EP2154257B1 - Cu-ni-si-based alloy for electronic material - Google Patents

Cu-ni-si-based alloy for electronic material Download PDF

Info

Publication number
EP2154257B1
EP2154257B1 EP08739256.9A EP08739256A EP2154257B1 EP 2154257 B1 EP2154257 B1 EP 2154257B1 EP 08739256 A EP08739256 A EP 08739256A EP 2154257 B1 EP2154257 B1 EP 2154257B1
Authority
EP
European Patent Office
Prior art keywords
mass
particles
compounds
strength
alloy
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP08739256.9A
Other languages
German (de)
French (fr)
Other versions
EP2154257A1 (en
EP2154257A4 (en
Inventor
Naohiko Era
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
JX Nippon Mining and Metals Corp
Original Assignee
JX Nippon Mining and Metals Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JX Nippon Mining and Metals Corp filed Critical JX Nippon Mining and Metals Corp
Publication of EP2154257A1 publication Critical patent/EP2154257A1/en
Publication of EP2154257A4 publication Critical patent/EP2154257A4/en
Application granted granted Critical
Publication of EP2154257B1 publication Critical patent/EP2154257B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/02Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working in inert or controlled atmosphere or vacuum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/08Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B1/00Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
    • H01B1/02Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B1/00Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
    • H01B1/02Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
    • H01B1/026Alloys based on copper
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B5/00Non-insulated conductors or conductive bodies characterised by their form
    • H01B5/02Single bars, rods, wires, or strips

Definitions

  • the present invention relates to precipitation hardening copper alloys, and in particular, to Cu-Ni-Si-Cr system alloys suitable for use in components for various electronic devices.
  • Copper alloys for electronic materials used in components for various electronic devices such as lead frames, connectors, pins, terminals, relays, and switches must satisfy both high strength and high electrical conductivity (or high thermal conductivity) as basic characteristics. Recent rapid advances of high integration and reductions in size and thickness of electronic components have accelerated requirements for higher performances of copper alloys used in components for electronic devices.
  • Corson alloys are typical copper alloys having compatibility of relatively high electrical conductivity and strength, proper stress relaxation, and excellent bendability. Corson alloys are now being actively developed in the industry. In such copper alloys, fine particles of a NiSi intermetallic compound are precipitated in a copper matrix, thereby improving strength and electrical conductivity.
  • NiSi intermetallic compound generally has a stoichiometric composition.
  • Japanese Unexamined Patent Application Publication No. 2001-207229 discloses that satisfactory electrical conductivity is achieved by bringing the mass ratio Ni/Si in an alloy close to the mass composition ratio of the intermetallic compound Ni 2 Si [(Ni atomic weight) ⁇ 2/(Si atomic weight) ⁇ 1)], i.e. a weight concentration ratio of Ni/Si in the range of 3 to 7.
  • Japanese Patent Nos. 2862942 and 3049137 discloses a method of heat treatment of a Corson alloy containing 1.5-4.0% by weight of Ni, 0.35-1.0% by weight of Si, optionally 0.05-1.0% by weight of at least one metal selected from the group consisting of Zr, Cr, and Sn, and the balance being Cu and incidental impurities, wherein the Corson alloy is heated (or cooled) in the temperature range of 400 to 800°C, so as to reduce the tensile thermal strain of the Corson alloy to a level not exceeding 1 ⁇ 10 -4 .
  • the patent states that the method can prevent an ingot from cracking during the heat treatment.
  • Japanese Patent No. 3049137 discloses a high strength copper alloy containing 2-5% by weight of Ni, 0.5-1.5% by weight of Si, 0.1-2% by weight of Zn, 0.01-0.1% by weight of Mn, 0.001-0.1% by weight of Cr, 0.001-0.15% by weight of Al, 0.05-2% by weight of Co, not more than 15 ppm of S as an impurity, and the balance being Cu and incidental impurities.
  • This copper alloy exhibits excellent bendability.
  • Cr is an element which reinforces grain boundaries in an ingot and leads to an improvement in hot workability. It also states that a Cr content exceeding 0.1% by weight causes oxidation of molten metal and poor casting performance.
  • the copper alloy is covered with charcoal in a cryptol furnace to be melted and cast in the atmosphere.
  • a compound of Cr and Si is disclosed in Japanese Unexamined Patent Application Publication No. 2005-113180 .
  • This patent refers to the hot working temperature and heat treatment temperature for age hardening of an ingot of a copper alloy having excellent etching and punching workability for electronic devices.
  • the copper alloy contains 0.1-0.25% by weight of Cr, 0.005-0.1% by weight of Si, 0.1-0.5% by weight of Zn, 0.05-0.5% by weight of Sn, and the balance being Cu and incidental impurities, wherein the weight ratio Cr/Si is in the range of 3 to 25, particles of Cr-Si compounds having a size of 0.05 ⁇ m to 10 ⁇ m are present in a number density of 1 ⁇ 10 3 to 5 ⁇ 10 5 /mm 2 in the copper matrix while particles of Cr compounds (other than the Cr-Si compound) having a size greater than 10 ⁇ m are not present. According to this method, both etching and punching workability are preferably available.
  • Japanese Unexamined Patent Application Publication No. 2005-113180 discloses that etching and punching workabilities are improved by controlling the number density and size of the Cr-Si compounds, consideration is focused on the conditions for the formation of the Cr-Si compounds and no consideration is paid for the formation of NiSi compounds because no Ni is added. Accordingly, Japanese Unexamined Patent Application Publication No. 2005-113180 also does not suggest the solution achieved by the present invention.
  • An object of the present invention is to provide a Corson alloy having significantly improved characteristics, i.e. high strength and high electrical conductivity, by enhancing the effect of Cr contained in a Cu-Ni-Si system alloy.
  • the inventors have accomplished an invention as described below.
  • the Si content is in excess of the Ni content so that nickel silicide is surely precipitated from the contained Ni in order to improve the strength, while the excess Si is combined with the contained Cr to achieve high conductivity of the alloy.
  • the essence of the present invention is to control the excess growth of particles of Cr-Si compounds so as to prevent a shortage of Si, which combines with Ni.
  • the inventors have found that the control of the temperature and cooling rate of the heat treatment can enhance such effects, through investigation on the preferred composition, size, and number density of particles of the Cr-Si compounds.
  • the present invention includes the following Aspects:
  • the present invention can provide the Corson copper alloy having significantly improved strength and electrical conductivity suitable for electronic materials due to the positive effect of Cr, which is an element contained in the alloy.
  • Ni and Si form nickel silicides (e.g. Ni 2 Si) as an intermetallic compound through suitable heat treatment, resulting in high strength without a decrease in conductivity.
  • the mass ratio of Ni to Si is preferably close to the stoichiometric ratio as described above, i.e. 3 ⁇ Ni/Si ⁇ 5.5, more preferably 3.5 ⁇ Ni/Si ⁇ 5.0.
  • the ratio Ni/Si is within the range, desired strength is not achieved at a Si content of less than 0.5% by mass. Furthermore, a Si content of more than 1.2% by mass is not preferred because of significantly reduced conductivity and poor hot workability due to formation of a liquid phase in a segregation region, despite enhanced strength. As a result, the preferred Si content is in the range of 0.5% to 1.2% by mass, preferably 0.5% to 0.8% by mass.
  • the amount ofNi to be added may be determined so as to satisfy the preferable ratio described above.
  • the suitable Ni content is in the range of 2.5% to 4.5% by mass, preferably 3.2% to 4.2% by mass, more preferably 3.5% to 4.0% by mass.
  • particles primarily composed of elemental Cr having a bcc structure are readily precipitated as well as particles of Cr-Si compounds.
  • Cr can easily precipitate chromium silicides (e.g. Cr 3 Si) in the copper matrix through proper heat treatment, the dissolved Si component, which has not precipitated in the form such as Ni 2 Si during a combined process of solution treatment, cold rolling and aging, can be precipitated as Cr-Si compounds. This process can suppress a reduction in conductivity caused by the dissolved Si and thus achieve high conductivity without a reduction in strength.
  • a low concentration of Si in Cr particles leads to residual Si in the matrix, resulting in a reduction in conductivity.
  • a high concentration of Si in Cr particles causes a decreased concentration of Si contributing to precipitation of particles of a NiSi compound, resulting in a reduction in strength.
  • a high concentration of Si in Cr particles accelerates formation of coarse Cr-Si particles, resulting in decreases in bendability and fatigue strength.
  • a lower cooling rate after solution treatment and excess heating treatment for aging cause coarsening of particles of the Cr-Si compounds. This causes a decrease in Si concentration necessary for formation of a NiSi compound and thus precludes the formation of a NiSi compound contributing to strength. This is because diffusion rates in Cu of Si and Cr are higher than that of Ni, which accelerates coarsening of particles of the Cr-Si compounds. The precipitation rate of Cr-Si compounds is thus higher than that of NiSi compounds.
  • the composition, size and density of particles of the Cr-Si compounds can, therefore, be controlled by regulating the cooling rate after solution treatment and avoiding severer aging conditions such as higher temperature and longer time than the optimum conditions for maximum strength. Consequently, the Cr concentration should be 0.003% by mass to 0.3% by mass, and the atomic ratio of Cr to Si in Cr-Si compounds should be in the range of 1 to 5.
  • Cr is preferentially precipitated at crystal grain boundaries in the cooling process after melting and casting, it can strengthen the grain boundaries. As a result, cracking during hot working can be reduced, and thus a high yield can be achieved.
  • Cr precipitated at grain boundaries after melting and casting is redissolved during the solution treatment, it forms silicides during the subsequent age precipitation process.
  • part of the added Si does not contribute to age precipitation and remains dissolved in the matrix, obstructing an increase in conductivity.
  • the conductivity can be increased without a reduction in strength, compared to conventional Cu-Ni-Si system alloys.
  • the size of particles of the Cr-Si compounds has an effect on bendability and fatigue strength.
  • the particles of the Cr-Si compounds have a size of greater than 5 ⁇ m or when the dispersion density of particles of the Cr-Si compounds having a size in the range of 0.1 to 5 ⁇ m exceeds 1 ⁇ 10 6 /mm 2 , the bendability and the fatigue strength are significantly reduced.
  • the upper limit of the dispersion density is 1 ⁇ 10 6 /mm 2 , preferably 5 ⁇ 10 5 /mm 2 , more preferably 1 ⁇ 10 5 /mm 2 .
  • the density be more than 1 ⁇ 10 4 /mm 2 , in order to achieve the significant effect of the addition of Cr.
  • Addition of at least one element selected from Sn and Zn in a total amount of 0.05-2.0% by mass to the Cu-Ni-Si system alloy of the present invention can improve stress relaxation and other characteristics without significant reductions in strength and conductivity.
  • An amount of less than 0.05% by mass leads to insufficient effect of addition.
  • an amount of more than 2.0% by mass causes poor production characteristics such as castability and hot workability and low conductivity of the products. It is therefore preferred that the amount of these elements should be added from 0.05% by mass to 2.0% by mass.
  • Addition of appropriate amounts of Mg, Mn, Ag, P, As, Sb, Be, B, Ti, Zr, Al, Co and Fe brings about various effects that are complementary to each other, for example, enhanced strength and conductivity, and improved production characteristics such as bendability, plating property, and hot workability of an ingot due to the formation of a fine microstructure. Accordingly, at least one element selected from these elements may be added as necessary in a total amount of 2.0% by mass or less to the Cu-Ni-Si system alloy of the present invention, to meet required properties. An amount of less than 0.001% by mass cannot achieve the desired effects. On the other hand, an amount of more than 2.0% by mass causes a significant decrease in conductivity and poor production characteristics.
  • the total amount of the elements to be added is preferably 0.001 to 2.0% by mass, more preferably 0.01 to 1.0% by mass.
  • elements not specified in this specification may be added in a range causing no negative effect on the characteristics of the Cu-Ni-Si system alloy of the present invention.
  • the method of producing alloys of the present invention is described below.
  • the Cu-Ni-Si system alloy of the present invention can be produced by any conventional method, except for conditions of solution treatment and aging treatment for control of Ni-Si compounds and Cr-Si compounds. Although no specific explanation would be necessary for those skilled in the art who can select an optimal method depending on the composition and required properties, a typical method is described below for illustrative purposes.
  • raw materials such as electrolytic copper, Ni, Si, and Cr are melted in a melting furnace in atmosphere to obtain molten metal having a desired composition.
  • this molten metal is cast into an ingot.
  • strips and foils having a desired thickness and properties are formed.
  • the heat treatment includes solution treatment and aging treatment.
  • the solution treatment the Ni-Si compounds and the Cr-Si compounds are dissolved into the copper matrix while the copper matrix is recrystallized at the same time, during heating at a high temperature of 700 to 1000°C.
  • the hot rolling may combine with the solution treatment.
  • the important factors in the solution treatment are a heating temperature and a cooling rate.
  • the cooling rate after heating was not controlled, and water-cooling using a water tank provided at a furnace outlet or air-cooling in the atmosphere was employed. In that case, the cooling rate easily varied depending on the set heating temperature.
  • the conventional cooling rate varied in a wide range of 1°C/s or less to 10°C/s or more. Consequently, in the conventional cooling, it was difficult to control properties of alloys, such as an alloy of the present invention.
  • the cooling rate is in the range of 1°C/s to 10°C/s.
  • the Ni-Si compounds and the Cr-Si compounds dissolved during the solution treatment are precipitated as fine particles by heating at a temperature in the range of 350 to 550°C for at least 1 hour, typically for 3 to 24 hours.
  • the strength and conductivity increases through the aging treatment.
  • cold-rolling may be employed for higher strength.
  • stress relief annealing annealing at low temperature
  • the Cu-Ni-Si copper alloy of the present invention may have a 0.2% yield strength of not less than 780 MPa and a conductivity of not less than 45% IACS; may further have a 0.2% yield strength of not less than 860 MPa and a conductivity of not less than 43% IACS; or may still further have a 0.2% yield strength of not less than 890 MPa and a conductivity of not less than 40% IACS.
  • the Cu-Ni-Si system alloy of the present invention can be shaped into various wrought copper products such as strips, ribbons, pipes, rods and bars. Furthermore, the Cu-Ni-Si system alloy of the present invention can be used in components for electronic devices such as lead frames, connectors, pins, terminals, relays, switches and foils for secondary batteries, which require both high strength and high electrical conductivity (or thermal conductivity).
  • the copper alloys used in Examples of the present invention are copper alloys containing various amounts of Ni, Si and Cr and further containing optional Sn, Zn, Mg, Mn, Co and Ag, as shown in Table 1.
  • the copper alloys used in Comparative Examples are Cu-Ni-Si copper alloys having parameters out of the range of the present invention.
  • the copper alloys having various compositions described in Table 1 were melted in a high-frequency melting furnace at 1300°C and each alloy was cast into an ingot having a thickness of 30 mm. Next, this ingot was heated to 1000°C, then was hot-rolled into a plate having a thickness of 10 mm, and was cooled immediately. After the plate was planed for removal of scales to a thickness of 8 mm, it was cold-rolled into a thickness of 0.2 mm. Subsequently, solution treatment was conducted in argon gas atmosphere at a temperature of 800 to 900°C for 120 seconds, depending on the addition amount ofNi and Cr, followed by cooling down to room temperature at various cooling rates. The cooling rate was controlled by varying the flow rate of gas blowing against the sample.
  • the cooling rate was determined by the measurement of the time required for the sample to be cooled from its attained maximum temperature to 400°C.
  • the cooling rate of the furnace without gas blow was 5°C/s, and the lower cooling rate was set at 1°C/s in the case of cooling along with controlled heating output.
  • the plate was cold-rolled into a thickness of 0.1 mm, and was finally aged in inert atmosphere at 400 to 550°C for 1 to 12 hours depending on the amount of added elements, thereby samples were produced.
  • the strength and conductivity of each alloy produced as described above were evalulated.
  • the strength was evaluated by 0.2% yield strength (YS; MPa) measured by a tensile test in the direction of rolling.
  • the electric conductivity (EC; %IACS) was determined from the volume electrical resistivity measured by double bridges.
  • the bendability was evaluated by W bend test using a W-shaped mold at a ratio of the bending radius to the thickness of the sample plate of 1. The evaluation was performed through observation of the bent surface with an optical microscope. For samples where no crack was observed, Rank A was given indicating a satisfactory level in practical use. For samples any crack was observed, Rank F was given. In a fatigue test, symmetrically reversed stress load according to JIS Z 2273 was loaded to determine the fatigue strength (MPa) where the alloy was broken at 10 7 cycles.
  • composition (Cr/Si), size, and dispersion density of particles of the Cr-Si compounds were respectively defined as the average Cr/Si ratio, the minimum inside diameter, and the average number in each observation view for the particles of the Cr-Si compounds having a size of 0.1 to 5 ⁇ m analyzed at many places by FE-AES observation.
  • the results are shown in Tables 1 and 2.
  • Examples 1 to 25 of the present invention show satisfactory properties, since particles of Cr-Si compounds have a dispersion density of no more than 1 ⁇ 10 6 and a Cr/Si ratio in the range of 1 to 5 due to a proper cooling rate.
  • Comparative Examples 1 to 3 show insufficient strength and poor bendability due to excess grow of particles of Cr-Si compounds caused by a slow cooling rate.
  • Comparative Examples 4 and 5 show poor strength and conductivity due to insufficient grow of the particles and excess Si dissolved in the alloy caused by a rapid cooling rate.
  • Comparative Examples 6 and 7 show insufficient strength and poor bendability due to excess grow of particles of Cr-Si compounds caused by a high aging temperature.
  • Comparative Examples 8 and 9 show poor strength and poor bendability due to excess grow of particles of Cr-Si compounds caused by an excess concentration of Cr.

Description

    FIELD OF THE INVENTION
  • The present invention relates to precipitation hardening copper alloys, and in particular, to Cu-Ni-Si-Cr system alloys suitable for use in components for various electronic devices.
  • BACKGROUND OF THE INVENTION
  • Copper alloys for electronic materials used in components for various electronic devices such as lead frames, connectors, pins, terminals, relays, and switches must satisfy both high strength and high electrical conductivity (or high thermal conductivity) as basic characteristics. Recent rapid advances of high integration and reductions in size and thickness of electronic components have accelerated requirements for higher performances of copper alloys used in components for electronic devices.
  • In recent years, in consideration of high strength and high electrical conductivity of copper alloys for electronic materials, the use of precipitation hardening copper alloys has increased, in place of traditional solid solution strengthened copper alloys such as phosphor bronze and brass. In the precipitation hardening copper alloys, age hardening of supersaturated solid solution after solution treatment facilitates uniform dispersion of fine precipitates and thus an increase in strength of the alloys. It also leads to a decrease in amount of solute elements in copper matrix and thus an improvement in electrical conductivity. The resulting materials have superior mechanical properties such as strength and spring properties, as well as high electrical and thermal conductivities.
  • Among precipitation hardening copper alloys, Cu-Ni-Si copper alloys known as Corson alloys are typical copper alloys having compatibility of relatively high electrical conductivity and strength, proper stress relaxation, and excellent bendability. Corson alloys are now being actively developed in the industry. In such copper alloys, fine particles of a NiSi intermetallic compound are precipitated in a copper matrix, thereby improving strength and electrical conductivity.
  • The precipitation of a NiSi intermetallic compound generally has a stoichiometric composition. For example, Japanese Unexamined Patent Application Publication No. 2001-207229 discloses that satisfactory electrical conductivity is achieved by bringing the mass ratio Ni/Si in an alloy close to the mass composition ratio of the intermetallic compound Ni2Si [(Ni atomic weight)×2/(Si atomic weight)×1)], i.e. a weight concentration ratio of Ni/Si in the range of 3 to 7.
  • Although characteristics may be improved by bringing the mass ratio Ni/Si close to the mass composition ratio of the intermetallic compound Ni2Si [(Ni atomic weight)×2/(Si atomic weight×1)] as mentioned in Japanese Unexamined Patent Application Publication No. 2001-207229 , the presence of an excess amount of Si leads to some reductions in electrical conductivity. A possible countermeasure to increase the electrical conductivity is addition of elements that form compounds with excess Si. Cr is one of these elements, and forms Cr-containing Cu-Ni-Si system alloys.
  • Examples of the Cu-Ni-Si system alloys containing Cr as an alloy element are disclosed in Japanese Patent Nos. 2862942 and 3049137 . Japanese Patent No. 2862942 discloses a method of heat treatment of a Corson alloy containing 1.5-4.0% by weight of Ni, 0.35-1.0% by weight of Si, optionally 0.05-1.0% by weight of at least one metal selected from the group consisting of Zr, Cr, and Sn, and the balance being Cu and incidental impurities, wherein the Corson alloy is heated (or cooled) in the temperature range of 400 to 800°C, so as to reduce the tensile thermal strain of the Corson alloy to a level not exceeding 1×10-4. The patent states that the method can prevent an ingot from cracking during the heat treatment.
  • Japanese Patent No. 3049137 discloses a high strength copper alloy containing 2-5% by weight of Ni, 0.5-1.5% by weight of Si, 0.1-2% by weight of Zn, 0.01-0.1% by weight of Mn, 0.001-0.1% by weight of Cr, 0.001-0.15% by weight of Al, 0.05-2% by weight of Co, not more than 15 ppm of S as an impurity, and the balance being Cu and incidental impurities. This copper alloy exhibits excellent bendability. This patent states that Cr is an element which reinforces grain boundaries in an ingot and leads to an improvement in hot workability. It also states that a Cr content exceeding 0.1% by weight causes oxidation of molten metal and poor casting performance. In addition, it states that the copper alloy is covered with charcoal in a cryptol furnace to be melted and cast in the atmosphere.
  • A compound of Cr and Si is disclosed in Japanese Unexamined Patent Application Publication No. 2005-113180 . This patent refers to the hot working temperature and heat treatment temperature for age hardening of an ingot of a copper alloy having excellent etching and punching workability for electronic devices. The copper alloy contains 0.1-0.25% by weight of Cr, 0.005-0.1% by weight of Si, 0.1-0.5% by weight of Zn, 0.05-0.5% by weight of Sn, and the balance being Cu and incidental impurities, wherein the weight ratio Cr/Si is in the range of 3 to 25, particles of Cr-Si compounds having a size of 0.05 µm to 10 µm are present in a number density of 1×103 to 5×105/mm2 in the copper matrix while particles of Cr compounds (other than the Cr-Si compound) having a size greater than 10 µm are not present. According to this method, both etching and punching workability are preferably available.
  • SUMMARY OF THE INVENTION
  • Rapid advances of high integration and reductions in size and thickness of electronic components in recent years have also placed a requirement on Cr-containing Cu-Ni-Si system alloys to have significantly improved performance. In Japanese Unexamined Patent Application Publication No. 2001-207229 , Cr is not added and the excess Ni and Si actually reduce electrical conductivity in some degree. This means the significant progress in performance is unfulfilled yet. Although Cr is added in Cu-Ni-Si system alloys in Japanese Patent Nos. 2862942 and 3049137 , it is added for solid solution hardening in Japanese Patent No. 2862942 and for an improvement in hot workability in Japanese Patent No. 3049137 . No description of Cr-Si compounds, which is a key component of the present invention, is found in these documents. Accordingly, these patent documents do not suggest the solution achieved by the present invention.
  • Although Japanese Unexamined Patent Application Publication No. 2005-113180 discloses that etching and punching workabilities are improved by controlling the number density and size of the Cr-Si compounds, consideration is focused on the conditions for the formation of the Cr-Si compounds and no consideration is paid for the formation of NiSi compounds because no Ni is added. Accordingly, Japanese Unexamined Patent Application Publication No. 2005-113180 also does not suggest the solution achieved by the present invention.
  • An object of the present invention is to provide a Corson alloy having significantly improved characteristics, i.e. high strength and high electrical conductivity, by enhancing the effect of Cr contained in a Cu-Ni-Si system alloy.
  • Through extensive research for solving the problem, the inventors have accomplished an invention as described below. In a Cu-Ni-Si system alloy, the Si content is in excess of the Ni content so that nickel silicide is surely precipitated from the contained Ni in order to improve the strength, while the excess Si is combined with the contained Cr to achieve high conductivity of the alloy. The essence of the present invention is to control the excess growth of particles of Cr-Si compounds so as to prevent a shortage of Si, which combines with Ni. In particular, the inventors have found that the control of the temperature and cooling rate of the heat treatment can enhance such effects, through investigation on the preferred composition, size, and number density of particles of the Cr-Si compounds.
  • The present invention includes the following Aspects:
    1. (1) A copper alloy for electronic materials, comprising 1.0-4.5% by mass Ni, 0.50-1.2% by mass Si, 0.003-0.3% by mass Cr (wherein the weight ratio of Ni to Si satisfies the expression: 3≤Ni/Si≤5.5), and the balance being Cu and incidental impurities, wherein particles of Cr-Si compounds having a size of 0.1 µm to 5 µm are dispersed in the alloy, the dispersed particles having an atomic concentration ratio of Cr to Si of 1 to 5 and a dispersion density of no more than 1×106/mm2.
    2. (2) The copper alloy for electronic materials according to Aspect (1), wherein the dispersion density of the particles of the Cr-Si compounds having a size of 0.1 µm to 5 µm is higher than 1×104/mm2.
    3. (3) The copper alloy for electronic materials according to Aspect (1) or (2), further comprising 0.05-2.0% by mass of at least one element selected from Sn and Zn.
    4. (4) The copper alloy for electronic materials according to any one of Aspects (1) to (3), further comprising 0.001-2.0% by mass of at least one element selected from Mg, Mn, Ag, P, As, Sb, Be, B, Ti, Zr, Al, Co and Fe.
    5. (5) A wrought copper product comprising the copper alloy according to any one of Aspects (1) to (4).
    6. (6) A component for electronic devices, comprising the copper alloy according to any one of Aspects (1) to (4).
  • The present invention can provide the Corson copper alloy having significantly improved strength and electrical conductivity suitable for electronic materials due to the positive effect of Cr, which is an element contained in the alloy.
  • DESCRIPTION OF THE PREFERRED EMBODIMENTS Amounts of Ni and Si to be added
  • Ni and Si form nickel silicides (e.g. Ni2Si) as an intermetallic compound through suitable heat treatment, resulting in high strength without a decrease in conductivity. The mass ratio of Ni to Si is preferably close to the stoichiometric ratio as described above, i.e. 3≤Ni/Si≤5.5, more preferably 3.5≤Ni/Si≤5.0.
  • However, even if the ratio Ni/Si is within the range, desired strength is not achieved at a Si content of less than 0.5% by mass. Furthermore, a Si content of more than 1.2% by mass is not preferred because of significantly reduced conductivity and poor hot workability due to formation of a liquid phase in a segregation region, despite enhanced strength. As a result, the preferred Si content is in the range of 0.5% to 1.2% by mass, preferably 0.5% to 0.8% by mass. The amount ofNi to be added may be determined so as to satisfy the preferable ratio described above. In view of balance with the Si content, the suitable Ni content is in the range of 2.5% to 4.5% by mass, preferably 3.2% to 4.2% by mass, more preferably 3.5% to 4.0% by mass.
  • Amount of Cr to be added
  • In general Cu-Ni-Si system alloys, increased concentrations of Ni and Si raise the total number of precipitated particles, and thus enhance strength through precipitation strengthening. Such increased concentrations, however, are accompanied by an increased amount of solid solution that does not contribute to precipitation. This causes a reduction in conductivity at a maximum strength, regardless of an increase in the maximum strength after age precipitation. In this regard, when 0.003% to 0.3% by mass of, preferably 0.01% to 0.1% by mass of Cr is added to the Cu-Ni-Si system alloy, higher conductivity can be achieved without a reduction in strength compared to a Cu-Ni-Si system alloy having the same Ni-Si concentrations. Furthermore, a higher yield can be achieved due to improved hot workability,.
  • Regarding the composition of particles precipitated in the Cr-containing Cu-Ni-Si system alloy, particles primarily composed of elemental Cr having a bcc structure are readily precipitated as well as particles of Cr-Si compounds. Since Cr can easily precipitate chromium silicides (e.g. Cr3Si) in the copper matrix through proper heat treatment, the dissolved Si component, which has not precipitated in the form such as Ni2Si during a combined process of solution treatment, cold rolling and aging, can be precipitated as Cr-Si compounds. This process can suppress a reduction in conductivity caused by the dissolved Si and thus achieve high conductivity without a reduction in strength.
  • A low concentration of Si in Cr particles leads to residual Si in the matrix, resulting in a reduction in conductivity. On the other hand, a high concentration of Si in Cr particles causes a decreased concentration of Si contributing to precipitation of particles of a NiSi compound, resulting in a reduction in strength. Furthermore, a high concentration of Si in Cr particles accelerates formation of coarse Cr-Si particles, resulting in decreases in bendability and fatigue strength. Moreover, a lower cooling rate after solution treatment and excess heating treatment for aging cause coarsening of particles of the Cr-Si compounds. This causes a decrease in Si concentration necessary for formation of a NiSi compound and thus precludes the formation of a NiSi compound contributing to strength. This is because diffusion rates in Cu of Si and Cr are higher than that of Ni, which accelerates coarsening of particles of the Cr-Si compounds. The precipitation rate of Cr-Si compounds is thus higher than that of NiSi compounds.
  • The composition, size and density of particles of the Cr-Si compounds can, therefore, be controlled by regulating the cooling rate after solution treatment and avoiding severer aging conditions such as higher temperature and longer time than the optimum conditions for maximum strength. Consequently, the Cr concentration should be 0.003% by mass to 0.3% by mass, and the atomic ratio of Cr to Si in Cr-Si compounds should be in the range of 1 to 5.
  • Since Cr is preferentially precipitated at crystal grain boundaries in the cooling process after melting and casting, it can strengthen the grain boundaries. As a result, cracking during hot working can be reduced, and thus a high yield can be achieved. Although Cr precipitated at grain boundaries after melting and casting is redissolved during the solution treatment, it forms silicides during the subsequent age precipitation process. In general Cu-Ni-Si system alloys, part of the added Si does not contribute to age precipitation and remains dissolved in the matrix, obstructing an increase in conductivity. Since the addition of Cr, which is an element to form silicides, leads to further precipitation of silicides and a reduction in dissolved Si, the conductivity can be increased without a reduction in strength, compared to conventional Cu-Ni-Si system alloys.
  • Size and dispersion density of particles of Cr-Si compounds
  • The size of particles of the Cr-Si compounds has an effect on bendability and fatigue strength. When the particles of the Cr-Si compounds have a size of greater than 5 µm or when the dispersion density of particles of the Cr-Si compounds having a size in the range of 0.1 to 5 µm exceeds 1×106/mm2, the bendability and the fatigue strength are significantly reduced. Furthermore, since the number density has an effect on the excess and deficiency of the concentration of Si in the matrix, the presence of large particles dispersed in large quantities will become an obstacle to the desired strength. Consequently, the upper limit of the dispersion density is 1×106/mm2, preferably 5×105/mm2, more preferably 1×105/mm2. In addition, it is preferred that the density be more than 1×104/mm2, in order to achieve the significant effect of the addition of Cr.
  • Sn and Zn
  • Addition of at least one element selected from Sn and Zn in a total amount of 0.05-2.0% by mass to the Cu-Ni-Si system alloy of the present invention can improve stress relaxation and other characteristics without significant reductions in strength and conductivity. An amount of less than 0.05% by mass leads to insufficient effect of addition. On the other hand, an amount of more than 2.0% by mass causes poor production characteristics such as castability and hot workability and low conductivity of the products. It is therefore preferred that the amount of these elements should be added from 0.05% by mass to 2.0% by mass.
  • Other elements to be added
  • Addition of appropriate amounts of Mg, Mn, Ag, P, As, Sb, Be, B, Ti, Zr, Al, Co and Fe brings about various effects that are complementary to each other, for example, enhanced strength and conductivity, and improved production characteristics such as bendability, plating property, and hot workability of an ingot due to the formation of a fine microstructure. Accordingly, at least one element selected from these elements may be added as necessary in a total amount of 2.0% by mass or less to the Cu-Ni-Si system alloy of the present invention, to meet required properties. An amount of less than 0.001% by mass cannot achieve the desired effects. On the other hand, an amount of more than 2.0% by mass causes a significant decrease in conductivity and poor production characteristics. Accordingly, the total amount of the elements to be added is preferably 0.001 to 2.0% by mass, more preferably 0.01 to 1.0% by mass. Incidentally, elements not specified in this specification may be added in a range causing no negative effect on the characteristics of the Cu-Ni-Si system alloy of the present invention.
  • The method of producing alloys of the present invention is described below. The Cu-Ni-Si system alloy of the present invention can be produced by any conventional method, except for conditions of solution treatment and aging treatment for control of Ni-Si compounds and Cr-Si compounds. Although no specific explanation would be necessary for those skilled in the art who can select an optimal method depending on the composition and required properties, a typical method is described below for illustrative purposes.
  • First, raw materials such as electrolytic copper, Ni, Si, and Cr are melted in a melting furnace in atmosphere to obtain molten metal having a desired composition. Next, this molten metal is cast into an ingot. Through subsequent hot-rolling and repeated processes of cold-rolling and heat treatment, strips and foils having a desired thickness and properties are formed. The heat treatment includes solution treatment and aging treatment. In the solution treatment, the Ni-Si compounds and the Cr-Si compounds are dissolved into the copper matrix while the copper matrix is recrystallized at the same time, during heating at a high temperature of 700 to 1000°C. The hot rolling may combine with the solution treatment.
  • The important factors in the solution treatment are a heating temperature and a cooling rate. In conventional methods, the cooling rate after heating was not controlled, and water-cooling using a water tank provided at a furnace outlet or air-cooling in the atmosphere was employed. In that case, the cooling rate easily varied depending on the set heating temperature. The conventional cooling rate varied in a wide range of 1°C/s or less to 10°C/s or more. Consequently, in the conventional cooling, it was difficult to control properties of alloys, such as an alloy of the present invention.
  • Preferably the cooling rate is in the range of 1°C/s to 10°C/s. In aging treatment, the Ni-Si compounds and the Cr-Si compounds dissolved during the solution treatment are precipitated as fine particles by heating at a temperature in the range of 350 to 550°C for at least 1 hour, typically for 3 to 24 hours. The strength and conductivity increases through the aging treatment. Before and/or after the aging, cold-rolling may be employed for higher strength. When the cold-rolling is performed after the aging treatment, stress relief annealing (annealing at low temperature) may be performed after the cold-rolling.
  • In one embodiment, the Cu-Ni-Si copper alloy of the present invention may have a 0.2% yield strength of not less than 780 MPa and a conductivity of not less than 45% IACS; may further have a 0.2% yield strength of not less than 860 MPa and a conductivity of not less than 43% IACS; or may still further have a 0.2% yield strength of not less than 890 MPa and a conductivity of not less than 40% IACS.
  • The Cu-Ni-Si system alloy of the present invention can be shaped into various wrought copper products such as strips, ribbons, pipes, rods and bars. Furthermore, the Cu-Ni-Si system alloy of the present invention can be used in components for electronic devices such as lead frames, connectors, pins, terminals, relays, switches and foils for secondary batteries, which require both high strength and high electrical conductivity (or thermal conductivity).
  • EXAMPLES
  • The following examples are merely illustrative for further understanding of the present invention and its advantages, and not limiting to the disclosure in any way.
  • The copper alloys used in Examples of the present invention are copper alloys containing various amounts of Ni, Si and Cr and further containing optional Sn, Zn, Mg, Mn, Co and Ag, as shown in Table 1. The copper alloys used in Comparative Examples are Cu-Ni-Si copper alloys having parameters out of the range of the present invention.
  • The copper alloys having various compositions described in Table 1 were melted in a high-frequency melting furnace at 1300°C and each alloy was cast into an ingot having a thickness of 30 mm. Next, this ingot was heated to 1000°C, then was hot-rolled into a plate having a thickness of 10 mm, and was cooled immediately. After the plate was planed for removal of scales to a thickness of 8 mm, it was cold-rolled into a thickness of 0.2 mm. Subsequently, solution treatment was conducted in argon gas atmosphere at a temperature of 800 to 900°C for 120 seconds, depending on the addition amount ofNi and Cr, followed by cooling down to room temperature at various cooling rates. The cooling rate was controlled by varying the flow rate of gas blowing against the sample. The cooling rate was determined by the measurement of the time required for the sample to be cooled from its attained maximum temperature to 400°C. The cooling rate of the furnace without gas blow was 5°C/s, and the lower cooling rate was set at 1°C/s in the case of cooling along with controlled heating output. After this, the plate was cold-rolled into a thickness of 0.1 mm, and was finally aged in inert atmosphere at 400 to 550°C for 1 to 12 hours depending on the amount of added elements, thereby samples were produced.
  • The strength and conductivity of each alloy produced as described above were evalulated. The strength was evaluated by 0.2% yield strength (YS; MPa) measured by a tensile test in the direction of rolling. The electric conductivity (EC; %IACS) was determined from the volume electrical resistivity measured by double bridges. The bendability was evaluated by W bend test using a W-shaped mold at a ratio of the bending radius to the thickness of the sample plate of 1. The evaluation was performed through observation of the bent surface with an optical microscope. For samples where no crack was observed, Rank A was given indicating a satisfactory level in practical use. For samples any crack was observed, Rank F was given. In a fatigue test, symmetrically reversed stress load according to JIS Z 2273 was loaded to determine the fatigue strength (MPa) where the alloy was broken at 107 cycles.
  • For observation of particles of the Cr-Si compounds by FE-AES, a plate surface of the samples was electropolished. Particles having a size of not smaller than 0.1 µm were observed at many places. Adsorbed elements (C and O) on the surface layer were removed by Ar+ sputtering. Auger spectra of individual particles were measured and the weight concentrations of detected elements were determined by semiquantitative analysis using sensitivity coefficients. Particles containing the detected Cr and Si were extracted as objects. The composition (Cr/Si), size, and dispersion density of particles of the Cr-Si compounds were respectively defined as the average Cr/Si ratio, the minimum inside diameter, and the average number in each observation view for the particles of the Cr-Si compounds having a size of 0.1 to 5 µm analyzed at many places by FE-AES observation. The results are shown in Tables 1 and 2.
    Figure imgb0001
    Figure imgb0002
  • Examples 1 to 25 of the present invention show satisfactory properties, since particles of Cr-Si compounds have a dispersion density of no more than 1×106 and a Cr/Si ratio in the range of 1 to 5 due to a proper cooling rate. In contrast, Comparative Examples 1 to 3 show insufficient strength and poor bendability due to excess grow of particles of Cr-Si compounds caused by a slow cooling rate. Comparative Examples 4 and 5 show poor strength and conductivity due to insufficient grow of the particles and excess Si dissolved in the alloy caused by a rapid cooling rate. Comparative Examples 6 and 7 show insufficient strength and poor bendability due to excess grow of particles of Cr-Si compounds caused by a high aging temperature. Comparative Examples 8 and 9 show poor strength and poor bendability due to excess grow of particles of Cr-Si compounds caused by an excess concentration of Cr.

Claims (5)

  1. A copper alloy for electronic materials, comprising 1.0-4.5% by mass Ni, 0.50-1.2% by mass Si, 0.003-0.3% by mass Cr wherein the weight ratio of Ni to Si satisfies the expression: 3≤Ni/Si≤5.5, optionally comprising 0.05-2.0% by mass of at least one element selected from Sn and Zn, and optionally further comprising 0.001-2.0% by mass of at least one element selected from Mg, Mn, Ag, P, As, Sb, Be, B, Ti, Zr, Al, Co and Fe and the balance being Cu and incidental impurities, characterised in that particles of Cr-Si compounds having a size of 0.1 µm to 5 µm are dispersed in the alloy, the dispersed particles having an atomic concentration ratio of Cr to Si in the range of 1 to 5 and a dispersion density of higher than 1×104/mm2 and no more than 1×106/mm2.
  2. The copper alloy for electronic materials according to Claim 1, further comprising 0.05-2.0% by mass of at least one element selected from Sn and Zn.
  3. The copper alloy for electronic materials according to Claim 1 or 2 further comprising 0.001-2.0% by mass of at least one element selected from Mg, Mn, Ag, P, As, Sb, Be, B, Ti, Zr, Al, Co and Fe.
  4. A wrought copper product comprising the copper alloy according to any one of Claims 1 to 3.
  5. A component for electronic devices, comprising the copper alloy according to any one of Claims 1 to 3.
EP08739256.9A 2007-03-30 2008-03-28 Cu-ni-si-based alloy for electronic material Active EP2154257B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2007094441 2007-03-30
PCT/JP2008/056138 WO2008123433A1 (en) 2007-03-30 2008-03-28 Cu-ni-si-based alloy for electronic material

Publications (3)

Publication Number Publication Date
EP2154257A1 EP2154257A1 (en) 2010-02-17
EP2154257A4 EP2154257A4 (en) 2012-01-11
EP2154257B1 true EP2154257B1 (en) 2016-10-05

Family

ID=39830918

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08739256.9A Active EP2154257B1 (en) 2007-03-30 2008-03-28 Cu-ni-si-based alloy for electronic material

Country Status (7)

Country Link
US (1) US20100086435A1 (en)
EP (1) EP2154257B1 (en)
JP (1) JP4418028B2 (en)
KR (1) KR101211984B1 (en)
CN (1) CN101646792B (en)
TW (1) TWI395824B (en)
WO (1) WO2008123433A1 (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4653239B2 (en) * 2008-03-31 2011-03-16 古河電気工業株式会社 Copper alloy materials and electrical / electronic parts for electrical / electronic equipment
EP2270242B1 (en) * 2008-03-31 2014-06-04 The Furukawa Electric Co., Ltd. Copper alloy material for electric or electronic apparatuses, method for producing it and component
JP4809935B2 (en) * 2009-12-02 2011-11-09 古河電気工業株式会社 Copper alloy sheet having low Young's modulus and method for producing the same
KR20120130342A (en) * 2010-04-02 2012-11-30 제이엑스 닛코 닛세키 킨조쿠 가부시키가이샤 Cu-ni-si alloy for electronic material
JP5045784B2 (en) * 2010-05-14 2012-10-10 三菱マテリアル株式会社 Copper alloy for electronic equipment, method for producing copper alloy for electronic equipment, and rolled copper alloy material for electronic equipment
JP5714863B2 (en) * 2010-10-14 2015-05-07 矢崎総業株式会社 Female terminal and method for manufacturing female terminal
JP5712585B2 (en) * 2010-12-03 2015-05-07 三菱マテリアル株式会社 Copper alloy for electronic equipment, method for producing copper alloy for electronic equipment, and rolled copper alloy material for electronic equipment
JP5684022B2 (en) * 2011-03-28 2015-03-11 三菱伸銅株式会社 Cu-Ni-Si based copper alloy sheet excellent in stress relaxation resistance, fatigue resistance after bending and spring characteristics, and method for producing the same
US9159985B2 (en) * 2011-05-27 2015-10-13 Ostuka Techno Corporation Circuit breaker and battery pack including the same
JP5903842B2 (en) 2011-11-14 2016-04-13 三菱マテリアル株式会社 Copper alloy, copper alloy plastic working material, and method for producing copper alloy plastic working material
KR101274063B1 (en) * 2013-01-22 2013-06-12 한국기계연구원 A metal matrix composite with two-way shape precipitation and method for manufacturing thereof
KR101709560B1 (en) 2013-09-27 2017-02-23 주식회사 엘지화학 Secondary Battery with Electrode Tab Having Low Resistance
JP6452472B2 (en) * 2014-01-27 2019-01-16 古河電気工業株式会社 Copper alloy material and method for producing the same
CN105385890A (en) * 2015-11-27 2016-03-09 宁波博威合金材料股份有限公司 Nickel and silicon contained bronze alloy and application thereof
CN105821238B (en) * 2016-05-31 2018-01-02 黄河科技学院 A kind of Cu alloy material and preparation method thereof
CN106191725B (en) * 2016-06-24 2018-01-26 河南江河机械有限责任公司 High-intensity high-conductivity copper alloy nanometer phase precipitation technique method
CN108193080B (en) * 2016-12-08 2019-12-17 北京有色金属研究总院 High-strength high-conductivity stress relaxation-resistant copper-nickel-silicon alloy material and preparation method thereof
CN109609801A (en) * 2018-12-06 2019-04-12 宁波博威合金材料股份有限公司 High property copper alloy and preparation method thereof
CN115386766A (en) * 2022-08-11 2022-11-25 中国科学院金属研究所 Cu-Ni-Si-Cr-Mg quinary copper alloy and preparation method thereof

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61115249A (en) 1984-11-09 1986-06-02 Sanyo Electric Co Ltd Supporting device of electromechanical transducer
JP2862942B2 (en) 1990-03-20 1999-03-03 古河電気工業株式会社 Heat treatment method of Corson alloy
JP3049137B2 (en) * 1991-12-27 2000-06-05 株式会社神戸製鋼所 High strength copper alloy excellent in bending workability and method for producing the same
JPH0718356A (en) * 1993-07-01 1995-01-20 Mitsubishi Electric Corp Copper alloy for electronic equipment, its production and ic lead frame
JP2001207229A (en) * 2000-01-27 2001-07-31 Nippon Mining & Metals Co Ltd Copper alloy for electronic material
JP4177221B2 (en) 2003-10-06 2008-11-05 古河電気工業株式会社 Copper alloy for electronic equipment
JP3864965B2 (en) * 2004-06-08 2007-01-10 日立電線株式会社 Manufacturing method of copper alloy for terminals and connectors
CN101166840B (en) * 2005-02-28 2012-07-18 古河电气工业株式会社 Copper alloy
CN1776997B (en) * 2005-12-13 2010-05-05 江苏科技大学 Large-capacity steam turbine generator rotor copper alloy slot wedge and its preparing method

Also Published As

Publication number Publication date
JPWO2008123433A1 (en) 2010-07-15
EP2154257A1 (en) 2010-02-17
KR20090123017A (en) 2009-12-01
EP2154257A4 (en) 2012-01-11
JP4418028B2 (en) 2010-02-17
WO2008123433A1 (en) 2008-10-16
US20100086435A1 (en) 2010-04-08
CN101646792A (en) 2010-02-10
TW200902732A (en) 2009-01-16
CN101646792B (en) 2012-02-22
TWI395824B (en) 2013-05-11
KR101211984B1 (en) 2012-12-13

Similar Documents

Publication Publication Date Title
EP2154257B1 (en) Cu-ni-si-based alloy for electronic material
JP4937815B2 (en) Cu-Ni-Si-Co-based copper alloy for electronic materials and method for producing the same
KR100929276B1 (en) Copper alloy
JP4440313B2 (en) Cu-Ni-Si-Co-Cr alloy for electronic materials
EP2508632B1 (en) Copper alloy sheet material
KR101331339B1 (en) Cu-ni-si-co based copper ally for electronic materials and manufacturing method therefor
JP4596490B2 (en) Cu-Ni-Si-Co-based copper alloy for electronic materials and method for producing the same
JP5506806B2 (en) Cu-Ni-Si-Co-based copper alloy for electronic materials and method for producing the same
EP2692879B1 (en) Cu-co-si-based copper alloy strip for electron material, and method for manufacturing same
CN110923499B (en) Ce and B-containing titanium bronze alloy strip and preparation method thereof
JP2006283120A (en) Cu-Ni-Si-Co-Cr BASED COPPER ALLOY FOR ELECTRONIC MATERIAL, AND ITS PRODUCTION METHOD
JPH0841612A (en) Copper alloy and its preparation
JP2008081762A (en) Cu-Cr-BASED COPPER ALLOY FOR ELECTRONIC MATERIAL
WO2012132765A1 (en) Cu-si-co-base copper alloy for electronic materials and method for producing same
JP4754930B2 (en) Cu-Ni-Si based copper alloy for electronic materials
KR20010006488A (en) Grain refined tin brass
JP4166196B2 (en) Cu-Ni-Si copper alloy strip with excellent bending workability
US20080175746A1 (en) Cu-Ni-Si system copper alloy for electronic materials
JP4166197B2 (en) Cu-Ni-Si-based copper alloy strips with excellent BadWay bending workability
CN112281023A (en) Copper alloy material with excellent bending property and preparation method and application thereof
KR100878165B1 (en) Copper-nickel-silicon based copper alloy for electronic material, wrought copper and copper alloy using thereof and electronic device part using therof
JP5623960B2 (en) Cu-Ni-Si based copper alloy strip for electronic materials and method for producing the same
JP5595961B2 (en) Cu-Ni-Si based copper alloy for electronic materials and method for producing the same
JPS6148545A (en) High strength copper alloy for electrically conductive material

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20091014

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

DAX Request for extension of the european patent (deleted)
RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: JX NIPPON MINING & METALS CORPORATION

A4 Supplementary search report drawn up and despatched

Effective date: 20111212

RIC1 Information provided on ipc code assigned before grant

Ipc: C22F 1/02 20060101ALI20111206BHEP

Ipc: C22C 9/10 20060101ALI20111206BHEP

Ipc: C22C 9/05 20060101ALI20111206BHEP

Ipc: C22C 9/02 20060101ALI20111206BHEP

Ipc: C22C 9/00 20060101ALI20111206BHEP

Ipc: C22C 9/04 20060101ALI20111206BHEP

Ipc: C22F 1/00 20060101ALI20111206BHEP

Ipc: H01B 1/02 20060101ALI20111206BHEP

Ipc: C22C 9/06 20060101AFI20111206BHEP

Ipc: H01B 5/02 20060101ALI20111206BHEP

Ipc: C22F 1/08 20060101ALI20111206BHEP

Ipc: C22C 9/01 20060101ALI20111206BHEP

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20160504

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 834742

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161015

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 602008046646

Country of ref document: DE

REG Reference to a national code

Ref country code: NL

Ref legal event code: MP

Effective date: 20161005

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 10

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 834742

Country of ref document: AT

Kind code of ref document: T

Effective date: 20161005

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCOW

Free format text: NEW ADDRESS: 1-2 OTEMACHI 1-CHOME CHIYODAKU, TOKYO (JP)

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170105

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170106

REG Reference to a national code

Ref country code: CH

Ref legal event code: PCOW

Free format text: NEW ADDRESS: 1-2 OTEMACHI 1-CHOME CHIYODA-KU, TOKYO (JP)

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170205

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170206

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602008046646

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20170105

26N No opposition filed

Effective date: 20170706

REG Reference to a national code

Ref country code: FR

Ref legal event code: CA

Effective date: 20170912

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20170328

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170328

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 11

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170328

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170328

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170328

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20080328

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20161005

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20161005

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20230208

Year of fee payment: 16

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20230131

Year of fee payment: 16

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230517

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20230401

Year of fee payment: 16