EP0668375B1 - 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 PDF

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EP0668375B1
EP0668375B1 EP95102258A EP95102258A EP0668375B1 EP 0668375 B1 EP0668375 B1 EP 0668375B1 EP 95102258 A EP95102258 A EP 95102258A EP 95102258 A EP95102258 A EP 95102258A EP 0668375 B1 EP0668375 B1 EP 0668375B1
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microcracks
layer
particles
matrix
chromium
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German (de)
French (fr)
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EP0668375A1 (en
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Giulio Capezzuoli
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Koncentra Holding AB
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INDUSTRIALE Srl
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    • 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

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  • 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; 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, said chromium plat
  • 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 ⁇ 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 ⁇ 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 - Al 2 O 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 - Al 2 O 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; a first number of said particles being included in the microcracks of the matrix, and a second number of said particles being embedded directly in parts of the matrix with no microcracks; characterized in that it 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 superimposed layers, deposited on the first layer, presenting the microcracks offset depthwise in relation to those of the adjacent layers.
  • the first layer presents a thickness of at least 50 ⁇ m; the width of the microcracks, measured parallel to the layer, is at least 1 ⁇ m; the density of the microcracks ranges from 100 to 300 per centimeter; and the size of the nonmetal particles embedded in the matrix ranges from 0.1 to 20 ⁇ 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 ⁇ 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 ⁇ 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:
  • a bath with the following composition is prepared: CrO 3 250.0 gr/lt; FeSiF 6 1.5 gr/lt; H 2 SO 4 2.5 gr/lt SiC 50.0 gr/lt;
  • 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 lt/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:

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  • Chemical Kinetics & Catalysis (AREA)
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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, said chromium plating bath is a chromic acid based bath, containing in solution prevalently hexavalent chromium.
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 µm, 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 µm) 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 - Al2O3) 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; a first number of said particles being included in the microcracks of the matrix, and a second number of said particles being embedded directly in parts of the matrix with no microcracks; characterized in that it 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 superimposed layers, deposited on the first layer, presenting the microcracks offset depthwise in relation to those of the adjacent layers. Preferably, the first layer presents a thickness of at least 50 µm; the width of the microcracks, measured parallel to the layer, is at least 1 µm; the density of the microcracks ranges from 100 to 300 per centimeter; and the size of the nonmetal particles embedded in the matrix ranges from 0.1 to 20 µm.
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 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 µm 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 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.
    According to the present invention, and as shown clearly, albeit schematically, in Figure 1, 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. For example, as shown in the Figure 1 section, 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. When viewed from above, 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.
    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 of nonmetal particles 8 ranges from 0.1 to 20 µm.
    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 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:
    • 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.
    EXAMPLE
    Using a 1500 lt tank, a bath with the following composition is prepared:
    CrO3 250.0 gr/lt; FeSiF6 1.5 gr/lt;
    H2SO4 2.5 gr/lt SiC 50.0 gr/lt;
    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 lt/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)

    1. 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 combination:
      (i)- 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;
      (ii)- said chromium plating bath is a chromic acid based bath, containing in solution prevalently hexavalent chromium.
    2. A process as claimed in Claim 1, characterized in that said deposition step is preceded by the step of depositing on the substrate a continuous hard chromium base layer with substantially no microcracks or porosity and which covers the whole of the substrate; said base layer being formed by galvanically depositing chromium in a chromium plating bath of the type forming no microcracks.
    3. A process as claimed in Claim 2, characterized in that, on said base layer, there are deposited galvanically a number of said hard chromium layers, each comprising a microcracked matrix and a disperse phase; said layers being so formed that the microcracks of each layer are offset depthwise in relation to the microcracks of the adjacent layers.
    4. A process as claimed in one of the foregoing Claims, characterized in that said nonmetal particles insoluble in the bath consist of one or more materials in the group comprising: tungsten carbide, silicon carbide, chromium carbide, aluminium oxide, silicon nitride, boron carbide, diamond, graphite, and hexagonal boron nitride.
    5. A process as claimed in one of the foregoing Claims, characterized in that, during the step of 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 in 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.
    6. A process as claimed in Claim 5, characterized in that, in said second step, the cathode current is varied in a square wave pattern; and in said first and third steps, the cathode current is varied in steps.
    7. A wear-resistant hard chromium coating, characterized in that it is formed using the process as claimed in one of the foregoing Claims from 1 to 6, so as to present a relatively low hydrogen content
    8. A wear-resistant hard chromium coating formed electrolytically, comprising a layer in turn comprising a microcracked hard chromium matrix and a disperse phase, in the matrix, consisting of a number of particles of a nonmetal material, and particularly suitable for mechanical components subjected to high-temperature chafing; a first number of said particles being included in the microcracks of the matrix, and a second number of said particles being embedded directly in parts of the matrix with no microcracks;
         characterized in that, in combination:
      (i)- it comprises a first hard chromium layer with substantially no microcracks or porosity and without said particles; and, deposited on said first layer, a number of said layers comprising a microcracked matrix and a disperse phase consisting of said particles;
      (ii)- the microcracks of said layers deposited on the first layer being provided offset depthwise in relation to the microcracks of the adjacent layers.
    9. A wear-resistant hard chromium coating as claimed in Claim 8, characterized in that the first layer presents a thickness of at least 50 µm.
    10. A wear-resistant hard chromium coating as claimed in Claim 8 or 9, characterized in that the width of the microcracks, measured parallel to the layer, is at least 1 µm; the density of the microcracks ranges from 100 to 300 microcracks per centimeter; and the size of said nonmetal particles ranges from 0.1 to 20 µm.
    EP95102258A 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 Expired - Lifetime EP0668375B1 (en)

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    ITTO940101 1994-02-18
    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

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    EP0668375B1 true EP0668375B1 (en) 1999-01-13

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    Cited By (4)

    * Cited by examiner, † Cited by third party
    Publication number Priority date Publication date Assignee Title
    DE19931829A1 (en) * 1999-07-08 2001-01-18 Federal Mogul Burscheid Gmbh Galvanic hard chrome layer
    DE102007050811A1 (en) * 2007-10-24 2009-04-30 Robert Bosch Gmbh Wear protection layer and method for its production
    CN1764745B (en) * 2004-01-30 2012-01-11 株式会社理研 Composite chromium plating film and sliding member having the same and method for manufacture thereof
    KR101589892B1 (en) 2008-04-04 2016-01-27 페데랄-모굴 부르샤이트 게엠베하 Structured chrome solid particle layer and method for the production thereof

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    DE19745811C2 (en) * 1997-10-16 2002-06-13 Federal Mogul Burscheid Gmbh Electroplated hard chrome layer, use and method for the production thereof
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    CN1764745B (en) * 2004-01-30 2012-01-11 株式会社理研 Composite chromium plating film and sliding member having the same and method for manufacture thereof
    DE102007050811A1 (en) * 2007-10-24 2009-04-30 Robert Bosch Gmbh Wear protection layer and method for its production
    KR101589892B1 (en) 2008-04-04 2016-01-27 페데랄-모굴 부르샤이트 게엠베하 Structured chrome solid particle layer and method for the production thereof

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    ITTO940101A1 (en) 1995-08-18
    ITTO940101A0 (en) 1994-02-18
    DE69507172T2 (en) 1999-07-22
    DE69507172D1 (en) 1999-02-25
    IT1267394B1 (en) 1997-02-05
    EP0668375A1 (en) 1995-08-23

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