EP0668375A1 - Process for forming composite galvanic coatings of hard chromium with a disperse phase, and wear-resistant coating formed thereby - Google Patents
Process for forming composite galvanic coatings of hard chromium with a disperse phase, and wear-resistant coating formed thereby Download PDFInfo
- Publication number
- EP0668375A1 EP0668375A1 EP95102258A EP95102258A EP0668375A1 EP 0668375 A1 EP0668375 A1 EP 0668375A1 EP 95102258 A EP95102258 A EP 95102258A EP 95102258 A EP95102258 A EP 95102258A EP 0668375 A1 EP0668375 A1 EP 0668375A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- microcracks
- layer
- particles
- matrix
- hard chromium
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D15/00—Electrolytic or electrophoretic production of coatings containing embedded materials, e.g. particles, whiskers, wires
- C25D15/02—Combined electrolytic and electrophoretic processes with charged materials
Definitions
- the present invention relates to a process for forming, on a substrate, a composite hard chromium coating comprising a disperse phase consisting of nonmetal particles; and to a wear-resistant coating formed using such a process and particularly suitable for mechanical components subjected to high-temperature chafing, such as internal combustion engine piston rings and components.
- US Patent n. 4,846,940 relates to galvanic hard chromium coatings characterized by a Cr matrix with a large number of micro- and macrocracks combined with a disperse phase, in the matrix, consisting of hard particles embedded in the micro- and macrocracks of the matrix.
- Such coatings are formed by means of a galvanic electrodeposition process characterized by comprising a current inversion step, i.e. by alternately switching the substrate from cathode to anode potential and vice versa.
- Such coatings present a small amount of incorporated hydrogen, a large number of even relatively large cracks, and a large number of particle inclusions in the cracks, which make them highly susceptible to corrosion. Moreover, depositing the coating by inverting the polarity of the electrodes poses practical problems which complicate the fabrication process.
- a process for forming, on a substrate, a composite hard chromium coating comprising a disperse phase and particularly suitable for mechanical components subjected to high-temperature chafing comprising the step of galvanically depositing at least one layer of hard chromium in a chromium plating bath of the type forming microcracks and in which is dispersed in suspension a predetermined concentration of given sized particles of a nonmetal insoluble in the bath;
- a pulsating cathode current varying cyclically in time between a minimum and maximum value, is supplied to achieve a chromium layer comprising a matrix with microcracks of a given distribution, and a disperse phase consisting of said nonmetal particles, some of which are included in the microcracks, and some of which are directly embedded in the matrix.
- This provides for achieving a so-called "disperse chromium" coating comprising a Cr matrix containing dispersing agents, which is extremely hard (over 1,000 Vickers), includes dispersing agents in the form of nonmetal particles of hard materials such as oxides, carbides and nitrides of very low thermal conductivity and high thermal stability, and which, combined with a low hydrogen content, presents a high degree of thermal stability characterized by a reduced loss in hardness alongside an increase in temperature, and a small amount of incorporated hydrogen in the Cr matrix.
- variation of the cathode current may be achieved easily using known facilities, and fully automatically by means of appropriate programming, thus enabling troublefree, low-cost formation of the coating according to the present invention.
- the above deposition step is preferably preceded by the step of depositing on the substrate a continuous hard chromium base layer with substantially no microcracks or porosity, which covers the whole of the substrate, and which is formed, preferably to a thickness of roughly 50 /1.m, by galvanically depositing chromium in a chromium plating bath of the type forming no microcracks and containing no particles in suspension.
- a number of said "disperse" layers comprising a microcracked Cr matrix and including hard particles are then deposited successively on the continuous base layer.
- the substrate-coating interface thus presents a fairly thick layer (in relation to the total thickness of the coating, which is roughly 500 /1.m) with absolutely no cracks or dispersing agent particles (at least none detectable by standard metallographic techniques), and which prevents the microcracks in the upper layers of the coating from propagating towards the substrate, thus ensuring absolute protection of the substrate and greatly enhancing the corrosion resistance of both the substrate and the coating.
- the cathode current is supplied according to a cycle comprising the following steps:
- the cathode current is varied in a square wave pattern; and in said first and third steps, it is varied in steps.
- the "disperse chromium" layers are therefore formed with the microcracks of one layer offset, depthwise of the coating, in relation to those of the adjacent "disperse” layers, so that any depthwise propagation of the microcracks in one layer (due to mechanical stress in the layer) is prevented from being transmitted to those of the adjacent underlying layer, thus preventing the formation of macrocracks as in galvanic Cr coatings formed using known processes.
- This provides for obtaining a much more stable coating, and for further improving the corrosion resistance of the substrate, without, however, affecting the in-service lubricant collecting and distribution function of the microcracks.
- nonmetal dispersing agent particles substantially consisting of oxides (e.g. aluminium oxide - A1 2 0 3 ) and/or carbides (tungsten, chromium, silicon, boron) and/or nitrides (silicon, boron), i.e. extremely hard compounds, and both included inside the microcracks and embedded directly in the chromium matrix, provides for obtaining a coating which is extremely resistant to wear caused by abrasion or adhesion typical of high-temperature, mutually sliding metal surfaces.
- oxides e.g. aluminium oxide - A1 2 0 3
- carbides tungsten, chromium, silicon, boron
- nitrides silicon, boron
- the coating according to the present invention therefore comprises a layer comprising a microcracked hard chromium matrix and a disperse phase, in the matrix, consisting of a number of particles of a nonmetal material, and is characterized by a first number of said particles being included in the microcracks of the matrix, and by a second number of said particles being embedded directly in parts of the matrix with no microcracks.
- the wear-resistant coating according to the present invention comprises a first hard chromium layer with substantially no microcracks or porosity and without said particles; and, deposited on the first layer, a number of said layers comprising a microcracked matrix and a disperse phase consisting of said particles; the first layer presenting a thickness of at least 50 /1.m; the superimposed layers, deposited on the first layer, presenting the microcracks offset depthwise in relation to those of the adjacent layers; the width of the microcracks, measured parallel to the layer, being at least 1 ⁇ m; the density of the microcracks ranging from 100 to 300 per centimeter; and the size of the nonmetal particles embedded in the matrix ranging from 0.1 to 20 /1.m.
- cylinder liners such as the piston rings of four- and two-stroke engines or piston pumps
- the cylinder liners are normally made of lamellar, nodular or vermicular cast iron, either natural or hardened (e.g. laser quenched) or nitrided (e.g. using the TENIFER (registered trade mark) process or similar), or present surfaces with hot spray coatings such as FK1008 formed using the HVOF process (both registered trade marks).
- Number 1 in Figure 1 indicates a wear-resistant coating formed according to the present invention on a substrate 2, e.g. any known mechanical component made of cast iron.
- Coating 1 comprises a first layer 3, preferably no more than 50 /1.m deep, formed of hard Cr, and characterized by being continuous, i.e. by presenting no detectable microcracks or porosity, and no inclusions of any sort.
- layer 3 On top of layer 3, there are deposited a given number (four in the example) of substantially identical layers 5a, 5b, 5c, 5d, each comprising a hard chromium matrix 6 in which are formed a number of microcracks 7 extending radially depthwise of layer 5 towards substrate 2, and a disperse phase in matrix 6 and consisting of a number of particles 8 of any hard nonmetal material.
- a first number of particles 8 is included in microcracks 7 of matrix 6, and a second number of particles 8 is embedded directly inside parts of matrix 6 with no microcracks 7; and the microcracks 7 of layers 5 deposited on first layer 3 are offset depthwise in relation to those of the adjacent layers 5.
- microcracks 7 of layer 5b extend depthwise towards underlying layer 5a and substantially towards the portions between microcracks 7 of layer 5a, i.e. towards matrix 6 portions of layer 5a presenting no microcracks.
- the microcracks 7 of each layer 5 present a "spiderweb" pattern along the interface surface 9 of each layer 5, as shown in Figure 5.
- the width of the microcracks, measured parallel to each layer 5, is at least 1 ⁇ m; the microcrack density measured at surfaces 9 ranges from 100 to 300 microcracks per centimeter of surface; and the size of nonmetal particles 8 ranges from 0.1 to 20 /1.m.
- a coating as described above may be formed electrolytically; layer 3 being formed by galvanically depositing Cr in known manner using any known chromium plating bath of the type resulting in no microcracks and containing no particles in suspension, or operating accordingly with a bath containing particles in suspension; and layers 5 being formed using known chromium plating baths of the type for forming microcracks and containing particles 8 in suspension.
- a further precaution to ensure layer 3 presents no microcracks is to limit its thickness, and to use such operating parameters (current cycles and density, etc.) as to limit the formation of stress within the layer due to excessive energy supply.
- the baths for forming layers 5 and containing particles 8 in suspension are preferably agitated at all times, e.g. by means of mechanical, fluidodynamics, energetic agitators, or by air injection.
- the nonmetal particles 8 included in the coating must be insoluble in the baths which present a chromic acid, sulphuric acid and catalyst base, are maintained at a temperature of about 55 ° C, and present a 20 to 400 gr/liter concentration of particles 8 (ranging in size between 0.1 and 20 micron).
- Particles 8 therefore consist of one or more materials in the group comprising: tungsten carbide, silicon carbide, chromium carbide, aluminium oxide, silicon nitride, boron carbide, diamond, graphite, hexagonal boron nitride.
- Each layer 5 may of course include particles 8 all of the same material or of different materials, and likewise from one layer to another.
- the cathode current supply cycle comprises the following steps:
- Lead anodes and a cathode consisting of rings of lamellar cast iron are immersed in the bath, and a chromium coating is deposited, agitating the bath by recirculating roughly 300 It/min and injecting air at roughly 5 bar pressure, and operating with a potential difference of 15 volts and a continuous cathode current of a mean density of 70 A per square decimeter, which is varied during deposition according to the following cycle:
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Electroplating Methods And Accessories (AREA)
Abstract
Description
- The present invention relates to a process for forming, on a substrate, a composite hard chromium coating comprising a disperse phase consisting of nonmetal particles; and to a wear-resistant coating formed using such a process and particularly suitable for mechanical components subjected to high-temperature chafing, such as internal combustion engine piston rings and components.
- US Patent n. 4,846,940 relates to galvanic hard chromium coatings characterized by a Cr matrix with a large number of micro- and macrocracks combined with a disperse phase, in the matrix, consisting of hard particles embedded in the micro- and macrocracks of the matrix. Such coatings are formed by means of a galvanic electrodeposition process characterized by comprising a current inversion step, i.e. by alternately switching the substrate from cathode to anode potential and vice versa.
- Such coatings present a small amount of incorporated hydrogen, a large number of even relatively large cracks, and a large number of particle inclusions in the cracks, which make them highly susceptible to corrosion. Moreover, depositing the coating by inverting the polarity of the electrodes poses practical problems which complicate the fabrication process.
- It is an object of the present invention to provide a process for forming hard chromium coatings comprising at least one layer with a microcracked matrix and a disperse phase, and which is both straightforward and economical while at the same time providing for good quality coatings characterized by a small amount of incorporated hydrogen. It is a further object of the present invention to provide a composite hard chromium coating of good quality and strength, which remains extremely hard even at high temperature, and which is highly resistant to corrosion and wear both of itself and the mating part.
- According to the present invention, there is provided a process for forming, on a substrate, a composite hard chromium coating comprising a disperse phase and particularly suitable for mechanical components subjected to high-temperature chafing; the process comprising the step of galvanically depositing at least one layer of hard chromium in a chromium plating bath of the type forming microcracks and in which is dispersed in suspension a predetermined concentration of given sized particles of a nonmetal insoluble in the bath;
- characterized in that, in the course of said deposition step, the substrate is maintained permanently at cathode potential; and a pulsating cathode current, varying cyclically in time between a minimum and maximum value, is supplied to achieve a chromium layer comprising a matrix with microcracks of a given distribution, and a disperse phase consisting of said nonmetal particles, some of which are included in the microcracks, and some of which are directly embedded in the matrix.
- This provides for achieving a so-called "disperse chromium" coating comprising a Cr matrix containing dispersing agents, which is extremely hard (over 1,000 Vickers), includes dispersing agents in the form of nonmetal particles of hard materials such as oxides, carbides and nitrides of very low thermal conductivity and high thermal stability, and which, combined with a low hydrogen content, presents a high degree of thermal stability characterized by a reduced loss in hardness alongside an increase in temperature, and a small amount of incorporated hydrogen in the Cr matrix. Moreover, variation of the cathode current may be achieved easily using known facilities, and fully automatically by means of appropriate programming, thus enabling troublefree, low-cost formation of the coating according to the present invention.
- The above deposition step is preferably preceded by the step of depositing on the substrate a continuous hard chromium base layer with substantially no microcracks or porosity, which covers the whole of the substrate, and which is formed, preferably to a thickness of roughly 50 /1.m, by galvanically depositing chromium in a chromium plating bath of the type forming no microcracks and containing no particles in suspension. A number of said "disperse" layers comprising a microcracked Cr matrix and including hard particles are then deposited successively on the continuous base layer.
- The substrate-coating interface thus presents a fairly thick layer (in relation to the total thickness of the coating, which is roughly 500 /1.m) with absolutely no cracks or dispersing agent particles (at least none detectable by standard metallographic techniques), and which prevents the microcracks in the upper layers of the coating from propagating towards the substrate, thus ensuring absolute protection of the substrate and greatly enhancing the corrosion resistance of both the substrate and the coating.
- When galvanically depositing each said hard chromium layer comprising a microcracked matrix and a disperse phase consisting of said particles embedded in the layer, the cathode current is supplied according to a cycle comprising the following steps:
- - a first step wherein the cathode current is brought to and maintained for a first predetermined time at a first threshold value other than zero;
- - a second step, superimposed on the first, wherein the cathode current is varied alternately, in a wave pattern and for a second predetermined time, between said first threshold value and a second threshold value higher than the first; and
- - a third step wherein the cathode current is zeroed and maintained at zero for a third predetermined time.
- More specifically, in said second step, the cathode current is varied in a square wave pattern; and in said first and third steps, it is varied in steps.
- The "disperse chromium" layers are therefore formed with the microcracks of one layer offset, depthwise of the coating, in relation to those of the adjacent "disperse" layers, so that any depthwise propagation of the microcracks in one layer (due to mechanical stress in the layer) is prevented from being transmitted to those of the adjacent underlying layer, thus preventing the formation of macrocracks as in galvanic Cr coatings formed using known processes. This provides for obtaining a much more stable coating, and for further improving the corrosion resistance of the substrate, without, however, affecting the in-service lubricant collecting and distribution function of the microcracks.
- Finally, the presence of nonmetal dispersing agent particles substantially consisting of oxides (e.g. aluminium oxide - A1203) and/or carbides (tungsten, chromium, silicon, boron) and/or nitrides (silicon, boron), i.e. extremely hard compounds, and both included inside the microcracks and embedded directly in the chromium matrix, provides for obtaining a coating which is extremely resistant to wear caused by abrasion or adhesion typical of high-temperature, mutually sliding metal surfaces.
- The coating according to the present invention therefore comprises a layer comprising a microcracked hard chromium matrix and a disperse phase, in the matrix, consisting of a number of particles of a nonmetal material, and is characterized by a first number of said particles being included in the microcracks of the matrix, and by a second number of said particles being embedded directly in parts of the matrix with no microcracks. More specifically, the wear-resistant coating according to the present invention comprises a first hard chromium layer with substantially no microcracks or porosity and without said particles; and, deposited on the first layer, a number of said layers comprising a microcracked matrix and a disperse phase consisting of said particles; the first layer presenting a thickness of at least 50 /1.m; the superimposed layers, deposited on the first layer, presenting the microcracks offset depthwise in relation to those of the adjacent layers; the width of the microcracks, measured parallel to the layer, being at least 1 µm; the density of the microcracks ranging from 100 to 300 per centimeter; and the size of the nonmetal particles embedded in the matrix ranging from 0.1 to 20 /1.m.
- The favourable tribological properties of such coatings make them particularly suitable for sliding components cooperating with cylinder liners, such as the piston rings of four- and two-stroke engines or piston pumps, wherein the cylinder liners are normally made of lamellar, nodular or vermicular cast iron, either natural or hardened (e.g. laser quenched) or nitrided (e.g. using the TENIFER (registered trade mark) process or similar), or present surfaces with hot spray coatings such as FK1008 formed using the HVOF process (both registered trade marks).
- A number of non-limiting embodiments of the present invention will be described by way of example with reference to the accompanying Figures, in which:
- Figure 1 shows a schematic section, perpendicular to the surface extension, i.e. in the direction of the thickness, of a coating in accordance with the present invention;
- Figure 2 shows a hardness graph of different materials as a function of temperature;
- Figures 3, 4 and 5 show microphotographs of galvanic coatings formed using the process according to the present invention;
- Figure 6 shows a graph of a spot EDS analysis of the Cr matrix of a coating in accordance with the present invention.
-
Number 1 in Figure 1 indicates a wear-resistant coating formed according to the present invention on asubstrate 2, e.g. any known mechanical component made of cast iron.Coating 1 comprises a first layer 3, preferably no more than 50 /1.m deep, formed of hard Cr, and characterized by being continuous, i.e. by presenting no detectable microcracks or porosity, and no inclusions of any sort. On top of layer 3, there are deposited a given number (four in the example) of substantiallyidentical layers hard chromium matrix 6 in which are formed a number ofmicrocracks 7 extending radially depthwise of layer 5 towardssubstrate 2, and a disperse phase inmatrix 6 and consisting of a number ofparticles 8 of any hard nonmetal material. - According to the present invention, and as shown clearly, albeit schematically, in Figure 1, a first number of
particles 8 is included inmicrocracks 7 ofmatrix 6, and a second number ofparticles 8 is embedded directly inside parts ofmatrix 6 with nomicrocracks 7; and themicrocracks 7 of layers 5 deposited on first layer 3 are offset depthwise in relation to those of the adjacent layers 5. For example, as shown in the Figure 1 section,microcracks 7 oflayer 5b extend depthwise towardsunderlying layer 5a and substantially towards the portions betweenmicrocracks 7 oflayer 5a, i.e. towardsmatrix 6 portions oflayer 5a presenting no microcracks. When viewed from above, themicrocracks 7 of each layer 5 present a "spiderweb" pattern along theinterface surface 9 of each layer 5, as shown in Figure 5. - According to the present invention, the width of the microcracks, measured parallel to each layer 5, is at least 1 µm; the microcrack density measured at
surfaces 9 ranges from 100 to 300 microcracks per centimeter of surface; and the size ofnonmetal particles 8 ranges from 0.1 to 20 /1.m. - According to the present invention, a coating as described above may be formed electrolytically; layer 3 being formed by galvanically depositing Cr in known manner using any known chromium plating bath of the type resulting in no microcracks and containing no particles in suspension, or operating accordingly with a bath containing particles in suspension; and layers 5 being formed using known chromium plating baths of the type for forming microcracks and containing
particles 8 in suspension. A further precaution to ensure layer 3 presents no microcracks is to limit its thickness, and to use such operating parameters (current cycles and density, etc.) as to limit the formation of stress within the layer due to excessive energy supply. - According to the present invention, to achieve the above characteristics of layers 5 (
particles 8 included both inside the microcracks and directly in the matrix, and microcracks offset between one layer and another), when depositing the layer on to the substrate (or underlying layer 5),substrate 2 is maintained permanently at cathode potential, and a pulsating cathode current varying cyclically in time between a minimum and maximum value is supplied. Also, the baths for forming layers 5 and containingparticles 8 in suspension are preferably agitated at all times, e.g. by means of mechanical, fluidodynamics, energetic agitators, or by air injection. - The
nonmetal particles 8 included in the coating must be insoluble in the baths which present a chromic acid, sulphuric acid and catalyst base, are maintained at a temperature of about 55 ° C, and present a 20 to 400 gr/liter concentration of particles 8 (ranging in size between 0.1 and 20 micron).Particles 8 therefore consist of one or more materials in the group comprising: tungsten carbide, silicon carbide, chromium carbide, aluminium oxide, silicon nitride, boron carbide, diamond, graphite, hexagonal boron nitride. Each layer 5 may of course includeparticles 8 all of the same material or of different materials, and likewise from one layer to another. - The cathode current supply cycle comprises the following steps:
- - a first step wherein the cathode current is increased in steps to a first threshold value other than zero (roughly 70 amps per square decimeter) and maintained at that value for a first predetermined time ranging from 10 to 60 seconds;
- - a second step, superimposed on the first, wherein the cathode current is varied alternately, in a square wave pattern, between the first threshold value and a second threshold value higher than the first; in particular, using a pulse amplitude of 0.2-0.5 times the first threshold value, i.e. 0.2-0.5 x 70 = 14-35 A/dm2, and an oscillation period of 0.01 to 1 second; and for a time ranging from 10 to 60 seconds;
- - a third step wherein the cathode current is zeroed in steps and maintained at zero for a third predetermined time ranging from 0.03 to 60 seconds.
- The following is a non-limiting embodiment by way of example of the present invention.
-
- Lead anodes and a cathode consisting of rings of lamellar cast iron are immersed in the bath, and a chromium coating is deposited, agitating the bath by recirculating roughly 300 It/min and injecting air at roughly 5 bar pressure, and operating with a potential difference of 15 volts and a continuous cathode current of a mean density of 70 A per square decimeter, which is varied during deposition according to the following cycle:
- - a first step wherein the cathode current is increased in steps from zero to 70 A/dm2 and maintained at that value for 20 seconds;
- - a second step, superimposed on the first, wherein the cathode current is oscillated in a square wave pattern with a bandwidth of 18 A/dm2 and a frequency of 16 Hz for the same time of 20 seconds;
- - a third step wherein the cathode current is zeroed in steps and maintained at zero for 0.03 seconds;
- - repetition of the cycle from the beginning.
- This eventually produces the coating shown in the Figure 4 section, which presents excellent adherence at the coating-substrate interface. The Figure 3 photograph (enlarged 625 times) of the unetched coating, and the similar top plan view in Figure 5 show the characteristics of the coating: good adherence, low microcrack density, and inclusion of silicon carbide particles both inside and outside the cracks. This is confirmed by EDS analysis (Figure 6) of specimen pieces, which shows the typical Cr and Si peaks of a spot analysis of the matrix far from the cracks.
Claims (10)
characterized in that, in the course of said deposition step, the substrate is maintained permanently at cathode potential; and a pulsating cathode current, varying cyclically in time between a minimum and maximum value, is supplied to achieve a chromium layer comprising a matrix with microcracks of a given distribution, and a disperse phase consisting of said nonmetal particles, some of which are included in the microcracks, and some of which are directly embedded in the matrix.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT94TO000101A IT1267394B1 (en) | 1994-02-18 | 1994-02-18 | PROCEDURE FOR THE PRODUCTION OF HARD CHROME COMPOSITE GALVANIC FINISHINGS WITH A DISPERSED PHASE AND ANTI-WEAR FINISHING MADE WITH |
ITTO940101 | 1994-02-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0668375A1 true EP0668375A1 (en) | 1995-08-23 |
EP0668375B1 EP0668375B1 (en) | 1999-01-13 |
Family
ID=11412164
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP95102258A Expired - Lifetime EP0668375B1 (en) | 1994-02-18 | 1995-02-17 | Process for forming composite galvanic coatings of hard chromium with a disperse phase, and wear-resistant coating formed thereby |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0668375B1 (en) |
DE (1) | DE69507172T2 (en) |
IT (1) | IT1267394B1 (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0841413A1 (en) * | 1996-11-11 | 1998-05-13 | Teikoku Piston Ring Co., LTd. | Composite chromium plating film and sliding member covered thereof |
EP0909839A1 (en) * | 1997-10-16 | 1999-04-21 | Federal-Mogul Burscheid GmbH | Galvanic hard chromium layer |
WO2000056953A1 (en) * | 1999-03-19 | 2000-09-28 | Koncentra Verkstads Ab | Process for electrolytic coating of a substrate |
WO2001004386A1 (en) * | 1999-07-08 | 2001-01-18 | Federal Mogul Burscheid Gmbh | Hard-chrome plated layer |
EP1253220A1 (en) * | 1999-12-27 | 2002-10-30 | Nippon Piston Ring Co., Ltd. | Sliding member |
US6596410B2 (en) * | 2000-09-29 | 2003-07-22 | Nippon Piston Ring Co., Ltd. | Chrome-plated sliding member and manufacturing method thereof |
US6838196B2 (en) | 2001-03-27 | 2005-01-04 | Koncentra Holding Ab | Nickel-aluminide based wear resistant material for piston rings |
EP1719827A1 (en) * | 2004-01-30 | 2006-11-08 | Kabushiki Kaisha Riken | Composite chromium plating film and sliding member having the same and its production method |
DE102005023627A1 (en) * | 2005-05-21 | 2006-11-30 | Federal-Mogul Burscheid Gmbh | Steel piston ring has chromium ceramic anti-wear coating with micro-cracks around its peripheral edge, top and bottom faces of ring having nitride anti-wear coatings and forming sharp corners where they meet peripheral edge |
WO2009021494A1 (en) * | 2007-08-10 | 2009-02-19 | Mahle International Gmbh | Hard chrome layer, coated substrate and tribological system |
WO2009121443A1 (en) * | 2008-04-04 | 2009-10-08 | Federal-Mogul Burscheid Gmbh | Structured chrome solid particle layer and method for the production thereof |
US8110087B2 (en) | 2004-04-21 | 2012-02-07 | Federal-Mogul Burscheid Gmbh | Production of a structured hard chromium layer and production of a coating |
US8277953B2 (en) | 2002-11-29 | 2012-10-02 | Federal-Mogul Burscheid Gmbh | Production of structured hard chrome layers |
EP2660362B1 (en) | 2010-12-27 | 2019-06-26 | Nippon Piston Ring Co., Ltd. | Composite chromium plating film, and sliding member equipped with the film |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE69704752T3 (en) † | 1996-11-11 | 2005-08-04 | Teikoku Piston Ring Co., Ltd. | Galvanic composite chromium coating and coated sliding part |
DE102007050811A1 (en) * | 2007-10-24 | 2009-04-30 | Robert Bosch Gmbh | Wear protection layer and method for its production |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0217126A1 (en) * | 1985-09-03 | 1987-04-08 | Goetze Ag | Galvanic hard chromium layer |
DE3933896C1 (en) * | 1989-10-11 | 1990-10-11 | Lpw-Chemie Gmbh, 4040 Neuss, De |
-
1994
- 1994-02-18 IT IT94TO000101A patent/IT1267394B1/en active IP Right Grant
-
1995
- 1995-02-17 EP EP95102258A patent/EP0668375B1/en not_active Expired - Lifetime
- 1995-02-17 DE DE69507172T patent/DE69507172T2/en not_active Expired - Fee Related
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0217126A1 (en) * | 1985-09-03 | 1987-04-08 | Goetze Ag | Galvanic hard chromium layer |
DE3933896C1 (en) * | 1989-10-11 | 1990-10-11 | Lpw-Chemie Gmbh, 4040 Neuss, De |
Non-Patent Citations (1)
Title |
---|
TAKAYA: "trivalent chromium composite coatings containing silicon carbide or diamond particles", PLATING & SURFACE FINISHING, vol. 74, no. 9, September 1987 (1987-09-01), USA, pages 70 - 72 * |
Cited By (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6013380A (en) * | 1996-11-11 | 2000-01-11 | Teiko Piston Ring Co., Ltd. | Composite chromium plating film and sliding member covered thereof |
EP0841413A1 (en) * | 1996-11-11 | 1998-05-13 | Teikoku Piston Ring Co., LTd. | Composite chromium plating film and sliding member covered thereof |
EP0909839A1 (en) * | 1997-10-16 | 1999-04-21 | Federal-Mogul Burscheid GmbH | Galvanic hard chromium layer |
DE19745811A1 (en) * | 1997-10-16 | 1999-04-22 | Federal Mogul Burscheid Gmbh | Galvanic hard chrome layer |
DE19745811C2 (en) * | 1997-10-16 | 2002-06-13 | Federal Mogul Burscheid Gmbh | Electroplated hard chrome layer, use and method for the production thereof |
US6703145B1 (en) | 1999-03-19 | 2004-03-09 | Koncentra Holding Ab | Process for electrolytic coating of a substrate and product produced |
WO2000056953A1 (en) * | 1999-03-19 | 2000-09-28 | Koncentra Verkstads Ab | Process for electrolytic coating of a substrate |
WO2001004386A1 (en) * | 1999-07-08 | 2001-01-18 | Federal Mogul Burscheid Gmbh | Hard-chrome plated layer |
US6503642B1 (en) | 1999-07-08 | 2003-01-07 | Federal Mogul Burscheid Gmbh | Hard-chrome plated layer |
EP1253220A4 (en) * | 1999-12-27 | 2006-03-22 | Nippon Piston Ring Co Ltd | Sliding member |
EP1253220A1 (en) * | 1999-12-27 | 2002-10-30 | Nippon Piston Ring Co., Ltd. | Sliding member |
US6596410B2 (en) * | 2000-09-29 | 2003-07-22 | Nippon Piston Ring Co., Ltd. | Chrome-plated sliding member and manufacturing method thereof |
US7144017B2 (en) | 2001-03-27 | 2006-12-05 | Koncentra Marine & Power Ab | Piston ring having wear resistant composition |
US6838196B2 (en) | 2001-03-27 | 2005-01-04 | Koncentra Holding Ab | Nickel-aluminide based wear resistant material for piston rings |
US7052018B2 (en) | 2001-03-27 | 2006-05-30 | Koncentra Marine & Power Ab | Piston ring having wear resistant composition |
US8277953B2 (en) | 2002-11-29 | 2012-10-02 | Federal-Mogul Burscheid Gmbh | Production of structured hard chrome layers |
US7318963B2 (en) * | 2004-01-30 | 2008-01-15 | Kabushiki Kaisha Riken | Composite chromium plating film and sliding member having the same and method for manufacture thereof |
EP1719827A4 (en) * | 2004-01-30 | 2007-05-02 | Riken Kk | Composite chromium plating film and sliding member having the same and its production method |
EP1719827A1 (en) * | 2004-01-30 | 2006-11-08 | Kabushiki Kaisha Riken | Composite chromium plating film and sliding member having the same and its production method |
US8110087B2 (en) | 2004-04-21 | 2012-02-07 | Federal-Mogul Burscheid Gmbh | Production of a structured hard chromium layer and production of a coating |
DE102005023627A1 (en) * | 2005-05-21 | 2006-11-30 | Federal-Mogul Burscheid Gmbh | Steel piston ring has chromium ceramic anti-wear coating with micro-cracks around its peripheral edge, top and bottom faces of ring having nitride anti-wear coatings and forming sharp corners where they meet peripheral edge |
DE102005023627B4 (en) * | 2005-05-21 | 2010-05-06 | Federal-Mogul Burscheid Gmbh | Steel Kolbe ring |
WO2009021494A1 (en) * | 2007-08-10 | 2009-02-19 | Mahle International Gmbh | Hard chrome layer, coated substrate and tribological system |
WO2009121443A1 (en) * | 2008-04-04 | 2009-10-08 | Federal-Mogul Burscheid Gmbh | Structured chrome solid particle layer and method for the production thereof |
KR20110008027A (en) * | 2008-04-04 | 2011-01-25 | 페데랄-모굴 부르샤이드 게엠베하 | Structured chrome solid particle layer and method for the production thereof |
US8337687B2 (en) | 2008-04-04 | 2012-12-25 | Federal-Mogul Burscheid Gmbh | Structured chrome solid particle layer and method for the production thereof |
EP2660362B1 (en) | 2010-12-27 | 2019-06-26 | Nippon Piston Ring Co., Ltd. | Composite chromium plating film, and sliding member equipped with the film |
Also Published As
Publication number | Publication date |
---|---|
EP0668375B1 (en) | 1999-01-13 |
ITTO940101A0 (en) | 1994-02-18 |
IT1267394B1 (en) | 1997-02-05 |
DE69507172D1 (en) | 1999-02-25 |
ITTO940101A1 (en) | 1995-08-18 |
DE69507172T2 (en) | 1999-07-22 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0668375B1 (en) | Process for forming composite galvanic coatings of hard chromium with a disperse phase, and wear-resistant coating formed thereby | |
Aal et al. | Enhancement of wear resistance of ductile cast iron by Ni–SiC composite coating | |
KR101153048B1 (en) | - iron-phosphorus electroplating bath and method | |
Sohi et al. | Comparative tribological study of hard and crack-free electrodeposited chromium coatings | |
US6503642B1 (en) | Hard-chrome plated layer | |
EP1719827B1 (en) | Composite chromium plating film and sliding member having the same and its production method | |
US4886583A (en) | Formation of protective coatings by electrolytic codeposition of a nickel-cobalt matrix and ceramic particles | |
KR20110008027A (en) | Structured chrome solid particle layer and method for the production thereof | |
US20050112399A1 (en) | Erosion resistant coatings and methods thereof | |
US4323257A (en) | Piston ring with a Cr-C-Fe inlaid ring in its outer surface, and a method of making it | |
EP2980280A1 (en) | Composite rigid chromium coating film, and sliding member coated with said coating film | |
US10428437B2 (en) | Wear-resistant coating produced by electrodeposition and process therefor | |
US6354358B1 (en) | Continuous casting mold with tungsten alloy plating and method of producing the same | |
CA1316482C (en) | Method for producing a zn-series electroplated steel sheet | |
CN103184457B (en) | Surface alloying strengthening method | |
Kir et al. | Effect of hard chrome plating parameters on the wear resistance of low carbon steel | |
JPH02217497A (en) | Nickel-tungsten-silicon carbide composite plating method | |
CN1255579C (en) | Method for in situ growing high-hardness wear resistant ceramic coating layer on titanium alloy surface | |
US5543029A (en) | Properties of the surface of a titanium alloy engine valve | |
Hui et al. | A study of wear resistance of a new brush-plated alloy Ni-Fe-WS | |
Ibrahim et al. | Enhanced wear resistance of cast ductile iron by Ni-SiC composite coating | |
Bapui | Electrodeposition and characterization of nickel-molybdenum disulfide composites | |
Jones | Corrosion of Electroplated Hard Chromium | |
Huang et al. | Properties of Cr–C–Al 2 O 3 Deposits Prepared on a Cu Substrate Using Cr 3+-Based Plating Baths | |
Berkh et al. | Electrodeposition and properties of NiP alloys and their composites-a literature survey |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE GB NL |
|
17P | Request for examination filed |
Effective date: 19951130 |
|
17Q | First examination report despatched |
Effective date: 19961011 |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAG | Despatch of communication of intention to grant |
Free format text: ORIGINAL CODE: EPIDOS AGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAH | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOS IGRA |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): DE GB NL |
|
REF | Corresponds to: |
Ref document number: 69507172 Country of ref document: DE Date of ref document: 19990225 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: 732E |
|
NLS | Nl: assignments of ep-patents |
Owner name: KONCENTRA HOLDING AB |
|
NLT1 | Nl: modifications of names registered in virtue of documents presented to the patent office pursuant to art. 16 a, paragraph 1 |
Owner name: KONCENTRA MARINE & POWER AB |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20090204 Year of fee payment: 15 Ref country code: DE Payment date: 20090205 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20090204 Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: V1 Effective date: 20100901 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20100217 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100901 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100901 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20100217 |