Classifications

• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C9/00—Alloys based on copper
  • C22C9/06—Alloys based on copper with nickel or cobalt as the next major constituent
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
  • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
  • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
  • C22F1/02—Changing 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
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
  • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
  • C22F1/08—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of copper or alloys based thereon
• • H—ELECTRICITY
  • H01—ELECTRIC ELEMENTS
  • H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
  • H01B1/00—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
  • H01B1/02—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
• • H—ELECTRICITY
  • H01—ELECTRIC ELEMENTS
  • H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
  • H01B1/00—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
  • H01B1/02—Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
  • H01B1/026—Alloys based on copper
• • H—ELECTRICITY
  • H01—ELECTRIC ELEMENTS
  • H01B—CABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
  • H01B5/00—Non-insulated conductors or conductive bodies characterised by their form
  • H01B5/02—Single 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:
• 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 ⁇ m to 5 ⁇ m 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 ⁇ 10 6 /mm 2 .
• a wrought copper product comprising the copper alloy according to any one of Aspects (1) to (4).
• 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.
• 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 of Ni 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 of Ni 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 evaluated.
• 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.

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• 2008
  • 2008-03-28 JP JP2009509224A patent/JP4418028B2/ja active Active
  • 2008-03-28 WO PCT/JP2008/056138 patent/WO2008123433A1/ja active Application Filing
  • 2008-03-28 CN CN2008800101895A patent/CN101646792B/zh active Active
  • 2008-03-28 TW TW097111276A patent/TWI395824B/zh active
  • 2008-03-28 KR KR1020097022449A patent/KR101211984B1/ko active IP Right Grant
  • 2008-03-28 US US12/532,929 patent/US20100086435A1/en not_active Abandoned
  • 2008-03-28 EP EP08739256.9A patent/EP2154257B1/de active Active

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