As can be seen, the AISI440B steel has a complex mix of small and large carbides present, which increases the hardness of the overall material. Carbides with hardened matrix increases the fatigue strength, wear resistance, and galling resistance of the piston ring. In addition, the AISI440B steel with the mix of carbides allows increasing wear resistance and fatigue improvements even without additional plating, and no nitride or case hardening processing. The AISI440B uses the hard carbide compounds as added wear protection. Having been through hardened, the ring has no soft matrix and exhibits improved wear surface as compared to case hardened materials, as the case hardened surface may wear through, possibly causing failure of the ring. The carbides in combination with a through hardened ring remove one failure mode of the ring and the case hardened surface. The through hardened metal with the even distribution of the complex carbides provide a hard compound that protects against wear and galling of the lateral sides. At lower HRC of 42-43, there will be galling. The combination of the increased carbides within a high hardness martensitic matrix of the steel of the present invention improves galling resistance and reduces the fatigue failure of case hardened materials.

(14) FIG. 1 illustrates the improvement of the subject invention, as after 1000 hours there is no visible galling of the lateral surfaces. In contrast, FIG. 1B illustrates a prior art case hardened ring and galling is noted on the lateral side surfaces. In addition, the increased hardness and through hardening treatment increase the fatigue strength by approximately 20% and greatly reduces the likelihood of crack propagation due to the lateral wearing through the case hardened depth.

(15) In comparison, other materials such as hardened ductile iron, which is shown in FIG. 4, is lacking the complex distribution of carbide particles of ANSI440B. AISI9254 (FIG. 5) has no carbides at all. As shown in FIG. 6, basic Martensite, which is similar to AISI9254, a CrSi steel shown in FIG. 5, has substantially lower hardness than Fe.sub.3C (cementite), which is similar to hardened ductile iron (FIG. 4) and especially lower hardness when compared to the complex carbides of MC, M.sub.2C, M.sub.6C and that are present in the AISI440B steel of the present invention.

(16) Through-hardening the formed ring that is made with the carbide-rich steel, such as the composition disclosed above for the AISI440B steel, results in a ring that exhibits substantial hardness and resistance to bending or flexing of the outer surface of the coating, especially when compared to case-hardened materials. The coating thus adheres exceptionally well and is more resistant to flaking, since the ring metal does not have a soft metal matrix below the case hardened surface depth that may flex to propagate cracks in the OD coating. In addition, by through hardening the ring, some typical failure modes with the ring are avoided, such as nitriding or case hardening wearing through on the lateral sides, causing galling and at time ring failures.

(17) In addition, the increased lateral side protection is achieved with of the steel of the present invention, which provides for a harder lateral surface, since the complex mix of carbides in the material of the present invention provides increased wear resistance. Also, since the steel is through hardened, there is no case hardened surface to wear through in high load applications. Therefore, increasing the hardness of an AISI440B metal with the carbides may reduce the periodic galling of the ring, particularly on the lateral sides of the piston ring. In some instances the through hardening may also eliminate the need for side chrome plating, and/or nitriding of the ring material before applying the coating. The hardened ring according to the invention has an increased hardness to a range greater than 45 HRC and in some embodiments above 48 HRC. In one example, the hardness is further increased, targeting above 50 HRC and with the range of 46-54 HRC. The increased hardness and formation of the complex carbides in the AISI440B ring results in an improvement to the fatigue strength by a minimum of 20% compared to the same base material that has been nitrided, chrome plated, and OD coated with a similar coating composition.

(18) The through hardening heat treatment further provides improvement to the manufacturing process of the piston ring, by lowering the machining cost. The process allows for the removal of the typical additional keystone grinding operation after the case hardening treatment of the ring.

(19) Accordingly, while only a few embodiments of the present invention have been shown and described, it is obvious that many changes and modifications may be made thereunto without departing from the spirit and scope of the invention.