GB2112025A

GB2112025A - Surface treatment of metal rings

Info

Publication number: GB2112025A
Application number: GB08235341A
Authority: GB
Inventors: Norman Tommis
Original assignee: AE PLC
Current assignee: AE PLC
Priority date: 1981-12-16
Filing date: 1982-12-10
Publication date: 1983-07-13
Also published as: AU554451B2; CA1207642A; YU277882A; DD208830A5; AU9153682A; KR890001030B1; IT8224766A0; ES518226A0; IT8224766A1; FR2518209B1; US4531985A; BR8207278A; JPS58189369A; DE3245689C2; GB2112025B; DE3245689A1; TR22003A; FR2518209A1; AR229485A1; ZA829284B

Description

1 GB 2 112 025 A 1

SPECIFICATION Surface treatment of metal rings

The invention relates to nitro-carburised metal rings for use as piston rings or sealing rings.

Piston rings and sealing rings are commonly made of steel or cast iron and are generally rectangular in cross-section. The ring is located in and projects from a groove and has a radially outer surface in sliding contact with a co- operating surface of, for example, a cast iron cylinder. Two generally radially extending surfaces (herein after called "sides") engage with walls of the groove during the sliding movement. As a result of this both the radially outer surface and the sides are subjected to wear. Various techniques have been proposed for reducing some of this wear in order to increase the life of the ring and particular attention has been given to the reduction of the wear of the radially outer surfaces and the co- operating cylinder or liner. More recently, however, engine life requirements require not only reduced wear of the radially outer surfaces but also reduced wear of the sides and the cooperating groove walls.

One technique for reducing wear of the radially outer piston ring surfaces is immersing the rings in a nitro-carburising salt bath containing sodium and potassium salts with the rings heated to a temperature of, say, 4000C. In this nitro-carburising process, certain steels and cast irons of all types, e.g. grey irons, carbidic, martensitic, bainitic and spheroidal (nodular graphitic irons), have nitrogen and carbon simultaneously diffused into their surface to form a hardened surface layer.

British Patent Specification No. 1,576,143 discloses a process of salt bath nitro-carbu rising the surface of a sintered metal piston ring or sealing ring. The rings are immersed in the salt bath in a stack 20 i.e. with their sides in contact under the pressure of a weight. This is necessary because, if spaced apart, the rings will warp and lose their shape and flatness and also because individual treatment of each ring would be time consuming and expensive.

In this process, however, only the radially outer surfaces of the rings are nitro-carburised, because the rings are in a closed stack. In addition, the use of a salt bath is both slow and messy.

An alternative technique has been chromium plating in which the rings are again placed in a closed stack with their radially extending side surfaces in contact and then plated on their radially outer surfaces with chromium in a conventional way. In order to prevent the plating bridging adjacent rings, it is necessary to chamfer the edges of the rings between the radially outer surface and the sides. This is shown in Fig. 1 which is a photo-micrograph of a part of a cross- section of a piston ring at the corner 30 between a radially outer surface of the ring and a side of the ring.

In this process only the radially outer surfaces of the rings are plated as will be seen from Figure 1. The sides can be chromium plated in a subsequent plating operation but this is relatively expensive. The chamfered edges of the rings, when in use, tend to increase oil. seepage past the rings and thus tend to increase oil consumption, as well as reducing the effectiveness of the seal between the ring and 35 cylinder so increasing blow-by. Thus chamfers are undesirable. Further, chromium plating softens progressively at temperatures above 2500C to 3000C and this is also a disadvantage. In addition, the chromium plated rings require finishing operations which involve lapping and this increases the cost of their production.

According to a first aspect of the invention, there is provided a process for nitro-carburising metal 40 rings of generally rectangular cross-section for use as piston rings or sealing rings, and comprising forming a stack of rings with adjacent rings in contact, placing the stack of rings in a chamber from which air is excluded and then supplying to the chamber a gaseous mixture of a carburising gas and a nitrogeneous gas in the ratio of from 25:75 to 75:25 (% by volume) at a temperature of from 450'C to 6501C to nitro-carburise the radially outer surface and the sides of the rings. 45 It has been found that the use of gaseous nitro-carburising allows the nitro-carbu rising treatment to extend not only over the radially outer surfaces of the rings in a stack but also over the sides even though the rings are in a stack. This therefore gives all these three surfaces a hardened finish, thus increasing their overall wear resistance.

According to a second aspect of the invention, there is provided a piston ring for an engine or a 50 compressor or a sealing ring for a shock absorber when made by the method of the first aspect of the invention.

According to a third aspect of the invention, there is provided a metal ring of generally rectangular cross-section for use as a piston ring or a sealing ring, the ring having a radially outer surface and sides hardened by n itro-ca rbu rising and being finish machined before nitro-carbu rising. 55 The following is a more detailed description of some embodiments of the invention, by way of example, reference being made to the accompanying Figure 2 which is a photo-micrograph of a cross section of a part of a nitro-carburised piston ring at the corner between a radially outer surface of the ring and a side of the ring.

A piston ring is prepared and is finished machined to be of generally rectangular cross-section 60 with a gap cut through the ring to afford two free ends. The ring thus has a radially outer surface which, in use, will be in sliding contact with an engine cylinder, and two radially extending surfaces or'sides' which will contact the walls of a piston ring groove in a piston in which the ring is mounted. The piston 2 GB 2 112 025 A 2 ring may be of the rail type used as oil control rings or a top ring (i.e. the ring closest to the crown of the associated piston), in particular a top compresssion ring.

The ring may be of any suitable ferrous material which can be satisfactorily nitro-carburised and which maintains its hardness, and hence its spring and resistance-to-set, both when treated and when run in an engine. Two such materials are high strength carbitic cast irons and steel. For example, a suitable steel has the composition 0.47% carbon, 0.25% silicon, 0.75% manganese, 0.55% nickel, 1 % chromium, 1 %, molybdenum, 0. 1 % vanadium, remainder iron (all by weight) hardened and tempered to a hardness of 450-500 HV.

A plurality of such finish machined rings are placed on a jig in a stack with their sides in contact and with their gaps open. This ensures that during subsequent operations the rings remain flat and 10 undistorted.

The stack of rings are then placed in a chamber from which air is excluded. Next a nitrogenous gas, such as ammonia, and a carburising gas, such as an exothermic hydrocarbon gas, are fed into the chamber at a temperature of between 4500C and 6500C. The proportion of the two gases, nitrogenous to carburising, may be between 25:75 (% by volume) and 75:25 (% by volume) although tests with ammonia and exothermic hydrocarbon gas have shown that ratios of 50:50 (% by volume) or 60-40 (% by volume) give improved results.

The gases reach the radially outer surfaces of the stacked rings and also penetrate between the rings to reach the sides of the rings. Carbon and nitrogen from the gases diffuses from these surfaces into the cast iron of the rings forming a white " " layer between 2 and 10 micrometers thick from which diffusion takes place into the body of the rings. For a particular material, the total depth of penetration depends on the time for which the gases are supplied and this may be regulated to give, for example, a white layer 5 micrometers thick and a total penetration of 0. 1 m to 0.3 mm. A surface hardness of 700-800 HV is achievable decreasing progressively to the hardness of the basic material.

This hardness is maintained on subsequent exposure of the rings to temperatures of up to 6000C.

The stack of rings is then removed from the chamber and the rings separated from the stack. This is achieved without difficulty and the rings are ready for use forthwith without any further treatment.

The piston rings so produced may be compression rings or oil control rings. The treatment is rapid and clean and provides in a single treatment a ring which is hardened on three surfaces.

A part of the finished ring is shown in Figure 2. It will be seen that the nitro-carburised surface 30 extends over both the radially outer surface 10 and the side 11. It will also be seen that the corner between these two surfaces is a sharp right angle.

The following Examples are given by way of illustration.

Example 1

A piston ring of high strength carbitic steel was nitro-carburised as described above at a 35 temperature of 5500C. In one embodiment, the piston ring was exposed to the nitro-carburising gases for a time which gave a total penetration of 0. 10 mm and a compound white surface "" layer whose thickness was 0.005 mm. The surface layer had a hardness of HVIV1 700-800.

A typical hardness penetration curve for such a piston ring is as followsa 1 80a 700 HARDNESS 600 MM). 500 400 300 v 1 0-b5 040 0 k o.o FENETRATION (mm) Nitro-carburised piston rings prepared as described above were used as the top compression piston rings in a two litre engine of a motor car. The rings were found not to scuff and to give satisfactory peormance. In contrast, chromium plated piston rings prepared as described above with reference to Figurg-1 were found to scuff and be unusable. As a result of this, the engine had previously 45 used hard flame sprayed molybdenum rings, which are expensive and difficult to manufacture.

Nitro-carburised piston rings, prepared as described above with reference to Example 1 were also compared with chromium plated piston rings prepared as described above with reference to Figure 1 by fitting the nitro-carburised rings in the top ring grooves of the piston in cylinders 1 and 3 of a 4cylinder 1.3 litre petrol engine. The chrome plated rings were fitted in the top ring grooves of cylinders 50 2 and 4.

After 50,000 miles the following results were obtained- 3 GB 2 112 025 A 3 Cylinder Surface Ring side Groove side Ring radial Max. bore No. treatment wear (M x 10-4) wear (m x 10-4j wear (m x 10-4) wear (m x 10-4) 1. N.C. 0.25 0.104 1.65 0.63 2. Chrome 0.61 0.12 1.9 0.51 3. N.C. 0.18 0.11 2.03 0.51 4. Chrome 0.76 0.12 1.9 0.63 v N.C.-Ring nitro-carburised on O.D. and side faces as described above b way of example. Chrome-Plated on outside diameter only-not treated on side faces. The piston ring of Example 1 has an elastic modulus and core hardness which are unaffected by the treatment. The fatigue strength is increased by approximately 10%. Although the piston ring of 10 Example 1 is more brittle than an untreated ring, when subjected to excessive twisting or gap opening, the ring still meets the required minimum ring tensile and bending strengths as laid down for untreated rings.

Example 2

A piston ring of steel was prepared, the steel having the following composition by weight:- 15 carbon silicon manganese nickel chromium molybdenum vanadium balance iron 0.47% 0.25% 0.75% 0.55% 1 % 1 % 0.1% The piston ring was hardened and tempered to a hardness of 450-500 HV and then nitro25 carburised as described above. In one embodiment, the piston ring was exposed to the nitrocarburising gases for a time which gave a total penetration of 0.015-0.020 mm and a compound white surface "" layer whose thickness was 0.005--0.008 mm. The surface layer had a hardness of about HVM 800.

A typical hardness penetration curve for such a ring is as follows:-, 800 MICRO 700 HESS (HVM) 600 500 400 O.b5 0.'10 0.15 020 0.25 PENETRATION (mm) Nitro-carburised piston rings prepared as described above were used in the top compression piston rings in a two litre engine of a motor car. The rings were found not to scuff and to give satisfactory performance. In contrast, chromium plated piston rings prepared as described above with reference to Figure 1 were found to scuff and be unusable. As a result of this the engine had previously 35 hard flame sprayed molybdenum rings, which are expensive and difficult to manufacture.

Nitro-carburised piston rings, prepared as described above with reference to Example 2 were also compared with chromium plated piston rings prepared as described above with reference to Figure 1 by fitting the nitro-carburised rings in the top ring grooves of the piston in cylinders 1 and 3 of a 4cylinder litre petrol engine. The chrome plated rings were fitted in the top rings grooves of cylinders 2 40 and 4.

After 180 hours (equivalent to 15,000 miles under high speed test conditions) the following results were obtained:- Cylinder Surface Ring side Groove side Ring radial Max. bore No. treatment wear (m X 10-4) wear (m x 10) wear (m x 10-4) wear (m x 10- 4) 1. N.C. 0.013 0.10 0.025 0.08 45 2. Chrome 0.051 0.10 0.51 0.15 3. N.C. 0.025 0.08 0.025 0.13 4. Chrome 0.08 0.08 0.38 0.18 N.C.-Ring nitro-carburised on O.D. and side faces as described above by way of example. 50 Chrome-Plated on outside diameter only-not treated on side faces.

4 GB 2 112 025 A The piston ring of Example 2 maintained its spring and wall pressure at top ring groove operating temperatures. Its loss in gap when enclosed in a sleeve of bore diameter equal to the ring diameter and heated for 6 hours at 35011C and cooled in the sleeve, was 5.5%. This compares with 7- 10% for martensitic spheroidal grey modular cast iron rings (not nitro- carburised) and 15% or more for medium 5 phospherous grey cast iron rings (not nitro-carburised) individually cast.

It will be seen from the foregoing Examples 1 and 2 that the wear on the radially outermost surface of the nitro-carburised rings is comparable with that of chromium plated rings but that the wear of the sides is very much less than the side wear of the chromium plated rings. It will be appreciated that this wear resistance is achieved in a single treatment step. This reduction in wear improves the sealing performance of the rings and also increases their life because the increase in 10 fatigue strength coupled with reduced side wear reduces the incidence of breakage and reduces the rate of increase of blowby.

The radially outer surfaces of nitro-carburlsed rings have a better scuffresistance than the corresponding surfaces of chromium plated rings. This is partly because of the better resistance of nitro- carburised surfaces to temperatures above 2500C to 3000C and because oil does not readily wet 15 chromium whereas the nitro-carburised surface retains the cavities formed by graphite flakes in the iron and these act as oil reservoirs.

It will further be appreciated that the n itro-ca rbu rising process described above with reference to Figure 2 may be used to harden the surfces of any form of piston ring such as oil control rings or intermediate compression rings, or any form of sealing ring, such as sealing rings for shock absorbers. 20 When the rings are made of steel, the use of the nitro-carbu rising technique described above by way of example allows the width of the rings to be reduced to 1 mm or less because the reduced side wear reduces the incidence of breakage. Where the rings are of the rail type, the nitro- carburising of the sides of the ring reduces wear between the ring and the expander used in such oil control ring assemblies and minimises the cut into the rail of lugs provided on the expander.

Claims

1. A process for nitro-carburising metal rings of generally rectangular cross-section for use as piston rings or sealing rings, and comprising forming a stack of rings with adjacent rings in contact, placing the stack of rings in a chamber from which air is excluded and then supplying to the chamber a gaseous mixture of a carburising gas and a nitrogenous gas in the ratio of from 25:75 to 75:25 (% by 30 volume) at a temperature of from 4500C to 6500C to nitro-carburise the radially outer surface and the sides of the rings.

2. A process according to Claim 1 wherein the nitrogenous gas is ammonia.

3. A process according to Claim 2 wherein the carburising gas is an exothermic hydrocarbon gas.

4. A process according to any one of Claims 1 to 3 wherein the proportions of the gases are 35 50:50 (% by volume).

5. A process according to any one of Claims 1 to 3 wherein the proportions of the gases are 60:40 (% by volume).

6. A process according to any one of Claims 1 to 5 wherein the temperature is 5500C.

7. A process according to any one of Claims 1 to 6 wherein the rings are finish machined before 40 being stacked, so that- after the n ltro-ca rbu rising process they are ready for use.

8. A process according to any one of Claims 1 to 7 and in which the rings have a gap therein, and are to form piston rings, the rings being stacked with their gaps open.

9. A process according to any one of Claims 1 to 8 wherein the time for which nitro-carburising takes place is such that the total depth of nitro-carbu rising on the surfaces of the rings is from 0.015 mm to 0.3 mm.

10. A nitro-carburising process substantially as hereinbefore described with reference to Figure 2 of the accompanying drawings and/or in the foregoing Examples 1 and 2.

11. A piston ring for an engine or a compressor or a sealing ring for a shock absorber when made by the method of any one of Claims 1 to 10.

12. A metal ring of generally rectangular cross-section for use as a piston ring or as a sealing ring, the ring having a radially outer surface and sides hardened by nitro-carburising and being finish machined before nitro-carbu rising.

13. A metal ring according to Claim 12 wherein the depth of the nitrocarburisation is from 0.015 mm to 0.3 mm.

14. A metal ring according to Claim 12 or Claim 13 wherein the ring is of cast iron or steel.

15. A metal ring substantially as hereinbefore described with reference to Figure 2 of the accompanying drawings and/or in the foregoing Examples 1 and 2.

Printed for Her Majesty's i 1.

1 Stationery office by the Courier Press, Leamington Spa, 1983. Published by the Patent Office, 25 Southampton Buildings, London, WC2A lAY, from which copies may be obtained