EP1873266A1 - Kupferlegierung - Google Patents

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Publication number
EP1873266A1
EP1873266A1 EP06728554A EP06728554A EP1873266A1 EP 1873266 A1 EP1873266 A1 EP 1873266A1 EP 06728554 A EP06728554 A EP 06728554A EP 06728554 A EP06728554 A EP 06728554A EP 1873266 A1 EP1873266 A1 EP 1873266A1
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EP
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Prior art keywords
precipitate
mass
copper alloy
bending property
present
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English (en)
French (fr)
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EP1873266A4 (de
EP1873266B1 (de
Inventor
Kuniteru Mihara
Nobuyuki Tanaka
Tatsuhiko Eguchi
Kiyoshige Hirose
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Furukawa Electric Co Ltd
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Furukawa Electric Co Ltd
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C9/00Alloys based on copper
    • C22C9/06Alloys based on copper with nickel or cobalt as the next major constituent

Definitions

  • the present invention relates to a copper alloy applicable as materials for electric and electronic instruments.
  • copper-based materials such as phosphor bronze, red brass, and brass, which are excellent in electrical conductivity and thermal conductivity, have been used widely as materials for electric and electronic instruments (electrical and electronic machinery and tools).
  • copper-based materials such as phosphor bronze, red brass, and brass, which are excellent in electrical conductivity and thermal conductivity
  • demands for miniaturization, weight saving, and associated high-density packaging of parts of electric and electronic instruments have increased, and various characteristics of higher levels are required for the copper-based materials applied thereto.
  • Examples of basic characteristics required include mechanical properties, electrical conductivity, stress relaxation resistance, bending property, and spring property.
  • improvements in stress relaxation resistance, tensile strength, and bending property are strongly required, for satisfying the recent demands for the miniaturization of parts or components for the products described above.
  • tensile strength and bending property are necessary for lead frame materials, while stress relaxation resistance as well as tensile strength is necessary for connectors and terminal materials.
  • the requirements for those materials differ form each other little by little, depending on uses, kinds, shapes, or the like of the parts, and specific requirements include: a tensile strength of 700 MPa or more and a bending property of R/t ⁇ 1.0 (in which R represents a bending radius, and t represents a sheet thickness), or a tensile strength of 800 MPa or more and a bending property of R/t ⁇ 2.0; more preferably a tensile strength of 800 MPa or more and a bending property of R/t ⁇ 1.5, or a tensile strength of 900 MPa or more and a bending property of R/t ⁇ 2.0. Thinning of the material is inevitable in association with miniaturization of the parts.
  • Minimum stress relaxation resistance is a value defined by the Standard of the Electronic Materials Manufacturers Association of Japan (EMAS-3003), wherein the copper alloy material is desired to satisfy a stress relaxation ratio of less than 20% at a temperature condition of 150°C.
  • EANS-3003 Standard of the Electronic Materials Manufacturers Association of Japan
  • the required characteristics have reached a level that cannot be satisfied with conventional commercially available, mass-produced alloys, such as phosphor bronze, red brass, and brass.
  • such alloys each have an increased strength by: allowing Sn or Zn having a very different atomic radius from that of copper as a matrix phase, to be contained as a solid solution in Cu; and subjecting the resultant alloy having the solid solution to cold-working such as rolling or drawing.
  • the method can provide high-strength materials by employing a large cold-working ratio, but employment of a large cold-working ratio (generally 50% or more) is known to conspicuously degrade bending property of the resultant alloy material.
  • the method generally involves a combination of solid solution strengthening and working strengthening.
  • An alternative strengthening method is a precipitation strengthening method (a precipitation hardening method) that involves formation of a precipitate of a nanometer order in the materials.
  • the precipitation strengthening method has merits of increasing strength and improving electrical conductivity at the same time, and is used for many alloys.
  • a strengthened alloy prepared by forming a precipitate composed of Ni and Si by adding Ni and Si into Cu so-called a Corson alloy, has a remarkably high strengthening ability compared with many other precipitation-type alloys.
  • This strengthening method is also used for some commercially available alloys (e.g. CDA70250, a registered alloy of Copper Development Association (CDA)).
  • the alloy When the alloy generally subjected to precipitating strengthening is used for terminal/connector materials, the alloy is produced through a production process incorporating the following two important heat treatments.
  • One is a heat treatment which involves heat treatment at a high temperature (generally 700°C or higher) near a melting point, so-called solution treatment, to allow Ni and Si precipitated through casting or hot-rolling to be contained as a solid solution into a Cu matrix.
  • the other is a heat treatment which involves heat treatment at a lower temperature than that of the solution treatment, so-called aging treatment, to precipitate Ni and Si, which are in the solid solution caused at the high temperature, as a precipitate.
  • the strengthening method utilizes a difference in concentrations of Ni and Si entering Cu as a solid solution at high temperatures and low temperatures.
  • Corson alloy applicable for electric and electronic instruments includes an alloy having a defined grain size of precipitate (see, for example, Patent Document 1).
  • the precipitation-type alloy has such problems that the crystal grain size increases to cause giant crystal grains upon the solution treatment, and that the crystal grain size upon the solution treatment remains unchanged and becomes the crystal grain size of a product since the aging treatment generally does not involve recrystallization.
  • An increased amount of Ni or Si to be added requires a solution treatment at a higher temperature, and it results in that the crystal grain size tends to increase to cause giant crystal grains, through a heat treatment in a short period of time. The resultant giant crystal grains occurred in this way cause problems of conspicuous deterioration in bending property.
  • a method of improving the bending property of a copper alloy involves addition of Mn, Ni, and P for a mutual reaction to precipitate a compound, without use of a Ni-Si precipitate (see, for example, Patent Document 2).
  • the resultant alloy has a tensile strength of about 640 MPa at most, which is not sufficient for satisfying the recent demands for high strength through miniaturization of parts.
  • Addition of Si to the copper alloy decreases the amount of the Ni-P precipitate, to thereby reduce the mechanical strength and electrical conductivity. Further, excess Si and P cause problems of occurrence of crack upon hot working. As is apparent from the above, the bending property is hardly maintained with increasing tensile strength.
  • the present invention contemplates providing a copper alloy having high bending property and excellent tensile strength, electrical conductivity and stress relaxation resistance, wherein characteristics of the copper alloy may be readily balanced depending on uses, and the copper alloy is favorable for materials of lead frames, connectors, terminals or the like of electric and electronic instruments, particularly for materials of vehicle connectors, terminals, relays and switches or the like.
  • the inventors of the present invention have conducted intensive studies on a copper alloy suitably used for electrical and electronic parts, and have noticed the relations between characteristics of the alloy and grain diameters of Ni-Si precipitates and other precipitates in a copper alloy structure, and between the proportions of the distribution density of the precipitates and suppression of coarsening of crystal grains.
  • the inventors have completed, through intensive studies, the copper alloy of the present invention that is able to form a material having excellent tensile strength and being excellent in bending property, electrical conductivity, and stress relaxation resistance. According to the present invention, there is provided the following means:
  • the copper alloy of the present invention compatibly has a tensile strength and a bending property (R/t) at high levels, without impairing electrical conductivity, while stress relaxation resistance that may largely affect reliability of connectors and terminals is further improved.
  • the copper alloy of the present invention is excellent in bending property and stress relaxation resistance, as compared with conventional copper alloys having the same level of tensile strength.
  • the copper alloy of the present invention is a copper alloy favorable for use in electric and electronic instruments that are required for higher characteristics upon miniaturization. In addition to the above, the copper alloy of the present invention is excellent in other properties such as spring property.
  • the copper alloy of the present invention is an inexpensive, high-performance copper alloy maintaining high electrical conductivity, having excellent bending property and other favorable properties, and it is preferable for a variety of electric and electronic instruments including electronic parts, e.g. vehicle terminals/connectors, relays, and switches.
  • the present invention relates to controlling of a grain size of a precipitate of a copper alloy.
  • a method of controlling a grain size has been realized from two standpoints.
  • the method of controlling a grain size can be realized by using an element that does not allow a crystal grain size to increase to cause giant grains upon a solution treatment.
  • Each of precipitates composed of Ni, Si and ⁇ ; Ni, ⁇ and ⁇ ; Si, ⁇ and ⁇ ; and ⁇ , ⁇ and ⁇ does not form any solid solution in a Cu matrix phase even at high temperatures of the solution treatment, and that the precipitate exists in crystal grains of the Cu matrix phase and the precipitate grains, to exhibit an action and effect of suppressing growth of the crystal grains of the matrix.
  • the method of controlling a grain size can be realized by using an element that serves as a nucleus at initial recrystallization upon the solution treatment.
  • An intermetallic compound which is a precipitate composed of Ni, Si and ⁇ ; Ni, ⁇ and ⁇ ; Si, ⁇ and ⁇ ; and ⁇ , ⁇ and ⁇ (herein ⁇ , ⁇ and ⁇ each are an element other than Ni and Si) serves as a nucleation site for recrystallization at a solution treatment temperature, and that more crystal grains are formed (nucleation) than that in the case where the precipitate is not added. Formation of more crystal grains causes mutual interference of the crystal grains during grain growth, to thereby suppress the grain growth.
  • Multi-component precipitates are preferable for the action and effect of the nucleation site for recrystallization.
  • the term "precipitate” means to include intermetallic compounds, carbides, oxides, sulfides, nitride, compounds (solid solutions), and element metals.
  • the aforementioned precipitate is not to form any solid solution in the Cu matrix even during the solution treatment. That is, the precipitate must have a melting point higher than the solution treatment temperature.
  • the precipitate is not limited to the aforementioned precipitates as long as it has a melting point higher than the solution treatment temperature. Further, the precipitate is not limited as long as it provides an effect of preventing growth of too large crystal grains during the solution treatment or forming many crystal grains (nucleation) by serving as a nucleation site for recrystallization.
  • the copper alloy of the present invention is an inexpensive, high-performance copper alloy maintaining high electrical conductivity, having excellent bending property and other favorable properties, and it is preferable for a variety of electric and electronic instruments including electronic parts, e.g. vehicle terminals/connectors, relays, and switches.
  • the grain diameter of the precipitate X composed of Ni and Si is preferably 0.001 to 0.1 ⁇ m, more preferably from 0.003 to 0.05 ⁇ m, and further preferably 0.005 to 0.02 ⁇ m.
  • the strength is not improved when the grain diameter is too small, while the bending property decreases when the grain diameter is too large.
  • the precipitate Y composed of Ni and/or Si and at least one or more selected from the group consisting of B, Al, As, Hf, Zr, Cr, Ti, C, Fe, P, In, Sb, Mn, Ta, V, S, O, N, Misch metal (MM), Co and Be;
  • the precipitate Y1 composed of Ni, Si and Cr;
  • the precipitate Y2 composed of Ni, Si and Co;
  • the precipitate Y3 composed of Ni, Si and Zr each have larger effects for fining crystal grains than Ni-Si precipitate X does, during the solid solution treatment as a heat treatment at high temperatures. Those effects become particularly large by the precipitate Y1 and the precipitate Y2. This effect acts for improving bending property.
  • this effect can contribute to improvements of the tensile strength and the stress relaxation resistance by increasing the amount of the solid solution in the copper alloy as well as the amount of precipitates during aging treatments.
  • This effect is particularly enhanced when the melting point of precipitate Y is higher than the melting point of precipitate X.
  • the melting point of precipitate X is preferably from 650 to 1,050°C, and the melting point of precipitate Y is preferably higher than the melting point of precipitate X and 1,100°C or less.
  • the grain diameter of precipitate Y is preferably 0.01 to 2.0 ⁇ m, more preferably 0.05 to 0.5 ⁇ m, and most preferably from 0.05 to 0.13 ⁇ m. This is because an effect for suppressing growth of crystal grains and an effect for increasing the number of nucleation sites are not exhibited when the grain diameter is too small, while the bending property decreases when the grain diameter is too large.
  • the grain diameter of precipitate Y is preferably larger than the grain diameter of precipitate X.
  • the ratio of the grain diameters between Y and X (Y/X) preferably exceeds 1 and 2,000 or less, more preferably 5 to 500.
  • Ni and Si are elements that can be added in a controlled addition ratio of Ni to Si for forming a Ni-Si precipitate for precipitation strengthening, to thereby enhance the mechanical strength of the copper alloy.
  • the amount of Ni to be added is generally 2.0 to 5.0 mass%, preferably 2.1 to 4.6 mass%.
  • the Ni amount is more preferably 3.5 to 4.6 mass%, for satisfying a tensile strength of 800 MPa or more and a bending property of R/t ⁇ 1.5, or a tensile strength of 900 MPa or more and a bending property of R/t ⁇ 2.
  • a too small Ni amount provides a small precipitated and hardened amount that results in insufficient mechanical strength, and a too large Ni amount results in a conspicuously low electrical conductivity.
  • the ratio of the addition amount of Ni to Si of about 1 to 4 i.e. the amount of Ni to be added being 4 vs. that of Si being about 1 in terms of mass ratio, is known to provide the largest strengthening effect.
  • the Si addition amount exceeds 1.5 mass%, it is apt to cause cracking of an ingot of the copper alloy during hot working.
  • the Si addition amount is generally 0.3 to 1.5 mass%, preferably 0.5 to 1.1 mass%, more preferably 0.8 to 1.1 mass%.
  • precipitate Y serves for suppressing crystal grains from coarsening during the solid solution treatment as described above, it is not responsible for or does not largely contribute to precipitation strengthening.
  • the content of each of the above-mentioned elements is generally 0.005 to 1.0 mass%, preferably 0.007 to 0.5 mass%, and more preferably 0.01 to 0.1 mass%. The quality of an ingot is impaired by forming large crystals during melt-casting when the amount of addition of these elements is too large, while attainment of desired effects is impossible when the amount is too small.
  • Cr, Co and Zr form precipitates in combination with main components, Ni and Si. While the effect is to suppress crystal grains from being coarsened during the solid solution treatment, to thereby control the crystal grain diameter as described above, it does not largely contribute to precipitation strengthening.
  • the amount of addition of these elements is preferably 0.005 to 1.0 mass%, more preferably 0.1 to 0.3 mass% for permitting the effect to be exhibited.
  • the quality of the ingot may be impaired by forming large crystals during melt-casting when the amount of addition of these elements is too large, while the effect of addition is not exhibited when the amount is too small.
  • B forms a precipitate with main constituents Ni and Si.
  • the effect of B as the same manner as the above Cr, Co or Zr is that B is an element for suppressing increase of the crystal grain size to become too large (giant) during the solution treatment, but B takes no part in the precipitation strengthening.
  • the B addition amount is preferably 0.005 to 0.1 mass%, more preferably 0.01 to 0.07 mass%, for exhibiting the effect.
  • a too large B addition amount results in too large crystallized product during melt-casting to cause problems in ingot quality, and a too small B addition amount provides no addition effect.
  • Zn, Sn, and/or Mg are preferably added to further improve the characteristics.
  • Zn is an element which forms a solid solution in a matrix, but Zn addition significantly alleviates solder embrittlement.
  • Zn is added preferably in an amount of 0.1 to 1.0 mass%.
  • the preferable primary uses of the alloy of the present invention are electric and electronic instruments and electronic part terminal materials such as vehicle terminals/connectors, relays, and switches. Most of them are joined by solder, and thus the enhancement of reliability in the joined portions is one of the important elemental techniques.
  • Zn addition may lower the melting point of the alloy, to control the states of formation of the precipitate composed of Ni and B and the precipitate composed of Mn and P. Both the precipitates are formed during solidification.
  • a high solidification temperature of the alloy increases the grain size, to provide a small contribution of the precipitates to the effects of suppressing increase of the crystal grain size and forming a nucleation site for the crystal grains.
  • the lower limit of Zn addition is defined as 0.1 mass%, because it is a minimum necessary amount that provides alleviations in solder embrittlement.
  • the upper limit of Zn addition is defined as 1.0 mass%, because a Zn addition amount more than 1.0 mass% may degrade the electrical conductivity.
  • Sn and Mg to be added are also preferable elements for their uses.
  • Sn and Mg addition provides an effect of improving creep resistance, which is emphasized in electronic instrument terminals/connectors.
  • the effect is also referred to as stress relaxing resistance, and it is an important characteristic that assumes reliability of the terminals/connectors.
  • Solely addition of Sn or Mg may improve the creep resistance, but the use in combination of Sn and Mg can further improve the creep resistance by a synergetic effect.
  • the lower limit of Sn addition is defined as 0.1 mass%, because it is a minimum necessary amount that provides improvements in creep resistance.
  • the upper limit of Sn addition is defined as 1 mass%, because a Sn addition amount more than 1 mass% may degrade the electrical conductivity.
  • the lower limit of Mg addition is defined as 0.05 mass%, because an addition amount of Mg less than 0.05 mass% provides no effect of improving the creep resistance.
  • the upper limit of Mg addition is defined as 0.5 mass%, because an Mg addition amount of more than 0.5 mass% not only saturates the effect. Further, when an Mg addition amount is more than 0.5 mass%, it may degrade hot-workability at a particularly-high temperature, depending on the composition of the alloy.
  • Sn and Mg have a function of accelerating formation of a precipitate composed of Ni and Si. It is important to add preferable amounts of these Sn and Mg, serving as fine nucleation sites for the precipitate.
  • the number of precipitate X per mm 2 on an arbitrary cross section in the copper alloy is preferably 20 to 2,000 times the number of corresponding precipitate Y per mm 2 . This is because the bending property is particularly enhanced among the characteristics, and a sufficient mechanical strength can be obtained.
  • the number of the precipitate X is more preferably 100 to 1,500 times the number of the precipitate Y.
  • the number of precipitates X is preferably 10 8 to 10 12 per mm 2
  • the number of precipitates Y that correspond to the precipitates X is preferably 10 4 to 10 8 per mm 2 . This is because the aforementioned ranges provide particularly excellent bending property. If the number of precipitates is too small, the resultant alloy may not have a targeted mechanical strength. On the other hand, if the number of precipitates is too large, the resultant alloy may be poor in bending property.
  • the number of precipitates X is more preferably 5 ⁇ 10 9 to 6 ⁇ 10 11 per mm 2
  • the number of precipitates Y is more preferably 10 4 to 4 ⁇ 10 7 per mm 2 . The effect of precipitates becomes remarkable as the amounts of Ni and Si are increased.
  • a tensile strength of 800 MPa or more with the bending property of R/t ⁇ 2.0, or a tensile strength of 700 MPa or more with the bending property of R/t ⁇ 1.0 may be attained, by controlling the number of precipitates Y as described above. It is also possible to attain a tensile strength of 800 MPa or more with the bending property of R/t ⁇ 1.5, or a tensile strength of 900 MPa or more with the bending property of R/t ⁇ 2.
  • the stress relaxation ratio of the copper alloy is preferably less than 20%, more preferably less than 18%, and further preferably 15% or less, in which an open-sided block method prescribed in the Standard of the Electronic Materials Manufacturers Association of Japan (EMAS-3003) is employed with load stress set to be a surface maximum stress of 80%-yield strength (80%-YS, 0.2%-proof stress), and the stress relaxation ratio is measured under the conditions of at 150°C for 1,000 hours.
  • the number of precipitates is represented by an average number per unit area.
  • the copper alloy of the present invention may have a crystal grain diameter (i.e. an average of a minor axis diameter and a major axis diameter) of generally 20 ⁇ m or less, preferably 10.0 ⁇ m or less. If the crystal grain diameter is longer than 10.0 ⁇ m, it may be impossible to obtain a tensile strength of 720 MPa or more and a bending property of R/t ⁇ 2. More preferably, the crystal grain diameter of the copper alloy is 8.5 ⁇ m or less. The lower limit of the crystal grain diameter may be generally 0.5 ⁇ m or more.
  • the aforementioned crystal grain diameters are measured in the following manner:
  • the crystal grain diameters are measured in two directions parallel to or perpendicular to the finally cold-rolled direction, respectively, on cross sections parallel to the direction of thickness of the alloy sheet and parallel to the finally cold-rolled direction (the direction of the final plastic-working), thereby to determine larger lengths as major axis diameters and smaller lengths as minor axis diameters in respective directions.
  • An average value of each four lengths of the major axis diameters and minor axis diameters is rounded up as a product of multiplying 0.005 mm times an integer, to determine the crystal grain diameter.
  • a specific example of a preferable production method for the copper alloy according to the present invention involves: melting a copper alloy having the aforementioned preferable element composition; casting into an ingot; and hot-rolling the ingot. More specifically, the production method involves: heating the ingot at a temperature rising rate of 20 to 200°C/hr; holding the resultant ingot at 850 to 1,050°C for 0.5 to 5 hours; hot-rolling; and, after finishing the hot-rolling at a finishing temperature of 300 to 700°C, quenching the hot-rolled product. In this way, the precipitate X, and the precipitate Y corresponding to the element composition are formed.
  • the resultant alloy is formed into a given thickness, through a combination of solution treatment, annealing, and cold-rolling.
  • the purpose of the solution treatment is to allow Ni and Si precipitated during casting or hot-rolling, to form a solid solution again and to recrystallize at the same time. This permits the amount of the elements in the solid solution to be increased and accumulated distortion during working to be removed, and a basic treatment for improving the strength and bending property can be provided.
  • the temperature of the solution treatment may be adjusted according to a Ni addition amount.
  • the solution treatment temperature is preferably 600 to 820°C for an Ni amount of 2.0 mass% or more but less than 2.5 mass%, 700 to 870°C for an Ni amount of 2.5 mass% or more but less than 3.0 mass%, 750 to 920°C for an Ni amount of 3.0 mass% or more but less than 3.5 mass%, 800 to 970°C for an Ni amount of 3.5 mass% or more but less than 4.0 mass%, 850 to 1,020°C for an Ni amount of 4.0 mass% or more but less than 4.5 mass%, and 920 to 1,050°C for an Ni amount of from 4.5 mass% or more but less than 5.0 mass%.
  • the amount of elements in the solid solution is increased by applying the solid solution treatment at higher temperatures, to thereby enable a high strength to be obtained.
  • the heat treatment at 900°C of an alloy material composed of Ni 3.0 mass% and Si 0.7 mass% allows sufficient Ni-Si precipitates that have already been precipitated, to form again the solid solution.
  • the size of the crystal grain far exceeds 10 ⁇ m, and the bending property is conspicuously decreased.
  • crystal grains with a size of 10 ⁇ m or less may be obtained, even by a solid solution treatment at 900°C, from an alloy material to which any one of Cr, Co, Zr, and B is further added.
  • the heat treatment at 850°C of an alloy material whose Ni content is 3.0 mass% and Si content is 0.7 mass% allows sufficiently precipitated Ni and Si, to form again the solid solution and thereby to give crystal grains of 10 ⁇ m or less.
  • the heat treatment at the same temperature of an alloy having a too small Ni amount causes growth of crystal grains into too large grains to thereby fail in obtaining a grain size of 10 ⁇ m or less.
  • a too large Ni amount may not provide an ideal solution state, and the mechanical strength may not be enhanced through the subsequent aging treatment.
  • the size of the precipitate (e.g. precipitate Y) may be changed, by changing the conditions of the solid solution treatment, i.e.
  • the temperature of the solid solution treatment by appropriately selecting the temperature of the solid solution treatment, as described above. For example, a higher temperature of the solid solution treatment (a temperature higher by 50°C than a standard temperature) is selected for the heat treatment when the size of precipitate Y1 is to be increased, while a lower temperature of solid solution treatment (a temperature lower by 50°C than a standard temperature) is selected for the heat treatment when the size of precipitate Y1 is to be decreased.
  • the change of the density is coupled with the change of the crystal grain size, and the density becomes lower as the size is larger, while the density becomes higher as the size is smaller.
  • the copper alloy of the present invention apparently provides improvement in, in particular, bending property, and optionally stress relaxation resistance, of a high strength copper alloy having a tensile strength of 800 MPa or more, while high electrical conductivity is maintained. Further, the copper alloy of the present invention provides similar improvement in bending property of a copper alloy having a tensile strength of less than 800 MPa.
  • the copper alloy according to the present invention is also excellent in other properties, such as spring property and the like.
  • the resultant ingot was subjected to hot-rolling, to give a hot-rolled sheet with a sheet thickness (t) of 12 mm, each of the surfaces of the sheet was chamfered by 1 mm, to adjust the thickness (t) at 10 mm, and then the sheet was finished at a thickness (t) of 0.167 mm by cold-rolling.
  • the sheet material was then subjected to solid solution treatment. The temperature of the solid solution treatment was selected, in accordance with the conditions described in the foregoing paragraph [0026].
  • a higher solid solution treatment temperature (a temperature higher by 50°C than a standard temperature) was selected when the size of precipitate Y1 was to be increased, while a lower solid solution temperature (a temperature lower by 50°C than a standard temperature) was selected when the size of precipitate Y1 was to be decreased, for conducting the heat treatment.
  • the change of the density was coupled with the change of the crystal grain size, and the density became lower as the size was larger, while the density became higher as the size was smaller.
  • the samples according to the present invention have excellent properties in both of the mechanical strength and the bending property.
  • the samples in Comparative examples 100, 101, 102 and 103 each were poor in the bending property, as compared with the samples in the examples according to the present invention having the same level of mechanical strength, and the mechanical strength in the comparative examples was not compatible to the bending property.
  • the bending property (R/t) while high strength is maintained, by controlling the grain diameter of precipitate Y1 in the Cu alloy system containing Ni, Si, and Cr.
  • the copper alloys of the examples according to the present invention can be considered to be favorable for materials of lead frames or the like. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property.
  • Example 3 With respect to the copper alloys containing the elements in the amounts, as shown in Table 3, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1, except that the measurement was made on the precipitate Y2 in place of the precipitate Y1. The results are shown in Table 4. The production and measurement methods were also performed in the same manner as in Example 1.
  • the samples according to the present invention have excellent properties in both of the mechanical strength and the bending property.
  • the samples in Comparative examples 105, 106, 107 and 108 each were poor in the bending property, as compared with the samples in the examples according to the present invention having the same level of mechanical strength, and the mechanical strength in the comparative examples was not compatible to the bending property.
  • the bending property (R/t) while high strength is maintained, by controlling the grain diameter of precipitate Y2 in the Cu alloy system containing Ni, Si, and Co.
  • the copper alloys of the examples according to the present invention can be considered to be favorable for materials of lead frames or the like. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property.
  • Example 5 With respect to the copper alloys containing the elements in the amounts, as shown in Table 5, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1, except that the measurement was made on the precipitate Y3 in place of the precipitate Y1. The results are shown in Table 6. The production and measurement methods were also performed in the same manner as in Example 1.
  • the samples according to the present invention have excellent properties in both of the mechanical strength and the bending property.
  • the samples in Comparative examples 109, 110, 111 and 112 each were poor in the bending property, as compared with the samples in the examples according to the present invention having the same level of mechanical strength, and the mechanical strength in the comparative examples was not compatible to the bending property.
  • the bending property (R/t) while high strength is maintained, by controlling the grain diameter of precipitate Y3 in the Cu alloy system containing Ni, Si, and Zr.
  • the copper alloys of the examples according to the present invention can be considered to be favorable for materials of lead frames or the like. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property.
  • Example 7 With respect to the copper alloys containing the elements in the amounts, as shown in Table 7, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1, except that the measurement was made on the precipitate Z in place of the precipitate Y1. The results are shown in Table 8. The production and measurement methods were also performed in the same manner as in Example 1.
  • the samples according to the present invention have excellent properties in both of the mechanical strength and the bending property.
  • the samples in Comparative examples 113, 114, 115 and 116 each were poor in the bending property, as compared with the samples in the examples according to the present invention having the same level of mechanical strength, and the mechanical strength in the comparative examples was not compatible to the bending property.
  • the bending property (R/t) while high strength is maintained, by controlling the grain diameter of precipitate Z in the Cu alloy containing Ni, Si, and B.
  • the copper alloys of the examples according to the present invention can be considered to be favorable for materials of lead frames or the like. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property.
  • Example 9 With respect to the copper alloys containing the elements in the amounts, as shown in Table 9, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1, except that the measurement was made on the precipitate Y2, Y3 or Z in place of a part of the precipitate Y1. The results are shown in Table 10. The production and measurement methods were also performed in the same manner as in Example 1.
  • the samples according to the present invention have excellent properties in both of the mechanical strength and the bending property.
  • the grain diameter of precipitate Y1, Y2, Y3 or Z was outside of the range defined in the present invention
  • the samples in Comparative examples 117, 118, 119, 120, 121 and 122 each were poor in the bending property, as compared with the samples in the examples according to the present invention having the same level of mechanical strength, and the mechanical strength in the comparative examples was not compatible to the bending property.
  • the bending property (R/t) while high strength is maintained, by controlling the grain diameter of precipitate Y1 or the like.
  • the copper alloys of the examples according to the present invention can be considered to be favorable for materials of lead frames or the like. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property.
  • Example 11 With respect to the copper alloys containing Ni, Si, and elements in the given amounts as shown in Table 11, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1.
  • the contents of Ni and Si were as follows: 3.5 mass% of Ni and 0.8 mass% of Si in the samples of Examples according to the present invention Nos. 1-4 and 1-11; 4.0 mass% of Ni and 0.95 mass% of Si in the sample of Example according to the present invention No. 1-6; and 3.8 mass% of Ni and 0.86 mass% of Si in the samples of other Examples according to the present invention and Comparative examples.
  • the production and measurement methods for the samples were also performed in the same manner as in Example 1. Further, the stress relaxation resistance was evaluated by the following manner.
  • GW denotes bending with a bend axis perpendicular to the direction of rolling, by using a test piece sampled in parallel to the direction of rolling; and BW denotes bending with a bend axis parallel to the direction of rolling, by using a test piece sampled perpendicular to the direction of rolling.
  • GW means that the longitudinal direction of the test piece is parallel to the direction of rolling, and BW means that the longitudinal direction of the test piece is perpendicular to the direction of rolling.
  • the samples according to the present invention each have excellent properties with respect to the mechanical strength, electrical conductivity, bending property, and stress relaxation resistance.
  • the grain size of Y within the range from 0.02 to 0.9 ⁇ m, it was possible to attain a good stress relaxation ratio, which was a stress relaxation ratio of 13% or less, while maintaining excellent mechanical strength, electrical conductivity, and bending property.
  • the alloys of the examples according to the present invention can be considered to be favorable, for example, for materials of terminals and connectors.
  • the similar effects can be exhibited when the grain size of Y is within the range from 0.01 to 2.0 ⁇ m.
  • the sample in Comparative example 1-1 was poor in the mechanical strength and the stress relaxation resistance.
  • the sample in Comparative example 1-2 was poor in the stress relaxation resistance.
  • the amount of P was too large
  • the sample in Comparative example 1-3 was poor in the stress relaxation resistance.
  • the sample in Comparative example 1-4 was poor in the bending property and the stress relaxation resistance.
  • the sample in Comparative example 1-5 was poor in the stress relaxation resistance. Since the grain size of precipitate Y was too small, the sample in Comparative example 1-6 was poor in the stress relaxation resistance.
  • Table 11 Component Precipitate X Precipitate Y Number of X/ number of Y TS EC Bending property SRR ⁇ Size Density Composition Size Density GW BW mass% ⁇ m /mm 2 Compound ⁇ m /mm 2 MPa %IACS R/t R/t %
  • 1-1 Cr 0.2 0.03 3 x 10 9 Ni-Si-Cr 0.2 2 x 10 7 150 862 36 1.0 1.0 9
  • This invention 1-3 B 0.008 0.04 1 x 10 10 Ni-Si-B 0.8 2 x 10 9 5 833 40 1.5 1.0 12
  • Example 12 With respect to the copper alloys containing Ni, Si, and elements in the given amounts as shown in Table 12, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1.
  • the contents of Ni and Si were as follows: 3.5 mass% of Ni and 0.8 mass% of Si in the samples of Examples according to the present invention Nos. 2-4 and 2-11; 4.0 mass% of Ni and 0.95 mass% of Si in the sample of Example according to the present invention No. 2-2; and 3.8 mass% of Ni and 0.86 mass% of Si in the samples of other Examples according to the present invention and Comparative examples.
  • the production and measurement methods for the samples were also performed in the same manner as in Example 1. Further, the stress relaxation resistance was evaluated in the same manner as in Example 6.
  • the samples according to the present invention each have excellent properties with respect to the mechanical strength, electrical conductivity, bending property, and stress relaxation resistance.
  • the examples according to the present invention by making the grain size of Y within the range from 0.05 to 0.9 ⁇ m, it was possible to attain a stress relaxation ratio of 14% or less, while maintaining excellent mechanical strength, electrical conductivity, and bending property.
  • the copper alloys of the examples according to the present invention can be considered to be favorable, for example, for materials of terminals and connectors. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property. Contrary to the above, since the values of the precipitates Y were outside of the range of from 0.01 to 2.0 ⁇ m, the samples in Comparative examples each were poor in the stress relaxation ratio of 21% or more.
  • Table 12 Component Precipitate X Precipitate Y Number of X/ number of Y TS EC Bending property SRR ⁇ ⁇ Size Density Composition Size Density GW BW mass% mass% ⁇ m /mm 2 Compound ⁇ m /mm 2 MPa %IACS R/t R/t %
  • Example 13 With respect to the copper alloys containing Ni, Si, and elements in the given amounts as shown in Table 13, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1.
  • the contents of Ni and Si were as follows: 3.5 mass% of Ni and 0.8 mass% of Si in the samples of Examples according to the present invention Nos. 3-4 and 3-11; 4.0 mass% of Ni and 0.95 mass% of Si in the samples of Examples according to the present invention Nos. 3-8 and 3-15; and 3.8 mass% of Ni and 0.86 mass% of Si in the samples of other Examples according to the present invention and Comparative examples.
  • the production and measurement methods for the samples were also performed in the same manner as in Example 1. Further, the stress relaxation resistance was evaluated in the same manner as in Example 6.
  • the samples according to the present invention each have excellent properties with respect to the mechanical strength, electrical conductivity, bending property, and stress relaxation resistance.
  • the examples according to the present invention by making the grain size of Y within the range from 0.2 to 0.6 ⁇ m, it was possible to attain a stress relaxation ratio of 15% or less, while maintaining excellent mechanical strength, bending property, and electrical conductivity.
  • the copper alloys of the examples according to the present invention can be considered to be favorable, for example, for materials of terminals and connectors. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property. Contrary to the above, since the values of the precipitates Y were outside of the range of from 0.01 to 2.0 ⁇ m, the samples in Comparative examples each were poor in the stress relaxation ratio of 21% or more.
  • Table 13 Component Precipitate X Precipitate Y Number of X/ number of Y TS EC Bending property SRR ⁇ ⁇ Size Density Composition Size Density GW BW mass% mass% ⁇ m /mm 2 Compound ⁇ m /mm 2 MPa %IACS R/t R/t %
  • This invention 3-5 MM 0.005
  • Example 14 With respect to the copper alloys containing Ni, Si, and elements in the given amounts as shown in Table 14, with the balance being made of Cu and inevitable impurities, the test was conducted in the same manner as in Example 1.
  • the contents of Ni and Si were as follows: 3.5 mass% of Ni and 0.8 mass% of Si in the samples of Examples according to the present invention Nos. 4-1 and 4-4; 4.0 mass% of Ni and 0.95 mass% of Si in the samples of Examples according to the present invention Nos. 4-2 and 4-9; and 3.8 mass% of Ni and 0.86 mass% of Si in the samples of other Examples according to the present invention and Comparative examples.
  • the production and measurement methods for the samples were also performed in the same manner as in Example 1. Further, the stress relaxation resistance was evaluated in the same manner as in Example 6.
  • the samples according to the present invention each have excellent properties with respect to the mechanical strength, electrical conductivity, bending property, and stress relaxation resistance.
  • the examples according to the present invention by making the grain size of Y within the range from 0.1 to 0.6 ⁇ m, it was possible to attain a stress relaxation ratio of 15% or less, while maintaining excellent mechanical strength, bending property, and electrical conductivity.
  • the copper alloys of the examples according to the present invention can be considered to be favorable, for example, for materials of terminals and connectors. Further, the copper alloys of the examples according to the present invention are also excellent in other properties, such as spring property. Contrary to the above, since the values of the precipitates Y were outside of the range of from 0.01 to 2.0 ⁇ m, the samples in Comparative examples each were poor in the stress relaxation ratio of 21% or more.
  • Table 14 Component Precipitate X Precipitate Y Number of X/ number of Y TS EC Bending property SRR ⁇ ⁇ ⁇ Size Density Composition Size Density GW BW mass% mass% mass% ⁇ m /mm 2 Compound ⁇ m /mm 2 MPa %IACS R/t R/t %
  • the copper alloy of the present invention can be preferably applied, for example, to lead frame, connector, or terminal materials for electric and electronic instrument materials, e.g. connector/terminal materials, relays, and switches for electric and electronic instruments, such as on-vehicle/automobile electric and electronic instruments.
  • electric and electronic instrument materials e.g. connector/terminal materials, relays, and switches for electric and electronic instruments, such as on-vehicle/automobile electric and electronic instruments.

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2221391A1 (de) * 2007-11-05 2010-08-25 The Furukawa Electric Co., Ltd. Kupferlegierungsblechmaterial
EP2256219A1 (de) * 2008-02-18 2010-12-01 The Furukawa Electric Co., Ltd. Kupferlegierungswerkstoff
RU2566097C1 (ru) * 2014-12-22 2015-10-20 Юлия Алексеевна Щепочкина Сплав на основе меди
US9460825B2 (en) 2010-05-31 2016-10-04 Jx Nippon Mining & Metals Corporation Cu-Co-Si-based copper alloy for electronic materials, and method of manufacturing same
US10056166B2 (en) 2010-08-24 2018-08-21 Jx Nippon Mining & Metals Corporation Copper-cobalt-silicon alloy for electrode material
RU2677902C1 (ru) * 2017-12-27 2019-01-22 Федеральное государственное автономное образовательное учреждение высшего образования "Белгородский государственный национальный исследовательский университет" (НИУ "БелГУ") Высокопрочный медный сплав

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4357536B2 (ja) * 2007-02-16 2009-11-04 株式会社神戸製鋼所 強度と成形性に優れる電気電子部品用銅合金板
TWI395824B (zh) * 2007-03-30 2013-05-11 Jx Nippon Mining & Metals Corp Cu-Ni-Si alloy for electronic materials
US8287669B2 (en) 2007-05-31 2012-10-16 The Furukawa Electric Co., Ltd. Copper alloy for electric and electronic equipments
EP2330231B1 (de) * 2008-09-30 2017-02-22 JX Nippon Mining & Metals Corporation Verfahren zur herstellung einer zerstäubungsquelle für hochreines kupfer oder für eine hochreine kupferlegierung
US20110123389A1 (en) 2008-09-30 2011-05-26 Jx Nippon Mining & Metals Corporation High Purity Copper and Method of Producing High Purity Copper Based on Electrolysis
JP5261161B2 (ja) * 2008-12-12 2013-08-14 Jx日鉱日石金属株式会社 Ni−Si−Co系銅合金及びその製造方法
WO2012081573A1 (ja) * 2010-12-13 2012-06-21 国立大学法人東北大学 銅合金及び銅合金の製造方法
TWI440727B (zh) * 2010-12-13 2014-06-11 Nippon Seisen Co Ltd 銅合金線及銅合金彈簧
CN102140594B (zh) * 2011-03-11 2012-10-03 无锡日月合金材料有限公司 一种高强高导高韧铜合金及其制备方法
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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04180531A (ja) * 1990-11-14 1992-06-26 Nikko Kyodo Co Ltd 通電材料
US5846346A (en) * 1995-12-08 1998-12-08 Poongsan Corporation High strength high conductivity Cu-alloy of precipitate growth suppression type and production process
EP0949343A1 (de) * 1998-03-26 1999-10-13 KABUSHIKI KAISHA KOBE SEIKO SHO also known as Kobe Steel Ltd. Bleche aus Kupferlegierung für Elektronikbauteile
US20040079456A1 (en) * 2002-07-02 2004-04-29 Onlin Corporation Copper alloy containing cobalt, nickel and silicon
JP2004307905A (ja) * 2003-04-03 2004-11-04 Sumitomo Metal Ind Ltd Cu合金およびその製造方法
US20050028907A1 (en) * 2002-03-12 2005-02-10 The Furukawa Electric Co., Ltd. High-strength, high-conductivity copper alloy wire excellent in resistance to stress relaxation
JP2005048262A (ja) * 2003-07-31 2005-02-24 Nikko Metal Manufacturing Co Ltd 疲労特性に優れたCu−Ni−Si系合金

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6376839A (ja) * 1986-09-18 1988-04-07 Furukawa Electric Co Ltd:The 電子機器用銅合金とその製造法
DE3773470D1 (de) * 1986-11-13 1991-11-07 Ngk Insulators Ltd Herstellung von kupfer-berylliumlegierungen.
JPH0830234B2 (ja) * 1987-07-24 1996-03-27 古河電気工業株式会社 高力高導電性銅合金
JP3520046B2 (ja) * 2000-12-15 2004-04-19 古河電気工業株式会社 高強度銅合金
US20050236074A1 (en) * 2004-02-27 2005-10-27 Kuniteru Mihara Copper alloy
JP4646192B2 (ja) * 2004-06-02 2011-03-09 古河電気工業株式会社 電気電子機器用銅合金材料およびその製造方法

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04180531A (ja) * 1990-11-14 1992-06-26 Nikko Kyodo Co Ltd 通電材料
US5846346A (en) * 1995-12-08 1998-12-08 Poongsan Corporation High strength high conductivity Cu-alloy of precipitate growth suppression type and production process
EP0949343A1 (de) * 1998-03-26 1999-10-13 KABUSHIKI KAISHA KOBE SEIKO SHO also known as Kobe Steel Ltd. Bleche aus Kupferlegierung für Elektronikbauteile
US20050028907A1 (en) * 2002-03-12 2005-02-10 The Furukawa Electric Co., Ltd. High-strength, high-conductivity copper alloy wire excellent in resistance to stress relaxation
US20040079456A1 (en) * 2002-07-02 2004-04-29 Onlin Corporation Copper alloy containing cobalt, nickel and silicon
JP2004307905A (ja) * 2003-04-03 2004-11-04 Sumitomo Metal Ind Ltd Cu合金およびその製造方法
JP2005048262A (ja) * 2003-07-31 2005-02-24 Nikko Metal Manufacturing Co Ltd 疲労特性に優れたCu−Ni−Si系合金

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO2006093140A1 *

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2221391A1 (de) * 2007-11-05 2010-08-25 The Furukawa Electric Co., Ltd. Kupferlegierungsblechmaterial
EP2221391A4 (de) * 2007-11-05 2012-06-27 Furukawa Electric Co Ltd Kupferlegierungsblechmaterial
EP2256219A1 (de) * 2008-02-18 2010-12-01 The Furukawa Electric Co., Ltd. Kupferlegierungswerkstoff
EP2256219A4 (de) * 2008-02-18 2012-06-27 Furukawa Electric Co Ltd Kupferlegierungswerkstoff
US9460825B2 (en) 2010-05-31 2016-10-04 Jx Nippon Mining & Metals Corporation Cu-Co-Si-based copper alloy for electronic materials, and method of manufacturing same
US10056166B2 (en) 2010-08-24 2018-08-21 Jx Nippon Mining & Metals Corporation Copper-cobalt-silicon alloy for electrode material
RU2566097C1 (ru) * 2014-12-22 2015-10-20 Юлия Алексеевна Щепочкина Сплав на основе меди
RU2677902C1 (ru) * 2017-12-27 2019-01-22 Федеральное государственное автономное образовательное учреждение высшего образования "Белгородский государственный национальный исследовательский университет" (НИУ "БелГУ") Высокопрочный медный сплав

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