WO2007119842A1 - チタン製の部材に対して行う貴金属めっき - Google Patents
チタン製の部材に対して行う貴金属めっき Download PDFInfo
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- WO2007119842A1 WO2007119842A1 PCT/JP2007/058230 JP2007058230W WO2007119842A1 WO 2007119842 A1 WO2007119842 A1 WO 2007119842A1 JP 2007058230 W JP2007058230 W JP 2007058230W WO 2007119842 A1 WO2007119842 A1 WO 2007119842A1
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- titanium
- temperature
- plate
- degrees celsius
- separator
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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
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/04—Treatment of selected surface areas, e.g. using masks
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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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/322—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
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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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
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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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/341—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one carbide layer
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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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
- C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
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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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/36—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
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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
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/40—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using liquids, e.g. salt baths, liquid suspensions
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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
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/80—After-treatment
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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
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/38—Pretreatment of metallic surfaces to be electroplated of refractory metals or nickel
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/02—Details
- H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
- H01M8/0204—Non-porous and characterised by the material
- H01M8/0206—Metals or alloys
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/02—Details
- H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
- H01M8/0204—Non-porous and characterised by the material
- H01M8/0213—Gas-impermeable carbon-containing materials
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/02—Details
- H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
- H01M8/0204—Non-porous and characterised by the material
- H01M8/0223—Composites
- H01M8/0228—Composites in the form of layered or coated products
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M8/00—Fuel cells; Manufacture thereof
- H01M8/02—Details
- H01M8/0202—Collectors; Separators, e.g. bipolar separators; Interconnectors
- H01M8/0204—Non-porous and characterised by the material
- H01M8/0206—Metals or alloys
- H01M8/0208—Alloys
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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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/30—Hydrogen technology
- Y02E60/50—Fuel cells
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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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Definitions
- the present invention relates to noble metal plating, and more particularly to a technique for performing noble metal plating on a member made of titanium or a titanium alloy.
- the separator in a fuel cell, if the separator is made of a material that will increase the contact resistance with the fuel cell electrode if it is used as it is, the contact portion with the electrode on the surface of the separator will be gold-plated. I have given it.
- a separator when a separator is formed of titanium or a titanium alloy, it is difficult to perform electrolytic gold plating directly on the surface. This is because a titanium oxide film, which is a passive state, is formed on the surface of a titanium or titanium alloy separator (hereinafter collectively referred to as “titanium separator j”).
- the gold plating can be performed overnight on the titanium separator.However, in such a separator evening, there is a defect in the surface metal plating. If present, nickel may leach out of it, and nickel has a negative impact on the environment, so there is a need for a technique for direct gold plating on titanium. Widely used for precious metal plating in titanium or titanium alloy products and parts that require low contact resistance with other conductive members The present invention has been made to solve at least a part of the above-described problems, and an object of the present invention is to provide a technique for performing electrolytic noble metal plating on the surface of titanium. Note that the disclosure of Japanese Patent Application No. 2 0 0 6— 1 1 1 5 1 4 is incorporated into this specification for reference. Disclosure of the invention
- the present invention performs the following treatment when manufacturing a fuel cell separator overnight that is at least partially plated with a noble metal. That is, first, (a) titanium carbide is formed on at least a part of the surface of a titanium member provided with titanium or a titanium alloy and used for a separator of a fuel cell. Thereafter, (b) noble metal plating is performed on at least a part of the surface of the titanium member. Gold adheres to titanium carbide more strongly than titanium oxide. Therefore, with such an embodiment, noble metal plating can be performed on the surface of titanium. In addition, when forming titanium carbide on at least a part of the surface of the titanium member, it is preferable to perform the following treatment.
- a titanium member having a carbon-containing substance attached to the surface is prepared as a chidan member.
- a 2 The first heat treatment is performed on the titanium member at a predetermined first temperature higher than room temperature.
- titanium carbide can be formed on at least a part of the surface of the titanium member.
- the titanium member having a carbon-containing substance attached to the surface thereof can be a titanium member to which the rolling oil used when the titanium member is rolled.
- the carbon containing material is rolling oil. If it is set as such an aspect, titanium carbide can be formed using the rolling oil adhering in the manufacturing process of a titanium member.
- the first temperature is preferably a temperature included in the range of 300 to 700 degrees Celsius.
- the first temperature is in the range of 45 to 50 degrees Celsius It is more preferable that the temperature be included.
- titanium carbide is formed with a non-uniform density on at least a part of the surface of the titanium member by the first treatment. Further, when titanium carbide is formed on the surface of the titanium member, it can be formed as follows. That is, titanium carbide is formed with a first thickness at a first location included in at least part of the surface of the titanium member.
- titanium carbide is formed with a second thickness different from the first thickness at a second location that is included in at least part of the surface of the titanium member and is different from the first location.
- titanium hydride present at the interface between the noble metal plating layer and the titanium member can be diffused into the titanium member.
- the second temperature is preferably a temperature included in the range of 220 degrees Celsius to 400 degrees Celsius.
- the present invention can be realized in various forms.
- a fuel cell separator for example, a fuel cell separator, a method for manufacturing a fuel cell separator, a fuel cell including a titanium separator, and a fuel cell It can be realized in the form of a manufacturing method or the like.
- a fuel cell separator for example, a fuel cell separator, a method for manufacturing a fuel cell separator, a fuel cell including a titanium separator, and a fuel cell It can be realized in the form of a manufacturing method or the like.
- FIG. 1 is a flowchart showing a method for manufacturing a separator according to an embodiment of the present invention.
- FIG. 2 is a cross-sectional view illustrating a separator plate-like member at each stage of the method for manufacturing a separator according to the embodiment.
- Fig. 3 shows the adhesion test of the plating layer by changing the target temperature of the heat treatment in step S20 while changing the conditions of the other steps in Fig. 1 and performing the process of Fig. 1. It is a graph which shows the result.
- FIG. 1 is a flowchart showing a method for manufacturing a separator according to an embodiment of the present invention.
- FIG. 2 is a cross-sectional view showing a plate member for a separate night at each stage of the manufacturing method for a separate night of the embodiment.
- a titanium separator plate member 10 made of gold is prepared.
- the material of the plate-like member 10 can be, for example, JIS type 1 pure titanium.
- This plate-like member ⁇ 0 is a plate-like member provided by rolling a titanium member, and rolling oil 20 is attached to the surface thereof (see FIG. 2 (a)).
- the rolling oil is provided with oil and fat containing carbon.
- the surface of the titanium member is usually covered with passive titanium oxide i 0 2 .
- the pure titanium T i portion of the plate-like member 10 is denoted by 1 1
- the titanium oxide T i 0 2 portion of the surface is denoted by 1 2.
- the plate member 10 is subjected to a conductive treatment.
- plate-like member 1 0 is the argon atmosphere of 1 0- 2 T orr, between about 3 0 seconds is heat treated 4 0 0 degrees to 5 0 0 degrees Celsius.
- the target temperature for temperature control is set to 4500 degrees.
- the carbon in the rolling oil 20 reacts with the surface portion of the plate member 10 made of titanium to become titanium carbide Ti 1 C.
- Plate member The portion of titanium carbide out of 10 is shown as 30 in FIG. 2 (b). Note that the rolling oil 20 attached to the surface of the plate-like member 10 did not adhere to each portion in a strictly homogeneous amount and density. For this reason, the density and thickness of the titanium carbide portion 30 vary depending on the location. In some cases, the passive titanium oxide T i 0 2 remains as it is. That is, the surface of the plate member 1 0, titanium carbide T i-C is a rich portion, titanium oxide Ding I 0 2 is that exist and the rich portion.
- Step S20 can be realized by adjusting the temperature to 400 degrees Celsius to 500 degrees Celsius in the final stage of the annealing process.
- the set temperature of 400 degrees Celsius to 500 degrees Celsius in Step S 20 is a temperature lower than the temperature of the annealing process.
- the cleaning process is performed first. However, even after the cleaning process, sufficient rolling oil that can form titanium carbide in step S20 is made of titanium. It remains on the surface of the plate member.
- step S 3 a pretreatment is performed prior to the subsequent electrolytic gold plating.
- step S 30 buffing is performed on the plate-like member 10.
- the carbonized rolling oil and the like adhering to the surface of the plate-like member 10 by this buffing is mechanically removed by the abrasive.
- step S 40 buffing is removed from the plate-like member 10. In this buff removal, the abrasive attached to the surface of the plate-like member 10 is removed by the surfactant.
- step S 50 immersion degreasing is performed on the plate-like member 10.
- the plate-like member 0 is immersed in an alkaline solution mainly containing Na OH. as a result, Oils and fats on the surface of the plate member 10 are removed by the hatching reaction.
- electrolytic degreasing is performed on the plate-like member 10. Specifically, electrolysis of the plate member 10 is performed in an alkaline solution containing NaOH as a main component. As a result, the dirt on the surface of the plate-like member 10 is removed by the gas generated by the electrolysis along with the hatching reaction.
- acid activity is performed on the plate-like member 10. Specifically, the plate member 10 is immersed in a hydrofluoric acid-based solution.
- step S 70 electrolytic gold plating is performed on the plate-like member 10. Specifically, in a sulfite-based bath containing gold ions or gold complex ions, a plate-like member 10 is disposed on the cathode, and an electric current is applied to deposit metal gold on the surface of the plate-like member 10.
- step S 80 gold plating can be performed on the surface of the plate-like member 10.
- gold adheres more strongly to titanium carbide than titanium oxide, which is in a passive state.
- a gold plating layer 40 is provided on the surface of the plate-like member ⁇ 0 as shown in FIG. 2 (c). At this time, a layer 50 of titanium hydride T i H and T i H 2 is formed between the metallized layer 40 and the titanium carbide portion 30.
- step S 90 the plate member 10 is cleaned. Specifically, the plate-like member 10 is immersed in warm water and cleaned with ultrasonic waves. In step S 1 0 0, heat treatment is performed on the plate-like member 10.
- the plate-like member 1 0 is the argon atmosphere of 1 0- 2 T 0 rr, C 3 0 0 degrees to 3 5 0 degrees to about 9 minutes, it is heat treated.
- the target temperature is 3 30 degrees Celsius.
- the titanium hydride in the titanium hydride layer 50 diffuses into the plate member 10.
- the titanium hydride layer 50 disappears as shown in FIG. 2 (d). Titanium hydride is fragile. For this reason, if the layer 50 of titanium hydride T i H and T i H 2 exists between the gold plating layer 40 and the titanium carbide portion 30, the gold plating layer 40 is easily peeled off.
- titanium hydride between the gold-plated layer 40 and the titanium carbide portion 30 is diffused by heat treatment. For this reason, the gold-plated layer 40 and the titanium carbide portion 30 are firmly adhered, and the gold-plated layer 40 is hardly peeled off from the plate-like member 10.
- Step S 20 the target temperature of the heat treatment in Step S 20 was changed, and the treatment was performed while keeping the conditions of the other steps constant.
- the conditions are as follows.
- Conductive treatment for generating Ti and C on the surface of the plate-like member 10 is about 10 to 2 Torr in argon atmosphere. For 30 seconds, the target temperature was set at various temperatures ranging from 30 to 700 degrees.
- Electrolytic degreasing and immersion degreasing were performed with an alkaline solution containing NaOH as a main component.
- Gold plating (see step S 80) was performed in a sulfite-based bath containing gold complex ions.
- FIG. 3 shows the process of Fig. 1 by changing the target temperature of the heat treatment in step S20 while keeping the conditions of the other steps in Fig. 1 constant.
- Fig. 3 is a graph showing the results of a test of adhesion force V s The test in Fig. 3 was conducted according to the tape peeling method specified in JIS, and as can be seen from the graph in Fig. 3, titanium carbide was generated.
- the heat treatment in step S20 is preferably performed in the range of 400 degrees Celsius to 600 degrees Celsius, and more preferably performed at a temperature of 45 degrees Celsius to 5500 degrees Celsius.
- the adhesion force of the adhesion layer is lower when the temperature is lower than 400 degrees Celsius because of the following reasons: That is, when the temperature of the heat treatment is lower than 400 degrees Celsius, carbonization of the rolling oil, which is a compound containing carbon, is not promoted, and the rolling oil is hardly decomposed. This is probably because Ti i C is not easily generated.
- the reason why the adhesion of the plating layer is reduced is considered to be as follows.
- the titanium plate member 10 in which titanium carbide is nonuniformly formed on the surface by heat treatment as described above (see FIG. 2 (b)), and the same titanium plate member A test was conducted to compare the adhesion strength of the gold plating with each of the titanium carbide layer uniformly provided on the surface by sputtering rather than heat treatment. The test was conducted according to the tape peeling method specified in JIS. As a result, the plate-like member 10 that produced non-uniform titanium carbide on the surface by heat treatment is more firmly attached to the plate-like member that produced uniform titanium carbide by spattering. I found out that
- the present invention is not limited to the above-described examples and embodiments, and can be implemented in various modes without departing from the gist thereof.
- the following modes are also possible.
- the plate-like member 10 is gold-plated.
- the material to be plated on the surface of the member is not limited to gold (A u), but silver (A g), platinum (P t), palladium (P d), rhodium (R h), iridium (I r), ruthenium Other noble metals such as (R u), osmium (O s), etc. can be employed.
- the plate member 10 is made of JIS 1 type titanium.
- the material of the member that performs gold plating is not limited to this.
- the material of the member to be plated can be JIS type 2 or type 3 titanium.
- titanium alloys containing a larger amount of other metals can also be used.
- the titanium carbide is generated by the reaction of carbon in the rolling oil adhering to the surface of the plate-like member 10 and titanium of the plate-like member 10.
- the carbon used to produce titanium carbide may be supplied in other ways.
- a suitable material containing carbon may be applied to the surface of the plate-like member 10 prior to the heat treatment.
- the temperature, pressure, and heating time can be set to various values.
- the heating temperature is preferably 300 ° C. or more and 70 ° C. or less, and preferably 400 ° C. or more and 60 ° C. or less. It is more preferable that the heating temperature be 4500 ° C. or higher and 55 ° C. or lower.
- the step of generating titanium carbide on the surface of the plate-like member 10 (FIG. 1 step S 2 0) is performed at the final stage of the annealing step.
- the process of generating titanium carbide on the surface of the titanium member is not limited to such an embodiment, and can be performed as a process independent of the annealing process.
- titanium carbide is unevenly distributed on the surface of the plate-like member 10 by heat treatment. -It is provided with a certain thickness.
- titanium carbide can also be provided on the surface of the titanium member by other processes such as sputtering. Titanium carbide can also be provided on the surface of the titanium member with a substantially uniform thickness.
- the titanium carbide provided on the surface of the titanium member is more preferably provided with a non-uniform thickness.
- the phrase “titanium carbide is provided with a non-uniform thickness” includes an aspect in which a portion of the surface of the titanium member is not provided with titanium carbide.
- the heat treatment is performed at a target temperature of 3 30 ° C for about 9 minutes in an argon atmosphere of 10 0 to 2 Torr. I do.
- the temperature, pressure, and heating time can be set to various values. It can also be carried out in an atmosphere of other inert gas such as in a helium atmosphere.
- the heating temperature is preferably 300 ° C. or more and 400 ° C. or less, and more preferably 3 20 ° C. or more and 380 ° C. or less.
- This fuel cell is a fuel cell including a membrane electrode assembly that generates power by an electrochemical reaction of a reaction gas, and the separator.
- the membrane electrode assembly includes an electrolyte membrane and electrodes provided on both sides of the electrolyte membrane.
- the separator is provided on the side opposite to the electrolyte membrane with respect to the electrode, and is in contact with the electrode through a gold-plated portion.
- the separator since the separator is made of titanium, the separator can exhibit stable performance over a long period of time without causing corrosion.
- the contact resistance between the separator evening and the electrode is small because the separator evening is in contact with the electrode through the gold-plated portion.
- the power generation efficiency is higher than when there is no gold plating at the contact portion between the separator and the electrode. And in the Separat evening In this case, since the gold plating layer and the titanium member are in contact with each other through titanium carbide, the gold plating layer is difficult to peel from the titanium member.
- the present invention has been described in detail above with reference to preferred exemplary embodiments thereof. However, the present invention is not limited to the embodiments and configurations described above. The present invention includes various modifications and equivalent configurations. Furthermore, although the various elements of the disclosed invention have been disclosed in various combinations and configurations, they are exemplary and each element may be more or less. And there may be one element. These embodiments are included in the scope of the present invention.
- the present invention can be applied to a fuel cell, a fuel cell system, a prime mover using the fuel cell as a power source, and a vehicle having a power source using the fuel cell.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Electrochemistry (AREA)
- Sustainable Development (AREA)
- Manufacturing & Machinery (AREA)
- Sustainable Energy (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Composite Materials (AREA)
- Electroplating Methods And Accessories (AREA)
- Fuel Cell (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Physical Vapour Deposition (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE112007000680T DE112007000680B8 (de) | 2006-04-14 | 2007-04-10 | Edelmetallplattierung von Titankomponenten |
JP2008511015A JP5088318B2 (ja) | 2006-04-14 | 2007-04-10 | チタン製の部材に対して行う貴金属めっき |
CA2646189A CA2646189C (en) | 2006-04-14 | 2007-04-10 | Noble metal plating of titanium components |
US12/282,003 US8211495B2 (en) | 2006-04-14 | 2007-04-10 | Noble metal plating of titanium components |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006111514 | 2006-04-14 | ||
JP2006-111514 | 2006-04-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2007119842A1 true WO2007119842A1 (ja) | 2007-10-25 |
Family
ID=38609601
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2007/058230 WO2007119842A1 (ja) | 2006-04-14 | 2007-04-10 | チタン製の部材に対して行う貴金属めっき |
Country Status (6)
Country | Link |
---|---|
US (1) | US8211495B2 (ja) |
JP (1) | JP5088318B2 (ja) |
CN (1) | CN101421875A (ja) |
CA (1) | CA2646189C (ja) |
DE (1) | DE112007000680B8 (ja) |
WO (1) | WO2007119842A1 (ja) |
Cited By (6)
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JP2009123528A (ja) * | 2007-11-15 | 2009-06-04 | Kobe Steel Ltd | 燃料電池セパレータ用チタン基材およびこれを用いた燃料電池セパレータの製造方法 |
JP2009289511A (ja) * | 2008-05-28 | 2009-12-10 | Kobe Steel Ltd | 燃料電池セパレータ用チタン基材、および、燃料電池セパレータ、ならびに燃料電池セパレータの製造方法 |
WO2010119313A1 (en) * | 2009-04-15 | 2010-10-21 | Toyota Jidosha Kabushiki Kaisha | Titanium-based material, method of manufacturing titanium-based material and fuel cell separator |
WO2011016465A1 (ja) * | 2009-08-03 | 2011-02-10 | 新日本製鐵株式会社 | 固体高分子型燃料電池セパレータ用チタン材およびその製造方法 |
JP2012028046A (ja) * | 2010-07-20 | 2012-02-09 | Kobe Steel Ltd | チタン製燃料電池セパレータ |
WO2014156673A1 (ja) * | 2013-03-27 | 2014-10-02 | 株式会社神戸製鋼所 | 燃料電池セパレータ用チタン板材およびその製造方法 |
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US20040118553A1 (en) * | 2002-12-23 | 2004-06-24 | Graftech, Inc. | Flexible graphite thermal management devices |
CN102051647A (zh) * | 2010-12-29 | 2011-05-11 | 东莞市泰赛特汽车用品科技有限公司 | 钛及钛合金的无氰无镍水电镀工艺 |
JP5108976B2 (ja) * | 2011-02-14 | 2012-12-26 | 株式会社神戸製鋼所 | 燃料電池セパレータ |
JP2013174261A (ja) * | 2012-02-23 | 2013-09-05 | Advics Co Ltd | ディスクロータ |
WO2015111652A1 (ja) * | 2014-01-22 | 2015-07-30 | 新日鐵住金株式会社 | 表面の導電性を有するチタン材又はチタン合金材、これを用いた燃料電池セパレータと燃料電池 |
CN105750842B (zh) * | 2016-04-29 | 2018-03-13 | 成都九十度工业产品设计有限公司 | 一种贵金属纪念币的加工方法 |
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JP2009123528A (ja) * | 2007-11-15 | 2009-06-04 | Kobe Steel Ltd | 燃料電池セパレータ用チタン基材およびこれを用いた燃料電池セパレータの製造方法 |
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WO2010119313A1 (en) * | 2009-04-15 | 2010-10-21 | Toyota Jidosha Kabushiki Kaisha | Titanium-based material, method of manufacturing titanium-based material and fuel cell separator |
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DE112010001642B4 (de) * | 2009-04-15 | 2019-05-02 | Toyota Jidosha Kabushiki Kaisha | Verfahren zum herstellen eines materials auf titanbasis |
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WO2011016465A1 (ja) * | 2009-08-03 | 2011-02-10 | 新日本製鐵株式会社 | 固体高分子型燃料電池セパレータ用チタン材およびその製造方法 |
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JP2012028046A (ja) * | 2010-07-20 | 2012-02-09 | Kobe Steel Ltd | チタン製燃料電池セパレータ |
JP2014192039A (ja) * | 2013-03-27 | 2014-10-06 | Kobe Steel Ltd | 燃料電池セパレータ用チタン板材およびその製造方法 |
RU2633173C2 (ru) * | 2013-03-27 | 2017-10-11 | Кабусики Кайся Кобе Сейко Се (Кобе Стил, Лтд.) | Материал титанового листа для сепараторов топливных элементов и способ его получения |
WO2014156673A1 (ja) * | 2013-03-27 | 2014-10-02 | 株式会社神戸製鋼所 | 燃料電池セパレータ用チタン板材およびその製造方法 |
Also Published As
Publication number | Publication date |
---|---|
DE112007000680B8 (de) | 2013-10-31 |
CN101421875A (zh) | 2009-04-29 |
DE112007000680B4 (de) | 2013-08-14 |
CA2646189C (en) | 2011-07-26 |
JPWO2007119842A1 (ja) | 2009-08-27 |
US20090087558A1 (en) | 2009-04-02 |
DE112007000680T5 (de) | 2009-02-19 |
US8211495B2 (en) | 2012-07-03 |
JP5088318B2 (ja) | 2012-12-05 |
CA2646189A1 (en) | 2007-10-25 |
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