WO2018116532A1 - 耐食部材 - Google Patents
耐食部材 Download PDFInfo
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- WO2018116532A1 WO2018116532A1 PCT/JP2017/031528 JP2017031528W WO2018116532A1 WO 2018116532 A1 WO2018116532 A1 WO 2018116532A1 JP 2017031528 W JP2017031528 W JP 2017031528W WO 2018116532 A1 WO2018116532 A1 WO 2018116532A1
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- WIPO (PCT)
- Prior art keywords
- corrosion
- resistant member
- coating material
- dlc film
- coating
- Prior art date
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- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47J—KITCHEN EQUIPMENT; COFFEE MILLS; SPICE MILLS; APPARATUS FOR MAKING BEVERAGES
- A47J36/00—Parts, details or accessories of cooking-vessels
- A47J36/02—Selection of specific materials, e.g. heavy bottoms with copper inlay or with insulating inlay
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
- B32B15/092—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin comprising epoxy resins
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- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
- C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
- C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D163/00—Coating compositions based on epoxy resins; Coating compositions based on derivatives of epoxy resins
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- C—CHEMISTRY; METALLURGY
- C09—DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
- C09D—COATING COMPOSITIONS, e.g. PAINTS, VARNISHES OR LACQUERS; FILLING PASTES; CHEMICAL PAINT OR INK REMOVERS; INKS; CORRECTING FLUIDS; WOODSTAINS; PASTES OR SOLIDS FOR COLOURING OR PRINTING; USE OF MATERIALS THEREFOR
- C09D7/00—Features of coating compositions, not provided for in group C09D5/00; Processes for incorporating ingredients in coating compositions
- C09D7/40—Additives
- C09D7/60—Additives non-macromolecular
- C09D7/61—Additives non-macromolecular inorganic
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/024—Deposition of sublayers, e.g. to promote adhesion of the coating
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0605—Carbon
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/0605—Carbon
- C23C14/0611—Diamond
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/08—Oxides
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/14—Metallic material, boron or silicon
- C23C14/16—Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/22—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the process of coating
- C23C14/24—Vacuum evaporation
- C23C14/32—Vacuum evaporation by explosion; by evaporation and subsequent ionisation of the vapours, e.g. ion-plating
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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
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/58—After-treatment
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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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/02—Pretreatment of the material to be coated
- C23C16/0272—Deposition of sub-layers, e.g. to promote the adhesion of the main coating
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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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/22—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the deposition of inorganic material, other than metallic material
- C23C16/26—Deposition of carbon 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
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/56—After-treatment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/043—Sliding surface consisting mainly of ceramics, cermets or hard carbon, e.g. diamond like carbon [DLC]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2202/00—Metallic substrate
- B05D2202/20—Metallic substrate based on light metals
- B05D2202/25—Metallic substrate based on light metals based on Al
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2350/00—Pretreatment of the substrate
- B05D2350/60—Adding a layer before coating
- B05D2350/63—Adding a layer before coating ceramic layer
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/30—Coating surfaces
- F16C2223/60—Coating surfaces by vapour deposition, e.g. PVD, CVD
Definitions
- the present invention relates to a corrosion-resistant member in which a diamond-like carbon film is formed on the surface of a base material made of aluminum or an aluminum alloy.
- devices that handle foods and beverages may come into contact with water, salt water, acidic or alkaline foods and beverages, cleaning agents, disinfecting / disinfecting agents, and the like.
- a corrosion-resistant member having corrosion resistance.
- Such a corrosion-resistant member is generally made of stainless steel as described in, for example, Japanese Patent Application Laid-Open No. 2003-160839.
- stainless steel is excellent in corrosion resistance, it has a high density among metal materials and tends to have high material costs and processing costs. For this reason, in the corrosion-resistant member made of stainless steel, there is a concern that the weight increases or the manufacturing cost increases. Further, stainless steel has low lubricity and is likely to be worn by adhesion. That is, since the slidability is low, it is difficult to use the corrosion-resistant member as a shaft member that slides against a mating member such as a bearing.
- Japanese Patent Application Laid-Open No. 2001-191292 discloses a corrosion-resistant member that is improved in corrosion resistance and the like by forming an anodized film on the surface of a base material made of aluminum by anodizing or coating with a fluororesin. Proposed.
- Aluminum has a lower density than stainless steel and can reduce material costs and processing costs. Therefore, by using aluminum instead of stainless steel, it is possible to reduce the weight and cost of the corrosion-resistant member.
- the main object of the present invention is to provide a corrosion-resistant member capable of reducing the weight and cost, and improving the slidability and wear resistance without reducing the hardness of the base material. is there.
- Another object of the present invention is to provide a corrosion-resistant member exhibiting excellent corrosion resistance against strong acids and strong alkalis.
- a corrosion-resistant member which is a base material made of aluminum or an aluminum alloy, amorphous carbon (aC) or hydrogenated amorphous carbon (a-).
- a corrosion-resistant member comprising a diamond-like carbon film made of C: H) and a coating material filled with at least open pores of the diamond-like carbon film and containing an epoxy resin.
- the corrosion-resistant member according to the present invention has a lower density than stainless steel and the like, and is provided with a base material made of aluminum or aluminum alloy capable of reducing material costs and processing costs, thereby reducing weight and cost. Can be achieved.
- a diamond-like carbon film (hereinafter also simply referred to as a DLC film) made of aC or aC: H is formed on the surface of the substrate.
- aC and aC: H are ratios of sp 2 bonds to sp 3 bonds compared to tetrahedral amorphous carbon (ta-C) and hydrogenated tetrahedral amorphous carbon (ta-C: H). Is large and flexible.
- the DLC film made of aC or aC: H can be satisfactorily bonded to the surface of a base material made of relatively soft aluminum or aluminum alloy with a desired thickness. Difficult to peel from.
- this DLC film has high hardness and excellent lubricity. That is, the corrosion resistant member provided with the DLC film on the base material can exhibit excellent slidability and wear resistance over a long period of time.
- the open pores which are pores communicating with the outside of the DLC film, are filled with a coating material.
- the DLC film is sealed with the coating material.
- This coating material contains an epoxy resin having higher corrosion resistance than other resin materials. Accordingly, as described above, the corrosion resistance of the corrosion-resistant member can be improved satisfactorily due to the fact that the DLC film is difficult to peel from the substrate.
- this coating material can be formed by a so-called baking process in which a resin material containing an epoxy resin or a solvent is applied to a base material on which a DLC film is formed and heated.
- This baking process can be performed, for example, at a temperature of 140 to 180 ° C. or lower, in other words, a temperature at which the hardness of the base material does not decrease. Therefore, for example, unlike the case where the fluororesin coating is provided by high-temperature baking, there is no concern that the base material becomes high temperature when the coating material is provided, and the hardness thereof decreases. For this reason, the corrosion-resistant member which can be used suitably as a machine part can be obtained.
- this corrosion-resistant member by providing a base material made of aluminum or an aluminum alloy, the weight can be reduced and the cost can be reduced, and the DLC film formed on the surface of the base material is slidable. Also excellent in wear resistance. Furthermore, since the DLC film is sealed with the above-mentioned coating material, it is excellent not only against water and salt water, but also against sterilizing / disinfecting agents such as strong acids and strong alkalis and sodium hypochlorite. Shows corrosion resistance. Furthermore, the coating material can be provided without a high temperature that lowers the hardness of the substrate.
- the coating material further contains titanium oxide and carbon black.
- the corrosion resistance of the corrosion resistant member can be further improved, and in particular, the acid resistance can be significantly improved. Therefore, it is possible to obtain a corrosion-resistant member that exhibits excellent corrosion resistance even against strong acids.
- the coating material preferably has a mass ratio of epoxy resin, titanium oxide, and carbon black of 5: 1: 1 to 20:10:10.
- the corrosion resistance of the corrosion resistant member in particular, the acid resistance can be improved more effectively.
- the coating material preferably further contains chromium oxide.
- the corrosion resistance of the corrosion-resistant member can be further improved, and in particular, the alkali resistance can be remarkably improved. Therefore, it is possible to obtain a corrosion-resistant member that exhibits excellent corrosion resistance even against strong alkalis.
- the coating material preferably has a mass ratio of 5: 1 to 20:10 between the epoxy resin and chromium oxide.
- the corrosion resistance of the corrosion resistant member in particular, the alkali resistance can be improved more effectively.
- the diamond-like carbon film includes an intermediate layer containing aluminum and amorphous carbon (aC) or hydrogenated amorphous carbon (aC: H) constituting the diamond-like carbon film. It is preferably formed on the surface of the substrate.
- the intermediate layer constituted in this manner is well adapted to the base material because it contains aluminum which is a constituent metal of the base material, and contains aC or aC: H constituting the DLC film. Fits well with DLC film. For this reason, the intermediate layer is firmly bonded to both the base material and the DLC film. Through this intermediate layer, the DLC film can be firmly bonded to the substrate. As a result, it is possible to maintain excellent slidability and wear resistance based on the high hardness and high lubricity of the DLC film and excellent corrosion resistance based on the DLC film and coating material over a long period of time.
- the coating material preferably forms a coating layer that covers at least a part of the diamond-like carbon film.
- the acid or alkali reaches the DLC film or the base material because at least a part of the DLC film is covered with the coating layer. it can. Thereby, the corrosion resistance of the corrosion-resistant member can be further improved.
- the surface of the diamond-like carbon film is exposed from the coating layer in a state where the open pores are filled with the coating material.
- the sliding surface exposed by the DLC film can utilize the excellent slidability and wear resistance of the DLC film as it is. Can be suitably used.
- the open pores of the DLC film on the sliding surface are filled with coating material, excellent corrosion resistance against water, salt water, strong acid, strong alkali, disinfectant / disinfectant (sodium hypochlorite), etc. is maintained. can do. That is, this corrosion-resistant member has excellent slidability and wear resistance, and corrosion resistance.
- the sliding surface slides with a counterpart material and the material of the counterpart material is any one of stainless steel, polyacetal resin, and polytetrafluoroethylene (PTFE).
- the wear of both the sliding surface and the mating member and the wear of the corrosion-resistant member can be effectively suppressed, and the durability of the corrosion-resistant member and the mating material can be improved.
- the material of the counterpart material is stainless steel
- the stainless steel is more preferably one of SUS304, SUS303, and SUS316.
- fluorine-based grease is interposed between the sliding surface and the counterpart material.
- the wear of the sliding surface and the mating member can be further satisfactorily suppressed by the fluorine-based grease.
- This fluorine-based grease is excellent in corrosion resistance compared to other greases. Moreover, even if it contacts a drink or a foodstuff, it can be set as a safe structure by using the fluorine-type grease of the lubricant for food machinery.
- the above corrosion-resistant member can be suitably used as a shaft member having the counterpart material as a bearing member. This is because the corrosion-resistant member has both the slidability and wear resistance of the sliding surface with respect to the bearing member and the corrosion resistance of the entire shaft member.
- the above-mentioned corrosion-resistant member preferably constitutes an apparatus for handling beverages or foods.
- the corrosion-resistant member is excellent in corrosion resistance, for example, even when it comes into contact with water, salt water, acidic or alkaline foods and beverages, cleaning agents, disinfecting / disinfecting agents, etc., corrosion can be effectively avoided.
- both the DLC film and the coating material can be configured to be safe even when they come into contact with beverages or foods. Therefore, by configuring a device for handling beverages or foods with the corrosion-resistant member, it is possible to improve the corrosion resistance while maintaining the food safety of the device, and it is also possible to reduce the weight and cost. It becomes.
- FIG. 1 is a schematic cross-sectional view of a main part of a corrosion-resistant member and a counterpart material according to an embodiment of the present invention.
- FIG. 2 is an enlarged cross-sectional view of a main part of the corrosion-resistant member of FIG.
- the corrosion-resistant member according to the present invention can be suitably used as, for example, a device for handling beverages or foods.
- the apparatus include machinery used when mixing, kneading, stirring, pulverizing, heating, drying, cooling, filling, packaging, storage, and the like of beverages or foods.
- this corrosion-resistant member can be particularly suitably applied as a shaft member constituting a rotating shaft or a linear motion shaft of various processing machines used for, for example, kneading, stirring, and pulverizing beverages or foods. Therefore, in this embodiment, the corrosion-resistant member is a shaft member, and an example in which a sliding bearing device for food processing is configured together with a counterpart material that is a bearing member that slidably supports the corrosion-resistant member will be described.
- the apparatus to which the corrosion-resistant member is applied is not limited to one that handles beverages or foods, and may not include a counterpart material.
- Each of the corrosion-resistant member and the mating member is not limited to the shaft member and the bearing member.
- the corrosion-resistant member may be a cylinder body, and the mating member may be a piston or the like.
- the corrosion-resistant member 10 is a shaft member that constitutes a rotating shaft, and constitutes a sliding bearing device 14 together with a mating member 12 that is a bearing member.
- the corrosion-resistant member 10 includes a base material 16, a diamond-like carbon film (DLC film) 18, and a coating material 20.
- DLC film diamond-like carbon film
- the base material 16 is a solid shaft made of aluminum or an aluminum alloy.
- A2017, A6060, ADC12, A5052 etc. which are specified by Japanese Industrial Standard (JIS) are mentioned.
- the DLC film 18 is formed on the surface of the base material 16 via the intermediate layer 22, and is made of amorphous carbon (aC) or hydrogenated amorphous carbon (aC: H).
- aC and aC: H are ratios of sp 2 bonds to sp 3 bonds compared to tetrahedral amorphous carbon (ta-C) and hydrogenated tetrahedral amorphous carbon (ta-C: H). Is a large diamond-like carbon. Further, aC is composed only of carbon elements, and ac: H contains hydrogen.
- the preferred thickness of the DLC film 18 is 1 to 4 ⁇ m, more preferably 2.5 to 3.5 ⁇ m.
- the preferred Vickers hardness of the DLC film 18 is 1000 to 4000 HV, and more preferably 1400 to 3000 HV.
- the intermediate layer 22 contains a metal (aluminum) constituting the base material 16 and aC or aC: H (hereinafter collectively referred to as DLC) constituting the DLC film 18.
- DLC a metal (aluminum) constituting the base material 16 and aC or aC: H (hereinafter collectively referred to as DLC) constituting the DLC film 18.
- the composition ratio of aluminum increases as it approaches the base material 16, while the composition ratio of DLC decreases. In other words, as the distance from the base material 16 decreases, the composition ratio of aluminum decreases. It is preferable that the composition ratio of DLC becomes large.
- the intermediate layer 22 becomes an inclined layer in which the composition ratio of aluminum / DLC changes in the thickness direction, and the intermediate layer 22 can be more firmly bonded to each of the base material 16 and the DLC film 18.
- the thickness of the intermediate layer 22 is not particularly limited, but it is sufficient to set it to about 0.01 to 1.0 ⁇ m.
- FIG. 2 is an enlarged cross-sectional view of the main part of the corrosion-resistant member 10. As shown in FIG. 2, among the defects generated in the DLC film 18 and the intermediate layer 22, there are open pores 24 that communicate with the outside through the surface of the DLC film 18. The coating material 20 is filled in at least such open pores 24. That is, the DLC film 18 is sealed with the coating material 20.
- the coating material 20 fills the open pores 24 and forms the coating layer 20a that covers the portion of the DLC film 18 excluding the sliding surface 26.
- the sliding surface 26 is a portion that slides with the counterpart material 12.
- the open pores 24 of the sliding surface 26 are also filled with the coating material 20.
- the thickness of the coating layer 20a may be appropriately set according to the application, shape, usage environment, and the like of the corrosion resistant member 10. For example, when the thickness is 5 to 30 ⁇ m, the corrosion resistance of the corrosion resistant member 10 is good. It becomes possible to improve.
- Coating material 20 contains an epoxy resin, and preferably further contains titanium oxide and carbon black, or chromium oxide.
- the coating material 20 contains an epoxy resin, titanium oxide, and carbon black, these suitable mass ratios (epoxy resin: titanium oxide: carbon black) are 5: 1: 1 to 20:10:10. . Thereby, the corrosion resistance of the corrosion-resistant member 10, especially the acid resistance can be effectively improved.
- the coating material 20 contains an epoxy resin and chromium oxide
- the preferred mass ratio (epoxy resin: chromium oxide) is 5: 1 to 20:10.
- the corrosion resistance of the corrosion-resistant member 10, especially the alkali resistance can be effectively improved.
- the mating member 12 is a bearing member that holds the corrosion-resistant member 10 so as to be capable of rotating and sliding, and the inner peripheral surface of the mating material 12 and the sliding surface 26 of the corrosion-resistant member 10 slide.
- the material of the counterpart material 12 is not particularly limited, but for example, stainless steel, polyacetal resin, polytetrafluoroethylene (PTFE), and the like are suitable.
- the stainless steel used as the material of the counterpart material 12 is SUS304, SUS303, SUS316, or the like.
- a fluorine grease 28 of a food machine lubricant is interposed between the sliding surface 26 of the corrosion-resistant member 10 and the inner peripheral surface of the mating member 12 so as to cover the sliding surface 26. It is preferable to do. In this case, the wear of the sliding surface 26 and the counterpart material 12 can be satisfactorily suppressed by the fluorine-based grease 28. Further, the fluorine-based grease 28 is excellent in corrosion resistance as compared with other greases, and is safe even when in contact with a beverage or food.
- the corrosion resistant member 10 according to the present embodiment is basically configured as described above. Hereinafter, an example of the manufacturing method of the corrosion-resistant member 10 will be described.
- the substrate 16 is subjected to plasma cleaning using argon ions or the like. Thereby, the adhesion of the intermediate layer 22 formed thereafter can be further strengthened.
- the intermediate layer 22 and the DLC film 18 are formed on the base material 16 by sputtering using an inert gas such as argon and a graphite target.
- middle layer 22 and the DLC film 18 can be formed into a film by not only said method but a well-known method.
- various physical vapor deposition methods PVD
- various chemical vapor deposition methods are adopted. (CVD) can be employed.
- a coating process for coating the DLC film 18 with a resin material for forming the coating material 20 is performed.
- the resin material for forming the coating material 20 that does not contain any of titanium oxide, carbon black, and chromium oxide include those containing 3% by mass of an epoxy resin and the remaining solvent.
- the resin material for forming the coating material 20 containing titanium oxide and carbon black As a suitable example of the resin material for forming the coating material 20 containing titanium oxide and carbon black, 5 to 20% by mass of an epoxy resin, 1 to 10% by mass of titanium oxide, and 1 to 10%. What contains the carbon black of a mass% and the remainder solvent is mentioned.
- the resin material for forming the coating material 20 containing chromium oxide contains 5 to 20% by mass of an epoxy resin, 1 to 10% by mass of chromium oxide, and the remaining solvent. To do.
- the resin material is filled in the open pores 24 of the DLC film 18, and a coating film that covers the entire DLC film 18 is formed by the resin material.
- known coating methods such as brush coating, roller coating, spray coating, bar coater, roll coater, baking coating, and dip coating can be employed.
- the resin material coated on the base material 16 is heated at, for example, a temperature of 180 ° C. or less to perform a baking process. Thereby, the resin material is cured and the coating material 20 is formed. That is, the coating material 20 is filled in the open pores 24 of the DLC film 18, and the entire DLC film 18 is covered with the coating layer 20a that is a cured coating film.
- the coating material 20 can be formed by a baking process at a relatively low temperature without lowering the hardness of the base material. Therefore, for example, unlike the case where the fluororesin coating is provided by high-temperature baking, there is no concern that the base material 16 becomes high temperature when the coating material 20 is provided, and the hardness thereof decreases.
- a removal step of removing the coating material 20 at the site that becomes the sliding surface 26 of the corrosion-resistant member 10 is performed to expose the DLC film 18 from the coating layer 20a.
- the removing step can be performed using a known method such as cutting or polishing.
- the corrosion-resistant member 10 is obtained.
- the sliding bearing device 14 is obtained by assembling the mating member 12 to the corrosion-resistant member 10 so that the inner peripheral surface of the mating member 12 slides on the sliding surface 26.
- the corrosion-resistant member 10 includes the base material 16 made of aluminum or an aluminum alloy.
- Aluminum or aluminum alloy has a lower density than stainless steel and the like, and can reduce material costs and processing costs. For this reason, by providing said base material 16, it becomes possible to aim at the weight reduction of the corrosion-resistant member 10, and cost reduction.
- the DLC film 18 covering the substrate 16 is made of aC or aC: H having a large ratio of sp 2 bonds to sp 3 bonds, so that the DLC film 18 is rich in flexibility. Therefore, the DLC film 18 can be formed with a desired thickness even on the surface of the base material 16 made of relatively soft aluminum or aluminum alloy, and the base material 16 and the DLC film 18 can be bonded well. can do.
- the DLC film 18 exhibits good slidability based on a low coefficient of friction, and also exhibits good wear resistance based on high hardness. Therefore, by providing such a DLC film 18, the slidability and wear resistance of the corrosion-resistant member 10 can be improved satisfactorily.
- An intermediate layer 22 containing aluminum and aC or aC: H is interposed between the DLC film 18 and the substrate 16. Since the intermediate layer 22 configured in this manner includes the constituent metals of the base material 16, the intermediate layer 22 conforms well to the base material 16 and includes aC or aC: H constituting the DLC film 18. Furthermore, it is well adapted to the DLC film 18. For this reason, the intermediate layer 22 is firmly bonded to both the base material 16 and the DLC film 18. Through the intermediate layer 22, the DLC film 18 can be firmly bonded to the base material 16.
- the DLC film 18 and the intermediate layer 22 are sealed with a coating material 20, and the portion of the DLC film 18 excluding the sliding surface 26 is further covered with a coating layer 20 a made of the coating material 20.
- the coating material 20 contains an epoxy resin having higher corrosion resistance than other resin materials.
- the corrosion-resistant member 10 By sealing with such a coating material 20, even when acid, alkali, or the like is in contact, it can be prevented that they reach the substrate 16 through the open pores 24. In addition, at the portion covered with the coating layer 20a of the corrosion-resistant member 10, it is possible to more effectively avoid acid, alkali, or the like from reaching the DLC film 18 or the base material 16. As a result, the corrosion-resistant member 10 exhibits excellent corrosion resistance not only against water and salt water, but also against strong acids and strong alkalis and sterilizing / disinfecting agents such as sodium hypochlorite.
- the corrosion resistance of the corrosion-resistant member 10 can be further improved, and particularly the acid resistance can be remarkably improved. Therefore, it is possible to obtain the corrosion-resistant member 10 that exhibits excellent corrosion resistance against strong acids.
- the corrosion resistance of the corrosion-resistant member 10 can be further improved, and in particular, the alkali resistance can be remarkably improved. Therefore, it is possible to obtain the corrosion-resistant member 10 exhibiting excellent corrosion resistance against strong alkalis.
- the corrosion-resistant member 10 can be improved by providing the sliding surface 26.
- the coating material 20 is also filled in the open pores 24 of the DLC film 18 on the sliding surface 26, excellent corrosion resistance can be maintained even if the sliding surface 26 is provided. That is, the corrosion-resistant member 10 can have both excellent slidability and wear resistance and corrosion resistance.
- the intermediate layer 22 is provided, but the intermediate layer 22 may not be provided.
- the sliding surface 26 is provided.
- the entire DLC film 18 may be covered with the coating layer 20a without providing the sliding surface 26.
- the corrosion-resistant member 10 can be suitably used for applications other than sliding members as members that require high corrosion resistance.
- the entire DLC film 18 may be exposed without providing the coating layer 20 a on the corrosion-resistant member 10. In this case, the entire corrosion-resistant member 10 exhibits excellent slidability and wear resistance.
- Example 1 As the base material 16, a solid shaft body made of A6061-T6, having a diameter of 10 mm and a length of 50 mm, was subjected to mirror polishing. The intermediate layer 22 and the DLC film 18 were formed on the base material 16 so as to have a total thickness of 2.0 to 2.2 ⁇ m. The average Vickers hardness on the surface of the DLC film 18 was 1350 HV. In addition, average Vickers hardness is measured according to the test method of JIS Z 2244, and is a three-point average value when the load is 10 gf. The same applies to the average Vickers hardness shown below.
- epoxy resin is 3.0% by mass
- xylene is 17.0% by mass
- ethylbenzene is 11.0% by mass
- n-butanol is 5.0 to 10.0% by mass.
- 1.0-5.0% by mass of isobotanol 1.0-5.0% by mass of ethylene glycol monobutyl ether, 0.1-1.0% by mass of methanol, 0.8% by mass of formaldehyde, melamine resin Containing 16.0% by mass of alkyd resin and 37.0% by mass of alkyd resin.
- the resin member is applied to the DLC film 18 and subjected to a baking process, whereby the open pores 24 of the DLC film 18 are sealed with the coating material 20 and the thickness of the DLC film 18 is covered so as to cover the entire DLC film 18.
- a corrosion resistant member 10 was obtained by forming a coating layer 20a having a thickness of 0.0 to 26.0 ⁇ m. This is the test member of Example 1.
- the average Vickers hardness of the coating layer 20a surface of Example 1 was 12HV.
- Example 2 As a resin material for forming the coating material 20, epoxy resin is 5 to 20% by mass, titanium oxide is 1 to 10% by mass, carbon black is 1 to 10% by mass, xylene is 5 to 15% by mass, and methyl ethyl ketone is 15%. -25% by mass, 2-ethoxyethyl acetate 5-15% by mass, toluene 10-20% by mass, ethylene glycol monobutyl ether 1-10% by mass, and coating layer 20a
- the corrosion-resistant member 10 was obtained in the same manner as in Example 1 except that the thickness of was 21.0 to 25.0 ⁇ m.
- Example 3 As resin materials, 5-20% by mass of epoxy resin, 1-10% by mass of chromic oxide, 15-25% by mass of 1,2-dichloroethane, 5-15% by mass of methyl isobutyl ketone, 5% of methyl ethyl ketone -15% by weight, diacetone alcohol 10-20% by weight, ethanol containing 10-20% by weight, and the thickness of the coating layer 20a was 25.0-30.0 ⁇ m Except for this, the corrosion-resistant member 10 was obtained in the same manner as in Example 1. This is the test member of Example 3. That is, the test member of Example 3 includes the coating material 20 containing chromium oxide. In addition, the average Vickers hardness of the coating layer 20a surface of Example 3 was 20HV.
- Example 4 A corrosion-resistant member 10 obtained in the same manner as in Example 1 except that A2017 is selected as the material of the base material 16 is used as a test member in Example 4.
- a corrosion-resistant member 10 obtained in the same manner as in Example 2 except that A2017 is selected as the material of the base material 16 is used as a test member of Example 5.
- a corrosion-resistant member 10 obtained in the same manner as the test member of Example 2 is used as the test member of Example 6 except that ADC 12 is selected as the material of the base material 16.
- Comparative Example 1 For comparison, a test member made of only the same base material 16 as in Example 1 was used as Comparative Example 1. That is, the test member of Comparative Example 1 does not include any of the intermediate layer 22, the DLC film 18, and the coating material 20.
- Comparative Example 2 A test member produced in the same manner as in Example 1 except that the coating material 20 was not provided was designated as Comparative Example 2. That is, in the test member of Comparative Example 2, the DLC film 18 is not sealed with the coating material 20.
- Comparative Example 3 A test member in which the same base material 16 as in Example 1 was anodized to form an anodized film (Al 2 O 3 ) having a thickness of 13.0 to 16.0 ⁇ m was defined as Comparative Example 3.
- the anodized film of the test member of Comparative Example 3 was sealed and coated with the same coating material 20 as in Example 1 to form a coating layer 20a having a thickness of 22.0 to 26.0 ⁇ m.
- the test member of Comparative Example 4 was obtained.
- a test member of Comparative Example 5 was obtained in the same manner as Comparative Example 4 except that the same coating material 20 as in Example 2 was selected.
- the average Vickers hardness on the surface of the anodized film in the test members of Comparative Examples 3 to 5 was 320 HV.
- Comparative Example 6 A test member produced in the same manner as in Example 4 except that the coating material 20 was not provided was designated as Comparative Example 6. That is, in the test member of Comparative Example 6, the DLC film 18 is not sealed with the coating material 20.
- Corrosion resistance evaluation tests were performed using the test members of Examples 1 to 6 and Comparative Examples 1 to 6 described above and seven different liquids A to G.
- the test members of Examples 1 to 3 and Comparative Examples 1 to 3 and 5 were subjected to a corrosion resistance evaluation test for liquid A (pH 3.5) which is a Pilsner beer.
- liquid A pH 3.5
- the amount of change in weight before and after the entire test member was immersed in liquid A at room temperature for 30 days was determined. It can be determined that the smaller the change in weight, the more the corrosion of the test member is suppressed and the higher the corrosion resistance.
- Liquid B is a 3.0% by mass aqueous solution of a food-related acidic detergent containing 35.0% by mass of phosphoric acid as a main component.
- Liquid C is a 3.0% by mass aqueous solution of a food-related alkaline detergent containing 15.0% by mass of sodium hydroxide as a main component.
- test members of Examples 1 to 6 having both the DLC film 18 and the coating material 20 are the test members of the comparative example 1 consisting of only the base material 16 and the DLC film for all liquids A to G. It turned out that the corrosion resistance superior to the test member of the comparative examples 2 and 6 which consists only of 18 and the test member of the comparative example 3 which consists only of an anodic oxide film is shown.
- test members of Examples 2, 5, and 6 including the coating material 20 containing the epoxy resin, titanium oxide, and carbon black exhibit excellent corrosion resistance against all the liquids A to G, but are strong acids. It was found that A and B exhibit particularly excellent corrosion resistance.
- test member of Example 3 including the coating material 20 containing an epoxy resin and chromium oxide exhibits excellent corrosion resistance against all liquids, but is particularly excellent against liquids C to F which are strong alkalis. It was found to show corrosion resistance.
- the corrosion-resistant member 10 includes the DLC film 18 sealed and covered with the coating material 20 containing the epoxy resin, thereby sterilizing strong acid and strong alkali, sodium hypochlorite, and the like. -Excellent corrosion resistance against disinfectants.
- the corrosion resistance can be improved as compared with the case where only the epoxy resin is contained, and in particular, the acid resistance can be remarkably improved.
- the corrosion resistance can be improved as compared with the case where only the epoxy resin is contained, and in particular, the alkali resistance can be remarkably improved.
- the Vickers hardness of the DLC film 18 of Examples 1 to 6 is 1350 HV, which is significantly higher than the Vickers hardness 320 HV of the anodic oxide films of Comparative Examples 3 to 5.
- the corrosion-resistant member 10 provided with the DLC film 18 is excellent also in slidability and abrasion resistance.
- test members of Comparative Examples 4 and 5 including the anodized film sealed with the coating material 20 it is possible to improve the corrosion resistance as compared with the test member of Comparative Example 1 including no film. Although there is a lack of slidability and wear resistance.
- Example 5 except that the base material 16 has a disk shape with a diameter of 40 mm and a thickness of 7 mm, and the sliding surface 26 is formed by removing the coating layer 20a on the end surface.
- the corrosion-resistant member 10 was obtained and used as a test member.
- the frictional wear characteristic evaluation between the sliding surface 26 and a mating material made of a plurality of types of materials was performed by a ball-on-disk method using the test member as a disk and the mating material as a pin.
- the load, linear velocity, rotational speed, and sliding distance were set to 1 kgf, 1000 mm / second, 660 rpm, and 1 km, respectively.
- the counterpart material was a solid shaft having a diameter of 10 mm.
- the material of this counterpart is stainless steel (SUS303), polyacetal resin (POM), polytetrafluoroethylene (PTFE), high silicon alloy (NH41), die casting aluminum alloy (ADC12), lead bronze casting (LBC) Brass (C3604), cast aluminum bronze (CAC703), carbon steel for machine structure (S45C) were selected.
- SUS303 stainless steel
- POM polyacetal resin
- PTFE polytetrafluoroethylene
- NH41 high silicon alloy
- ADC12 die casting aluminum alloy
- LBC lead bronze casting
- CAC703 cast aluminum bronze
- carbon steel for machine structure S45C
- the material of the counterpart material 12 is any one of stainless steel, polyacetal resin (POM), and polytetrafluoroethylene (PTFE). Both wears can be effectively suppressed, and the durability of the corrosion-resistant member 10 and the counterpart material 12 can be improved.
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Abstract
Description
基材16として、A6061-T6からなり、直径が10mm、長さが50mmである中実軸体の表面に鏡面研磨を施したものを選定した。この基材16に対して、中間層22及びDLC皮膜18を合計厚さが2.0~2.2μmとなるように形成した。DLC皮膜18表面の平均ビッカース硬さは1350HVであった。なお、平均ビッカース硬さは、JIS Z 2244の試験方法に従って測定したものであり、荷重を10gfとした場合の3点平均値である。以下に示す平均ビッカース硬さについても同じである。
コーティング材20を形成するための樹脂材料として、エポキシ樹脂を5~20質量%、酸化チタンを1~10質量%、カーボンブラックを1~10質量%、キシレンを5~15質量%、メチルエチルケトンを15~25質量%、酢酸2-エトキシエチルを5~15質量%、トルエンを10~20質量%、エチレングリコールモノブチルエーテルを1~10質量%の割合で含有するものを選定したこと、及びコーティング層20aの厚さを21.0~25.0μmとしたことを除いて、実施例1と同様にして耐食部材10を得た。これを実施例2の試験部材とする。すなわち、実施例2の試験部材は、酸化チタン及びカーボンブラックを含有するコーティング材20を備える。なお、実施例2のコーティング層20a表面の平均ビッカース硬さは50HVであった。
樹脂材料として、エポキシ樹脂を5~20質量%、酸化第2クロムを1~10質量%、1,2ジ-クロロエタンを15~25質量%、メチルイソブチルケトンを5~15質量%、メチルエチルケトンを5~15質量%、ジアセトンアルコールを10~20質量%、エタノールを10~20質量%の割合で含有するものを選定したこと、及びコーティング層20aの厚さを25.0~30.0μmとしたことを除いて、実施例1と同様にして耐食部材10を得た。これを実施例3の試験部材とする。すなわち、実施例3の試験部材は、酸化クロムを含有するコーティング材20を備える。なお、実施例3のコーティング層20a表面の平均ビッカース硬さは20HVであった。
基材16の材料としてA2017を選定したことを除いて、実施例1と同様にして得た耐食部材10を実施例4の試験部材とする。基材16の材料としてA2017を選定したことを除いて、実施例2と同様にして得た耐食部材10を実施例5の試験部材とする。基材16の材料としてADC12を選定したことを除いて、実施例2の試験部材と同様にして得た耐食部材10を実施例6の試験部材とする。
比較のため、実施例1と同一の基材16のみからなる試験部材を比較例1とした。すなわち、比較例1の試験部材は、中間層22、DLC皮膜18、コーティング材20の何れも備えていない。
コーティング材20を設けていないことを除いて、実施例1と同様に作製した試験部材を比較例2とした。すなわち、比較例2の試験部材では、DLC皮膜18がコーティング材20によって封孔されていない。
実施例1と同一の基材16に対して陽極酸化処理を施して、厚さ13.0~16.0μmの陽極酸化皮膜(Al2O3)を形成した試験部材を比較例3とした。比較例3の試験部材の陽極酸化皮膜を、実施例1と同一のコーティング材20で封孔するとともに被覆して、厚さが22.0~26.0μmのコーティング層20aを形成し、これを比較例4の試験部材とした。実施例2と同一のコーティング材20を選定したことを除いて、比較例4と同様にして比較例5の試験部材を得た。なお、比較例3~5の試験部材における陽極酸化皮膜表面の平均ビッカース硬さは320HVであった。
コーティング材20を設けていないことを除いて、実施例4と同様に作製した試験部材を比較例6とした。すなわち、比較例6の試験部材は、DLC皮膜18がコーティング材20によって封孔されていない。
Claims (13)
- アルミニウム又はアルミニウム合金からなる基材(16)と、
前記基材(16)の表面に形成されるアモルファスカーボン(a-C)又は水素化アモルファスカーボン(a-C:H)からなるダイヤモンドライクカーボン皮膜(18)と、
少なくとも前記ダイヤモンドライクカーボン皮膜(18)の開気孔(24)に充填されエポキシ樹脂を含有するコーティング材(20)と、を備えることを特徴とする耐食部材(10)。 - 請求項1記載の耐食部材(10)において、
前記コーティング材(20)は、酸化チタンと、カーボンブラックとをさらに含有することを特徴とする耐食部材(10)。 - 請求項2記載の耐食部材(10)において、
前記コーティング材(20)は、質量比で、エポキシ樹脂:酸化チタン:カーボンブラック=5:1:1~20:10:10であることを特徴とする耐食部材(10)。 - 請求項1記載の耐食部材(10)において、
前記コーティング材(20)は、酸化クロムをさらに含有することを特徴とする耐食部材(10)。 - 請求項4記載の耐食部材(10)において、
前記コーティング材(20)は、質量比で、エポキシ樹脂:酸化クロム=5:1~20:10であることを特徴とする耐食部材(10)。 - 請求項1記載の耐食部材(10)において、
前記ダイヤモンドライクカーボン皮膜(18)は、アルミニウムと、前記ダイヤモンドライクカーボン皮膜(18)を構成するアモルファスカーボン(a-C)又は水素化アモルファスカーボン(a-C:H)とを含有する中間層(22)を介して前記基材(16)の表面に形成されることを特徴とする耐食部材(10)。 - 請求項1~6の何れか1項に記載の耐食部材(10)において、
前記コーティング材(20)は、前記ダイヤモンドライクカーボン皮膜(18)の少なくとも一部を覆うコーティング層(20a)を形成することを特徴とする耐食部材(10)。 - 請求項7記載の耐食部材(10)において、
前記開気孔(24)に前記コーティング材(20)が充填された状態で、前記ダイヤモンドライクカーボン皮膜(18)の表面を、前記コーティング層(20a)から露呈させた摺動面(26)を有することを特徴とする耐食部材(10)。 - 請求項8記載の耐食部材(10)において、
前記摺動面(26)は、相手材(12)と摺動し、
前記相手材(12)の材料は、ステンレス鋼、ポリアセタール樹脂、ポリテトラフルオロエチレンの何れかであることを特徴とする耐食部材(10)。 - 請求項9記載の耐食部材(10)において、
前記相手材(12)の材料となるステンレス鋼は、SUS304、SUS303、SUS316の何れかであることを特徴とする耐食部材(10)。 - 請求項9記載の耐食部材(10)において、
前記摺動面(26)と前記相手材(12)との間に、フッ素系グリス(28)が介在することを特徴とする耐食部材(10)。 - 請求項9に記載の耐食部材(10)において、
前記相手材(12)を軸受部材とする軸部材であることを特徴とする耐食部材(10)。 - 請求項1記載の耐食部材(10)において、
飲料又は食品を扱う装置を構成することを特徴とする耐食部材(10)。
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EP17884795.0A EP3556900B1 (en) | 2016-12-19 | 2017-09-01 | Corrosion-resistant member |
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