EP1253220A1 - Sliding member - Google Patents
Sliding member Download PDFInfo
- Publication number
- EP1253220A1 EP1253220A1 EP00985887A EP00985887A EP1253220A1 EP 1253220 A1 EP1253220 A1 EP 1253220A1 EP 00985887 A EP00985887 A EP 00985887A EP 00985887 A EP00985887 A EP 00985887A EP 1253220 A1 EP1253220 A1 EP 1253220A1
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- EP
- European Patent Office
- Prior art keywords
- hard
- plating layer
- cracks
- micro
- plating
- 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.)
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/023—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only
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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
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/04—Electroplating: Baths therefor from solutions of chromium
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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
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/10—Electroplating with more than one layer of the same or of different metals
- C25D5/12—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium
- C25D5/14—Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium two or more layers being of nickel or chromium, e.g. duplex or triplex layers
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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
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/18—Electroplating using modulated, pulsed or reversing current
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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
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/60—Electroplating characterised by the structure or texture of the layers
- C25D5/623—Porosity of the layers
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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
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/60—Electroplating characterised by the structure or texture of the layers
- C25D5/625—Discontinuous layers, e.g. microcracked layers
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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
- C25D7/00—Electroplating characterised by the article coated
- C25D7/10—Bearings
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12639—Adjacent, identical composition, components
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
- Y10T428/12826—Group VIB metal-base component
- Y10T428/12847—Cr-base component
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
- Y10T428/12826—Group VIB metal-base component
- Y10T428/12847—Cr-base component
- Y10T428/12854—Next to Co-, Fe-, or Ni-base component
Definitions
- the present invention relates to a sliding member comprising a lamination of a plurality of hard Cr plating layers on a sliding surface. More particularly, the invention relates to a sliding member suitably applicable to a piston ring for an internal combustion engine.
- sliding members such as piston rings
- a wear resistant surface treatment through, for example, hard Cr plating or nitriding to the sliding surface as means for improving durability.
- the nitriding treatment which gives an excellent wear resistance, attracts the general attention as being suitable as a surface treatment for sliding members including piston rings used under severe operating conditions, and is widely used in practice.
- the nitriding treatment while being excellent in resultant wear resistance, is not always sufficient for seizure resistance (scarfing resistance): there may occur an abnormal wear when used under severe operating conditions. Improvement has therefore been demanded.
- a conventional hard chrome plating layer hereinafter referred to as a "hard Cr plating layer” as required, having a slightly higher seizure resistance (scarfing resistance) as compared with the nitriding treatment, is not always sufficient in wear resistance. There has therefore been a demand for improvement in applications under severe operating conditions.
- porous chrome plating having fine cavities on the surface serving as lubricant oil sumps formed on the conventional hard Cr plating layer was studied for improving seizure resistance and wear resistance, and the result is actually applied in some cases.
- the present invention was achieved in view of the aforementioned problems, and has a main object to provide a sliding member in which surface cavities do not disappear even after grinding or in progress of wear of the sliding surface, seizure resistance and wear resistance can be maintained at a satisfactory level, and seizure resistance, wear resistance and strength are higher than in the conventional sliding member having a porous chrome plating layer formed thereon.
- the sliding member of the invention as recited in claim 1 has a laminated hard Cr plating layer comprising a plurality of hard Cr plating layers laminated on a sliding surface, micro-cracks being formed on the surface of each hard Cr plating layer, the micro-cracks of each hard Cr plating layer forming independent micro-pores in the film forming direction; wherein porosity on a cross-section of the laminated hard Cr plating layer is within a range of from 0.5 to 4.5%.
- a plurality of hard Cr plating layers having micro-cracks formed on the surface thereof are laminated, and micro-cracks in each layer form independent micro-pores in the film forming direction.
- micro-cracks disappear along with progress of wear, therefore, another micro-cracks immediately appear on the surface.
- micro-cracks serving as lubricant oil sumps on the surface. No problem is therefore posed in seizure resistance or wear resistance.
- the porosity on the cross-section of this laminated hard Cr plating layer is within a range of from 0.5 to 4.5%, resulting in a sliding member satisfactory seizure resistance, wear resistance and strength.
- the porosity on the surface of the hard Cr plating layer is within a range of from 0.5 to 30%, and the number of micro- cracks on the surface is within a range of from 50 to 1,200 cracks/10 mm.
- the invention by limiting the porosity and the number of micro-cracks within the above-mentioned ranges, it is possible to obtain a laminated hard Cr plating layer satisfying the seizure resistance, wear resistance and strength requirements, as in the case of above-mentioned porosity on the cross-section. Because many micro-cracks are formed on the hard chrome plating layer, seizure resistance or wear resistance never poses problems.
- the thickness per layer of the hard Cr plating layer should preferably be within a range of from 0.1 to 60 ⁇ m.
- the thickness when the thickness is smaller than 0.1 ⁇ m, it is necessary to laminate many hard Cr plating layers in order to obtain a laminated hard Cr plating layer having a necessary thickness, and this may result in a cost problem.
- the thickness is over 60 ⁇ m, after disappearance of micro-cracks by wear, the thickness before appearance of micro-cracks of the next layer becomes too large, and in the meantime, problems may be encountered in seizure resistance or wear resistance.
- the invention provides a sliding member having a laminated hard Cr plating layer comprising a plurality of hard Cr plating layers laminated on a sliding surface, micro-cracks being formed on the surface of each hard Cr plating layer, the micro-cracks of each hard Cr plating layer forming independent micro-pores in the film forming direction; wherein porosity of the surface of the hard Cr plating layer is within a range of from 0.5 to 5.0%, and the number of micro-cracks on the surface is within a range of from 50 to 1,200 cracks/10 mm.
- a plurality of hard Cr plating layers thus having micro-cracks on the surface thereof are laminated, and micro-cracks in each layer form independent micro-pores in the film forming direction. Even when micro-cracks disappear along with progress of wear, new micro-cracks appear on the surface immediately.
- presence of micro-cracks serving as lubricant oil sumps always on the surface makes the sliding member free from any problem in seizure resistance or wear resistance.
- the porosity of the surface resulting from the micro-cracks on the surface of each hard Cr plating layer is within a range of from 0.5 to 5.0%, and the number of these micro-cracks is within a range of from 50 to 1,200 cracks/10 mm. Cracks on the surface of the hard Cr plating layer in the invention therefore largely comprise many micro-cracks. Since many micro-cracks are formed on the surface of the hard Cr plating layer, no problem is caused in seizure resistance or wear resistance, although the porosity of the surface based on the micro-cracks is within a relatively low range of from 0.5 to 5.0%.
- the present invention have these features is particularly suitably applicable to uses in which the total thickness of the laminated hard Cr plating layer is relatively small as in piston rings of automobile.
- the thickness per layer of the hard Cr plating layer should preferably be within a range of from 0.1 to 60 ⁇ m.
- the thickness is smaller than 0.1 ⁇ m in the invention, it is necessary to laminate many hard Cr plating layers for the purpose of obtaining a laminated hard Cr plating layer having a necessary thickness, and this may pose a cost problem.
- the thickness is larger than 60 ⁇ m, the thickness becomes excessively large during the period from disappearance of micro-cracks by wear to appearance of micro-cracks on the next layer, during which a problem may be encountered in seizure resistance or wear resistance.
- a first feature of the sliding member of the invention is that the sliding member has a laminated hard Cr plating layer comprising a lamination of a plurality of hard Cr plating layers on a sliding surface; micro-cracks are formed on the surface of each hard Cr plating layer; and the micro-cracks of each hard Cr plating layer have micro-pores independent in the film-forming direction.
- the sliding member of the invention comprises a lamination of the hard Cr plating layers having micro-cracks on the surfaces thereof. Therefore, for example, in the case of a sliding member having only a single hard Cr plating layer on the sliding surface, wear causes most of micro-cracks to disappear in a short period of time, thus posing a problem of a decrease in seizure resistance and wear resistance.
- a plurality of hard Cr plating layers having such micro- cracks on the surfaces thereof are laminated so that, even when the portion of the surfaces containing micro-cracks disappears as a result of wear or working, micro-cracks (forming micro-pores independent in the film-forming direction) appear on the next surfaces, thus permitting maintenance of satisfactory seizure resistance and wear resistance for a long period of time.
- the thickness per layer of the hard Cr plating layer should preferably be within a range of from 0.1 to 60 ⁇ m.
- the thickness per layer of the hard Cr plating layer should preferably be within a range of from 0.1 to 15 ⁇ m, or more preferably, from 2 to 15 ⁇ m.
- the thickness per layer of the hard Cr plating layer should preferably be within a range of from 15 to 60 ⁇ m, or more preferably, from 15 to 40 ⁇ m.
- the thickness per layer of the hard Cr plating layer is smaller than the aforementioned range, it is necessary to laminate many layers when forming a laminated hard Cr plating layer having a prescribed thickness. This is not desirable because of the possibility of posing a cost problem and since a small thickness of each layer may cause a problem in strength of each layer.
- the thickness is larger than the aforementioned range, on the other hand, it would take a long period of time from disappearance of most of the micro-cracks to appearance of micro-cracks on the surface of the next layer. A larger thickness is not desirable because of the possibility of posing a seizure resistance problem.
- the surface portion of the substrate should preferably be flat.
- the substrate surface may have fine irregularities to some extent, and after lamination of hard Cr plating layers thereon in a prescribed number, smoothed by wrapping or the like. Presence of such fine irregularities on the substrate surface causes irregularities also in all the hard Cr plating layers. This reduces the possibility of disappearance of fine cracks in a stroke upon progress of wear, and this may improve seizure resistance.
- the hard Cr plating layer of the invention laminated by a method described later is observed, varying with plating conditions, to have fine cavities over the entire area in the thickness direction formed thereon. A solid portion free from fine cavities is therefore hard to appear.
- Rz of the substrate surface should preferably be within a range of from 0.3 to 3.0 ⁇ m.
- Rz of the substrate surface should preferably be within a range of from 1 to 20 ⁇ m.
- the number of laminated hard Cr plating layers in the sliding member of the invention is the result of division of the necessary thickness of the hard Cr plating layers by the thickness of the individual layers, to be appropriately selected in response to the circumstances of application of the sliding member.
- the generally applicable number of layers is within a range of from about 5 to 30 layers, or more preferably, from 8 to 20 layers.
- a number of laminated layers larger than the aforementioned range requires more time and labor to conduct hard Cr plating, and this may cause a cost problem.
- the number of laminated layers is smaller than the range shown, on the other hand, an increase in the thickness of the individual layers is generally expected, so that seizure resistance may be deteriorated.
- a second feature of the sliding member of the invention is that the porosity on a cross-section of the laminated hard Cr plating layer is within a range of from 0.5 to 4.5%.
- the number of cavities such as cracks present on the surface should be the smallest possible, considering properties related with strength by the porous chrome plating layer itself such as peeling resistance. Particularly, under severe service conditions as in a sliding member for marine applications, strength-related properties become more important.
- seizure resistance and wear resistance problems cannot be ignored, however, there occurs a serious problem in that reduction of the number of micro-cracks of the porous chrome plating layer results in deterioration of seizure resistance and wear resistance. Therefore, the number of micro-cracks in this porous chrome plating layer is an important factor for satisfying property requirements of strength, seizure resistance and wear resistance.
- the number of micro-cracks in this hard Cr plating layer was evaluated in terms of the porosity on a cross- section of the laminated hard Cr plating layer and possibility was found to maintain satisfactory strength properties, seizure resistance and wear resistance as described above by limiting the porosity on the cross-section of the laminated hard Cr plating layer within a range of from 0.5 to 4.5%.
- the term the porosity on a cross-section of the laminated hard Cr plating layer as used in the invention shall mean a value determined by first applying polishing to the cross- section by use of water-proof polishing sheets of paper in a sequence of #180, #240, #320, #600, #800, and then #1000, then applying buffing by use of alumina having a particle size of up to 1 ⁇ m for 20 seconds, finally applying buffing by use of alumina having a particle size of up to 0.1 ⁇ m for seven seconds, and analyzing the cross-section by means of an image analyzer.
- the porosity on the cross-section of the laminated hard Cr plating layer in the invention means a porosity after polishing as described in the above-mentioned definition in all cases.
- the porosity on the surface of the laminated hard Cr plating layer should preferably be within a range of from 0.5 to 30%, and the number of micro-cracks on this surface should preferably be within a range of from 50 to 1,200 cracks/10 mm.
- a porosity on the surface of under 0.5% leads to poorer seizure resistance or wear resistance, and a porosity on the surface of over 30% causes a decrease in strength and production of breakage and cracks.
- the porosity should preferably be within a range of from 0.5 to 5.0%, or more preferably, from 2.0 to 4.5%.
- the porosity should preferably be within a range of from 5 to 30%, or more preferably, from 10 to 20%.
- the formed micro-cracks have a width within a range of from 0.42 to 2.5 ⁇ m.
- the width is from 0.42 to 1.0 ⁇ m.
- a surface porosity of from 5.0 to 30% and a number of micro-cracks of from 50 to 1,200 cracks/10 mm result in a width within a range of from 1.0 to 2.5 ⁇ m.
- the sliding member of the invention particularly, in the sliding member in uses in which the total thickness of the entire laminated hard Cr plating layer is relatively small as in an automotive piston ring, as described above, it is possible to achieve the object of the invention by specifying the surface porosity (also referred as the surface area ratio) based on micro-cracks on the surface and the number of micro-cracks without the need to clearly specify the porosity on the cross-section.
- the surface porosity also referred as the surface area ratio
- the number of cavities such as cracks present on the surface should preferably be the smallest possible in terms of strength-related properties of the porous chrome plating layer itself including peeling resistance. Since seizure resistance and wear resistance are important properties, however, cavities are provided so that cracks are formed, for example, through an inverse current treatment on the surface of the hard Cr plating layer, and a prescribed porosity (surface area ratio) is achieved even when allowing a decrease in strength in the plating layer itself such as peeling resistance to some extent.
- micro-cracks are such that, as described above, in the case where the porosity of the surface based on surface micro-cracks of each hard Cr plating layer is within a range of from 0.5 to 5.0%, the number of micro-cracks is within a range of from 50 to 1,200 cracks/10 mm, or more preferably, that in the case where the porosity is within a range of from 2.0 to 4.5%, the number of micro- cracks is within a range of from 150 to 800 cracks/10 mm.
- the width of the formed cracks is within a range of from 0.42 to 1.0 ⁇ m.
- the sliding member of the invention described above is manufactured by repeating a hard Cr plating step and an etching step including an inverse current treatment prescribed times by use of a Cr plating bath on a substrate, and laminating hard Cr plating layers.
- hard Cr plating layers one on top of the others as described above, an excellent adhesion between plating layers can be obtained.
- a hard Cr plating layer having a porosity on the cross-section or the surface as shown in the invention is obtained by adjusting conditions for the plating step and conditions for the etching step including the inverse current treatment.
- a silicofluoride bath (CrO 3 : 250 g/L, H 2 SO 4 : 1.5 g/L. and NaSiF 6 : 5 g/L) held constantly at 60 oC was used as a chrome plating bath.
- the substrate surface was subjected to an inverse current treatment as an activation treatment at a current density of 60 A/dm 2 for 30 seconds (inverse current treatment 1).
- a positive current treatment was applied at a current density of 60 A/dm 2 for 17 minutes (positive current treatment 1).
- an inverse current treatment was carried out at a current density of 60 A/dm 2 for 60 seconds (inverse current treatment 2).
- the positive current treatment 1 and the inverse current treatment 2 were repeated 17 times so as to achieve a predetermined plating thickness, thereby forming a laminated hard Cr plating layer used in the sliding member of the invention.
- the resultant laminated hard Cr plating layer had a thickness per layer of about 10 ⁇ m and a total thickness of about 170 ⁇ m as a laminated hard Cr plating layer.
- the surface porosity based on micro-cracks on the surface was about 3.0%, and the number of micro-cracks was about 600 cracks/10 mm. Measurement of the sectional porosity in this state showed a porosity of about 3.0%.
- a silicofluoride bath (CrO 3 : 250 g/L, H 2 SO 4 : 1.5 g/L, and NaSiF 6 : 1 g/L) held constantly at 65 oC was used as a chrome plating bath.
- the substrate surface was subjected to an inverse current treatment as an activation treatment at a current density of 60 A/dm 2 for 30 seconds (inverse current treatment 1).
- a positive current treatment was applied at a current density of 60 A/dm 2 for 18 minutes (positive current treatment 1).
- an inverse current treatment was conducted at a current density of 60 A/dm 2 for 60 seconds (inverse current treatment 2).
- the positive current treatment 1 and the inverse current treatment 2 were repeated 17 times so as to achieve a predetermined plating thickness, thereby forming a laminated hard Cr plating layer used in the sliding member of the invention.
- the resultant laminated hard Cr plating layer had a thickness per layer of about 10 ⁇ m and a total thickness of about 170 ⁇ m as a laminated hard Cr plating layer.
- the surface porosity based on micro-cracks on the surface was about 0.5%, and the number of micro-cracks was about 50 cracks/10 mm. Measurement of the sectional porosity in this state showed a porosity of about 0.5%.
- a silicofluoride bath (CrO 3 : 250 g/L, H 2 SO 4 : 1.5g/L. and NaSiF 6 : 8 g/L) held constantly at 50 oC was used as a chrome plating bath.
- the substrate surface was subjected to an inverse current treatment as an activation treatment at a current density of 60 A/dm 2 for 30 seconds (inverse current treatment 1).
- a positive current treatment was applied at a current density of 60 A/dm 2 for 16 minutes (positive current treatment 1).
- an inverse current treatment was carried out at a current density of 60 A/dm 2 for 60 seconds (inverse current treatment 2).
- the positive current treatment 1 and the inverse current treatment 2 were repeated 17 times so as to achieve a predetermined plating thickness, thereby forming a laminated hard Cr plating layer used in the sliding member of the invention.
- the resultant laminated hard Cr plating layer had a thickness per layer of about 10 ⁇ m and a total thickness of about 170 ⁇ m as a laminated hard Cr plating layer.
- the surface porosity based on micro-cracks on the surface was about 4.5%, and the number of micro-cracks was about 1,200 cracks/10 mm. Measurement of the sectional porosity in this state showed a porosity of about 4.5%.
- a plating bath (CrO 3 : 256.7 g/L, trivalent chromium: 3.47 g/L, H 2 SO 4 : 3.00 g/L, and iron: 9.20 g/L) held at a temperature within a range of from 56 to 58 oC was used as a chrome plating bath.
- the substrate surface was subjected to a positive current treatment at a current density of 30 A/dm 2 for 110 minutes (positive current treatment 1). Then, an inverse current treatment was carried out at a current density of 30 A/dm 2 for three minutes (inverse current treatment 1). Then, a positive current treatment was conducted at a current density of 30 A/dm 2 for 80 minutes (positive current treatment 2).
- an inverse current treatment was applied at a current density of 30 A/dm 2 for three minutes (inverse current treatment 1).
- the positive current treatment 2 and the inverse current treatment 1 were repeated 11 times, thereby forming a sliding member having a hard Cr plating layer laminated on a sliding surface.
- a first layer had a thickness of about 50 ⁇ m, and a second and subsequent layers had a thickness of about 30 ⁇ m per layer.
- the thus obtained laminated hard Cr plating layer had a thickness of about 410 ⁇ m.
- the sectional porosity was measured by polishing a cross-section of this laminated hard Cr plating layer by the aforementioned method, a porosity was 2.1%.
- the surface porosity measured as above gave a porosity of about 15%.
- a silicofluoride bath (CrO 3 : 250 g/L, H 2 SO 4 : 2.5 g/L, and NaSiF 6 : 8 g/L) kept at a constant temperature of 55 oC was used as a chrome plating bath.
- a substrate was electrolytically polished, with the substrate as an anode and an opposite electrode comprising a tin-lead alloy as a cathode, by applying a selective uniform current corresponding to 60 A/dm 2 from a current controlling power source for a minute to electrolytically eluting the substrate surface.
- the anode and the cathode were rapidly reversed, and a selective uniform current of 60 A/dm 2 was applied from the current controlling power source until precipitation of a hard Cr plating layer having a prescribed thickness.
- a silicofluoride bath (CrO 3 : 250 g/L, H 2 SO 4 : 2.5 g/L, and NaSiF 6 : 8 g/L) kept at a constant temperature of 55 oC was used as a chrome plating bath.
- a substrate was electrolytically polished, with the substrate as an anode and an opposite electrode comprising a tin-lead alloy as a cathode, by applying a selective uniform current corresponding to 60 A/dm 2 from a current controlling power source for a minute to electrolytically eluting the substrate surface.
- the anode and the cathode were rapidly reversed, and a selective uniform current corresponding to 60 A/dm 2 was applied from the current controlling power source for 17 minutes to cause precipitation of a single hard Cr plating layer having a prescribed thickness.
- the cathode and the anode were rapidly reversed again, and a selective uniform current corresponding to 60 A/dm 2 was applied from the current controlling power source for a minute to electrolytically elute the surface of the precipitated hard Cr plating layer.
- the above- mentioned precipitation step and electrolytic elution step were continuously repeated until precipitation of a Cr plating layer having a prescribed thickness, and the process was completed by a precipitation step.
- Plating was performed while stirring the bath by aeration.
- a substrate was electrolytically polished by applying a selective uniform current of 60 A/dm 2 by a current controlling power source for a minute with the substrate as an anode and an opposite electrode comprising a tin-lead alloy as a cathode and electrolytically eluting the substrate surface.
- the anode and the cathode were rapidly reversed, and a selective uniform current corresponding to 60 A/dm 2 was applied from the current controlling power source for 17 minutes to cause precipitation of a single hard Cr plating layer having a prescribed thickness.
- the cathode and the anode were rapidly reversed again, and a selective uniform current corresponding to 60 A/dm 2 was applied from the current controlling power source for a minute, and the surface of a precipitated hard Cr plating layer was electrolytically eluted.
- the above-mentioned precipitation step and electrolytic eluting step were continuously repeated until precipitation of a Cr plating layer having a prescribed thickness, finally ending the process by the precipitation step.
- the wear resistance was evaluated by assuming the amount of wear for the test piece of Example 1 to be 1.00, by means of the amount of wear for the other test pieces (Examples 2 to 4 and Comparative Examples 1 to 3) as a wear index relative to the test piece of Example 1.
- the test result is shown in Table 1.
- Table 1 a smaller wear index than 1.00 suggests a smaller amount of wear.
- the seizure resistance was evaluated by assuming the amount of seizure causing load for the test piece in Example 1 to be 1.00, by means of the amount of seizure causing load for the other test pieces (Examples 2 to 4 and Comparative Examples 1 to 3) as a seizure resistance index relative to the test piece of Example 1.
- the result is shown in Table 1.
- Table 1 a larger seizure resistance index than 1.00 corresponds to a larger seizure causing load, suggesting a more excellent seizure resistance.
- the peeling resistance was evaluated by assuming the number of occurrences of peeling for the test piece of Example 1 to be 1.00, and comparing the same to the number of occurrences of peeling for the other test pieces (Examples 2 to 4 and Comparative Examples 1 to 3) as the peeling resistance index relative to the test piece of Example 1. The result is shown in Table 1.
- Table 1 a peeling resistance index smaller than 1.00 suggests that peeling occurred in a number of runs smaller than that for the test pieces of Example 1, revealing a poorer peeling resistance.
- test pieces of Examples 1 to 4 are confirmed to be superior to the test pieces of Comparative Examples 1 to 3. These properties were determined as a result of the comprehensive evaluation because, on a commercial equipment, a single poor property may lead to a defective result even when the other two properties are excellent. Determination was therefore made through comprehensive evaluation of the lowest property.
- the sliding member of the present invention has the following features: the sliding member has a laminated hard Cr plating layer comprising a plurality of hard Cr plating layers on the sliding surface thereof; micro-cracks are formed on the surface of each hard Cr plating layer; and the micro-cracks of each hard Cr plating layer form fine pores independent in the film-forming direction.
- the sliding member of the invention is characterized in that the porosity on a cross-section of the laminated hard Cr plating layer is within a range of from 0.5 to 4.5%. It is thus possible to obtain a sliding number excellent in strength properties, seizure resistance and wear resistance.
- the sliding member thus obtained is suitably applicable to automotive piston rings and marine piston rings exposed to severe service conditions such as a high-output engine and an engine used at high temperatures and a high load.
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Abstract
The present invention provides a sliding member, of which the surface cavities do not disappear even after progress of wear of the sliding surface, which permits maintenance of a satisfactory seizure resistance, and has better seizure resistance, wear resistance and strength properties than in a sliding member having a porous chrome plating layer formed thereon in the conventional art. The sliding member of the invention has a laminated hard Cr plating layer comprising a plurality of hard Cr plating layers laminated on the sliding surface. Micro-cracks are formed on each hard Cr plating layer surface, and the micro-cracks of each hard Cr plating layer form micro-pores independent in the film-forming direction. On the cross-section of the laminated hard Cr plating layer, the porosity should be within a range of from 0.5 to 4.5%. <IMAGE>
Description
The present invention relates to a sliding member comprising a
lamination of a plurality of hard Cr plating layers on a sliding surface. More
particularly, the invention relates to a sliding member suitably applicable to a
piston ring for an internal combustion engine.
Along with the recent tendency toward a lighter weight and a higher
output of internal combustion engines, the quality requirement is increasing
for sliding members such as piston rings. It is the conventional practice for
these sliding members such as piston rings for internal combustion engines to
apply a wear resistant surface treatment through, for example, hard Cr plating
or nitriding to the sliding surface as means for improving durability. Among
others, the nitriding treatment, which gives an excellent wear resistance,
attracts the general attention as being suitable as a surface treatment for
sliding members including piston rings used under severe operating
conditions, and is widely used in practice.
However, the nitriding treatment, while being excellent in resultant wear
resistance, is not always sufficient for seizure resistance (scarfing resistance):
there may occur an abnormal wear when used under severe operating
conditions. Improvement has therefore been demanded. A conventional
hard chrome plating layer (hereinafter referred to as a "hard Cr plating layer"
as required), having a slightly higher seizure resistance (scarfing resistance)
as compared with the nitriding treatment, is not always sufficient in wear
resistance. There has therefore been a demand for improvement in
applications under severe operating conditions.
In these respects, porous chrome plating having fine cavities on the
surface serving as lubricant oil sumps formed on the conventional hard Cr
plating layer was studied for improving seizure resistance and wear resistance,
and the result is actually applied in some cases.
In the conventional porous chrome plating, however, cavities are present
only on the surface, and cavities effective for improving sliding properties are
not existent in the interior of the plating layer. When applying grinding or
when the sliding surface is worn out, a solid portion not containing cavities on
the surface of the plating layer is exposed, leading to deterioration of seizure
resistance or wear resistance.
The present invention was achieved in view of the aforementioned
problems, and has a main object to provide a sliding member in which surface
cavities do not disappear even after grinding or in progress of wear of the
sliding surface, seizure resistance and wear resistance can be maintained at a
satisfactory level, and seizure resistance, wear resistance and strength are
higher than in the conventional sliding member having a porous chrome
plating layer formed thereon.
To achieve the aforementioned object, the sliding member of the
invention as recited in claim 1 has a laminated hard Cr plating layer
comprising a plurality of hard Cr plating layers laminated on a sliding surface,
micro-cracks being formed on the surface of each hard Cr plating layer, the
micro-cracks of each hard Cr plating layer forming independent micro-pores
in the film forming direction; wherein porosity on a cross-section of the
laminated hard Cr plating layer is within a range of from 0.5 to 4.5%.
In the invention, a plurality of hard Cr plating layers having
micro-cracks formed on the surface thereof are laminated, and micro-cracks in
each layer form independent micro-pores in the film forming direction.
When micro- cracks disappear along with progress of wear, therefore, another
micro-cracks immediately appear on the surface. Even when grinding is
applied or after a long use in service, therefore, there always exist
micro-cracks serving as lubricant oil sumps on the surface. No problem is
therefore posed in seizure resistance or wear resistance. The porosity on the
cross-section of this laminated hard Cr plating layer is within a range of from
0.5 to 4.5%, resulting in a sliding member satisfactory seizure resistance,
wear resistance and strength.
In the sliding member of claim 1 of the invention, the porosity on the
surface of the hard Cr plating layer is within a range of from 0.5 to 30%, and
the number of micro- cracks on the surface is within a range of from 50 to
1,200 cracks/10 mm.
According to the invention, by limiting the porosity and the number of
micro-cracks within the above-mentioned ranges, it is possible to obtain a
laminated hard Cr plating layer satisfying the seizure resistance, wear
resistance and strength requirements, as in the case of above-mentioned
porosity on the cross-section. Because many micro-cracks are formed on the
hard chrome plating layer, seizure resistance or wear resistance never poses
problems.
In the sliding member according to claim 1 or 2 of the invention, as
recited in claim 3, the thickness per layer of the hard Cr plating layer should
preferably be within a range of from 0.1 to 60 µm.
In the invention, when the thickness is smaller than 0.1 µm, it is
necessary to laminate many hard Cr plating layers in order to obtain a
laminated hard Cr plating layer having a necessary thickness, and this may
result in a cost problem. When the thickness is over 60 µm, after
disappearance of micro-cracks by wear, the thickness before appearance of
micro-cracks of the next layer becomes too large, and in the meantime,
problems may be encountered in seizure resistance or wear resistance.
To achieve the aforementioned object, the invention provides a sliding
member having a laminated hard Cr plating layer comprising a plurality of
hard Cr plating layers laminated on a sliding surface, micro-cracks being
formed on the surface of each hard Cr plating layer, the micro-cracks of each
hard Cr plating layer forming independent micro-pores in the film forming
direction; wherein porosity of the surface of the hard Cr plating layer is
within a range of from 0.5 to 5.0%, and the number of micro-cracks on the
surface is within a range of from 50 to 1,200 cracks/10 mm.
In the invention, a plurality of hard Cr plating layers thus having
micro-cracks on the surface thereof are laminated, and micro-cracks in each
layer form independent micro-pores in the film forming direction. Even
when micro-cracks disappear along with progress of wear, new micro-cracks
appear on the surface immediately. When applying grinding or using for a
long period of time, therefore, presence of micro-cracks serving as lubricant
oil sumps always on the surface makes the sliding member free from any
problem in seizure resistance or wear resistance. The porosity of the surface
resulting from the micro-cracks on the surface of each hard Cr plating layer is
within a range of from 0.5 to 5.0%, and the number of these micro-cracks is
within a range of from 50 to 1,200 cracks/10 mm. Cracks on the surface of
the hard Cr plating layer in the invention therefore largely comprise many
micro-cracks. Since many micro-cracks are formed on the surface of the
hard Cr plating layer, no problem is caused in seizure resistance or wear
resistance, although the porosity of the surface based on the micro-cracks is
within a relatively low range of from 0.5 to 5.0%. Because the porosity on
the surface is on such a low level, and cracks are fine in size, strength-related
properties such as peeling resistance of the hard Cr plating layer are
considerably improved. The present invention have these features is
particularly suitably applicable to uses in which the total thickness of the
laminated hard Cr plating layer is relatively small as in piston rings of
automobile.
In the sliding member of the invention according to claim 4, as recited in
claim 5 of the invention, the thickness per layer of the hard Cr plating layer
should preferably be within a range of from 0.1 to 60 µm.
When the thickness is smaller than 0.1 µm in the invention, it is
necessary to laminate many hard Cr plating layers for the purpose of obtaining
a laminated hard Cr plating layer having a necessary thickness, and this may
pose a cost problem. When the thickness is larger than 60 µm, the thickness
becomes excessively large during the period from disappearance of
micro-cracks by wear to appearance of micro-cracks on the next layer, during
which a problem may be encountered in seizure resistance or wear resistance.
The sliding member of the present invention will now be described in
detail.
A first feature of the sliding member of the invention is that the sliding
member has a laminated hard Cr plating layer comprising a lamination of a
plurality of hard Cr plating layers on a sliding surface; micro-cracks are
formed on the surface of each hard Cr plating layer; and the micro-cracks of
each hard Cr plating layer have micro-pores independent in the film-forming
direction.
As shown in Fig. 1, the sliding member of the invention comprises a
lamination of the hard Cr plating layers having micro-cracks on the surfaces
thereof. Therefore, for example, in the case of a sliding member having only
a single hard Cr plating layer on the sliding surface, wear causes most of
micro-cracks to disappear in a short period of time, thus posing a problem of a
decrease in seizure resistance and wear resistance. In the invention, however,
a plurality of hard Cr plating layers having such micro- cracks on the surfaces
thereof are laminated so that, even when the portion of the surfaces containing
micro-cracks disappears as a result of wear or working, micro-cracks (forming
micro-pores independent in the film-forming direction) appear on the next
surfaces, thus permitting maintenance of satisfactory seizure resistance and
wear resistance for a long period of time.
In the invention, the thickness per layer of the hard Cr plating layer
should preferably be within a range of from 0.1 to 60 µm. In the case where
the entire laminated hard Cr layer should have a relatively small total
thickness, as in the automotive piston ring, the thickness per layer of the hard
Cr plating layer should preferably be within a range of from 0.1 to 15 µm, or
more preferably, from 2 to 15 µm. In the case where the total thickness of
the entire laminated hard Cr plating layer is relatively large as in a marine
piston ring, the thickness per layer of the hard Cr plating layer should
preferably be within a range of from 15 to 60 µm, or more preferably, from 15
to 40 µm.
When the thickness per layer of the hard Cr plating layer is smaller than
the aforementioned range, it is necessary to laminate many layers when
forming a laminated hard Cr plating layer having a prescribed thickness.
This is not desirable because of the possibility of posing a cost problem and
since a small thickness of each layer may cause a problem in strength of each
layer. When the thickness is larger than the aforementioned range, on the
other hand, it would take a long period of time from disappearance of most of
the micro-cracks to appearance of micro-cracks on the surface of the next
layer. A larger thickness is not desirable because of the possibility of posing
a seizure resistance problem.
In the invention, the surface portion of the substrate should preferably be
flat. The substrate surface may have fine irregularities to some extent, and
after lamination of hard Cr plating layers thereon in a prescribed number,
smoothed by wrapping or the like. Presence of such fine irregularities on the
substrate surface causes irregularities also in all the hard Cr plating layers.
This reduces the possibility of disappearance of fine cracks in a stroke upon
progress of wear, and this may improve seizure resistance. As shown in Figs.
2 and 3, the hard Cr plating layer of the invention laminated by a method
described later is observed, varying with plating conditions, to have fine
cavities over the entire area in the thickness direction formed thereon. A
solid portion free from fine cavities is therefore hard to appear. As a result,
a substrate surface even with irregularities within a range of Rz (ten-point
average roughness) of from 0.3 to 20 µm is suitably applicable. In a use in
which the total thickness of the laminated hard Cr plating layer as a whole is
relatively small as in an automotive piston ring, Rz of the substrate surface
should preferably be within a range of from 0.3 to 3.0 µm. In a use in which
the total length of the entire laminated hard Cr plating layer is relatively large
as in a marine piston ring, Rz of the substrate surface should preferably be
within a range of from 1 to 20 µm.
The number of laminated hard Cr plating layers in the sliding member of
the invention is the result of division of the necessary thickness of the hard Cr
plating layers by the thickness of the individual layers, to be appropriately
selected in response to the circumstances of application of the sliding member.
The generally applicable number of layers is within a range of from about 5 to
30 layers, or more preferably, from 8 to 20 layers. A number of laminated
layers larger than the aforementioned range requires more time and labor to
conduct hard Cr plating, and this may cause a cost problem. When the
number of laminated layers is smaller than the range shown, on the other hand,
an increase in the thickness of the individual layers is generally expected, so
that seizure resistance may be deteriorated.
A second feature of the sliding member of the invention is that the
porosity on a cross-section of the laminated hard Cr plating layer is within a
range of from 0.5 to 4.5%.
In general, in a porous chrome plating layer used as a sliding surface,
when ignoring seizure resistance and wear resistance problems, the number of
cavities such as cracks present on the surface should be the smallest possible,
considering properties related with strength by the porous chrome plating
layer itself such as peeling resistance. Particularly, under severe service
conditions as in a sliding member for marine applications, strength-related
properties become more important. When seizure resistance and wear
resistance problems cannot be ignored, however, there occurs a serious
problem in that reduction of the number of micro-cracks of the porous chrome
plating layer results in deterioration of seizure resistance and wear resistance.
Therefore, the number of micro-cracks in this porous chrome plating layer is
an important factor for satisfying property requirements of strength, seizure
resistance and wear resistance. In the present invention, the number of
micro-cracks in this hard Cr plating layer was evaluated in terms of the
porosity on a cross- section of the laminated hard Cr plating layer and
possibility was found to maintain satisfactory strength properties, seizure
resistance and wear resistance as described above by limiting the porosity on
the cross-section of the laminated hard Cr plating layer within a range of from
0.5 to 4.5%.
It is necessary, as described above, to limit the porosity on the
cross-section of the laminated hard Cr plating layer of the invention within a
range of from 0.5 to 4.5%. With a porosity on the cross-section of under
0.5%, seizure resistance and wear resistance are low. A porosity on the
cross-section of over 4.5% leads to a decrease in strength, causing breakage
and cracks.
The term the porosity on a cross-section of the laminated hard Cr plating
layer as used in the invention (also referred to as the "porous degree") shall
mean a value determined by first applying polishing to the cross- section by
use of water-proof polishing sheets of paper in a sequence of #180, #240,
#320, #600, #800, and then #1000, then applying buffing by use of alumina
having a particle size of up to 1 µm for 20 seconds, finally applying buffing
by use of alumina having a particle size of up to 0.1 µm for seven seconds,
and analyzing the cross-section by means of an image analyzer.
This definition is adopted because it is experimentally revealed that the
value of porosity measured on the cross- section of the laminated hard Cr
plating layer varies with the sample polishing conditions and time, and the
necessity arises to set constant polishing conditions. The porosity on the
cross-section of the laminated hard Cr plating layer in the invention means a
porosity after polishing as described in the above-mentioned definition in all
cases.
In the invention, furthermore, the porosity on the surface of the
laminated hard Cr plating layer should preferably be within a range of from
0.5 to 30%, and the number of micro-cracks on this surface should preferably
be within a range of from 50 to 1,200 cracks/10 mm.
A porosity on the surface of under 0.5% leads to poorer seizure
resistance or wear resistance, and a porosity on the surface of over 30%
causes a decrease in strength and production of breakage and cracks. In this
case, in a use in which the total thickness of the entire laminated hard Cr
plating layer is relatively small as in an automotive piston ring, the porosity
should preferably be within a range of from 0.5 to 5.0%, or more preferably,
from 2.0 to 4.5%. In a use in which the total thickness of the entire
laminated hard Cr plating layer is relatively large as in a marine piston ring,
the porosity should preferably be within a range of from 5 to 30%, or more
preferably, from 10 to 20%. By limiting the number of micro-cracks on the
surface within the above-mentioned range, many micro- cracks are formed on
the hard chrome plating layer. No seizure resistance or wear resistance
problem is therefore encountered.
In the above case where the surface porosity is within a range of from 0.5
to 30% and the number of micro-cracks is within a range of from 50 to 1,200
cracks/10 mm, the formed micro-cracks have a width within a range of from
0.42 to 2.5 µm. In the case with a surface porosity of from 0.5 to 5.0% and a
number of micro-cracks of from 50 to 1,200 cracks/10 mm, the width is from
0.42 to 1.0 µm. A surface porosity of from 5.0 to 30% and a number of
micro-cracks of from 50 to 1,200 cracks/10 mm result in a width within a
range of from 1.0 to 2.5 µm.
In the sliding member of the invention, particularly, in the sliding
member in uses in which the total thickness of the entire laminated hard Cr
plating layer is relatively small as in an automotive piston ring, as described
above, it is possible to achieve the object of the invention by specifying the
surface porosity (also referred as the surface area ratio) based on
micro-cracks on the surface and the number of micro-cracks without the need
to clearly specify the porosity on the cross-section. More specifically, as
recited in claim 4 of the invention, it is possible to achieve the object by
limiting the surface porosity based on micro-cracks formed on the surface of
each hard Cr plating layer within a range of from 0.5 to 5.0%, and the number
of the micro-cracks within a range of from 1,200 cracks/10 mm.
As in the aforementioned second feature, when the problems of seizure
resistance and wear resistance are disregarded in a porous chrome plating
layer used generally as a sliding surface, the number of cavities such as cracks
present on the surface should preferably be the smallest possible in terms of
strength-related properties of the porous chrome plating layer itself including
peeling resistance. Since seizure resistance and wear resistance are
important properties, however, cavities are provided so that cracks are formed,
for example, through an inverse current treatment on the surface of the hard
Cr plating layer, and a prescribed porosity (surface area ratio) is achieved
even when allowing a decrease in strength in the plating layer itself such as
peeling resistance to some extent.
In an aspect of the invention, as recited in claim 4, new findings were
obtained that, by causing micro-cracks to serve as such surface cavities, no
problem was posed in seizure resistance or wear resistance even with a
porosity based on a smaller number of cavities than in an usual case. This
aspect of the invention has a marked feature in that it is intended to improve
strength of the plating layer itself such as peeling resistance without causing a
decrease in seizure resistance or wear resistance.
These micro-cracks are such that, as described above, in the case where
the porosity of the surface based on surface micro-cracks of each hard Cr
plating layer is within a range of from 0.5 to 5.0%, the number of micro-cracks
is within a range of from 50 to 1,200 cracks/10 mm, or more preferably,
that in the case where the porosity is within a range of from 2.0 to 4.5%, the
number of micro- cracks is within a range of from 150 to 800 cracks/10 mm.
In the case with a surface porosity within a range of from 0.5 to 5.0% and a
number of micro-cracks within a range of from 50 to 1,200 cracks/10 mm, the
width of the formed cracks is within a range of from 0.42 to 1.0 µm.
The sliding member of the invention described above is manufactured by
repeating a hard Cr plating step and an etching step including an inverse
current treatment prescribed times by use of a Cr plating bath on a substrate,
and laminating hard Cr plating layers. By forming hard Cr plating layers one
on top of the others as described above, an excellent adhesion between plating
layers can be obtained. A hard Cr plating layer having a porosity on the
cross-section or the surface as shown in the invention is obtained by adjusting
conditions for the plating step and conditions for the etching step including
the inverse current treatment.
The present invention is not limited to the aforementioned embodiments.
These embodiments are only examples, and any sliding members having
substantially the same configuration and providing the same advantages as in
the technical idea recited in the claims of the invention are included in the
technical scope of the invention.
The present invention will be described in detail by means of examples
and comparative examples.
A silicofluoride bath (CrO3: 250 g/L, H2SO4: 1.5 g/L. and NaSiF6: 5 g/L)
held constantly at 60 ºC was used as a chrome plating bath. First, the
substrate surface was subjected to an inverse current treatment as an
activation treatment at a current density of 60 A/dm2 for 30 seconds (inverse
current treatment 1). Then, a positive current treatment was applied at a
current density of 60 A/dm2 for 17 minutes (positive current treatment 1).
Then, an inverse current treatment was carried out at a current density of 60
A/dm2 for 60 seconds (inverse current treatment 2). The positive current
treatment 1 and the inverse current treatment 2 were repeated 17 times so as to
achieve a predetermined plating thickness, thereby forming a laminated hard
Cr plating layer used in the sliding member of the invention.
The resultant laminated hard Cr plating layer had a thickness per layer of
about 10 µm and a total thickness of about 170 µm as a laminated hard Cr
plating layer. The surface porosity based on micro-cracks on the surface was
about 3.0%, and the number of micro-cracks was about 600 cracks/10 mm.
Measurement of the sectional porosity in this state showed a porosity of about
3.0%.
A silicofluoride bath (CrO3: 250 g/L, H2SO4: 1.5 g/L, and NaSiF6: 1 g/L)
held constantly at 65 ºC was used as a chrome plating bath. First, the
substrate surface was subjected to an inverse current treatment as an
activation treatment at a current density of 60 A/dm2 for 30 seconds (inverse
current treatment 1). Then, a positive current treatment was applied at a
current density of 60 A/dm2 for 18 minutes (positive current treatment 1).
Then, an inverse current treatment was conducted at a current density of 60
A/dm2 for 60 seconds (inverse current treatment 2). The positive current
treatment 1 and the inverse current treatment 2 were repeated 17 times so as to
achieve a predetermined plating thickness, thereby forming a laminated hard
Cr plating layer used in the sliding member of the invention.
The resultant laminated hard Cr plating layer had a thickness per layer of
about 10 µm and a total thickness of about 170 µm as a laminated hard Cr
plating layer. The surface porosity based on micro-cracks on the surface was
about 0.5%, and the number of micro-cracks was about 50 cracks/10 mm.
Measurement of the sectional porosity in this state showed a porosity of about
0.5%.
A silicofluoride bath (CrO3: 250 g/L, H2SO4: 1.5g/L. and NaSiF6: 8 g/L)
held constantly at 50 ºC was used as a chrome plating bath. First, the
substrate surface was subjected to an inverse current treatment as an
activation treatment at a current density of 60 A/dm2 for 30 seconds (inverse
current treatment 1). Then, a positive current treatment was applied at a
current density of 60 A/dm2 for 16 minutes (positive current treatment 1).
Then, an inverse current treatment was carried out at a current density of 60
A/dm2 for 60 seconds (inverse current treatment 2). The positive current
treatment 1 and the inverse current treatment 2 were repeated 17 times so as to
achieve a predetermined plating thickness, thereby forming a laminated hard
Cr plating layer used in the sliding member of the invention.
The resultant laminated hard Cr plating layer had a thickness per layer of
about 10 µm and a total thickness of about 170 µm as a laminated hard Cr
plating layer. The surface porosity based on micro-cracks on the surface was
about 4.5%, and the number of micro-cracks was about 1,200 cracks/10 mm.
Measurement of the sectional porosity in this state showed a porosity of about
4.5%.
A plating bath (CrO3: 256.7 g/L, trivalent chromium: 3.47 g/L, H2SO4:
3.00 g/L, and iron: 9.20 g/L) held at a temperature within a range of from 56
to 58 ºC was used as a chrome plating bath. First, the substrate surface was
subjected to a positive current treatment at a current density of 30 A/dm2 for
110 minutes (positive current treatment 1). Then, an inverse current
treatment was carried out at a current density of 30 A/dm2 for three minutes
(inverse current treatment 1). Then, a positive current treatment was
conducted at a current density of 30 A/dm2 for 80 minutes (positive current
treatment 2). In addition, an inverse current treatment was applied at a
current density of 30 A/dm2 for three minutes (inverse current treatment 1).
The positive current treatment 2 and the inverse current treatment 1 were
repeated 11 times, thereby forming a sliding member having a hard Cr plating
layer laminated on a sliding surface.
In the resultant laminated hard Cr plating layer, a first layer, had a
thickness of about 50 µm, and a second and subsequent layers had a thickness
of about 30 µm per layer. The thus obtained laminated hard Cr plating layer
had a thickness of about 410 µm. The sectional porosity was measured by
polishing a cross-section of this laminated hard Cr plating layer by the
aforementioned method, a porosity was 2.1%. The surface porosity
measured as above gave a porosity of about 15%.
A silicofluoride bath (CrO3: 250 g/L, H2SO4: 2.5 g/L, and NaSiF6: 8 g/L)
kept at a constant temperature of 55 ºC was used as a chrome plating bath.
First, a substrate was electrolytically polished, with the substrate as an anode
and an opposite electrode comprising a tin-lead alloy as a cathode, by
applying a selective uniform current corresponding to 60 A/dm2 from a
current controlling power source for a minute to electrolytically eluting the
substrate surface. Then, the anode and the cathode were rapidly reversed,
and a selective uniform current of 60 A/dm2 was applied from the current
controlling power source until precipitation of a hard Cr plating layer having
a prescribed thickness.
A conventional single-layer chrome plating layer continuously formed
was obtained.
A silicofluoride bath (CrO3: 250 g/L, H2SO4: 2.5 g/L, and NaSiF6: 8 g/L)
kept at a constant temperature of 55 ºC was used as a chrome plating bath.
First, a substrate was electrolytically polished, with the substrate as an anode
and an opposite electrode comprising a tin-lead alloy as a cathode, by
applying a selective uniform current corresponding to 60 A/dm2 from a
current controlling power source for a minute to electrolytically eluting the
substrate surface. Then, the anode and the cathode were rapidly reversed,
and a selective uniform current corresponding to 60 A/dm2 was applied from
the current controlling power source for 17 minutes to cause precipitation of a
single hard Cr plating layer having a prescribed thickness. Then, the cathode
and the anode were rapidly reversed again, and a selective uniform current
corresponding to 60 A/dm2 was applied from the current controlling power
source for a minute to electrolytically elute the surface of the precipitated
hard Cr plating layer. Then, the above- mentioned precipitation step and
electrolytic elution step were continuously repeated until precipitation of a Cr
plating layer having a prescribed thickness, and the process was completed by
a precipitation step.
Thus, there was obtained a conventional chrome plating layer having a
multi-layer structure in which hard Cr plating layers were formed into a
thickness per layer of 10 µm, and micro-cracks were independently formed
without continuation between two adjacent layers.
A plating bath prepared by adding ceramic particles (size within a range
of from 0.05 to 1.0 µm; degree of suspension: 100 g/L) to a silicofluoride bath
(CrO3: 250 g/L, H2SO4: 2.5 g/L, and NaSiF6: 8 g/L) kept at a constant
temperature of 55 ºC was used. Plating was performed while stirring the
bath by aeration. First, a substrate was electrolytically polished by applying
a selective uniform current of 60 A/dm2 by a current controlling power source
for a minute with the substrate as an anode and an opposite electrode
comprising a tin-lead alloy as a cathode and electrolytically eluting the
substrate surface. Then, the anode and the cathode were rapidly reversed,
and a selective uniform current corresponding to 60 A/dm2 was applied from
the current controlling power source for 17 minutes to cause precipitation of a
single hard Cr plating layer having a prescribed thickness. Then, the cathode
and the anode were rapidly reversed again, and a selective uniform current
corresponding to 60 A/dm2 was applied from the current controlling power
source for a minute, and the surface of a precipitated hard Cr plating layer was
electrolytically eluted. Then, the above-mentioned precipitation step and
electrolytic eluting step were continuously repeated until precipitation of a Cr
plating layer having a prescribed thickness, finally ending the process by the
precipitation step.
In each of the Cr plating layers composing the Cr plating film having the
multi-layer structure, a conventional Cr plating film retaining ceramic
particles (size: 0.05 to 1.0 µm) in pores of chrome plating micro- cracks was
obtained.
The thus obtained Cr plating layers, serving as examples 1 to 4 and
comparative examples 1 to 3 were subjected to a wear test, a scarfing test and
a peeling resistance test. Test conditions were as follows:
The wear resistance was evaluated by assuming the amount of wear for
the test piece of Example 1 to be 1.00, by means of the amount of wear for the
other test pieces (Examples 2 to 4 and Comparative Examples 1 to 3) as a wear
index relative to the test piece of Example 1. The test result is shown in
Table 1. In Table 1, a smaller wear index than 1.00 suggests a smaller
amount of wear.
The seizure resistance was evaluated by assuming the amount of seizure
causing load for the test piece in Example 1 to be 1.00, by means of the
amount of seizure causing load for the other test pieces (Examples 2 to 4 and
Comparative Examples 1 to 3) as a seizure resistance index relative to the test
piece of Example 1. The result is shown in Table 1. In Table 1, a larger
seizure resistance index than 1.00 corresponds to a larger seizure causing load,
suggesting a more excellent seizure resistance.
The peeling resistance was evaluated by assuming the number of
occurrences of peeling for the test piece of Example 1 to be 1.00, and
comparing the same to the number of occurrences of peeling for the other test
pieces (Examples 2 to 4 and Comparative Examples 1 to 3) as the peeling
resistance index relative to the test piece of Example 1. The result is shown
in Table 1. In Table 1, a peeling resistance index smaller than 1.00 suggests
that peeling occurred in a number of runs smaller than that for the test pieces
of Example 1, revealing a poorer peeling resistance.
As is evident from Table 1, according to a comprehensive evaluation of
the three above-mentioned kinds of test results, the test pieces of Examples 1
to 4 are confirmed to be superior to the test pieces of Comparative Examples 1
to 3. These properties were determined as a result of the comprehensive
evaluation because, on a commercial equipment, a single poor property may
lead to a defective result even when the other two properties are excellent.
Determination was therefore made through comprehensive evaluation of the
lowest property.
As described above, the sliding member of the present invention has the
following features: the sliding member has a laminated hard Cr plating layer
comprising a plurality of hard Cr plating layers on the sliding surface thereof;
micro-cracks are formed on the surface of each hard Cr plating layer; and the
micro-cracks of each hard Cr plating layer form fine pores independent in the
film-forming direction. The sliding member of the invention is characterized
in that the porosity on a cross-section of the laminated hard Cr plating layer is
within a range of from 0.5 to 4.5%. It is thus possible to obtain a sliding
number excellent in strength properties, seizure resistance and wear resistance.
The sliding member thus obtained is suitably applicable to automotive piston
rings and marine piston rings exposed to severe service conditions such as a
high-output engine and an engine used at high temperatures and a high load.
The entire disclosure of Japanese Patent Application No. 11-371144
filed on December 27, 1999, including the specification, claims, drawings and
summary is incorporated herein by reference its entirety.
Claims (5)
- A sliding member having a laminated hard Cr plating layer comprising a plurality of hard Cr plating layers laminated on a sliding surface, micro-cracks being formed on the surface of each hard Cr plating layer, the micro- cracks of each hard Cr plating layer forming independent micro-pores in the film forming direction; wherein porosity on a cross-section of said laminated hard Cr plating layer is within a range of from 0.5 to 4.5%.
- A sliding member according to claim 1, wherein porosity on the surface of said hard Cr plating layer is within a range of from 0.5 to 30%, and the number of micro- cracks on said surface is within a range of from 50 to 1,200 cracks/10 mm.
- A sliding member according to claim 1 or 2, wherein the thickness per layer of said hard Cr plating layer is within a range of from 0.1 to 60 µm.
- A sliding member having a laminated hard Cr plating layer comprising a plurality of hard Cr plating layers laminated on a sliding surface, micro-cracks being formed on the surface of each hard Cr plating layer, the micro- cracks of each hard Cr plating layer forming independent micro-pores in the film forming direction; wherein porosity on the surface of said hard Cr plating layer is within a range of from 0.5 to 5.0%, and the number of micro-cracks on said surface is within a range of from 50 to 1,200 cracks/10 mm.
- A sliding member according to claim 4, wherein the thickness per layer of said hard Cr plating layer is within a range of from 0.1 to 60 µm.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP37114499 | 1999-12-27 | ||
| JP37114499 | 1999-12-27 | ||
| PCT/JP2000/009235 WO2001048267A1 (en) | 1999-12-27 | 2000-12-26 | Sliding member |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1253220A1 true EP1253220A1 (en) | 2002-10-30 |
| EP1253220A4 EP1253220A4 (en) | 2006-03-22 |
Family
ID=18498224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP00985887A Withdrawn EP1253220A4 (en) | 1999-12-27 | 2000-12-26 | Sliding member |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20020197504A1 (en) |
| EP (1) | EP1253220A4 (en) |
| KR (1) | KR100444566B1 (en) |
| WO (1) | WO2001048267A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2006097057A1 (en) * | 2005-03-12 | 2006-09-21 | Federal-Mogul Burscheid Gmbh | Method for generation of anti-wear protective layers on piston rings a a piston ring provided with an anti-wear layer |
| US7422797B2 (en) | 2005-01-12 | 2008-09-09 | Mazda Motor Corporation | Plating layer for sliding portion |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4878438B2 (en) * | 2005-03-08 | 2012-02-15 | 東京特殊電線株式会社 | Probe needle and manufacturing method thereof |
| JP5334052B2 (en) * | 2009-06-11 | 2013-11-06 | 独立行政法人産業技術総合研究所 | Structural member and manufacturing method thereof |
| US20150132604A1 (en) * | 2013-11-14 | 2015-05-14 | National Oilwell DHT, L.P. | Multilayered Coating for Downhole Tools with Enhanced Wear Resistance and Acidic Corrosion Resistance |
| US11162586B2 (en) | 2017-06-02 | 2021-11-02 | Mahle International Gmbh | Piston ring and method of manufacture |
| US11047478B2 (en) * | 2017-06-02 | 2021-06-29 | Mahle International Gmbh | Piston ring and method of manufacture |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3099609A (en) * | 1961-09-11 | 1963-07-30 | Katayose Kimiyoshi | Method of electroplating aluminum or its alloy with porous hard chromium |
| US4039399A (en) * | 1971-03-11 | 1977-08-02 | Dana Corporation | Method of making a bearing surface |
| US4094749A (en) * | 1976-07-06 | 1978-06-13 | Tools For Bending, Inc. | Surface treatment with durable low-friction material |
| DE3531410A1 (en) * | 1985-09-03 | 1987-03-05 | Goetze Ag | GALVANIC HARD CHROME LAYER |
| USH543H (en) * | 1986-10-10 | 1988-11-01 | The United States Of America As Represented By The Secretary Of The Army | Laminated chromium composite |
| DE3809702A1 (en) * | 1988-03-23 | 1989-10-05 | Schaeffler Waelzlager Kg | COMPONENT IN THE VALVE CONTROL DRIVE OF AN INTERNAL COMBUSTION ENGINE |
| JPH0637717B2 (en) * | 1989-06-30 | 1994-05-18 | 上村工業株式会社 | Method and apparatus for surface treatment of object to be treated |
| IT1267394B1 (en) * | 1994-02-18 | 1997-02-05 | Ind S R L | PROCEDURE FOR THE PRODUCTION OF HARD CHROME COMPOSITE GALVANIC FINISHINGS WITH A DISPERSED PHASE AND ANTI-WEAR FINISHING MADE WITH |
| JP3578873B2 (en) * | 1996-08-08 | 2004-10-20 | 帝国ピストンリング株式会社 | Sliding member |
| EP0841413B1 (en) * | 1996-11-11 | 2001-09-26 | Teikoku Piston Ring Co., LTd. | Composite chromium plating film and sliding member covered thereof |
| DE19745811C2 (en) * | 1997-10-16 | 2002-06-13 | Federal Mogul Burscheid Gmbh | Electroplated hard chrome layer, use and method for the production thereof |
| JP2000017482A (en) * | 1998-06-26 | 2000-01-18 | Nippon Piston Ring Co Ltd | Laminated chromium plating film excellent in wear resistance and fatigue strength |
| JP4059621B2 (en) * | 2000-09-29 | 2008-03-12 | 日本ピストンリング株式会社 | Chromium plating sliding member and manufacturing method thereof |
-
2000
- 2000-12-26 EP EP00985887A patent/EP1253220A4/en not_active Withdrawn
- 2000-12-26 KR KR10-2001-7013953A patent/KR100444566B1/en not_active Expired - Fee Related
- 2000-12-26 WO PCT/JP2000/009235 patent/WO2001048267A1/en not_active Ceased
- 2000-12-26 US US09/959,817 patent/US20020197504A1/en not_active Abandoned
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7422797B2 (en) | 2005-01-12 | 2008-09-09 | Mazda Motor Corporation | Plating layer for sliding portion |
| WO2006097057A1 (en) * | 2005-03-12 | 2006-09-21 | Federal-Mogul Burscheid Gmbh | Method for generation of anti-wear protective layers on piston rings a a piston ring provided with an anti-wear layer |
Also Published As
| Publication number | Publication date |
|---|---|
| US20020197504A1 (en) | 2002-12-26 |
| KR100444566B1 (en) | 2004-08-16 |
| EP1253220A4 (en) | 2006-03-22 |
| WO2001048267A1 (en) | 2001-07-05 |
| KR20020013531A (en) | 2002-02-20 |
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