WO2015082246A1 - Piston ring and heat treatment process - Google Patents
Piston ring and heat treatment process Download PDFInfo
- Publication number
- WO2015082246A1 WO2015082246A1 PCT/EP2014/075413 EP2014075413W WO2015082246A1 WO 2015082246 A1 WO2015082246 A1 WO 2015082246A1 EP 2014075413 W EP2014075413 W EP 2014075413W WO 2015082246 A1 WO2015082246 A1 WO 2015082246A1
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- WO
- WIPO (PCT)
- Prior art keywords
- piston
- ring
- laser beam
- carbon
- covering
- Prior art date
Links
- 238000000034 method Methods 0.000 title claims description 32
- 230000008569 process Effects 0.000 title claims description 31
- 238000010438 heat treatment Methods 0.000 title claims description 7
- 229910000975 Carbon steel Inorganic materials 0.000 claims abstract description 12
- 239000010962 carbon steel Substances 0.000 claims abstract description 12
- 238000005256 carbonitriding Methods 0.000 claims description 16
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 14
- 238000000576 coating method Methods 0.000 claims description 13
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 11
- 229910052799 carbon Inorganic materials 0.000 claims description 11
- 239000006229 carbon black Substances 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 8
- 238000009792 diffusion process Methods 0.000 claims description 7
- 229910052757 nitrogen Inorganic materials 0.000 claims description 7
- 239000007789 gas Substances 0.000 claims description 6
- 230000015572 biosynthetic process Effects 0.000 claims description 5
- 229910000734 martensite Inorganic materials 0.000 claims description 5
- 238000005240 physical vapour deposition Methods 0.000 claims description 4
- 230000007704 transition Effects 0.000 claims description 4
- 125000004432 carbon atom Chemical group C* 0.000 claims description 3
- 150000001875 compounds Chemical class 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 3
- 230000001737 promoting effect Effects 0.000 claims description 3
- 229910001566 austenite Inorganic materials 0.000 claims description 2
- 239000011159 matrix material Substances 0.000 claims 1
- 230000000717 retained effect Effects 0.000 claims 1
- 230000006835 compression Effects 0.000 abstract description 8
- 238000007906 compression Methods 0.000 abstract description 8
- 239000000463 material Substances 0.000 description 9
- 239000010410 layer Substances 0.000 description 8
- 230000008901 benefit Effects 0.000 description 3
- 229910001141 Ductile iron Inorganic materials 0.000 description 2
- 229910001060 Gray iron Inorganic materials 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000011156 metal matrix composite Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 125000004433 nitrogen atom Chemical group N* 0.000 description 2
- 230000003389 potentiating effect Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910019819 Cr—Si Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910011208 Ti—N Inorganic materials 0.000 description 1
- 230000003213 activating effect Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 239000008246 gaseous mixture Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 238000005121 nitriding Methods 0.000 description 1
- 229910001562 pearlite Inorganic materials 0.000 description 1
- 238000007712 rapid solidification Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000002344 surface layer Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/26—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction characterised by the use of particular materials
Definitions
- the present invention relates to a piston ring, being in particular a first-groove ring, which meets the performance requirements without having any type of coating on its lower surface.
- the ring is based on carbon steel and its lower surface is hardened by a process of cementation or laser carbonitriding .
- the first-groove piston ring also known as compression ring, is the one that is subjected to the largest forces and stresses when the engine is in operation.
- the ring moves slightly in the axial direction, causing wear on its upper and lower surfaces, and not only wear on the surface of the external diameter, facing the cylinder wall.
- TDC top dead centre
- BDC bottom dead centre
- Japanese patent JP4452641 relates to a piston ring comprising a ferrous-metal or aluminium base, a nitrided layer and a coating in the form of a film of a Cr-B-Ti-N alloy, applied by the PVD (physical vapour deposition) process.
- This coating was designed so as to offer good properties of hardness and ductility, however its application generates an increase in the cost of manufacture of the ring that may not be commercially viable in some applications.
- Japanese patent JP 3239610 relates to a piston ring for use in the groove of a piston made of an aluminium alloy (metal matrix composite - MMC) .
- the ring comprises a nitrided coating layer or a coating formed only on the outer lateral surface.
- the hardness of the upper and lower surfaces of the ring is from about 400HV to 600HV, obtained by the cementation or hardening process.
- US patent 4,531,985 relates to a piston ring whose outer surfaces are treated in a chamber with a gaseous mixture of a gas with carbon and a gas with nitrogen, at a temperature between 450°C and 650°C.
- the proportions of the gases have values between 25:75 and 75:25 and this gas mixture provides carbonitriding of the surfaces of the ring.
- the surfaces of the ring are finished mechanically before the treatment.
- a piston ring based on carbon steel whose lower lateral surface has a cemented or carbonitrided layer with thickness between lOOym and 300ym and hardness between 700HV and 1000HV has not yet been developed and described .
- One aim of the present invention is a piston ring based on carbon steel whose lower surface is hardened by a process of cementation or laser carbonitriding.
- Another aim of the present invention is a piston ring based on carbon steel whose lower surface is hardened by a process of cementation or laser carbonitriding to give a cemented or carbonitrided layer with thickness between lOOym and 300ym and hardness between 700HV and 1000HV.
- a piston ring in particular a compression ring, provided with a carbon steel base whose cross-section defines an outer surface slidably associable to the wall of a cylinder, an upper surface associable to the groove of a piston, facing the piston crown and a lower lateral surface associable to the groove of a piston, facing the piston skirt, wherein at least a portion of the lower surface comprises a carbonitrided layer that has a thickness between lOOym and 300ym and hardness between 700HV and 1000HV.
- Step (i) covering at least a portion of the lower surface of the ring with a covering of carbon black or any other carbon-based compound
- Step (ii) application of a laser beam on the covering of carbon black applied with precise control of location and depth.
- the laser beam is applied and heats the spot until the austenitizing temperature is reached, promoting diffusion of carbon atoms present in the covering of carbon black from the surface towards the interior of the base.
- Step (ii) comprises rapid cooling of the region where the laser beam is applied for formation of martensite.
- Fig. 1 - is a schematic partial view of a compression ring mounted on an engine piston that moves towards TDC, illustrating a critical situation of wear of its lower surface.
- Fig. 2 - is an enlarged photograph of a section of the piston ring according to the present invention, on its lower surface.
- Fig. 3 - is a schematic view of equipment for the process of laser carbonitriding applied to the piston ring according to the present invention.
- Fig. 4 - is a schematic comparative view of the lower surface of the piston ring before and after the process of laser carbonitriding.
- Fig. 5 - is a schematic sectional view of the piston ring according to the present invention before the process of laser carbonitriding.
- Fig. 6 - is a schematic sectional view of the piston ring according to the present invention after the process of laser carbonitriding.
- Fig. 7 - is a chart of wear of the piston ring according to the present invention compared with other piston rings of the prior art.
- the piston ring according to the present invention was developed after long studies with the objective of providing a long useful life and a cost of production that makes it viable for commercial application for engines .
- Piston rings undergo wear not only on their outer surface that faces the cylinder wall.
- the constant friction of the ring with the piston groove leads to wear on its upper surfaces (facing the piston top or crown) and lower surfaces (facing the piston skirt) .
- the first-groove piston ring also known as compression ring
- compression ring is the one that is subjected to the largest forces and stresses when the engine is in operation.
- the compression ring which is mounted in the (first) piston groove, moves slightly in the axial direction, causing wear on its upper and lower surfaces.
- TDC top dead centre
- This situation occurs thousands of times per minute in normal operation of an engine and is shown schematically in Fig. 1.
- piston ring 1 is a compression ring, but it is obvious that it may assume other configurations, such as that of a second-groove ring or of an oil scraper ring, without the resultant invention leaving the scope of protection of the appended claims.
- ring 1 according to the present invention meets the performance requirements without having any type of coating or nitriding on its lower surface, but does have hardening on at least a portion of this surface by means of a process of cementation or laser carbonitriding .
- Another imperative characteristic for this carbonitriding process to be effective is that the base material from which ring 1 is constituted is carbon steel, with any required or desirable composition.
- ring 1 is provided with a base 2 of carbon steel whose cross-section may assume the most varied configurations provided that they define an outer lateral surface 3 slidably associable to the wall D of a cylinder, an upper surface 4 associable to the groove C of a piston P, facing the piston crown and a lower surface 5 associable to the groove C of a piston P, facing the skirt S of the piston.
- FIG. 6 This is the basic geometry for a compression ring to perform its required function.
- a non-limiting configuration of the cross-section of the ring 1 may be seen in Fig. 6. It is precisely a portion of the lower surface 5, or all of it, that undergoes the process of laser carbonitriding that will be described hereunder, and that increases the surface hardness in that region, greatly reducing the wear of the ring in constant friction with the piston groove.
- Cementation or carbonitriding is a thermochemical treatment that consists of introducing carbon and/or nitrogen into the surface of a carbon-steel component with the aim of increasing the surface hardness.
- the carbon and/or nitrogen atoms supplied by a source material are inserted on the basis of heating of the region that is to undergo cementation, as will be described below. Then the surface is cooled rapidly, and the higher carbon content in the surface layers leads to an increase in surface hardness, increase in wear resistance and increase in tensile fatigue strength.
- Another characteristic feature resulting from this process is a change (generally increase) in grain size.
- ring 1 undergoes a process of cementation or laser carbonitriding.
- the equipment employed for carrying out the process comprises a source that emits laser rays, which serve as a heat source of high power and precision, activating the transfer of carbon and/or nitrogen from a source material.
- Fig. 3 shows, schematically, the equipment 10 for carrying out the process of carbonitriding with the laser beam 13. It comprises a source that emits laser rays 11, an optional mirror 12 for guiding this beam and one or more focusing lenses 14 to allow focusing of the entire spectrum of the laser beam 13 on quite a small area or point, thereby ensuring both high heating power and very precise control of the area be treated.
- the surface to be treated 5 is applied in an environment in the presence of a gas based on nitrogen, for the purpose of making diffusion of this element possible.
- the heat treatment process for treating at least a portion of the lower surface 5 of the piston ring according to the present invention is an invention included in the scope of protection of the appended claims and comprises step (i) , of covering at least a portion of the lower surface 5 of the ring with a covering of carbon black 6 or any other carbon- based compound; and step (ii) , of application of a laser beam 13 on the covering of carbon black 6 applied with precise control of location and depth.
- step (ii) the laser beam 13 is applied and heats the surface 5 until the austenitizing temperature is reached, promoting diffusion of carbon atoms present in the covering of carbon black (6) and the nitrogen atoms present in the gaseous atmosphere from the surface 5 towards the interior of the base.
- Step (ii) further comprises rapid cooling of the region where the laser beam is applied for formation of martensite. Formation of the carbonitrided layer 7 is illustrated schematically in Fig. 4.
- the laser beam causes rapid melting of the material, but as it is applied for a short time and only on the surface, the rest of the material remains at its initial temperature, called cold temperature hereinafter, and functions as a heat barrier.
- cold temperature the initial temperature
- the exposure time (or pulse) has a considerable influence on the depth of material that will be melted.
- long exposure times provide deeper fusion. Since a material melted to a greater depth obviously means a longer time that it remains in the molten state, there will be more time available for diffusion of one or more alloying elements (such as carbon or nitrogen) there. Thus, a material melted to a greater depth and for a longer time results in the formation of more dilute alloys, and vice-versa.
- the resultant ring 1 has, finally, a lower surface 5 in which the portion treated comprises a carbonitrided layer 7 that has a thickness between lOOym and 300ym and hardness between 700HV and 1000HV. More preferably, the carbonitrided layer 7 has a thickness of substantially lOOym and also has a transition layer 5' with a thickness of substantially 200ym, which begins at a depth of lOOym and reaches a depth of 300ym reckoned from the outer surface.
- the chart shown in Fig. 7 illustrates the values of wear resistance of the present ring 1 when compared to rings currently in use. Tests confirmed that ring 1 according to the present invention displays reduced wear values, almost as good as that displayed by rings of nitrided stainless steel (GNS) with 60ym and rings of grey cast iron (GCI), and far more advantageous than that displayed by rings of nodular cast iron (NCI) and by rings of Cr-Si steel.
- GGS nitrided stainless steel
- GCI grey cast iron
- NCI nodular cast iron
Abstract
The present invention relates to a piston ring, in particular a compression ring, provided with a base (2) of carbon steel whose cross-section defines an outer lateral surface (3) slidably associable to the wall (D) of a cylinder, an upper surface (4) associable to the groove (C) of a piston (P), facing the piston crown and a lower surface (5) associable to the groove (C) of a piston (P), facing the piston skirt (S), wherein at least a portion of the lower surface (5) comprises a carbonitrided layer (7) that has a thickness between 100pm and 300pm and hardness between 700HV and 1000HV.
Description
Specification of the Patent for "PISTON RING AND HEAT TREATMENT PROCESS".
The present invention relates to a piston ring, being in particular a first-groove ring, which meets the performance requirements without having any type of coating on its lower surface. The ring is based on carbon steel and its lower surface is hardened by a process of cementation or laser carbonitriding .
Description of the prior art
The first-groove piston ring, also known as compression ring, is the one that is subjected to the largest forces and stresses when the engine is in operation. When mounted in the first groove of the piston, the ring moves slightly in the axial direction, causing wear on its upper and lower surfaces, and not only wear on the surface of the external diameter, facing the cylinder wall.
One of the most critical situations for wear occurs at the moments when the piston moves towards top dead centre (TDC) , which generates interference of the lower surface of the ring with the cylinder groove, potentiating wear in that region. Another fairly critical situation occurs at the beginning of the expansion stroke (PCP) , i.e. when the piston moves towards bottom dead centre (BDC) , also generating interference on the lower surface.
One way of reducing this wear consists of applying coatings on the ring. As a rule, these coatings have advantageous properties with respect to hardness, which allows good performance of the ring with respect to wear; however, the low ductility of these hard coatings causes undesirable fractures, often with the occurrence of detachment, which reduces the useful life of the piston ring.
As another aspect, there are coatings that have good ductility values and as a corollary resist detachment quite well, but conversely they do not give the desired performance with respect to wear resistance.
Various solutions for piston ring coating have been proposed by experts in this area, some of which are described below.
Japanese patent JP4452641 relates to a piston ring comprising a ferrous-metal or aluminium base, a nitrided layer and a coating in the form of a film of a Cr-B-Ti-N alloy, applied by the PVD (physical vapour deposition) process. This coating was designed so as to offer good properties of hardness and ductility, however its application generates an increase in the cost of manufacture of the ring that may not be commercially viable in some applications.
Japanese patent JP 3239610 relates to a piston ring for use in the groove of a piston made of an aluminium alloy (metal matrix composite - MMC) . The ring comprises a nitrided coating layer or a coating formed only on the outer lateral surface. The hardness of the upper and lower surfaces of the ring is from about 400HV to 600HV, obtained by the cementation or hardening process.
US patent 4,531,985 relates to a piston ring whose outer surfaces are treated in a chamber with a gaseous mixture of a gas with carbon and a gas with nitrogen, at a temperature between 450°C and 650°C. The proportions of the gases have values between 25:75 and 75:25 and this gas mixture provides carbonitriding of the surfaces of the ring. The surfaces of the ring are finished mechanically before the treatment.
A piston ring based on carbon steel whose lower lateral surface has a cemented or carbonitrided layer with thickness between lOOym and 300ym and hardness between 700HV and 1000HV has not yet been developed and described .
Aims of the invention
One aim of the present invention is a piston ring based on carbon steel whose lower surface is hardened by a process of cementation or laser carbonitriding.
Another aim of the present invention is a piston ring based on carbon steel whose lower surface is
hardened by a process of cementation or laser carbonitriding to give a cemented or carbonitrided layer with thickness between lOOym and 300ym and hardness between 700HV and 1000HV.
Brief description of the invention
The aims of the present invention are achieved with a piston ring, in particular a compression ring, provided with a carbon steel base whose cross-section defines an outer surface slidably associable to the wall of a cylinder, an upper surface associable to the groove of a piston, facing the piston crown and a lower lateral surface associable to the groove of a piston, facing the piston skirt, wherein at least a portion of the lower surface comprises a carbonitrided layer that has a thickness between lOOym and 300ym and hardness between 700HV and 1000HV.
The aims of the present invention are also achieved by a heat treatment process for treating at least a portion of the lower surface of the piston ring defined in the preceding paragraph, comprising the following steps:
Step (i) : covering at least a portion of the lower surface of the ring with a covering of carbon black or any other carbon-based compound; and
Step (ii) : application of a laser beam on the covering of carbon black applied with precise control of location and depth.
The laser beam is applied and heats the spot until the austenitizing temperature is reached, promoting diffusion of carbon atoms present in the covering of carbon black from the surface towards the interior of the base.
Step (ii) comprises rapid cooling of the region where the laser beam is applied for formation of martensite.
Brief description of the drawings
The present invention will be described in more detail below, based on an embodiment example represented in the drawings. The figures show:
Fig. 1 - is a schematic partial view of a compression ring mounted on an engine piston that moves towards TDC, illustrating a critical situation of wear of its lower surface.
Fig. 2 - is an enlarged photograph of a section of the piston ring according to the present invention, on its lower surface.
Fig. 3 - is a schematic view of equipment for the process of laser carbonitriding applied to the piston ring according to the present invention.
Fig. 4 - is a schematic comparative view of the lower surface of the piston ring before and after the process of laser carbonitriding.
Fig. 5 - is a schematic sectional view of the piston ring according to the present invention before the process of laser carbonitriding.
Fig. 6 - is a schematic sectional view of the piston ring according to the present invention after the process of laser carbonitriding.
Fig. 7 - is a chart of wear of the piston ring according to the present invention compared with other piston rings of the prior art.
Detailed description of the figures
The piston ring according to the present invention was developed after long studies with the objective of providing a long useful life and a cost of production that makes it viable for commercial application for engines .
Piston rings undergo wear not only on their outer surface that faces the cylinder wall. The constant friction of the ring with the piston groove leads to wear on its upper surfaces (facing the piston top or crown) and lower surfaces (facing the piston skirt) .
The first-groove piston ring, also known as compression ring, is the one that is subjected to the largest forces and stresses when the engine is in operation. When the engine is running, the compression ring, which is mounted in the (first) piston groove, moves slightly in the axial direction, causing wear on
its upper and lower surfaces. One of the most critical wear situations occurs at the moment when the piston moves towards top dead centre (TDC) , which generates interference of the lower surface of the ring with the piston groove, potentiating wear in that region. This situation occurs thousands of times per minute in normal operation of an engine and is shown schematically in Fig. 1.
Preferably, but not necessarily, piston ring 1 according to the present invention is a compression ring, but it is obvious that it may assume other configurations, such as that of a second-groove ring or of an oil scraper ring, without the resultant invention leaving the scope of protection of the appended claims.
Regardless of its specific constitution, ring 1 according to the present invention meets the performance requirements without having any type of coating or nitriding on its lower surface, but does have hardening on at least a portion of this surface by means of a process of cementation or laser carbonitriding . Another imperative characteristic for this carbonitriding process to be effective is that the base material from which ring 1 is constituted is carbon steel, with any required or desirable composition.
Describing essentially, ring 1 according to the present invention is provided with a base 2 of carbon steel whose cross-section may assume the most varied configurations provided that they define an outer lateral surface 3 slidably associable to the wall D of a cylinder, an upper surface 4 associable to the groove C of a piston P, facing the piston crown and a lower surface 5 associable to the groove C of a piston P, facing the skirt S of the piston.
This is the basic geometry for a compression ring to perform its required function. A non-limiting configuration of the cross-section of the ring 1 may be seen in Fig. 6.
It is precisely a portion of the lower surface 5, or all of it, that undergoes the process of laser carbonitriding that will be described hereunder, and that increases the surface hardness in that region, greatly reducing the wear of the ring in constant friction with the piston groove.
Cementation or carbonitriding is a thermochemical treatment that consists of introducing carbon and/or nitrogen into the surface of a carbon-steel component with the aim of increasing the surface hardness. The carbon and/or nitrogen atoms supplied by a source material are inserted on the basis of heating of the region that is to undergo cementation, as will be described below. Then the surface is cooled rapidly, and the higher carbon content in the surface layers leads to an increase in surface hardness, increase in wear resistance and increase in tensile fatigue strength. Another characteristic feature resulting from this process is a change (generally increase) in grain size.
The rapid temperature drop and the higher carbon content adjacent to the surface lead to transformation of austenite to martensite, whereas the area not cemented still has a ferrite and/or pearlite microstructure, which is predominant in carbon steel, with higher ductility.
More specifically, ring 1 according to the present invention undergoes a process of cementation or laser carbonitriding. For this, the equipment employed for carrying out the process comprises a source that emits laser rays, which serve as a heat source of high power and precision, activating the transfer of carbon and/or nitrogen from a source material.
The great advantage of this process, relative to the existing technologies, besides the intrinsic disadvantages/characteristics of a coating that may crack and spall, lies in the possibility of careful control of the variables of this process so as to obtain the desirable tribological characteristics in
the treated region. More specifically, the ability to manipulate the source of laser rays for treating very small areas with great precision, with appropriate thermal control, of the depth to which diffusion of carbon and/or nitrogen is desired, and of the path of the laser beam combined with high capacity for automation of this process makes its use extremely advantageous .
In this connection, in extensive investigations, the applicant worked on all the variables until the ideal strength properties of the treated lower surface 5 were achieved.
Fig. 3 shows, schematically, the equipment 10 for carrying out the process of carbonitriding with the laser beam 13. It comprises a source that emits laser rays 11, an optional mirror 12 for guiding this beam and one or more focusing lenses 14 to allow focusing of the entire spectrum of the laser beam 13 on quite a small area or point, thereby ensuring both high heating power and very precise control of the area be treated.
Preferably, the surface to be treated 5 is applied in an environment in the presence of a gas based on nitrogen, for the purpose of making diffusion of this element possible.
Describing essentially, the heat treatment process for treating at least a portion of the lower surface 5 of the piston ring according to the present invention is an invention included in the scope of protection of the appended claims and comprises step (i) , of covering at least a portion of the lower surface 5 of the ring with a covering of carbon black 6 or any other carbon- based compound; and step (ii) , of application of a laser beam 13 on the covering of carbon black 6 applied with precise control of location and depth.
In step (ii) , the laser beam 13 is applied and heats the surface 5 until the austenitizing temperature is reached, promoting diffusion of carbon atoms present in the covering of carbon black (6) and the nitrogen atoms present in the gaseous atmosphere from the
surface 5 towards the interior of the base. Step (ii) further comprises rapid cooling of the region where the laser beam is applied for formation of martensite. Formation of the carbonitrided layer 7 is illustrated schematically in Fig. 4.
Describing in more detail, the laser beam causes rapid melting of the material, but as it is applied for a short time and only on the surface, the rest of the material remains at its initial temperature, called cold temperature hereinafter, and functions as a heat barrier. Thus, there is a large temperature gradient in the transition region between the molten material and the rest of the material that remained at the cold temperature. The result is rapid solidification as soon as application of the laser beam ceases.
For all sources emitting laser rays, the exposure time (or pulse) has a considerable influence on the depth of material that will be melted. Of course, long exposure times provide deeper fusion. Since a material melted to a greater depth obviously means a longer time that it remains in the molten state, there will be more time available for diffusion of one or more alloying elements (such as carbon or nitrogen) there. Thus, a material melted to a greater depth and for a longer time results in the formation of more dilute alloys, and vice-versa.
Other variables in the process are the power of the laser beam, the thickness of the covering of carbon black and the nature of the gaseous atmosphere in which the process takes place.
Regardless of its specific configuration, the resultant ring 1 has, finally, a lower surface 5 in which the portion treated comprises a carbonitrided layer 7 that has a thickness between lOOym and 300ym and hardness between 700HV and 1000HV. More preferably, the carbonitrided layer 7 has a thickness of substantially lOOym and also has a transition layer 5' with a thickness of substantially 200ym, which begins
at a depth of lOOym and reaches a depth of 300ym reckoned from the outer surface.
Use of the laser carbonitriding technique is quite advantageous as it offers benefits in comparison with the coating processes when it is desired to confer strength on specific surfaces of the piston ring. To summarize, the advantages are as follows:
- increase in toughness on the surface treated by diffusion of carbon, when compared with the prior art;
- increase in the useful life of the piston ring
(and, by inference, of the engine as a whole) through the increase in wear resistance in the place treated;
- possibility of extending the use of piston rings of carbon steel to more demanding applications (engines where the rings must meet more exacting performance requirements) ; and
- possibility of localized treatment, minimizing the undesirable influence of the temperature in other regions of the component.
The chart shown in Fig. 7 illustrates the values of wear resistance of the present ring 1 when compared to rings currently in use. Tests confirmed that ring 1 according to the present invention displays reduced wear values, almost as good as that displayed by rings of nitrided stainless steel (GNS) with 60ym and rings of grey cast iron (GCI), and far more advantageous than that displayed by rings of nodular cast iron (NCI) and by rings of Cr-Si steel.
A preferred embodiment example having been described, it must be understood that the scope of the present invention comprises other possible variations, thus being limited only by the content of the appended claims, including possible equivalents.
Claims
1. Piston ring provided with a base (2) of carbon steel whose cross-section defines an outer lateral surface (3) slidably associable to the wall (D) of a cylinder, an upper surface (4) associable to the groove (C) of a piston (P) , facing the piston crown and a lower surface (5) associable to the groove (C) of a piston (P) , facing the piston skirt (S) , characterized in that at least a portion of the lower surface (5) comprises a carbonitrided layer (7) that has a thickness between lOOym and 300ym and hardness between 700HV and 1000HV.
2. Ring according to Claim 1, characterized in that the carbonitrided layer (7) has a thickness of substantially lOOym.
3. Ring according to Claim 2, characterized in that it comprises a transition layer (5') with a thickness of substantially 200ym.
*4. Ring according to Claim 5, characterized in that the transition layer (5') begins at a depth of lOOym and reaches a depth of 300ym reckoned from the outer surface.
5. Ring according to Claim 1 or 2, characterized in that the carbonitrided layer (7) consists of an austenite matrix retained with martensite platelets incorporated .
6. Ring according to any one of the preceding claims, characterized in that the carbonitrided layer (7) is obtained by the process of laser carbonitriding.
7. Ring according to any one of the preceding claims, characterized in that the outer surface (3) has a coating applied by the process of physical vapour deposition (PVD) .
8. Heat treatment process for treating at least a portion of the lower surface (5) of the piston ring defined in Claims 1 to 7, characterized in that it comprises the following steps:
Step (i) : covering at least a portion of the lower surface (5) of the ring with a covering of carbon black (6) or any other carbon-based compound; and
Step (ii) : application of a laser beam on the covering of carbon black (6) applied with precise control of location and depth.
9. Process according to Claim 8, characterized in that, in step (ii) , the laser beam is applied and heats the spot until the austenitizing temperature is reached, promoting diffusion of carbon atoms present in the covering of carbon black (6) from the surface towards the interior of the base.
10. Process according to Claim 8 or 9, characterized in that step (ii) comprises rapid cooling of the region where the laser beam is applied for formation of martensite.
11. Process according to Claim 8, 9 or 10, characterized in that, in step (ii) , the laser beam is applied in an environment in which a gas containing nitrogen predominates.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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DE112014005584.0T DE112014005584T5 (en) | 2013-12-06 | 2014-11-24 | Piston ring and heat treatment process |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRBR102013031391-2A BR102013031391A2 (en) | 2013-12-06 | 2013-12-06 | Piston ring and heat treatment process |
BR1020130313912 | 2013-12-06 |
Publications (1)
Publication Number | Publication Date |
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WO2015082246A1 true WO2015082246A1 (en) | 2015-06-11 |
Family
ID=52002908
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2014/075413 WO2015082246A1 (en) | 2013-12-06 | 2014-11-24 | Piston ring and heat treatment process |
Country Status (3)
Country | Link |
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BR (1) | BR102013031391A2 (en) |
DE (1) | DE112014005584T5 (en) |
WO (1) | WO2015082246A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016104454A1 (en) * | 2016-03-11 | 2017-09-14 | Federal-Mogul Burscheid Gmbh | piston ring |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1320902A (en) * | 1969-07-24 | 1973-06-20 | Wellworthy Ltd | Hardmetal-corated articles |
US4531985A (en) | 1981-12-16 | 1985-07-30 | Ae Plc | Surface treatment of metal rings |
US5295696A (en) * | 1991-04-04 | 1994-03-22 | Teikoku Piston Ring Co., Ltd. | Combined oil ring |
US5773734A (en) * | 1995-12-21 | 1998-06-30 | Dana Corporation | Nitrided powdered metal piston ring |
JP3239610B2 (en) | 1994-05-06 | 2001-12-17 | トヨタ自動車株式会社 | Piston / piston ring assembly |
US6508473B1 (en) * | 1999-04-07 | 2003-01-21 | Teikoku Piston Ring Co., Ltd. | Piston ring |
JP4452641B2 (en) | 2005-03-24 | 2010-04-21 | 日本ピストンリング株式会社 | Sliding member |
US20100319647A1 (en) * | 2007-11-30 | 2010-12-23 | Nippon Piston Ring Co., Ltd. | Combination structure of piston ring and cylinder liner for internal combustion engine |
-
2013
- 2013-12-06 BR BRBR102013031391-2A patent/BR102013031391A2/en not_active Application Discontinuation
-
2014
- 2014-11-24 DE DE112014005584.0T patent/DE112014005584T5/en not_active Withdrawn
- 2014-11-24 WO PCT/EP2014/075413 patent/WO2015082246A1/en active Application Filing
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1320902A (en) * | 1969-07-24 | 1973-06-20 | Wellworthy Ltd | Hardmetal-corated articles |
US4531985A (en) | 1981-12-16 | 1985-07-30 | Ae Plc | Surface treatment of metal rings |
US5295696A (en) * | 1991-04-04 | 1994-03-22 | Teikoku Piston Ring Co., Ltd. | Combined oil ring |
JP3239610B2 (en) | 1994-05-06 | 2001-12-17 | トヨタ自動車株式会社 | Piston / piston ring assembly |
US5773734A (en) * | 1995-12-21 | 1998-06-30 | Dana Corporation | Nitrided powdered metal piston ring |
US6508473B1 (en) * | 1999-04-07 | 2003-01-21 | Teikoku Piston Ring Co., Ltd. | Piston ring |
JP4452641B2 (en) | 2005-03-24 | 2010-04-21 | 日本ピストンリング株式会社 | Sliding member |
US20100319647A1 (en) * | 2007-11-30 | 2010-12-23 | Nippon Piston Ring Co., Ltd. | Combination structure of piston ring and cylinder liner for internal combustion engine |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016104454A1 (en) * | 2016-03-11 | 2017-09-14 | Federal-Mogul Burscheid Gmbh | piston ring |
DE102016104454B4 (en) * | 2016-03-11 | 2021-05-27 | Federal-Mogul Burscheid Gmbh | Piston ring |
Also Published As
Publication number | Publication date |
---|---|
DE112014005584T5 (en) | 2016-08-18 |
BR102013031391A2 (en) | 2015-07-21 |
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