Contact materials

The contact material with a silver layer and particle-containing metal layer addresses cracking and wear issues in electric vehicle charging terminals, achieving cost-effective and durable performance.

JP7794885B2Active Publication Date: 2026-01-06KOBE STEEL LTD
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Patent Information

Application Number
JP2024073052
Authority / Receiving Office
JP · JP
Patent Type
Patents
Current Assignee / Owner
Filing Date
2024-04-26
Publication Date
2026-01-06
Estimated Expiration
2044-04-26

AI Technical Summary

Technical Problem

Electric vehicle charging terminals require thick silver plating to withstand frequent insertion and removal, leading to high material costs and productivity issues, while existing particle-eutectoid Ag plating films are prone to cracking and poor appearance due to particle-plating interface cracks.

Method used

A contact material design with a silver layer and a particle-containing metal layer, where the silver layer provides crack resistance and the particle-containing metal layer enhances wear resistance, using a specific thickness ratio and non-conductive particles to suppress crack growth.

Benefits of technology

The design effectively suppresses large cracks and ensures sufficient wear resistance while reducing manufacturing costs, maintaining conductivity and appearance quality.

✦ Generated by Eureka AI based on patent content.

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Patent Text Reader

Abstract

To provide a contact material having sufficient abrasion resistance while suppressing a production cost, and suppressing occurrence of a coarse crack.SOLUTION: A contact material comprises: a conductive substrate; a silver layer covering at least a part of the surface of the conductive substrate; and a particle-containing metal layer covering at least a part of the surface of the silver layer. The silver layer has the thickness of 1.0 μm or greater. The particle-containing metal layer includes a parent phase made of a metallic material and particles dispersed in the parent phase.SELECTED DRAWING: Figure 1
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Description

[Technical Field]

[0001] The present disclosure relates to contact materials. [Background technology]

[0002] As CO2 emissions regulations become stricter, the number of electric vehicles (EVs) and plug-in hybrid vehicles (PHEVs), which are less dependent on fossil fuels, is expected to increase. Because these vehicles require daily battery charging, the contact terminal materials connecting the vehicle to an external power source must be designed to withstand significantly more frequent insertion and removal than those used in conventional vehicles. Furthermore, shortening the charging process requires the passage of a large current. To minimize heat loss at the contacts, surface treatments with low surface contact resistance are required on both the vehicle body and power supply sides. In this field, highly conductive (low contact resistance) silver (Ag) plating is often used. However, Ag plating generally has low hardness and is prone to "seizing" when sliding between Ag electrodes. This poses a challenge: repeated insertion and removal (sliding) can easily lead to wear.

[0003] For this reason, current electric vehicle charging terminals require the formation of a significantly thicker Ag plating film (tens of microns thick) than the typical Ag plating film (several microns thick) applied to contact materials to prevent the base material from being exposed even when wear occurs due to repeated insertion and removal (sliding). This means an increase in the amount of Ag required for the terminal material, resulting in higher material costs. Furthermore, forming a thick Ag plating film using electroplating requires a long electroplating process, which also poses the issue of significantly reducing productivity.

[0004] To address these problems, it is known that a "particle eutectoid Ag plating film" in which particles of a non-conductive organic compound that has a wear-suppressing effect are contained in the Ag plating layer is effective (e.g., Patent Documents 1 and 2). [Prior art documents] [Patent documents]

[0005] [Patent Document 1] Japanese Patent Publication No. 2022-154356 [Patent Document 2] Japanese Patent Application Publication No. 2024-006857 [Patent Document 3] Japanese Patent Publication No. 2020-128575 Summary of the Invention [Problem to be solved by the invention]

[0006] When materials coated with particle-eutectoid Ag plating film are subjected to processing such as bending or punching, the plating film is prone to cracks. The main reason for this is that the particle-plating interface in the particle-eutectoid Ag plating film is likely to become the starting point for cracks. When cracks occur in the plating film provided on the contact material, they have little adverse effect on the functionality of the contact material, but they can cause a problem of poor visual appearance. In particular, when many large cracks occur, the appearance deteriorates significantly, which makes users dislike the product, so it is desirable to suppress the occurrence of large cracks.

[0007] JP 2020-128575 A (Patent Document 3) discloses a connector terminal material (contact material) that can improve abrasion resistance, heat resistance, and crack resistance. The terminal material includes a silver layer covering at least a portion of the surface of a substrate and a silver-platinum alloy layer covering at least a portion of the silver layer. The silver layer and the silver-platinum alloy layer are reacted to form an Ag3Pt intermetallic compound, improving abrasion resistance and heat resistance. The film thickness of the Ag3Pt intermetallic compound is reduced to 0.04 μm or more and 1.9 μm or less, improving crack resistance. However, since the platinum used in Patent Document 3 is expensive, there is a problem in that the cost of the contact material increases.

[0008] The present invention has been made in view of the above circumstances, and one of its objects is to provide a contact material that can suppress the occurrence of large cracks and has sufficient wear resistance while suppressing manufacturing costs. [Means for solving the problem]

[0009] Aspect 1 of the present invention is A conductive substrate; a silver layer covering at least a portion of the surface of the conductive substrate; a particle-containing metal layer covering at least a portion of the surface of the silver layer; the silver layer has a thickness of 1.0 μm or more, The particle-containing metal layer is a contact material that includes a matrix made of a metal material and particles dispersed in the matrix.

[0010] Aspect 2 of the present invention is In the contact material according to aspect 1, the silver layer has a silver content of 50% by mass or more and 100% by mass or less.

[0011] Aspect 3 of the present invention is In the contact material according to aspect 1 or 2, the thickness of the silver layer is 10 to 60% of the total thickness of the silver layer and the particle-containing metal layer.

[0012] A fourth aspect of the present invention is A contact material according to any one of Aspects 1 to 3, wherein the particles comprise non-conductive particles.

[0013] A fifth aspect of the present invention is The non-conductive particles have a unit molecular structure containing a fluoro group (-F), a methyl group (-CH3), a carbonyl group (-C(=O)-), an amino group (-NR 1 R 2 and R 1 and R 2 is hydrogen or a hydrocarbon group, and R 1 and R 2 may be the same or different), a hydroxy group (—OH), an ether bond (—O—), and an ester bond (—C(═O)—O—).

[0014] A sixth aspect of the present invention is In the contact material according to any one of Aspects 1 to 5, the matrix phase contains at least one material selected from the group consisting of silver and silver alloys.

[0015] A seventh aspect of the present invention is The contact material according to any one of Aspects 1 to 6, wherein the particle-containing metal layer satisfies the following formula (1): 2.0≦A p / (A p +A Ag )×100≦12.0 (1) In formula (1), A p is the area of ​​the part of the particle buried in the matrix in the cross section of the contact material in the thickness direction, and A Ag is the area of ​​the parent phase in a cross section of the contact material in the thickness direction. [Effects of the Invention]

[0016] According to the embodiments of the present invention, it is possible to provide a contact material that can suppress the occurrence of large cracks and has sufficient wear resistance while suppressing manufacturing costs. [Brief explanation of the drawings]

[0017] [Figure 1] FIG. 1 is a schematic cross-sectional view of an example of a contact material according to an embodiment of the present invention. [Figure 2] FIG. 2 is a schematic cross-sectional view of another example of a contact material according to an embodiment of the present invention. [Figure 3A] FIG. 3A is a cross-sectional SEM image of a particle eutectoid-plated sample of Sample No. 9 in Example 2, taken in a cross section in the thickness direction of the contact material. [Figure 3B] FIG. 3B is an image of only the particle-containing metal layer cropped from FIG. 3A. [Figure 3C] FIG. 3C is a binarized image of FIG. 3B. [Figure 4A]FIG. 4A is a graph showing the relationship between the particle eutectoid ratio and the coefficient of friction (□) and contact resistance (Δ), as determined from the particle eutectoid-plated sample of Sample No. 9 in Example 2. [Figure 4B] FIG. 4B is a graph showing the relationship between the particle eutectoid ratio and the coefficient of friction (□) and contact resistance (Δ), as determined from the particle eutectoid-plated sample of Sample No. 10 in Example 2. [Figure 5A] FIG. 5A is a cross-sectional SEM image of the contact material sample after the bending test. [Figure 5B] FIG. 5B is an enlarged view of the area enclosed by the dashed line in FIG. 5A. [Figure 6A] FIG. 6A is a cross-sectional SEM image of the contact material sample after the bending test. [Figure 6B] FIG. 6B is an enlarged view of the area enclosed by the dashed line in FIG. 6A. [Figure 7] FIG. 7 is a cross-sectional SEM image of the contact material sample after the bending test. [Figure 8] FIG. 8 is a cross-sectional SEM image of the contact material sample after the bending test. DETAILED DESCRIPTION OF THE INVENTION

[0018] 1 and 2 are schematic cross-sectional views in the thickness direction of contact materials 1 and 11 according to embodiments of the present invention. The contact materials 1 and 11 include a conductive substrate 4, a silver layer 3 covering at least a portion of the surface 4a of the conductive substrate 4, and a particle-containing metal layer 2 covering at least a portion of the surface 3a of the silver layer 3. The particle-containing metal layer 2 includes a matrix 2a made of a metal material and particles 2b dispersed in the matrix 2a, and the silver layer 3 is substantially free of particles 2b.

[0019] The particle-containing metal layer 2 has particles 2b dispersed in a matrix 2a made of a metal material, and therefore has higher wear resistance than a metal layer that does not contain particles 2b. In other words, the contact materials 1, 11 can have good wear resistance by including the particle-containing metal layer 2. Furthermore, because the particle-containing metal layer 2 includes a matrix 2a made of a metal material, the particle-containing metal layer 2 as a whole is conductive regardless of the type of particles 2b dispersed therein (for example, particles 2b made of conductive, non-conductive, inorganic, or organic materials).

[0020] The silver layer 3 is located between the conductive substrate 4 and the particle-containing metal layer 2. The silver layer 3 is a metal layer containing silver as a main component and has excellent ductility. The silver layer 3 is also substantially free of particles 2b. Therefore, the silver layer 3 has the characteristic that cracks are unlikely to occur inside the silver layer 3 and, even if cracks do occur, they are unlikely to grow (crack resistance). The silver layer 3 may contain a small amount of particles 2b as long as the crack resistance is not impaired. For example, if the content of particles 2b is 1% by volume or less with respect to the entire silver layer 3 (including particles 2b), the wear resistance can be slightly improved without substantially deteriorating the crack resistance.

[0021] When tensile stress is applied to the particle-containing metal layer 2 due to processing of the contact material 1, 11, etc., cracks may occur in the particle-containing metal layer 2, originating from particles 2b dispersed inside the particle-containing metal layer 2. These cracks grow further due to the tensile stress. Crack growth refers to the crack widening and extending in the depth direction. When observed from the surface side of the particle-containing metal layer 2, the grown cracks appear as wide cracks (referred to as "coarse cracks"). Furthermore, when observed in a cross section in the thickness direction of the contact material 1, 11, they appear as wide cracks on the surface side of the particle-containing metal layer 2 that extend long from there toward the conductive substrate 4 (depth direction).

[0022] If a crack that has occurred in the particle-containing metal layer 2 continues to grow, it will attempt to cross the silver layer 3 and reach the conductive substrate 4. However, because the silver layer 3 has crack resistance, the silver layer 3 can stop the crack from extending in the depth direction. When the extension of the crack in the depth direction stops (i.e., the growth of the crack stops), the crack width also stops expanding. In this way, by providing the silver layer 3 between the conductive substrate 4 and the particle-containing metal layer 2, the growth of the crack that has occurred in the particle-containing metal layer 2 can be stopped, and therefore the occurrence of large cracks in the particle-containing metal layer 2 can be suppressed.

[0023] In this way, in the contact materials 1 and 11 according to the embodiments, by laminating the silver layer 3 and the particle-containing metal layer 2 in this order on the surface of the conductive substrate 4, the particle-containing metal layer 2 present on the surface side of the contact materials 1 and 11 can improve the wear resistance, and the silver layer 3 located between the particle-containing metal layer 2 and the conductive substrate 4 can prevent the occurrence of large cracks in the particle-containing metal layer 2. Unlike the contact materials 1 and 11 in the cited document 3, the contact materials 1 and 11 according to the embodiments do not require the use of platinum, and therefore can reduce production costs.

[0024] Although Cited Document 3 also discloses that a silver layer is provided between the substrate and the silver-platinum alloy layer, this silver layer is provided as a silver source for forming an Ag3Pt intermetallic compound, and is not provided with the intention of suppressing cracks.

[0025] The silver layer 3 of the contact materials 1 and 11 according to the embodiments is formed from a metal material containing silver as a main component, such as pure silver or a silver alloy. That is, the silver content in the silver layer 3 is 50% by mass or more and 100% by mass or less, preferably 90% by mass or more and 100% by mass or less, and more preferably 99% by mass or more and 100% by mass or less. By increasing the silver content in the silver layer 3, a silver layer 3 with better ductility (i.e., better crack resistance) can be formed, and thereby the occurrence of coarse cracks in the particle-containing metal layer 2 can be more effectively suppressed.

[0026] The ratio of the thickness 3t of the silver layer 3 to the thickness 2t of the particle-containing metal layer 2 can affect the wear resistance and the effect of suppressing the occurrence of coarse cracks of the contact materials 1, 11. Therefore, it is preferable to control the thickness ratio to an appropriate value. In particular, the ratio of the thickness 3t of the silver layer 3 to the total thickness (3t+2t) of the silver layer 3 and the particle-containing metal layer 2 (referred to as the "thickness ratio of the silver layer 3") is preferably 10 to 60%. When the thickness ratio of the silver layer 3 is 10% or more, the occurrence of large cracks in the particle-containing metal layer 2 can be more effectively suppressed. When the thickness ratio of the silver layer 3 is 60% or less, the thickness 2t of the particle-containing metal layer 2 can be sufficiently ensured, thereby further improving the wear resistance of the contact materials 1, 11. The thickness ratio of the silver layer 3 is more preferably 15% or more, even more preferably 20% or more, and is preferably 50% or less, more preferably 45% or less, even more preferably 40% or less, and particularly preferably 30% or less.

[0027] The specific thickness 3t of the silver layer 3 is preferably determined in consideration of the balance with the particle-containing metal layer 2 formed on the contact materials 1, 11, but is at least 1.0 μm or more, and may be, for example, more than 1.0 μm and not more than 10 μm, preferably not less than 1.2 μm, more preferably not less than 1.5 μm, and preferably not more than 5.0 μm, more preferably not more than 3.0 μm. If the thickness is within this range, the production costs of the contact materials 1, 11 can be reduced while providing sufficient crack resistance to the contact materials 1, 11. The thickness 2t of the particle-containing metal layer 2 is not particularly limited and can be adjusted appropriately depending on the application, but may be, for example, 100 μm or less, or even 50 μm or less.

[0028] The thickness 3t of the silver layer 3 and the thickness 2t of the particle-containing metal layer 2 can be quantified from a cross-sectional SEM image of a cross section obtained by cutting a sample of the contact material 1, 11 in the thickness direction of the contact material 1, 11 (which essentially coincides with the direction perpendicular to the surface of the conductive substrate 4). The cross-sectional SEM image is taken at a magnification of 1000x, with the vertical direction of the observation field coinciding with the thickness direction of the contact material 1, 11. The field of view is, for example, 140 μm vertical × 200 μm horizontal.

[0029] To measure the thickness 3t of the silver layer 3, first, in a cross-sectional SEM image, the boundary between the silver layer 3 and the conductive substrate 4 (referred to as the "first boundary", which basically coincides with the surface 4a of the conductive substrate 4) and the boundary between the silver layer 3 and the particle-containing metal layer 2 (referred to as the "second boundary", which basically coincides with the surface 3a of the silver layer 3) are identified. The distance between the first boundary and the second boundary in the direction perpendicular to the surface 4a of the conductive substrate 4 is measured, and this is defined as the "thickness 3t of the silver layer 3."

[0030] The thickness 2t of the particle-containing metal layer 2 varies depending on the state of the particles 2b dispersed in the particle-containing metal layer 2. As will be described in detail later, the particle-containing metal layer 2 can have a form in which some of the particles 2b protrude outward from the surface 2c of the matrix 2a, as shown in Figure 1, or a form in which all of the particles 2b are completely buried in the matrix 2a, as shown in Figure 2.

[0031] In the case of a particle-containing metal layer 2 having the form shown in FIG. 1, the distance between the second boundary (surface 3a of the silver layer 3) and the top of the protruding particle 2b is defined as the "thickness 2t of the particle-containing metal layer 2." In a cross-sectional SEM image, the second boundary and the particle 2b that protrudes most from the surface 2c of the parent phase 2a are identified. The distance between the second boundary and the top of the most protruding particle 2b in the direction perpendicular to the surface 4a of the conductive substrate 4 is measured, and this is defined as the "thickness 2t of the particle-containing metal layer 2." In addition, in a portion where no protruding particles 2b exist, that is, a portion where the surface 2c of the mother phase 2a is exposed, the "thickness 2at of the mother phase 2a" can be measured. The distance between the second boundary and the surface 2c of the mother phase 2a in the direction perpendicular to the surface 4a of the conductive substrate 4 is the "thickness 2at of the mother phase 2a."

[0032] In the case of the particle-containing metal layer 2 having the form shown in FIG. 2, the distance between the second boundary (surface 3a of the silver layer 3) and the surface 2c of the parent phase 2a is defined as the "thickness 2t of the particle-containing metal layer 2." The second boundary and the surface 2c of the parent phase 2a are identified in a cross-sectional SEM image. The distance between the second boundary and the surface 2c of the parent phase 2a in the direction perpendicular to the surface 4a of the conductive substrate 4 is measured and defined as the "thickness 2t of the particle-containing metal layer 2." In the particle-containing metal layer 2 shown in FIG. 2, the thickness 2at of the matrix 2a is equal to the thickness 2t of the particle-containing metal layer 2.

[0033] The thickness of each layer may be measured once at any position within the field of view of the SEM image, or may be measured at any 2 to 5 positions and the arithmetic mean of the measurement results may be used. However, in the case of a particle-containing metal layer 2 having the form shown in Figure 1, the "thickness 2t of the particle-containing metal layer 2" is measured at the position where the particles 2b protrude most, as explained above.

[0034] The silver layer 3 and the particle-containing metal layer 2 can be distinguished from each other by the method described below.

[0035] The conductive substrate 4 can be formed from a plate, foil, wire, or rod made of metal such as copper, copper alloy, etc. The thickness 4t of the conductive substrate 4 is, for example, 1 μm to 100 mm.

[0036] As described above, the particle-containing metal layer 2 includes a matrix 2a made of a metal material and particles 2b dispersed in the matrix 2a. The dispersion states of the particles 2b in the matrix 2a can be roughly divided into two types (FIGS. 1 and 2).

[0037] In the contact material 1 of Fig. 1, most of the particles 2b are completely embedded in the matrix 2a. However, some of the particles 2b located near the surface 2c of the matrix 2a protrude outward from the surface 2c of the matrix 2a. In other words, some particles 2b are partially embedded in the matrix 2a near the surface 2c of the matrix 2a, with the remaining portions exposed from the surface 2c of the matrix 2a. If the wear resistance of the contact material 1 is improved by decomposition of the particles 2b, it is preferable that the particles 2b are partially exposed from the surface 2c of the matrix 2a, as shown in Fig. 1. This allows the particles 2b to be decomposed by insertion and removal (sliding) of the contact material 1 from the early stages of use, improving the wear resistance.

[0038] In the contact material 11 of Fig. 2, all of the particles 2b are completely buried in the matrix phase 2a. In other words, even when observing the particle-containing metal layer 2 from the surface side, the particles 2b cannot be directly observed. When the particles 2b are made of a non-conductive material, the electrical conductivity of the particle-containing metal layer 2 can be improved (contact resistance can be further reduced) by preventing the particles 2b from being exposed from the surface 2c of the matrix 2a, as shown in Figure 2. Furthermore, the matrix 2a is worn away by the insertion and removal (sliding) of the contact material 1, exposing the buried particles 2b, thereby improving wear resistance.

[0039] The metal material forming the matrix 2a preferably includes one or more selected from the group consisting of silver and silver alloys. In particular, the matrix 2a preferably includes 50% to 100% by mass of silver. The matrix 2a may include various silver platings (e.g., soft Ag plating, hard Ag plating, bright Ag plating, and semi-bright Ag plating) commonly used for terminal surface treatment. Alternatively, a silver alloy plating may be used to improve the corrosion resistance (e.g., sulfur resistance) and wear resistance of the matrix 2a. Examples of silver alloys suitable for the silver alloy plating include Ag-Sn, Ag-Sb, and Ag-Cu.

[0040] Furthermore, using pure silver plating for the matrix 2a makes it possible to obtain a particle-containing metal layer 2 with excellent conductivity. The matrix 2a may contain, for example, silver in the range of 90% by mass to 100% by mass, 95% by mass to 100% by mass, or 99% by mass to 100% by mass.

[0041] The silver material forming the silver layer 3 and the metal material forming the matrix 2a may be the same or different. When the silver layer 3 and the matrix 2a are formed from different metal materials, the types or contents of alloying elements contained in the silver layer 3 and the matrix 2a differ, and therefore the silver layer 3 and the matrix 2a can be distinguished by element mapping using cross-sectional SEM-EDX analysis. In other words, the cross-sectional SEM-EDX analysis makes it possible to distinguish between the area of ​​the silver layer 3 and the area of ​​the particle-containing metal layer 2 that includes the matrix 2a.

[0042] When the silver layer 3 and the matrix 2a are formed from the same metal material, it is not possible to distinguish between the silver layer 3 and the matrix 2a by cross-sectional SEM-EDX analysis. Therefore, another method is required to distinguish between the area of ​​the silver layer 3 and the area of ​​the matrix 2a (particle-containing metal layer 2). In this case, the area containing particles 2b is referred to as the "particle-containing metal layer 2," and the area not containing particles 2b is referred to as the "silver layer 3." As described above, the silver layer 3 may contain trace amounts of particles 2b. However, when the silver layer 3 and the matrix 2a are formed from the same metal material, the silver layer 3 is considered to contain no particles 2b in order to make it easier to identify the first boundary.

[0043] The boundary (second boundary) between the silver layer 3 and the particle-containing metal layer 2 is identified in an SEM image of a cross section of the contact material 1, 11 in the thickness direction. The cross-sectional SEM image is subjected to image processing using a method described below to identify all particles 2b contained in the particle-containing metal layer 2. Of these particles 2b, the boundary (second boundary) between the silver layer 3 and the conductive substrate 4 is determined based on the particle 2b closest to the conductive substrate 4. That is, on the cross-sectional SEM image, the second boundary is drawn so that the particle 2b closest to the conductive substrate 4 is located closer to the particle-containing metal layer 2 than the second boundary, and the particle 2b contacts the second boundary. The second boundary on the cross-sectional SEM image is linear and drawn approximately parallel to the surface of the conductive substrate 4.

[0044] Various types of particles can be used as the particles 2b, but non-conductive particles are particularly preferred. When the particle-containing metal layer 2 is applied to a contact material and sliding (insertion and removal) is repeated, the particles 2b held in the matrix 2a may fall off due to wear of the particle-containing metal layer 2. If the particles 2b are non-conductive particles, this is advantageous because there is a low possibility of a short circuit occurring even if the particles 2b fall off and accumulate near the contact. Here, "non-conductive" means that it does not exhibit conductivity, and for example, the volume resistivity measured according to ASTM D257 is approximately 10 3 This refers to a value of [Ω·cm] or more.

[0045] Non-conductive particles have a fluoro group (-F), a methyl group (-CH3), a carbonyl group (-C(=O)-), an amino group (-NR 1 R 2 and R 1 and R 2 is hydrogen or a hydrocarbon group, and R 1 and R 2 may be the same or different), a hydroxy group (—OH), an ether bond (—O—), and an ester bond (—C(═O)—O—).

[0046] Here, "organic compounds" refers to compounds containing carbon, excluding compounds with simple structures such as carbon monoxide, carbon dioxide, carbonates, hydrocyanic acid, cyanates, thiocyanates, BC, and SiC. For example, a silicone resin having a siloxane bond (-Si-O-Si-) in the main chain and organic groups in the side chains is considered to be included in the "organic compounds" in this specification.

[0047] The non-conductive organic compound forming the particles 2b contains the above-mentioned functional group, thereby improving the wear resistance of the particle-containing metal layer 2. Here, the term "unit molecular structure" refers to one repeating unit in the case of a polymer, or to an individual molecule in the case of a non-polymer.

[0048] The reason why the use of particles made of a non-conductive organic compound can improve the wear resistance of the particle-containing metal layer 2 is not clear, but the following mechanism is assumed. This is thought to be because, during sliding of the particle-containing metal layer 2, for example, part of the non-conductive organic compound decomposes and diffuses and migrates near the surface of the contact material, and / or part of the non-conductive organic compound reacts with the silver-containing layer near the surface of the contact material, thereby lowering the coefficient of friction near the surface of the contact material, thereby improving the wear resistance of the contact material. It is thought that the non-conductive organic compound having a specific functional group in its unit molecular structure is particularly effective in promoting the decomposition of the compound due to the influence of sliding. Furthermore, since the amount of decomposition products and reaction products is small, and the proportion of particles consisting of the specific non-conductive organic compound in the silver-containing film is controlled to a predetermined value or less, sufficient conductivity is thought to be ensured.

[0049] The particle size of the particles 2b is preferably such that they can be dispersed in the matrix 2a of the particle-containing metal layer 2 and do not impair the conductivity of the particle-containing metal layer 2. For example, the particle size (circle-equivalent diameter) of the particles 2b is set to be less than the thickness 2 at of the matrix 2a. This prevents the particles 2b from protruding too much from the surface 2c of the matrix 2a and impairing the electrical connection between the particle-containing metal layer 2 and the external terminals. Furthermore, it is more preferable that the circle-equivalent diameter of the particles 2b is sufficiently smaller than the thickness 2 at of the matrix 2a (for example, ½ or less of the thickness 2 at of the matrix 2a), allowing the particles 2b to be completely embedded in the matrix 2a (however, this does not mean that all the particles 2b are completely embedded, but rather that some particles 2b may be completely embedded in the matrix 2a). The average particle size (average circle equivalent diameter) of the particles 2b may be, for example, 50 μm or less, 10 μm or less, or 0.1 μm or more. The thickness 2at of the parent phase 2a was measured as described above.

[0050] The area of ​​the particles 2b (mainly non-conductive particles) and the matrix 2a in the particle-containing metal layer 2 that can be confirmed in a cross-sectional SEM image preferably satisfies the following formula (1). 2.0≦A p / (A p +A Ag )×100≦12.0 (1) In formula (1), A p is the area of ​​the part of the particle buried in the matrix 2 in the cross section of the contact material 1, 11 in the thickness direction, and A Ag is the area of ​​the parent phase 2 in the cross section of the contact material 1, 11 in the thickness direction.

[0051] Formula (1) means that the area ratio of the particles encapsulated in the particle-containing metal layer 2 is 2.0% to 12.0% with respect to the entire particle-containing metal layer 2. Note that, since the particle-containing metal layer 2 encapsulating particles 2b can be formed by a eutectoid plating method (a method in which particles are placed in a plating solution and electroplated while stirring), the area ratio of the encapsulated particles is sometimes referred to as the "eutectoid ratio of particles."

[0052] The particles contained in the particle-containing metal layer 2 contribute to the wear resistance of the particle-containing metal layer 2, but also reduce the conductivity of the particle-containing metal layer 2. When the particle area ratio (volume ratio) is 2.0% or more, the wear resistance of the particle-containing metal layer 2 can be significantly improved, while when it is 12.0% or less, the decrease in conductivity of the particle-containing metal layer 2 can be kept low. In other words, when the particle area ratio (volume ratio) is 2.0% to 12.0%, the particle-containing metal layer 2 can achieve both high levels of wear resistance and conductivity. The particle area ratio (particle co-deposition ratio) is more preferably 6.0% or more and more preferably 10.0% or less.

[0053] Area A of the parent phase 2a Ag can be obtained by binarizing a cross-sectional SEM image of the contact materials 1, 11 in the cross section in the thickness direction using image processing software (such as "ImageJ"). Specifically, in the cross-sectional SEM image, the parent phase 2a may appear relatively bright (i.e., white) and the protective layer of the cross-sectional SEM sample may appear relatively dark (i.e., black). Therefore, for example, after binarization using an intermediate brightness between the parent phase 2a and the protective layer as a threshold, the area of ​​the bright part is taken as the area A of the parent phase 2a. Ag If the cross-sectional SEM image shows irregularities on the upper surface of the silver-containing layer 2a, the area of ​​the parent phase 2a may be calculated by taking the average line of the irregularities as the boundary line between the parent phase 2a and an upper layer (for example, a protective layer of a cross-sectional SEM sample).

[0054] On the other hand, the area A of the part of the particle 2b buried in the matrix 2a p is a dark portion after binarization (in the case of non-conductive particles, the portion corresponds to the non-conductive organic compound), and can be taken as the area of ​​the portion buried in the mother phase 2a. If there are irregularities on the surface 2c of the mother phase 2a in the cross-sectional SEM image, the average line of the irregularities is taken as the boundary line between the mother phase 2a and an upper layer (for example, a protective layer of a cross-sectional SEM sample), and the portion below this average line is taken as the portion buried in the mother phase 2a.

[0055] Within the scope of the present invention, the contact materials 1 and 11 may contain particles other than the non-conductive particles 2b. For example, the contact materials 1 and 11 may contain particles made of a non-conductive organic compound that does not contain the specific functional groups described above, inorganic particles, or particles that are not embedded in the matrix phase 2a. The contact materials 1 and 11 may also contain conductive particles, but the fewer conductive particles they contain, the more preferable it is to prevent short circuits at the contact due to the conductive particles falling off. For example, the particles contained in the contact materials 1 and 11 preferably account for 50% or more by volume of the non-conductive particles 2b, more preferably 60% or more by volume, 70% or more by volume, 80% or more by volume, or 90% or more by volume, and even more preferably all (100% by volume) of the particles are non-conductive particles 2b. Furthermore, the ratio of particles 2b at least partially embedded in the matrix phase 2a to all particles contained in the contact materials 1 and 11 is preferably 50 area% or more in a cross section of the contact materials 1 and 11 in the thickness direction, more preferably 60 area% or more, 70 area% or more, 80 area% or more, 90 area% or more, and even more preferably 100 area%.

[0056] The contact materials 1 and 11 according to the embodiments of the present invention may contain other layers (e.g., a conductive substrate, a strike plating layer, etc.) to achieve the object of the present invention. For example, in the contact materials 1 and 11, a silver-containing film 2 may be formed on a conductive substrate (e.g., a substrate made of copper or a copper alloy).

[0057] The contact materials 1 and 11 according to the embodiments of the present invention are obtained by, for example, plating a silver layer 3 on a substrate, dispersing a predetermined amount of particles 2b in a silver (or silver alloy) plating solution, and applying an electric current while stirring to perform silver plating, thereby obtaining a contact material in which a predetermined amount of particles 2b are embedded (co-deposited) in a matrix 2a.

[0058] In the process of electroplating with particles 2b dispersed in a plating solution, the following reactions (A) and (B) proceed simultaneously. (A) A reaction in which particles dispersed in liquid are electrostatically or physically adsorbed (contacted) to the surface of a substrate. (B) Reaction in which the parent phase 2a is deposited (grows) on the substrate surface "Eutectoid" occurs when particles 2b adsorbed in (A) are incorporated into the matrix 2a in (B). Under conditions where eutectoid plating proceeds steadily, particles 2b adsorbed in the early stages of the reaction are incorporated into the matrix 2a, and at the same time, new particles 2b are adsorbed. For this reason, even when the plating process is stopped, particles 2b are often exposed on the outermost surface. In a typical eutectoid plating process, it is possible to easily produce contact materials 1 (see Figure 1) that contain particles 2b that are partly embedded in the matrix 2a and the remaining part exposed on the surface of the matrix 2a.

[0059] Here, the amount of particles 2b co-deposited into the matrix 2a (e.g., the area ratio of particles 2b) is determined by the balance between the frequency of adsorption of (A) and the growth rate of the plating film of (B). Therefore, it is possible to change the amount of co-deposition by changing plating conditions, such as the amount of particles 2b dispersed in the plating solution. For example, by using a plating solution that does not contain particles 2b dispersed in the plating solution at the final stage of the plating process, or by changing the stirring speed of the plating solution to reduce the frequency of adsorption of (A), a layer that prevents particles 2b from co-depositing can be formed on the outermost surface of the plating, making it possible to produce a contact material 11 (see Figure 1) in which all particles 2b are embedded in the matrix 2a. [Example]

[0060] The following examples are provided to more specifically describe the embodiments of the present invention. The embodiments of the present invention are not limited to the following examples, and may be modified as appropriate within the scope of the above-described and below-described aims, and all such modifications are within the technical scope of the embodiments of the present invention. [Example]

[0061] <Method for producing particle-coated plating> In order to easily identify the molecular structure conditions of particles that provide excellent wear resistance, the wear resistance and conductivity of Ag plating coated with particles were evaluated. A 0.3 mm thick pure copper plate was used as the plating substrate, and after degreasing the surface with acetone, a commercially available strike Ag plating solution (Dainsilver GPE-ST, manufactured by Daiwa Kasei Co., Ltd.) was used as the base for plating. A Pt-coated Ti plate was used as the counter electrode and the current was set at 5 A / dm 2 The substrate was then subjected to strike Ag plating treatment to a thickness of approximately 0.1 μm at a current density of 3 A / dm for 1 minute. The resulting plate was then plated with a pure Ag plate as the counter electrode using a commercially available non-cyanide semi-bright Ag plating solution (Daiwa Kasei Co., Ltd., Dyne Silver GPE-SB). 2 A current was passed through the plate for 5 minutes at a current density of 10 μm to form a semi-bright Ag plating layer having a thickness of approximately 10 μm. After plating, a liquid in which the particles shown in Tables 1 and 2 were suspended in alcohol was dropped onto the surface of the sample, and then dried to prepare a sample for evaluating wear resistance. Note that sample No. 1 was not coated with the alcohol suspension of particles.

[0062] <Wear resistance evaluation method> A 50μm layer of hard Ag plating (Vickers hardness HV: approximately 165) was formed on a 0.25mm thick pure copper plate, and an embossed shape with a radius of 1.8mm was formed using a hand press. This sample was used as the mating material, and a friction sliding test was carried out for up to 500 cycles between the sample for wear resistance evaluation (using an Aiko Engineering horizontal load testing machine). The applied vertical load was 3N, the sliding distance was 10mm, and the sliding speed was 80mm / min. The maximum value of the friction coefficient (ratio of horizontal load to vertical load) in each sliding cycle was measured, and the friction coefficient μ was read after 100, 300, and 500 cycles, respectively. Tests with μ≦0.50 at 100 cycles were rated "excellent" as having particularly excellent friction improvement effects, those with μ≦0.50 at 300 cycles were rated "good," and those with μ>0.50 at 500 cycles were rated "fail." Tests with "excellent" and "good" ratings were considered to be acceptable.

[0063] <Contact resistance test method> The contact resistance at the contact points was measured using a Yamazaki Seiki Laboratory fretting wear tester, focusing on the wear marks after the friction test. The applied load was 5N, and the average value measured at three locations was used to determine the contact resistance. Samples with a contact resistance of 0.500mΩ or less after the friction test were judged to have "excellent contact resistance" and passed the test. Note that contact resistance measurements were not performed on samples for which wear resistance was unsatisfactory.

[0064] The above results are summarized in Table 2.

[0065] [Table 1]

[0066] [Table 2]

[0067] It was confirmed that Samples Nos. 2 to 8, which satisfy the requirements of the embodiment of the present invention, were able to maintain a low friction coefficient after 300 and 500 cycles of friction testing, and also had good contact resistance after the friction testing. In sample No. 1, the evaluation material was a simple Ag plating layer and did not have a particle-containing metal layer 2, so seizure easily occurred between the material and the mating material, and the wear resistance was poor. [Example]

[0068] <How to prepare particle eutectoid plating samples> In order to confirm the effect of the particle-containing metal layer 2, samples (particle eutectoid-plated samples) with a particle eutectoid-plated layer in which particles were actually co-deposited into the Ag plating layer were prepared, and the wear resistance and conductivity were evaluated by varying the particle co-deposition rate of the particle eutectoid plating. In the process of forming a 10 μm thick Ag plating layer on a strike-plated copper substrate as described in Example 1, a predetermined amount of particles was dispersed in a plating solution, and electroplating was performed while stirring to obtain a plating layer in which each particle was incorporated (co-deposited) into the Ag plating layer. In some cases, the use of a surfactant (dispersant) was required to prevent the particles from agglomerating in the Ag plating layer and maintain a stable dispersion state. The obtained particle eutectoid plated samples were subjected to a friction test and contact resistance measurement evaluation in the same manner as in Example 1.

[0069] <Method for calculating particle deposition rate by observing the plating cross section> The particle co-deposition rate of the obtained particle co-deposition plated sample was calculated by the following formula. Using a scanning electron microscope (SEM, Hitachi S-3500N) at an accelerating voltage of 20 kV and a working distance of 15 mm, cross-sectional SEM images (secondary electron images) were taken of the particle-eutectoid plated samples No. 10 and No. 11 coated with a protective layer for cross-sectional SEM at the cross section in the thickness direction of contact materials 1 and 11. The area A of the parent phase 2 Ag The cross-sectional SEM image was binarized using the image processing software "ImageJ" as described above, and the area of ​​the bright part was taken as the area of ​​the bright part. In the cross-sectional SEM image, the average line of the irregularities on the upper surface of the mother phase 2 was taken as the boundary line between the mother phase 2 and the protective layer of the cross-sectional SEM sample. The area A of the part of the multiple particles buried in the silver-containing layer was taken as the area of ​​the bright part. p was defined as the area of ​​the dark portion (portion corresponding to the non-conductive organic compound) after the binarization process as described above, which was buried in the mother phase 2. In the cross-sectional SEM image, the average line of the irregularities on the upper surface of the mother phase 2 was defined as the boundary line between the particle-containing metal layer 2 and the protective layer of the cross-sectional SEM sample, and the portion below this average line was defined as the portion buried in the mother phase 2.

[0070] Figures 3A to 3C show examples of calculations of particle area ratios (particle co-deposition ratios). Figure 3A is a cross-sectional SEM image in the thickness direction of a particle co-deposition plating sample for sample No. 9, prepared with a particle dispersion of 3 g / L in the liquid. Figure 3B is an image of Figure 3A in which only the matrix 2 (and particles embedded in matrix 2) has been cropped. Figure 3C is a binarized image of Figure 3B. When the area of ​​the black portion in Figure 3C was divided by the area in Figure 3B, the area ratio (particle co-deposition ratio) was 2.51%.

[0071] These analysis results were compiled, and the range of particle co-deposition ratio that can achieve both wear resistance and conductivity was determined from the perspective of friction coefficient and contact resistance (Figs. 4A and 4B). Note that a particle co-deposition ratio that satisfies the criteria of "friction coefficient of 0.50 or less and contact resistance of 0.500 mΩ or less" was deemed to be acceptable. The measurement results are shown in Table 3.

[0072] [Table 3]

[0073] Sample No. 9 is a sample with cross-linked polymethyl methacrylate particle eutectoid plating. Figure 4A shows the relationship between the particle eutectoid ratio and the friction coefficient and contact resistance for Sample No. 9. With particle eutectoid plating with a particle eutectoid ratio of 2.0% to 12.0%, the friction coefficient after 20 sliding cycles was stable at around 0.4, and contact resistance remained below 0.500 mΩ, confirming that good wear resistance and conductivity were achieved.

[0074] Sample No. 10 is a sample with polyethylene oxide particle eutectoid plating. Figure 4B shows the relationship between the particle eutectoid ratio and the friction coefficient and contact resistance for Sample No. 10. With particle eutectoid plating with a particle eutectoid ratio of 0.5%, the friction coefficient after 20 sliding cycles dropped to about 0.2, and at particle eutectoid ratios of 2.0% or higher, the friction coefficient stabilized at about 0.1. Contact resistance remained almost unchanged at about 0.3 mΩ for particle eutectoid ratios between 0% and 8.0%. It was confirmed that at particle eutectoid ratios of 0.5% or higher, good wear resistance and conductivity were achieved.

[0075] It can be said that the range of particle co-deposition ratio that can achieve both a low friction coefficient and low contact resistance varies depending on the type of particle. [Example]

[0076] <Method for creating two-layer plating structure for bending tests> After degreasing the surface of a 0.3 mm thick pure copper plate with alkaline cleaning, a nickel sulfamate plating solution was used as a base treatment to prevent copper diffusion from the pure copper plate, and the plating was conducted at 5A / dm 2 A current was passed through the wire for 90 seconds at a current density of 1 μm to form a Ni plating layer having a thickness of approximately 1 μm. Next, as a base treatment to prevent Ag substitution reaction, a commercially available strike Ag plating solution (Dainsilver GPE-ST manufactured by Daiwa Kasei Co., Ltd.) was used, and an iridium oxide-coated Ti plate was used as the counter electrode at 3 A / dm 2 The wire was subjected to strike Ag plating treatment to a thickness of about 0.1 μm or less for 10 seconds at a current density of 1000 kJ / cm2, and used as a substrate.

[0077] A commercially available non-cyanide semi-bright Ag plating solution (Dyne Silver GPE-SB manufactured by Daiwa Kasei Co., Ltd.) was used to form the silver layer 3 on the substrate, and a pure Ag plate was used as the counter electrode at 3 A / dm 2 The current was passed for 270 seconds at a current density of 1000 kJ / min, forming an Ag plating layer having a thickness of approximately 5 μm.

[0078] Next, a commercially available non-cyanide semi-bright Ag plating solution (Dainsilver GPE-SB manufactured by Daiwa Kasei Co., Ltd.) was used to form the particle-containing metal layer 2. A surfactant (Surflon S231 manufactured by AGC Seimi Chemical Co., Ltd.) was added to the solution, and then the particles shown in Table 4 were added. While stirring, the solution was plated at 3 A / dm 2 The current was passed through the plate for 270 seconds at a current density of 1000 .mu.m to form a particle-deposited Ag plating layer having a thickness of approximately 5 μm. The ratio of the thickness of the silver layer 3 to the total thickness of the silver layer 3 and the particle-containing metal layer 2 was 50%.

[0079] Through these procedures, contact material samples (samples Nos. 11 and 12) were obtained that had a silver layer 3 (pure Ag) and a particle-containing metal layer 2 in which particles were co-deposited (embedded). For comparison, a contact material sample (sample No. 13) in which only the particle-containing metal layer 2 was formed (i.e., the silver layer 3 was not formed) and a contact material sample (sample No. 14) in which only the silver layer 3 was formed (i.e., the particle-containing metal layer 2 was not formed) were also prepared.

[0080] [Table 4]

[0081] <Evaluation method for bending workability> The obtained contact material samples (samples No. 11 to 14) were cut into pieces with a width of 10 mm and subjected to a bending test. The bending test was carried out using a W-bending test jig in accordance with JIS H 3110. In this case, R=0.5 mm was used. To check for cracking in the cross section of the bent portion of the sample, the cross section at the apex of the 90° bend in the bending test was observed. A scanning electron microscope (SEM: BRUKER-Hitachi, QUANTAX) was used to obtain a cross-sectional SEM image (secondary electron image) at a magnification of 1000x, an accelerating voltage of 20 kV, and a work distance of 15 mm. The field of view was 140 μm vertically and 200 μm horizontally, and the silver layer 3 and particle-containing metal layer 2 at the apex of the 90° bend were observed.

[0082] In the obtained cross-sectional SEM images, cracks were determined to be those that satisfied the following conditions A to D. In the cross-sectional SEM images, the silver layer 3 and the matrix 2a of the particle-containing metal layer 2 are observed as white or light gray areas, while the particles 2b of the particle-containing metal layer 2, the cracks, and the embedding resin (used when preparing the cross-sectional observation sample) are observed as dark gray areas.

[0083] A. A dark gray portion located inside the surface line of the particle-containing metal layer 2 (on the conductive substrate 4 side), and exposed from the surface of the particle-containing metal layer 2. B. The area is 2π (μm 2)That's all. C. The entire crack is visible within the field of view. D. The dimension (crack length) in the direction perpendicular to the surface 4a of the conductive substrate 4 is 2 μm or more. If the surface 4a of the conductive substrate 4 is curved, the perpendicular direction is determined by taking the tangent to the point on the surface 4a to which the perpendicular direction is to be defined as "surface 4a."

[0084] Condition A is a condition for eliminating the embedding resin covering the particle-containing metal layer 2 and internal defects (defects not exposed on the surface) of the particle-containing metal layer 2. This is because cracks observed from the surface in a plan view of the particle-containing metal layer 2 deteriorate the appearance. Condition B is a condition for excluding particle 2b. Since particle 2b has a D50 of 2 μm, the area in the cross-sectional SEM image is π (μm 2 ) is observed as a dark gray particulate area. Taking into account the variation in particle size of particle 2b, the area is assumed to be twice the estimated area, 2π (μm 2 ) are considered as "particle 2b" and are not cracks. Condition D is for eliminating minute irregularities on the surface of the particle-containing metal layer 2 .

[0085] Once the crack was identified, the crack width was measured at various positions on the crack, and the largest value (maximum crack width) was identified. Here, "crack width" refers to the dimension of the crack measured in a direction parallel to the surface 4a of the conductive substrate 4 on a cross-sectional SEM image. If the surface 4a of the conductive substrate 4 was not flat and the direction for measuring the crack width could not be determined unambiguously on the cross-sectional SEM image, the measurement direction was determined based on the contact point between the inner surface of the crack and the surface 4a of the conductive substrate 4. Because the inner surface of the crack is composed of two opposing surfaces, there are two contact points between the inner surface of the crack and the surface 4a of the conductive substrate 4. The direction parallel to the line connecting these contact points was determined as the crack width measurement direction.

[0086] The specimens with a maximum crack width of 10 μm or more were judged as "poor," those with a maximum crack width of less than 10 μm were judged as "good," and those with no cracks were judged as "excellent." If the judgment was "good" or "excellent," the bending workability was judged as "passed," and if the judgment was "poor," the bending workability was judged as "failed."

[0087] Figure 5A is a cross-sectional SEM image of the apex of a 90° bend after a bending test was performed on contact material sample No. 11 in Table 3, and it can be seen that a crack had occurred. As shown in Figure 5B, the maximum width of the crack was 4.4 μm (good), and the bending workability was "pass." Figure 6A is a cross-sectional SEM image of the apex of a 90° bend after a bending test was performed on contact material sample No. 12 in Table 3, and it can be seen that a crack had occurred. As shown in Figure 6B, the maximum width of the crack was 1.5 μm (good), and the bending workability was "pass." Figure 7 shows a cross-sectional SEM image of the apex of a 90° bend after a bending test was performed on the contact material sample of Sample No. 13 in Table 3, and it can be seen that a crack had occurred. Because the silver layer 3 was not formed, the maximum width of the crack was 19.2 μm (poor), and the bending workability was "failed." Figure 8 is a cross-sectional SEM image of the apex of a 90° bend after a bending test was performed on the contact material sample of Sample No. 14 in Table 3. Since the sample did not have a particle-containing metal layer 2, no cracks occurred (bendability evaluation: excellent). [Explanation of symbols]

[0088] 1, 11 Contact material 2 Particle-containing metal layer 2a Matrix 2b particles (non-conductive particles) 2c Mother phase surface 3 silver layer 3a Surface of the silver layer 4 Conductive base material 4a Surface of conductive substrate

Claims

1. A conductive substrate; a silver layer covering at least a portion of the surface of the conductive substrate; a particle-containing metal layer covering at least a portion of the surface of the silver layer; a Ni layer between the conductive substrate and the silver layer, the silver layer has a silver content of 50% by mass or more and 100% by mass or less and a thickness of 1.0 μm or more; the particle-containing metal layer includes a matrix made of a metal material and particles dispersed in the matrix, The particles are made of an inorganic material or an organic material and have an average particle size of 1 / 2 or less of the thickness of the matrix.

2. A contact material as described in claim 1, wherein the average particle size of the particles is 50 μm or less.

3. 2. The contact material according to claim 1, wherein the thickness of said silver layer is 10 to 60% of the total thickness of said silver layer and said particle-containing metal layer.

4. The contact material according to any one of claims 1 to 3, wherein the particles comprise non-conductive particles.

5. The non-conductive particles have a fluoro group (-F), a methyl group (-CH 3 ), a carbonyl group (—C(═O)—), an amino group (—NR 1 R 2 and R 1 and R 2 is hydrogen or a hydrocarbon group, and R 1 and R 2 may be the same or different), a hydroxy group (—OH), an ether bond (—O—), and an ester bond (—C(═O)—O—).

6. 4. The contact material according to claim 1, wherein the matrix phase contains at least one material selected from the group consisting of silver and silver alloys.

7. 4. The contact material according to claim 1, wherein the particle-containing metal layer satisfies the following formula (1): 2.0≦A p / (A p +A Ag )×100≦12.0 ・・・(1) In formula (1), A p is the area of ​​the part of the particle buried in the matrix in a cross section of the contact material in the thickness direction, and A Ag is the area of ​​the parent phase in a cross section of the contact material in the thickness direction.

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