Copper alloys, copper alloy plastic processing materials, electronic and electrical equipment parts, terminals, bus bars, lead frames

Abstract

This copper alloy has a composition containing 0.10 mass% to 2.6 mass% of Mg, with the balance being Cu and unavoidable impurities, and has at least five edge curves, wherein the edge curve has: an average value of a strain period of 0.01 % to 1.0 %; an average value of a difference in stress level of 0.1 MPa to 2 MPa; a strain period of 0.01 % to 1.0 %; and a stress level difference of 0.1 MPa to 2 MPa, in a plastic deformation region of a stress-strain curve obtained in a low speed tensile test having a strain rate of 1.0×10-6 / s.

Description

[Technical Field]

[0001] The present invention relates to a copper alloy suitable for electronic and electrical device parts such as terminals, bus bars, and lead frames, and to a copper alloy plastically processed material made of this copper alloy, electronic and electrical device parts, terminals, bus bars, and lead frames. This application claims priority based on Japanese Patent Application No. 2021-167385, filed on October 12, 2021, the contents of which are incorporated herein by reference. [Background technology]

[0002] Conventionally, highly conductive copper or copper alloys have been used for parts of electronic and electrical devices such as terminals, bus bars, and lead frame plates. Recently, electronic devices and electrical devices are often used in high temperature environments such as the engine compartment of an automobile, and there is a tendency for these devices to be subjected to large current loads.

[0003] To accommodate large currents, pure copper materials such as oxygen-free copper, which have excellent electrical conductivity, are used in the above-mentioned electronic and electrical equipment components. However, pure copper materials have poor stress relaxation resistance, which indicates the degree to which a spring will sag due to heat, and this has led to the problem that they cannot be used stably in high-temperature environments. Furthermore, terminals, especially female terminals, have springs to maintain connection with male terminals, but when used in high-temperature environments, creep can cause sagging, which can degrade connection reliability. Therefore, springs are required to have stress relaxation resistance, which indicates resistance to sagging. However, stress relaxation resistance and strength are in a trade-off relationship, and it has been difficult to achieve both. Therefore, Patent Document 1 discloses a copper rolled sheet containing Mg in the range of 0.005 mass % or more and less than 0.1 mass %.

[0004] The copper rolled sheet described in Patent Document 1 contains 0.005 mass% or more but less than 0.1 mass% of Mg, with the remainder being Cu and unavoidable impurities. By dissolving Mg in the copper matrix, it is possible to improve strength and stress relaxation resistance without significantly reducing electrical conductivity.

[0005] Recently, the components used in the above-mentioned electronic and electrical parts have become smaller, and the copper materials used are required to have both high strength and high bending workability at the same plate thickness. Because there is a trade-off between strength and bending workability, it has been difficult to achieve both. Furthermore, the electronic and electrical components described above are now being used in harsher high-temperature environments than ever before, and further improvements in strength and stress relaxation resistance are required. [Prior art documents] [Patent documents]

[0006] [Patent Document 1] Japanese Patent Application Laid-Open No. 2016-056414 Summary of the Invention [Problem to be solved by the invention]

[0007] The present invention has been made in view of the above-mentioned circumstances, and an object of the present invention is to provide a copper alloy, a copper alloy plastically worked material, an electronic / electric device component, a terminal, a bus bar, and a lead frame that have high strength and excellent stress relaxation resistance, as well as excellent bending workability. [Means for solving the problem]

[0008] In order to solve this problem, the present inventors have conducted extensive research and have come to the following findings. By using the added element Mg to form a Cottrell atmosphere and stabilize dislocations, it is possible to improve stress relaxation resistance while maintaining strength. Furthermore, by stably arranging dislocations, stress concentration is avoided, leading to improved elongation. When dislocations are stabilized by Mg, serrations appear in the plastic region of the stress-strain curve during a low-speed tensile test.

[0009] The present invention has been made based on the above findings, and one aspect of the present invention has the following requirements. [1] The composition contains Mg in the range of 0.10 mass% to 2.6 mass%, with the balance being Cu and unavoidable impurities, and the strain rate is 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in a low-speed tensile test at / s, Among the periodic stress fluctuations, the curve from one stress minimum point A to another stress minimum point B adjacent to that stress minimum point A is considered to be a single edge curve (however, minimum point B is not included), A copper alloy characterized in that the average value of the strain period of the edge curves is 0.01% or more and 1.0% or less, the average value of the stress difference between the edge curves is 0.1 MPa or more and 2 MPa or less, and the alloy has five or more edge curves with a strain period of 0.01% or more and 1.0% or less and a stress difference between the edge curves and 0.1 MPa or more and 2 MPa or less.

[0010] According to the copper alloy of this composition, Mg is contained in the above range, and the strain rate is 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in a low-speed tensile test at 1 / s, the average strain period of the edge curves is 0.01% to 1.0%, the average stress difference of the edge curves is 0.1 MPa to 2 MPa, and there are five or more edge curves with a strain period of 0.01% to 1.0% and a stress difference of 0.1 MPa to 2 MPa. Therefore, dislocations are stabilized by Mg, improving stress relaxation resistance while maintaining strength. It also improves elongation and bending workability.

[0011] [2] EBSD method, 1000 μm 2 The copper alloy according to [1], characterized in that when the above measurement area is measured at measurement intervals of 0.1 μm and the analysis is performed excluding measurement points where the CI value analyzed by the data analysis software OIM is 0.1 or less, the aspect ratio b / a, which is expressed by the major axis a and the minor axis b of the crystal grain size (including twin crystals), is 0.95 or less. In this case, the aspect ratio b / a, which is expressed by the long diameter a and the short diameter b of the crystal grain size (including twin crystals), is 0.95 or less, and therefore sufficient dislocations are introduced by processing. These dislocations are stabilized by Mg, which makes it possible to further improve stress relaxation resistance while maintaining strength, as well as improve elongation and bending workability.

[0012] [3] The copper alloy according to [1] or [2], characterized in that the tensile strength is 350 MPa or more. In this case, since the tensile strength is set to be 350 MPa or more, it does not easily deform and is particularly suitable as a copper alloy for electronic and electrical equipment parts such as terminals for connectors and press-fits, relays, lead frames, and bus bars.

[0013] [4] The copper alloy according to any one of [1] to [3], characterized in that when the content of Mg is A atomic %, the electrical conductivity σ (% IACS) satisfies the following relational expression: σ≦1.7680 / (-0.0200×A 2 +0.5769×A+1.7)×100 In this case, since the electrical conductivity σ is specified as described above, the added Mg is sufficiently dissolved in the copper matrix, suppressing the formation of precipitates containing Mg, thereby further improving the bending workability.

[0014] [5] The copper alloy according to any one of [1] to [4], further containing P in the range of 0.0005 mass% to 0.1 mass%. In this case, since the P content is set to 0.001 mass% or more, it is possible to improve castability. Also, since the P content is set to 0.1 mass% or less, even when P is added, it is possible to prevent a significant decrease in electrical conductivity.

[0015] [6] The Mg content is A atomic %, the P content is B atomic %, and the Mg equivalent A X A X= (A - 1.5 × B), the electrical conductivity σ (% IACS) satisfies the following relational expression: σ≦1.7680 / (-0.0200×A X 2 +0.5769×A X +1.7)×100 When Mg and P are co-doped, Mg3P2 is generated in the matrix, so when evaluating the degree of Mg solid solubility, it is important to consider the Mg equivalent A rather than the Mg content. X = (A-1.5 x B), and the conductivity must be specified. And the conductivity σ is Mg equivalent A X Since the above-mentioned formula defines the Mg content, the added Mg is sufficiently dissolved in the copper matrix, suppressing the formation of precipitates containing Mg, thereby further improving bending workability.

[0016] [7] A plastically worked copper alloy material, characterized by comprising the copper alloy according to any one of [1] to [6]. Since the copper alloy plastically processed material having this configuration is made of the above-mentioned copper alloy, it has excellent strength, stress relaxation resistance, and bending workability, and is particularly suitable as a material for electronic and electrical equipment components such as terminals, bus bars, and lead frames used in high current applications and high temperature environments.

[0017] [8] The plastically worked copper alloy material according to [7], which is a rolled plate having a thickness of 0.1 mm or more and 10 mm or less. In this case, since the thickness is a rolled plate within the range of 0.1 mm to 10 mm, this copper alloy plastically processed material (rolled plate) can be punched or bent to form parts for electronic and electrical devices such as terminals, bus bars, and lead frames.

[0018] [9] A plastically worked copper alloy material according to [7] or [8], characterized in that it has a metal plating layer on its surface. In this case, since the surface has a metal plating layer, it is particularly suitable as a material for parts of electronic and electrical equipment such as terminals, bus bars, and lead frames. Examples of metal plating layers include Sn plating, Ag plating, Ni plating, Au plating, Pd plating, Rh plating, etc. In one embodiment of the present invention, "Sn plating" includes pure Sn plating or Sn alloy plating, "Ag plating" includes pure Ag plating or Ag alloy plating, "Ni plating" includes pure Ni plating or Ni alloy plating, "Au plating" includes pure Au plating or Au alloy plating, "Pd plating" includes pure Pd plating or Pd alloy plating, and "Rh plating" includes pure Rh plating or Rh alloy plating.

[0019] [9a] This is a rolled material that has been processed by rolling. On the RD surface, EBSD analysis was performed to measure the thickness of 1000 μm. 2 The copper alloy plastically processed material according to any one of [7] to [9], characterized in that when the above measurement area is measured at a measurement interval of 0.1 μm and the analysis is performed excluding measurement points where the CI value analyzed by the data analysis software OIM is 0.1 or less, the aspect ratio b / a, which is expressed by the major axis a and the minor axis b of the crystal grain size (including twins), is 0.95 or less. In this case, the aspect ratio b / a, which is expressed by the long diameter a and the short diameter b of the crystal grain size (including twin crystals), is 0.95 or less, and therefore sufficient dislocations are introduced by the rolling process. These dislocations are stabilized by Mg, which makes it possible to further improve stress relaxation resistance while maintaining strength, as well as improve elongation and bending workability.

[0020]

[10] A component for electronic / electrical equipment, characterized by comprising the plastically worked copper alloy material according to any one of [7] to [9] and [9a]. Note that the component for electronic / electrical equipment in one aspect of the present invention includes terminals, bus bars, lead frames, etc. The electronic / electrical device part having this configuration is manufactured using the above-mentioned plastically worked copper alloy material, and therefore can exhibit excellent properties even in a high-temperature environment.

[0021]

[11] A terminal made of the plastically worked copper alloy material according to any one of [7] to [9] and [9a]. The terminal having this configuration is manufactured using the above-mentioned plastically worked copper alloy material, and therefore can exhibit excellent characteristics even in a high temperature environment.

[0022]

[12] A bus bar made of the plastically worked copper alloy material according to any one of [7] to [9] and [9a]. The bus bar having this configuration is manufactured using the above-mentioned plastically worked copper alloy material, and therefore can exhibit excellent characteristics even in a high-temperature environment.

[0023]

[13] A lead frame made of the plastically worked copper alloy material according to any one of [7] to [9] and [9a]. The lead frame having this configuration is manufactured using the above-mentioned copper alloy plastically processed material, and therefore can exhibit excellent characteristics even in a high-temperature environment. [Effects of the Invention]

[0024] According to one aspect of the present invention, it is possible to provide a copper alloy, a copper alloy plastically worked material, an electronic / electric device component, a terminal, a bus bar, and a lead frame that have high strength and excellent stress relaxation resistance, as well as excellent bending workability. [Brief explanation of the drawings]

[0025] [Figure 1A] 1 is a stress-strain curve obtained in a slow-speed tensile test for the copper alloy of this embodiment. [Figure 1B] FIG. 1B is an enlarged view of region X in FIG. 1A. [Figure 2] 1 is a flow diagram of a method for producing a copper alloy according to an embodiment of the present invention. DETAILED DESCRIPTION OF THE INVENTION

[0026] A copper alloy according to one embodiment of the present invention will be described below. The copper alloy of this embodiment has a composition containing Mg in the range of 0.10 mass % to 2.6 mass % and the balance being Cu and unavoidable impurities. The copper alloy of this embodiment may further contain P in a range of 0.0005 mass % to 0.1 mass %.

[0027] In the copper alloy of this embodiment, the strain rate is 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in a low-speed tensile test at 1 / s, the average strain cycle of the serrated curves is 0.01% to 1.0%, and the average difference in stress between the high and low levels of the serrated curves is 0.1 MPa to 2 MPa. Furthermore, in the plastic deformation region of the stress-strain curve, there are five or more serrated curves with a strain cycle of 0.01% to 1.0% and a difference in stress between the high and low levels of 0.1 MPa to 2 MPa. The strain rate of the copper alloy of this embodiment is 1.0 × 10 -6 An example of a stress-strain curve obtained in a low-speed tensile test at 1 / s is shown in Figures 1A and 1B. As shown in Figures 1A and 1B, in the plastic deformation region, the stress periodically rises and falls as the strain increases, forming a blade-like curve (serration).

[0028] In addition, in the copper alloy of this embodiment, the EBSD method was used to measure the thickness of 1000 μm 2 When the above measurement areas are measured at measurement intervals of 0.1 μm and analyzed excluding measurement points where the CI value analyzed by the data analysis software OIM is 0.1 or less, it is preferable that the aspect ratio b / a, represented by the major axis a and the minor axis b of the crystal grain size (including twins), is 0.95 or less. Furthermore, in the copper alloy of this embodiment, it is preferable that the tensile strength is 350 MPa or more.

[0029] In the copper alloy of this embodiment, when the content of Mg is A atomic %, the electrical conductivity σ (% IACS) preferably satisfies the following relational expression. σ≦1.7680 / (-0.0200×A 2 +0.5769×A+1.7)×100

[0030] Furthermore, in the copper alloy of this embodiment, when P is contained together with Mg, the content of Mg is A atomic %, the content of P is B atomic %, and the Mg equivalent A X A X = (A-1.5 x B), it is preferable that the conductivity σ (% IACS) satisfies the following relational expression: σ≦1.7680 / (-0.0200×A X 2 +0.5769×A X +1.7)×100

[0031] Here, the reasons for specifying the component composition, various properties, and crystalline structure of the copper alloy of this embodiment as described above will be explained below.

[0032] (Mg) Mg is an element that dissolves in the copper matrix and improves stress relaxation resistance without significantly reducing electrical conductivity. Furthermore, by using Mg to form a Cottrell atmosphere and stabilize dislocations, it is possible to improve strength, stress relaxation resistance, and elongation. If the Mg content is less than 0.10 mass%, the effect of the magnesium may not be fully achieved, whereas if the Mg content exceeds 2.6 mass%, the manufacturing load increases, resulting in increased costs and reduced yields, making the product unsuitable for industrial use. For these reasons, in this embodiment, the Mg content is set within the range of 0.10 mass% to 2.6 mass%.

[0033] In order to further improve the strength, stress relaxation resistance, and elongation, the lower limit of the Mg content is preferably set to 0.12 mass% or more, more preferably 0.15 mass% or more, and even more preferably 0.17 mass% or more. In order to further suppress an increase in manufacturing costs and a decrease in yield, the upper limit of the Mg content is preferably set to less than 2.5 mass%, more preferably set to less than 2.4 mass%, and even more preferably set to less than 2.3 mass%.

[0034] (P) In the copper alloy of this embodiment, when the P content is 0.0005 mass% or more, the fluidity of the molten metal is improved and the castability is improved. On the other hand, by limiting the P content to 0.1 mass% or less, it is possible to prevent a large decrease in electrical conductivity. In the copper alloy of this embodiment, in order to further improve castability, the lower limit of the P content is more preferably 0.0006 mass% or more, and more preferably 0.0007 mass% or more. In order to further suppress a decrease in electrical conductivity, the upper limit of the P content is more preferably 0.095 mass% or less, and more preferably 0.092 mass% or less. In the copper alloy of this embodiment, when P is contained as an impurity, the P content may be less than 0.0005 mass%.

[0035] (Other unavoidable impurities) Examples of inevitable impurities other than the above-mentioned elements include Ag, Al, B, Ba, Be, Ca, Cd, Cr, Sc, rare earth elements, V, Nb, Ta, Mo, Ni, W, Mn, Re, Ru, Sr, Ti, Os, Co, Rh, Ir, Pb, Pd, Pt, Au, Zn, Zr, Hf, Hg, Ga, In, Ge, Y, Tl, N, Si, Sn, Li, S, Se, Te, SbBi, As, etc. These inevitable impurities may be contained to the extent that they do not affect the characteristics.

[0036] Here, since these unavoidable impurities may reduce the electrical conductivity, the total amount is preferably 0.1 mass% or less, more preferably 0.05 mass% or less, even more preferably 0.03 mass% or less, and even more preferably 0.01 mass% or less. The upper limit of the content of each of these inevitable impurities is preferably 10 massppm or less, more preferably 5 massppm or less, and even more preferably 2 massppm or less.

[0037] (Stress-strain curve obtained by low-speed tensile test) In the copper alloy of this embodiment, as described above, Mg is used to form a Cottrell atmosphere and stabilize dislocations, thereby improving stress relaxation resistance while maintaining strength. Here, the strain rate is 1.0 × 10 -6 When a low-speed tensile test was conducted at 1 / s, a stress change occurred when one dislocation overcomes a dislocation stabilized by Mg, resulting in the appearance of an edge-like curve (serration) on the stress-strain curve. In this embodiment, in the stress-strain curve obtained by the low-speed tensile test, the stress is 0.2% proof stress σ 0.2 The above region is defined as the plastic deformation region. If the following requirements (1) and (2) are met in this plastic deformation region, it is determined that the edge curve (serration) defined in this embodiment is present. This makes it possible to distinguish between noise generated in the testing equipment and sudden fluctuations due to external factors. (1) The average value of the strain period of the edge curve is 0.01% or more and 1.0% or less, and the average value of the stress difference of the edge curve is 0.1 MPa or more and 2 MPa or less. (2) The strain period is 0.01% or more and 1.0% or less, and there are five or more edge curves with a stress difference of 0.1 MPa or more and 2 MPa or less. In a stress-strain curve, among the periodic stress fluctuations, a curve from one stress minimum point A to another stress minimum point B adjacent to that stress minimum point A is a single crest curve (but does not include minimum point B). A single crest curve has one stress minimum point (valley) and one stress maximum point (peak). The strain period is the difference in strain between two adjacent stress minimum points (valleys). The stress difference is the difference in stress between the stress maximum point (peak) and the stress minimum point (valley) on a single crest curve. The average strain period is the average value of the strain period of all the edge curves in the plastic deformation region, and the average stress difference is the average value of the stress difference of all the edge curves in the plastic deformation region. The average strain period is preferably 0.95% or less, and more preferably 0.90% or less. The average strain period is preferably 0.02% or more, and more preferably 0.03% or more. The average stress difference is preferably 1.90 MPa or less, and more preferably 1.80 MPa or less. The average stress difference is preferably 0.10 MPa or more.

[0038] (aspect ratio b / a) In the copper alloy of this embodiment, as described above, dislocations are stabilized by Mg, thereby improving strength, stress relaxation resistance, and elongation, and therefore it is preferable that the copper alloy have sufficient dislocations. Here, when crystal grains (including twin crystals) are formed such that the aspect ratio b / a, which is expressed by the long diameter a and the short diameter b, is 0.95 or less, sufficient dislocations are present, making it possible to further improve strength, stress relaxation resistance, and elongation. If the aspect ratio b / a is greater than 0.95, there are not enough dislocations, and dislocation stabilization by Mg cannot be achieved. In this embodiment, the aspect ratio b / a of the crystal grains (including twins), expressed by the major axis a and the minor axis b, is preferably 0.93 or less, and even more preferably 0.90 or less. The aspect ratio b / a is preferably 0.005 or more, and even more preferably 0.01 or more.

[0039] Here, in the copper alloy of this embodiment, 1000 μm 2 The above measurement areas were measured at 0.1 μm intervals, and the analysis was performed excluding measurement points where the CI value analyzed by the data analysis software OIM was 0.1 or less, and the aspect ratio b / a, represented by the major axis a and minor axis b of the crystal grain size (including twins), was set to 0.95 or less.

[0040] (tensile strength) In the copper alloy of this embodiment, when the tensile strength is 350 MPa or more, the strength is sufficiently ensured and the alloy is particularly suitable as a material for electronic and electrical device components such as terminals, bus bars, lead frames, etc. The tensile strength in this embodiment is defined as the tensile strength in the direction parallel to the rolling direction. In this embodiment, the tensile strength is more preferably 360 MPa or more, and even more preferably 370 MPa or more. Furthermore, in this embodiment, no upper limit is set for the tensile strength (tensile strength in the direction parallel to the rolling direction), but in order to avoid a decrease in productivity due to coil winding tendencies when using coiled strip material, the tensile strength is preferably 2000 MPa or less. It is more preferably 1700 MPa or less, and even more preferably 1500 MPa or less.

[0041] (conductivity) In the copper alloy of this embodiment, when Mg is sufficiently dissolved, the occurrence of Mg precipitates can be suppressed, and bending workability can be further improved. Here, when the Mg content is A atomic %, if the electrical conductivity σ (% IACS) satisfies the following relational expression, Mg is sufficiently dissolved in the copper matrix, and bending workability can be further improved. σ≦1.7680 / (-0.0200×A 2 +0.5769×A+1.7)×100

[0042] Furthermore, in the copper alloy of this embodiment, when P is contained together with Mg, Mg3P2 is generated in the matrix, so when evaluating the degree of solid solubility of Mg, it is not the Mg content but the Mg equivalent A X = (A-1.5 x B), and the conductivity must be specified. Therefore, the Mg content is A atomic %, the P content is B atomic %, and the Mg equivalent A X A X = (A - 1.5 × B), when the electrical conductivity σ (% IACS) satisfies the following relational expression, Mg is sufficiently dissolved in the copper matrix, and bending workability can be further improved. σ≦1.7680 / (-0.0200×A X 2 +0.5769×A X +1.7)×100

[0043] Next, the method for producing the copper alloy according to this embodiment having the above-described configuration will be described with reference to the flow diagram shown in FIG.

[0044] (Melting and casting process S01) First, the copper raw material is melted, and the above-mentioned elements are added to the resulting molten copper to adjust the composition, producing a molten copper alloy. The various elements can be added in the form of simple elements or master alloys. Raw materials containing the above-mentioned elements may also be melted together with the copper raw material. Recycled or scrap copper of this alloy may also be used. The molten copper used here is preferably so-called 4NCu, which has a purity of 99.99 mass% or higher, or so-called 5NCu, which has a purity of 99.999 mass% or higher. In the melting process, in order to suppress oxidation of Mg and reduce the hydrogen concentration, it is preferable to perform atmospheric melting in an inert gas atmosphere (e.g., Ar gas) with a low vapor pressure of HO, and to minimize the holding time during melting.

[0045] The molten copper alloy with the adjusted composition is then poured into a mold to produce an ingot. When mass production is taken into consideration, it is preferable to use a continuous casting method or a semi-continuous casting method. In this case, since crystallized substances containing Mg and P are formed during solidification of the molten metal, increasing the solidification rate makes it possible to make the crystallized substances finer in size. Therefore, the cooling rate of the molten metal is preferably 0.1°C / sec or more, more preferably 0.5°C / sec or more, and most preferably 1°C / sec or more.

[0046] (Homogenization / solution treatment step S02) Next, the resulting ingot is subjected to a heat treatment for homogenization and solution treatment. The ingot may contain intermetallic compounds, primarily composed of Cu and Mg, that are formed as a result of the segregation and concentration of Mg during the solidification process. To eliminate or reduce these segregations and intermetallic compounds, the ingot is heated to a temperature of 300°C to 900°C, thereby diffusing the Mg homogeneously within the ingot and dissolving it in the matrix. This homogenization / solution treatment step S02 is preferably performed in a non-oxidizing or reducing atmosphere.

[0047] If the heating temperature is below 300°C, the solution treatment will be incomplete, and there is a risk that a large amount of intermetallic compounds, primarily composed of Cu and Mg, will remain in the matrix. On the other hand, if the heating temperature exceeds 900°C, part of the copper material will become liquid, and there is a risk that the structure and surface condition will become non-uniform. Therefore, the heating temperature is set in the range of 300°C to 900°C. In order to improve the efficiency of the rough rolling and to homogenize the structure, which will be described later, hot working may be performed after the homogenization / solution treatment step S02. In this case, the working method is not particularly limited, and for example, rolling, wire drawing, extrusion, groove rolling, forging, pressing, etc. can be used. In addition, the hot working temperature is preferably in the range of 300°C or higher and 900°C or lower.

[0048] (Rough machining process S03) Rough processing is performed to process the material into a predetermined shape. The temperature conditions in this rough processing step S03 are not particularly limited, but in order to suppress recrystallization or improve dimensional accuracy, cold or warm rolling is preferably performed at a temperature in the range of -200°C to 200°C, with room temperature being particularly preferred. The processing rate is preferably 20% or more, and more preferably 30% or more. The processing method is not particularly limited, and examples that can be used include rolling, wire drawing, extrusion, groove rolling, forging, and pressing.

[0049] (Intermediate heat treatment process S04) After the rough processing step S03, a heat treatment is carried out for the purpose of thorough solutionization, recrystallization of the structure, or softening to improve workability. The heat treatment method is not particularly limited, but is preferably carried out at a holding temperature of 400°C to 900°C for a holding time of 10 seconds to 10 hours in a non-oxidizing or reducing atmosphere. The cooling method after heating is also not particularly limited, but it is preferable to use a method such as water quenching that provides a cooling rate of 200°C / min or more. The rough processing step S03 and the intermediate heat treatment step S04 may be carried out repeatedly.

[0050] (WORKING BEFORE FINISHING STEP S05) The copper material after the intermediate heat treatment step S04 is subjected to upper pre-processing to be processed into a predetermined shape. The temperature conditions in this upper pre-processing step S05 are not particularly limited, but in order to suppress recrystallization or softening during processing, it is preferable to perform cold or warm processing within the range of -200°C to 200°C, with room temperature being particularly preferable. The processing rate is appropriately selected to approximate the final shape, but is preferably 5% or more to improve strength through work hardening. The processing method is not particularly limited, and for example, rolling, drawing, extrusion, groove rolling, forging, pressing, etc. can be used.

[0051] (HEAT TREATMENT BEFORE FINISHING STEP S06) The plastically worked material obtained in the pre-upper processing step S05 is subjected to pre-upper heat treatment for the purpose of stabilization through dislocation pinning and dislocation rearrangement by Mg. The heat treatment temperature is preferably in the range of 100°C to 800°C. Note that the heat treatment conditions (temperature, time, cooling rate) must be set to avoid a significant decrease in strength due to recrystallization. For example, it is preferable to hold the material at 300°C for 1 second to 120 seconds. This heat treatment is preferably carried out in a non-oxidizing or reducing atmosphere. The heat treatment method is not particularly limited, but a short-time heat treatment in a continuous annealing furnace is preferable from the viewpoint of reducing manufacturing costs. Furthermore, the above-mentioned pre-upper processing step S05 and pre-upper heat treatment step S06 may be repeatedly performed.

[0052] (Light processing step S07) The plastically worked material that has undergone the pre-heat treatment step S06 is subjected to light plastic working to further develop serrations through dislocation pinning and stabilization by Mg. The temperature conditions in this light working step S07 are not particularly limited, but in order to suppress recrystallization or improve dimensional accuracy, it is preferable to set the temperature within the range of -200°C to 200°C, which results in cold or warm rolling, and room temperature is particularly preferable. In the light working step S07, a high working rate leads to a decrease in stress relaxation resistance, so it is preferable to set the total working rate within the range of 5% to 50% and limit the working rate per pass to 20% or less. Furthermore, a light working rate makes it difficult to achieve uniform deformation, which can cause deterioration of the sheet shape, so it is preferable to apply a tension of 50 MPa or more in the longitudinal direction during rolling.

[0053] (Finishing heat treatment process S08) Finally, the plastically worked material obtained in the light processing step S07 is subjected to a final heat treatment for the purpose of further stabilization through dislocation pinning and dislocation rearrangement using Mg. The heat treatment temperature is preferably in the range of 100°C to 800°C. Note that the heat treatment conditions (temperature, time, cooling rate) must be set to avoid a significant decrease in strength due to recrystallization. For example, a temperature of 300°C is preferably maintained for 1 second to 120 seconds. This heat treatment is preferably performed in a non-oxidizing or reducing atmosphere. The heat treatment method is not particularly limited, but a short-time heat treatment in a continuous annealing furnace is preferable in terms of the effect of reducing production costs. Furthermore, the light working step S07 and the finish heat treatment step S08 may be carried out repeatedly.

[0054] In this way, the copper alloy (plastically worked copper alloy material) of this embodiment is produced. The plastically worked copper alloy material produced by rolling is called a rolled copper alloy sheet.

[0055] Here, when the thickness of the plastically worked copper alloy material is 0.1 mm or more, it is suitable for use as a conductor in large current applications. Furthermore, when the thickness of the plastically worked copper alloy material is 10.0 mm or less, an increase in the load of the press machine is suppressed, productivity per unit time can be ensured, and manufacturing costs can be reduced. For this reason, it is preferable that the thickness of the plastically worked copper alloy material (rolled copper alloy material) be within the range of 0.1 mm to 10.0 mm. The lower limit of the thickness of the plastically worked copper alloy material (rolled copper alloy material) is preferably 0.5 mm or more, more preferably 1.0 mm or more, while the upper limit of the thickness of the plastically worked copper alloy material (rolled copper alloy material) is preferably less than 9.0 mm, more preferably less than 8.0 mm.

[0056] Furthermore, a metal plating layer (for example, Sn plating, Ag plating, Ni plating, Au plating, Pd plating, Rh plating, etc.) may be formed on the surface of the plastically worked copper alloy material (rolled copper alloy material) of this embodiment.

[0057] Furthermore, in the copper alloy (copper alloy plastically worked material) of this embodiment, when it is a rolled material (copper alloy rolled plate) that has been rolled, the RD surface is subjected to EBSD analysis to obtain a 1000 μm 2 When the above measurement areas are measured at measurement intervals of 0.1 μm and analyzed excluding measurement points where the CI value analyzed by the data analysis software OIM is 0.1 or less, it is preferable that the aspect ratio b / a, represented by the major axis a and the minor axis b of the crystal grain size (including twins), is 0.95 or less.

[0058] When the aspect ratio b / a, which is expressed by the long diameter a and the short diameter b of the crystal grain size (including twins), is 0.95 or less, sufficient dislocations are introduced by rolling, and by stabilizing these dislocations with Mg, it becomes possible to further improve the strength, stress relaxation resistance, and elongation. In this embodiment, the aspect ratio b / a is more preferably 0.93 or less, and even more preferably 0.90 or less.

[0059] The copper alloy of this embodiment having the above-described configuration contains Mg in the range of 0.10 mass% to 2.6 mass%. -6 In the plastic deformation region of the stress-strain curve obtained in a low-speed tensile test at 1 / s, the average strain period of the edge-shaped curves is 0.01% to 1.0%, and the average stress difference of the edge-shaped curves is 0.1 MPa to 2 MPa. Furthermore, within the plastic deformation region of the stress-strain curve, there are five or more edge-shaped curves with a strain period of 0.01% to 1.0% and a stress difference of 0.1 MPa to 2 MPa. Therefore, dislocations are stabilized by Mg, which improves stress relaxation resistance while maintaining strength. It also improves elongation and bending workability.

[0060] In addition, in the copper alloy of this embodiment, 1000 μm 2 When the above measurement areas are measured at 0.1 μm intervals and analyzed excluding measurement points where the CI value analyzed by the data analysis software OIM is 0.1 or less, if the aspect ratio b / a, represented by the major axis a and the minor axis b of the crystal grain size (including twins), is 0.95 or less, sufficient dislocations have been introduced by processing, and these dislocations are stabilized by Mg, which makes it possible to maintain strength while further improving stress relaxation resistance, as well as improving elongation and bending workability.

[0061] Furthermore, in the copper alloy of the present embodiment, when the tensile strength is 350 MPa or more, the tensile strength is sufficiently high and the copper alloy is not easily deformed, and is particularly suitable as a copper alloy for electronic and electric device parts such as terminals for connectors and press-fits, relays, lead frames, and bus bars.

[0062] Furthermore, in the copper alloy of this embodiment, when the Mg content is A atomic %, if the electrical conductivity σ (%IACS) satisfies the following relational expression, the added Mg is sufficiently dissolved in the copper matrix, and the formation of precipitates containing Mg is suppressed, thereby further improving the bending workability. σ≦1.7680 / (-0.0200×A 2 +0.5769×A+1.7)×100

[0063] Furthermore, in the copper alloy of the present embodiment, when P is further contained in the range of 0.0005 mass% or more and 0.1 mass% or less, it is possible to improve the castability and to suppress a significant decrease in electrical conductivity even when P is added.

[0064] In the copper alloy of this embodiment, the Mg content is A atomic %, the P content is B atomic %, and the Mg equivalent A X A X = (A - 1.5 × B), if the electrical conductivity σ (%IACS) satisfies the following relational expression, even if Mg and P are co-added and Mg3P2 is formed in the matrix, the added Mg is sufficiently dissolved in the copper matrix, and the formation of precipitates containing Mg is suppressed. Therefore, the bending workability can be further improved. σ≦1.7680 / (-0.0200×A X 2 +0.5769×A X +1.7)×100

[0065] The copper alloy plastically worked material of this embodiment is made of the above-mentioned copper alloy, and therefore has excellent electrical conductivity, stress relaxation resistance, and bending workability, and is particularly suitable as a material for electronic and electrical device parts such as terminals, bus bars, and lead frames.

[0066] Furthermore, when the copper alloy plastically worked material of this embodiment is made into a rolled plate having a thickness in the range of 0.1 mm to 10 mm, parts for electronic and electrical devices such as terminals, bus bars, and lead frames can be formed relatively easily by punching or bending the copper alloy plastically worked material (rolled plate).

[0067] In addition, when a metal plating layer (e.g., Sn plating, Ag plating, Ni plating, Au plating, Pd plating, Rh plating, etc.) is formed on the surface of the copper alloy plastically worked material of this embodiment, it is particularly suitable as a material for electronic and electrical device parts such as terminals and bus bars.

[0068] Furthermore, the electronic / electrical device components (terminals, bus bars, lead frames, etc.) of this embodiment are made of the above-mentioned copper alloy plastically processed material and copper alloy, and therefore can exhibit excellent properties even in high-temperature environments.

[0069] The copper alloy, the copper alloy plastically worked material, and the electronic and electrical device parts (terminals, bus bars, lead frames, etc.) according to the embodiments of the present invention have been described above, but the present invention is not limited thereto and can be modified as appropriate within the scope of the technical requirements of the invention.

[0070] For example, in the above-described embodiment, an example of a method for manufacturing a copper alloy (copper alloy plastically processed material) is described, but the method for manufacturing a copper alloy is not limited to that described in the embodiment, and an existing manufacturing method may be appropriately selected for manufacturing the copper alloy. [Example]

[0071] The results of confirmation experiments conducted to confirm the effects of the present invention will be described below.

[0072] A copper raw material consisting of oxygen-free copper (ASTM B152 C10100) with a purity of 99.99% by mass or higher was prepared and placed in a high-purity graphite crucible. This was then high-frequency melted in an atmosphere furnace with an Ar gas atmosphere. Various additive elements were added to the resulting molten copper to adjust the composition shown in Table 1, and the copper was poured into a carbon mold to produce an ingot. The size of the ingot was 10-30 mm thick, approximately 20 mm wide, and approximately 100-120 mm long. The obtained ingot was subjected to a heating step in which it was heated in an Ar gas atmosphere at a temperature of 715°C for 4 hours, and then water quenched.

[0073] The heat-treated ingot was cut and the surface ground to remove the oxide film. The thickness before rough processing was then adjusted appropriately to achieve the set final thickness, and the ingot was cut. Rough processing, intermediate heat treatment, pre-cold rolling, and pre-heat treatment were then performed under the processing rate and temperature conditions listed in Tables 2 and 3. Light processing (light rolling) and finish heat treatment were then performed under the same conditions listed in Tables 2 and 3, to produce strips approximately 20 mm wide with the thicknesses shown in Tables 2 and 3 for property evaluation.

[0074] The obtained strip material for property evaluation was evaluated for the following items.

[0075] (composition analysis) Measurement samples were taken from the resulting ingots, and the amount of Mg was measured by inductively coupled plasma atomic emission spectrometry, while the amounts of other elements were measured using a glow discharge mass spectrometer (GD-MS). The measurements were carried out by taking samples from two locations, the center and the end in the width direction, and the content of the sample with the larger content was recorded. As a result, it was confirmed that the composition was as shown in Table 1. The item "Mg equivalent" in Table 1 is Mg equivalent A X If the content of Mg is A atomic % and the content of P is B atomic %, then A X = (A-1.5×B).

[0076] (Low speed tensile test) A No. 13B test piece specified in JIS Z 2201 was taken from the strip material for property evaluation, and the strain rate was 1.0 × 10 -6 A low-speed tensile test was carried out at 1000 kJ / s to measure the tensile strength and elongation. The test pieces were taken so that the tensile direction in the tensile test was parallel to the rolling direction of the strip material for property evaluation.

[0077] The load-elongation curves obtained in the low-speed tensile test were analyzed to confirm the presence or absence of serrations. The obtained data shows that the 0.2% yield strength σ measured by the offset method of JIS Z 2241 0.2 The presence or absence of an edge curve (periodic stress fluctuation) was confirmed in the subsequent curves (plastic deformation region). In the "Presence / absence" column of Tables 4 and 5, if an edge curve was present, it was recorded as "Present" even if the strain period and stress difference were outside the ranges described in the embodiment. For those specimens in which these edge curves were found, the average value of the strain period of the edge curves in the plastic deformation region, the average value of the stress difference of the edge curves, and the number of edge curves are listed in Tables 4 and 5. The strain period of each edge curve in the plastic deformation region was measured, and the sum was divided by the number of edge curves to calculate an average value, which was used as the average strain period of the edge curves. Similarly, the stress difference of each edge curve in the plastic deformation region was measured, and the sum was divided by the number of edge curves to calculate an average value, which was used as the average stress difference of the edge curves. The number of edge curves is the number of edge curves in the plastic deformation region where the strain cycle is 0.01% or more and 1.0% or less and the stress difference is 0.1 MPa or more and 2 MPa or less.

[0078] (aspect ratio) The surface perpendicular to the rolling direction of the strip material for property evaluation, i.e., the RD (roll direction) surface, was mechanically polished using waterproof abrasive paper and diamond abrasive grains, and then finish-polished using colloidal silica solution. EBSD measurement equipment (FEI Quanta FEG 450, EDAX / TSL (now AMETEK) OIM Data Collection) and analysis software (EDAX / TSL (now AMETEK) OIM Data Analysis ver. 5.3) were used to measure the electron beam acceleration voltage of 20 kV, with a measurement interval of 1000 μm at 0.1 μm steps. 2 Within the above measurement area, the misorientation of each crystal grain (including twins) was analyzed, excluding measurement points where the CI value was 0.1 or less. Measurement points where the misorientation between adjacent measurement points was 15° or more were considered grain boundaries, and the aspect ratio, expressed as b / a, was measured, where a is the long diameter of the crystal grain and b is the short diameter of the crystal grain. Furthermore, in measuring the aspect ratio, the grain size on the EBSD was determined using a Grain Tolerance Angle of 5° and a Minimum Grain Size of 2 pixels. The average aspect ratio of the crystal grains was then calculated, and this average was used as the aspect ratio of the sample.

[0079] (conductivity) Test pieces measuring 10 mm wide and 60 mm long were taken from the strip material for property evaluation, and electrical resistance was measured using the four-terminal method. The dimensions of the test pieces were also measured using a micrometer, and the volume of the test pieces was calculated. The electrical conductivity was then calculated from the measured electrical resistance value and volume. The test pieces were taken so that their longitudinal direction was parallel to the rolling direction of the strip material for property evaluation.

[0080] (Stress relaxation resistance) In the stress relaxation resistance test, stress was applied by a method conforming to the cantilever screw method of the Japan Copper and Brass Association technical standard JCBA-T309:2004, and the residual stress rate was measured after holding at a temperature of 150°C for 1000 hours. The test method involved taking test pieces (10 mm wide) from each strip material for property evaluation in a direction parallel to the rolling direction, setting the initial deflection displacement to 2 mm, and adjusting the span length so that the maximum surface stress of the test piece was 80% of the yield strength. The maximum surface stress was determined by the following formula: Maximum surface stress (MPa) = 1.5Etδ0 / L s 2 where E,t,δ0,L s indicates the following value: E: Young's modulus (MPa) t: sample thickness (mm) δ0: Initial deflection displacement (mm) L s :Span length (mm)

[0081] Residual stress was measured from the bending tendency after holding at 150°C for 1000 hours, and stress relaxation resistance was evaluated. The residual stress was calculated using the following formula. Residual stress rate (%)=(1-δ t / δ0)×100 where δ t ,δ0 indicates the following values. δ t : (Permanent deflection (mm) after 1000 hours at 150°C) - (Permanent deflection (mm) after 24 hours at room temperature) δ0: Initial deflection displacement (mm)

[0082] (bending workability) Bending was carried out in accordance with the four test methods of the Japan Copper and Brass Association technical standard JBMA-T307:2007. Multiple test pieces measuring 10 mm wide x 30 mm long were taken from the strip material for property evaluation so that the rolling direction and the longitudinal direction of the test piece were parallel, and a W-bend test was carried out using a W-shaped jig with a bending angle of 90 degrees and a bending radius of 0.5 mm. The outer periphery of the bent part was then visually inspected, and if there was any fracture it was judged as "x" (poor), if only partial fracture occurred it was judged as "△" (fair), if there was no fracture and only fine cracks it was judged as "○" (good), and if no fracture or fine cracks were found it was judged as "◎" (excellent).

[0083] [Table 1]

[0084] [Table 2]

[0085] [Table 3]

[0086] [Table 4]

[0087] [Table 5]

[0088] In Comparative Example 1, the Mg content exceeded the range of the present embodiment, resulting in a low electrical conductivity of 32% IACS. -6 In the plastic deformation region of the stress-strain curve obtained in the low-speed tensile test at 1 / s, the average value of the difference in stress between the high and low points of the edge curve was higher than the range of the embodiment, and the bending workability was poor.

[0089] In Comparative Example 2, the strain rate was 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in the low-speed tensile test at 1 / s, the edge-like curve (serration) defined in this embodiment was not observed, and the bending workability was poor.

[0090] In Comparative Example 3, the strain rate was 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in a low-speed tensile test at 1 / s, the average value of the strain period of the edge curve was higher than the range of the embodiment, and the elongation was 2% and the residual stress rate was 52%, which was low.

[0091] In Comparative Example 4, the strain rate was 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in the low-speed tensile test at 1 / s, the average value of the stress difference in the edge curve was lower than the range of the embodiment, and the bending workability was poor.

[0092] In Comparative Example 5, the strain rate was 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in the low-speed tensile test at 1 / s, the edge-like curve (serration) defined in this embodiment was not observed, and the tensile strength was low at 330 MPa.

[0093] In Comparative Example 6, the Mg content was lower than the range of the present embodiment, and the residual stress rate was 58%, which resulted in poor stress relaxation resistance. -6 In the plastic deformation region of the stress-strain curve obtained in the low-speed tensile test at 1 / s, the edge-like curve (serration) defined in this embodiment was not observed, and the tensile strength was low at 320 MPa.

[0094] In Comparative Example 7, the strain rate was 1.0 × 10 -6 In the plastic deformation region of the stress-strain curve obtained in a low-speed tensile test at 1 / s, the strain cycle was 0.01% or more and 1.0% or less, and the number of edge-like curves (serrations) with a stress difference of 0.1 MPa or more and 2 MPa or less was 3, but less than 5. In addition, the average value of the stress difference in the edge-like curves was lower than the range of the embodiment. As a result, the residual stress rate was low at 57%.

[0095] In contrast, it was confirmed that in Examples 1 to 16 of the present invention, the tensile strength and stress relaxation resistance were improved in a well-balanced manner, and the bending workability was also sufficiently excellent. From the above, it was confirmed that the present invention can provide a copper alloy having high strength and excellent stress relaxation resistance, as well as excellent bending workability. [Industrial Applicability]

[0096] The copper alloy of this embodiment (copper alloy plastically worked material) is suitably applied to parts for electronic and electric devices such as terminals, bus bars, and lead frame plates.

Claims

1. The composition contains Mg in a range of 0.10 mass% or more and 2.6 mass% or less, with the balance being Cu and inevitable impurities, Strain rate 1.0 x 10 －６ In the plastic deformation region of the stress-strain curve obtained in a low-speed tensile test at 1 / s, the curve from one stress minimum point A to another stress minimum point B adjacent to the stress minimum point A is considered to be one edge-shaped curve (however, the minimum point B is not included), A copper alloy characterized in that the average value of the strain period of the edge curves is 0.01% or more and 1.0% or less, the average value of the stress difference between the edge curves is 0.1 MPa or more and 2 MPa or less, and the alloy has five or more edge curves having a strain period of 0.01% or more and 1.0% or less and a stress difference between the edge curves and 0.1 MPa or more and 2 MPa or less.

2. 1000 μm by EBSD method ２ The copper alloy according to claim 1, characterized in that, when the above measurement areas are measured at measurement intervals of 0.1 μm and analysis is performed excluding measurement points where the CI value analyzed by data analysis software OIM is 0.1 or less, the aspect ratio b / a, represented by the major axis a and the minor axis b of the crystal grain size (including twin crystals), is 0.95 or less.

3. 3. The copper alloy according to claim 1, wherein the tensile strength is 350 MPa or more.

4. 3. The copper alloy according to claim 1, wherein the electrical conductivity σ (% IACS) satisfies the following relational expression when the Mg content is A atomic %. σ≦1.7680 / (-0.0200×A ２ +0.5769×A+1.7)×100

5. 3. The copper alloy according to claim 1, further containing P in a range of 0.0005 mass% to 0.1 mass%.

6. The Mg content is A atomic %, the P content is B atomic %, and the Mg equivalent A Ｘ A Ｘ The copper alloy according to claim 5, characterized in that, when A = (A - 1.5 × B), the electrical conductivity σ (% IACS) satisfies the following relational expression: σ≦1.7680 / (-0.0200×A Ｘ ２ +0.5769×A Ｘ +1.7)×100

7. A plastically worked copper alloy material comprising the copper alloy according to claim 1 or 2.

8. 8. The plastically worked copper alloy material according to claim 7, which is a rolled plate having a thickness in the range of 0.1 mm to 10 mm.

9. 8. The plastically worked copper alloy material according to claim 7, characterized in that it has a metal plating layer on its surface.

10. 8. A part for electronic or electrical equipment, comprising the plastically worked copper alloy material according to claim 7.

11. A terminal made of the plastically worked copper alloy material according to claim 7.

12. A bus bar comprising the plastically worked copper alloy material according to claim 7.

13. A lead frame comprising the plastically worked copper alloy material according to claim 7.

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