EP3951000B1 - Zinc alloy and manufacturing method thereof - Google Patents

Zinc alloy and manufacturing method thereof Download PDF

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Publication number
EP3951000B1
EP3951000B1 EP20206431.7A EP20206431A EP3951000B1 EP 3951000 B1 EP3951000 B1 EP 3951000B1 EP 20206431 A EP20206431 A EP 20206431A EP 3951000 B1 EP3951000 B1 EP 3951000B1
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Prior art keywords
alloy
zinc
amount
ingots
refiner
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German (de)
French (fr)
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EP3951000A1 (en
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Chuankai Xu
Jia LONG
Zhenqing Hu
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Xiamen Lota International Co Ltd
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Xiamen Lota International Co Ltd
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    • 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
    • C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/165—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon of zinc or cadmium or alloys based thereon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C18/00—Alloys based on zinc
    • C22C18/04—Alloys based on zinc with aluminium as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/02—Making non-ferrous alloys by melting
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/06—Making non-ferrous alloys with the use of special agents for refining or deoxidising

Definitions

  • the invention relates to the technical field of alloys and specifically relates to a zinc alloy with excellent crack resistance and a manufacturing method thereof.
  • Zinc alloy for die casting is an alloy formed by adding other elements based on zinc. Commonly added alloying elements are aluminum, copper, magnesium, cadmium, lead, titanium, and the like. Zinc alloy has a low melting point and good fluidity and is convenient for welding, brazing and plastic processing. Zinc alloy is corrosion resistant in the atmosphere, and the residual material is easy to recycle and remelt. However, Zinc alloy has a low creep strength and is susceptible to natural aging, which may cause dimensional changes.
  • ZAMAK3 alloy and ZAMAK5 alloy Commonly used zinc alloys for die-casting are ZAMAK3 alloy and ZAMAK5 alloy.
  • the composition of these two alloys is relatively simple. Initially, they mainly contain zinc and aluminum, and sometimes copper is added. Such alloys have poor corrosion resistance. In order to improve the corrosion resistance, researchers introduced magnesium. As a result, it has been found that the intergranular corrosion performance was significantly improved after the addition of magnesium, and the alloy strength was improved. Therefore, the currently marketed ZAMAK3 alloy and ZAMAK5 alloy are both added with magnesium element and the amount of magnesium is controlled at 0.03-0.06%.
  • ZAMAK3 alloy has been widely used in the bathroom hardware industry due to its excellent comprehensive performance and low cost.
  • thermal cracks are likely to occur at the R angle, and the crack rate when forming is 100%.
  • the product design is limited by customer requirements, and the R angle cannot be modified at will, and thus the crack cannot be resolved.
  • ZAMAK5 alloy has higher hardness and strength, and lower flexibility.
  • this alloy also has similar defects as ZAMAK3 alloy that is prone to hot cracks.
  • DE 2142685 A1 discloses so-called superplastic zinc alloys that are processable with little effort and without crack formation.
  • Zinc alloys are rendered superplastic by thermal-mechanical treatment above half their absolute melting temperature. It is furthermore disclosed in DE 2142685 A1 that a significant increase in the creep strength can be achieved by subsequent heat treatment of the product at a temperature above 275° C and subsequent slow cooling. However, the high superplasticity of the alloy is lost as a result of such a treatment. In all examples, the zinc alloys are treated by hot and cold rolling. In contrast, the zinc alloy of the present invention is cast in the molten state.
  • CN 108504900 A1 discloses zinc alloys with 4.3% Al, 0.007% Mg and 0.4% Cu and, respectively, 4.35% Mg, 0.001 % Mg and 0.45% Cu.
  • the inventor of the present application has conducted thorough research on the existing zinc alloys and provided a method for producing a zinc alloy as specified in claims 1-4 with excellent thermal crack resistance.
  • the zinc alloy has excellent comprehensive properties.
  • the thermal crack resistance is significantly improved, which can meet the high surface quality requirements of castings, especially die-castings, and can also be used in recast castings. It is suitable for the production of components of plumbing and sanitary ware, hardware accessories, electronic appliances, toys, and the like.
  • the alloy can significantly increase the product forming yield rate, reduce the abnormal processing time of the product, and effectively increase the production capacity, thereby improving the market competitiveness of the product.
  • the present application provides a method for producing a zinc alloy with excellent crack resistance, wherein the alloy contains Al at an amount of 3.9-4.1 wt% and Mg at an amount of 0.005-0.018 wt%, optionally Cu at an amount of 0.2-1.0 wt%, and the rest of the alloy is Zn and unavoidable impurities.
  • the zinc alloy is obtainable by a method comprising the following steps: weighing zinc ingots, aluminum ingots, magnesium ingots and/or selectively added electrolytic copper according to the composition of the zinc alloy; adding the aluminum ingots, and/or selectively added electrolytic copper, and 1/3 of the zinc ingots at a bottom of a furnace, stirring evenly after all materials are melted, adding the remaining zinc ingots, and using a bell to press the magnesium ingot to the bottom of the furnace at about 540°C after the materials are all melted, after the magnesium ingot is melted, adding selectively a refiner, adding a purifying agent for purifying after the refiner is fully reacted, then removing residue and gas, allowing a product to stand after a composition test is qualified, and casting boat-shaped ingots after slagging and taking out of the furnace, wherein the refiner is a salt refiner containing a titanium salt or a boron salt or a composite of both, and is not an intermediate alloy containing RE or Zr or
  • the amount of Mg in the alloy is 0.005-0.015 wt%.
  • the amount of Cu in the zinc alloy is 0.5-1.0 wt%.
  • the alloy does not contain Zr, Sb, Cr, Mn, Ti, Bi, Se, Ni and the like, except that these elements are present as impurities in the zinc alloy each with an amount of less than 0.001 wt%.
  • Using the refiner of the present application can achieve the refining effect of the master alloy while ensuring good polishing performance.
  • the problem of polishing hardpoints caused by the use of intermediate alloy containing RE or Zr or B can be avoided.
  • the mirror polishing contour requirements can be met.
  • aluminum is the main alloy element, which functions to prevent the oxidation of zinc liquid, improve the surface quality of the casting, reduce the brittleness of the casting, and reduce the corrosion of zinc to the iron crucible.
  • the addition of aluminum can also modify the grains and improve the strength and hardness of the alloy.
  • the Al amount of the present application is 3.9-4.1 wt%. When the Al amount is less than 3.5 wt%, the fluidity of the alloy becomes poor, and the casting molding defect rate increases.
  • Adding magnesium to the zinc alloy of the present application can significantly reduce the intergranular corrosion tendency of the alloy and improve the corrosion resistance of the alloy. This is also the meaning of the initial addition of magnesium.
  • the addition of magnesium by those skilled in the art is generally controlled at 0.03-0.06%. This amount is not high in the entire alloy system. Therefore, those skilled in the art usually do not pay attention to the influence of this amount.
  • the inventors did not actually pay attention to the influence of this element, and mainly considered the influence of other main elements on alloy properties. However, it was found that the control of other elements could not solve the defect of hot cracking. In an accidental experiment, the inventor added an insufficient amount of magnesium and found that no hot cracking defect occurred.
  • the inventor began to study the influence of magnesium on zinc alloys. It was found that magnesium can not only modify the crystal grains and increase the strength of the alloy but more unexpectedly, by controlling the amount of magnesium, the defects of hot cracks can be significantly overcome.
  • the amount of Mg is controlled at 0.005 ⁇ 0.018 wt%. When the amount of Mg is less than 0.005 wt%, the alloy has poor corrosion resistance and reduced dimensional stability. When the amount of Mg is higher than 0.018 wt%, the alloy has an obvious hot cracking tendency and decreased plasticity.
  • the selective addition of a small amount of copper to the zinc alloy of the present application can improve the fluidity of the alloy and increase the strength of the alloy, and also help to improve the hot crack resistance of the alloy.
  • the amount of Cu amount added is controlled at 0.2-1.0 wt%. On the one hand, a higher Cu amount increases the cost of raw materials. On the other hand, as the Cu amount increases, although the strength of the alloy increases, it increases the intergranular corrosion tendency of the alloy.
  • the amount of any single element is less than 0.001 wt%. This is of great significance for ensuring the high-quality polishing performance of the alloy and reducing the tendency of forming cracks and intergranular corrosion.
  • the zinc alloy of the present application has at least the following beneficial effects:
  • the zinc alloy produced by the method of the present application has a significant thermal crack resistance effect.
  • the thermal crack defect rate can be reduced by more than 50%, and the abnormal processing time of the product can be reduced, thereby effectively increasing the production capacity and improving the market competitiveness of the product.
  • the zinc alloy resulting from the method of the present application has significant thermal crack resistance and polishability, and excellent electroplating performance.
  • the alloy can meet the high surface quality requirements of castings, and is suitable for die-casting production of components of plumbing and bathroom accessories, small hardware accessories, electronic appliances, toys, and the like, and is especially suitable for cast products prone to hot cracks.
  • compositions of the alloys of the present application and the comparative alloys are shown in Table 1.
  • the alloy of the present application and the comparative alloy are prepared according to the following steps: weighing zinc ingots, aluminum ingots, magnesium ingots and selectively electrolytic copper according to the composition of the zinc alloy; adding the aluminum ingots, and selectively electrolytic copper, and 1/3 of the zinc ingots at the bottom of a furnace, stirring evenly after all materials are melted, adding the remaining zinc ingots, and using a bell to press the magnesium ingot to the bottom of the furnace at about 540°C after the materials are all melted, after the magnesium ingot is melted, selectively adding a refiner; which may be titanium salt, adding a purifying agent for purifying after the refiner is fully reacted, then removing residue and gas, allowing a product to stand after a composition test is qualified and casting after slagging and taking out of the furnace.
  • a refiner which may be titanium salt, adding a purifying agent for purifying after the refiner is fully reacted, then removing residue and gas, allowing a product to stand after a composition
  • the alloy of the present application is a boat-shaped ingot for remelting.
  • Performance testing of the alloy of the present application and the comparative alloy is carried out.
  • the specific performance testing items and basis are as follows:
  • the flow length of the melt is measured using a spiral specimen commonly used in casting alloys, and the fluidity of the alloy is evaluated, which is used to evaluate the casting performance of alloys 1-8 of the present application and comparative alloys 1-6. All samples are cast by hand, and the casting temperature is 420°C ⁇ 2°C. The results are shown in Table 2.
  • the same mold, the same die-casting machine, the same die-casting parameters, the same operator are used to die cast the alloy 1-8 of the present application and the comparative alloy 1-6 to form the same product, with a die-casting temperature of 420°C ⁇ 10°C.
  • the defective rates regarding die-casting cracks are shown in Table 2.
  • Example alloys 1,2 and 4 fall outside the scope of protection.
  • Table 1 The composition of the alloys of the present application and the comparative alloys (wt%) Example Al Mg Cu Other elements Refiner Zn Alloys of the present application 1 3.50 0.005 added the remainder 2 3.70 0.01 the remainder 3 3.90 0.007 the remainder 4 4.30 0.01 the remainder 5 4.1 0.015 0.2 the remainder 6 3.90 0.008 0.5 the remainder 7 4.05 0.01 0.7 the remainder 8 3.98 0.01 1.0 added the remainder Comparative alloy 1 ZAMAK 3 4.05 0.03 not added the remainder Comparative alloy 2 ZAMAK 5 3.98 0.05 0.7 not added the remainder Comparative alloy 3 4.08 0.04 Zr:0.04 not added the remainder Comparative alloy 4 4.12 0.05 0.8 Ti:0.03 not added the remainder Comparative alloy 5 3.95 0.06 Mn:0.5 not added the remainder Bi:0.2 Comparative alloy 6 4.20 0.03 Sb:0.03 not added the remainder Table 2 Performances of the alloys of the present application and comparative alloys Example Casting performance Polishing performance Resistance to hot crack /hot crack defective rate flow length
  • the alloy of the present application has fluidity equivalent to that of ZAMAK3 and ZAMAK5 zinc alloys, but its resistance to hot cracking is significantly better than that of ZAMAK3 and ZAMAK5.
  • the polishing performance of alloys 1- 8 of the present application is better than that of comparative alloys 3 and 4.
  • alloys 3, 5, 6, 7, and 8 of the present application have the best comprehensive properties such as crack resistance and polishing performance relatively.
  • Alloys 3 and 8 of the present application which have an added refiner have better crack resistance.
  • the crack resistance of comparative alloys 1-6 is not as good as that of the alloy of the present application.
  • the crack resistance of comparative alloys 3-4 is relatively good, but the polishing performance thereof is poor, and thus they are not suitable for application to exterior parts of a bathroom with high polishing requirements.
  • the alloy resulting from the method of the present application has good casting properties, excellent crack resistance, excellent polishing, and electroplating properties, and is suitable for die-casting and gravity casting to produce components of plumbing, sanitary ware, hardware accessories, electronic appliances, toys, and the like, especially suitable for casting products prone to forming cracks.

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Description

    TECHNICAL FIELD
  • The invention relates to the technical field of alloys and specifically relates to a zinc alloy with excellent crack resistance and a manufacturing method thereof.
  • BACKGROUND
  • Zinc alloy for die casting is an alloy formed by adding other elements based on zinc. Commonly added alloying elements are aluminum, copper, magnesium, cadmium, lead, titanium, and the like. Zinc alloy has a low melting point and good fluidity and is convenient for welding, brazing and plastic processing. Zinc alloy is corrosion resistant in the atmosphere, and the residual material is easy to recycle and remelt. However, Zinc alloy has a low creep strength and is susceptible to natural aging, which may cause dimensional changes.
  • Commonly used zinc alloys for die-casting are ZAMAK3 alloy and ZAMAK5 alloy. The composition of these two alloys is relatively simple. Initially, they mainly contain zinc and aluminum, and sometimes copper is added. Such alloys have poor corrosion resistance. In order to improve the corrosion resistance, researchers introduced magnesium. As a result, it has been found that the intergranular corrosion performance was significantly improved after the addition of magnesium, and the alloy strength was improved. Therefore, the currently marketed ZAMAK3 alloy and ZAMAK5 alloy are both added with magnesium element and the amount of magnesium is controlled at 0.03-0.06%.
  • Among the alloys for die-casting, ZAMAK3 alloy has been widely used in the bathroom hardware industry due to its excellent comprehensive performance and low cost. However, for some three-way and four-way hardware products with small R angles, when using ZAMAK3 alloy, thermal cracks are likely to occur at the R angle, and the crack rate when forming is 100%. The product design is limited by customer requirements, and the R angle cannot be modified at will, and thus the crack cannot be resolved. Compared with ZAMAK3 alloy, ZAMAK5 alloy has higher hardness and strength, and lower flexibility. However, this alloy also has similar defects as ZAMAK3 alloy that is prone to hot cracks.
    DE 2142685 A1 discloses so-called superplastic zinc alloys that are processable with little effort and without crack formation. In the superplastic state, the resistance of such zinc alloys to deformation is low, so that when tensile strain of several 100% is used even 1000 to 2000% of the original length can be achieved. Zinc alloys are rendered superplastic by thermal-mechanical treatment above half their absolute melting temperature. It is furthermore disclosed in DE 2142685 A1 that a significant increase in the creep strength can be achieved by subsequent heat treatment of the product at a temperature above 275° C and subsequent slow cooling. However, the high superplasticity of the alloy is lost as a result of such a treatment. In all examples, the zinc alloys are treated by hot and cold rolling. In contrast, the zinc alloy of the present invention is cast in the molten state.
    CN 108504900 A1 discloses zinc alloys with 4.3% Al, 0.007% Mg and 0.4% Cu and, respectively, 4.35% Mg, 0.001 % Mg and 0.45% Cu.
  • SUMMARY
  • In order to overcome the above shortcomings of the prior art, the inventor of the present application has conducted thorough research on the existing zinc alloys and provided a method for producing a zinc alloy as specified in claims 1-4 with excellent thermal crack resistance. The zinc alloy has excellent comprehensive properties. In particular, the thermal crack resistance is significantly improved, which can meet the high surface quality requirements of castings, especially die-castings, and can also be used in recast castings. It is suitable for the production of components of plumbing and sanitary ware, hardware accessories, electronic appliances, toys, and the like. The alloy can significantly increase the product forming yield rate, reduce the abnormal processing time of the product, and effectively increase the production capacity, thereby improving the market competitiveness of the product.
  • The purpose of the present application is achieved through the following technical solutions.
  • The present application provides a method for producing a zinc alloy with excellent crack resistance, wherein the alloy contains Al at an amount of 3.9-4.1 wt% and Mg at an amount of 0.005-0.018 wt%, optionally Cu at an amount of 0.2-1.0 wt%, and the rest of the alloy is Zn and unavoidable impurities. The zinc alloy is obtainable by a method comprising the following steps: weighing zinc ingots, aluminum ingots, magnesium ingots and/or selectively added electrolytic copper according to the composition of the zinc alloy; adding the aluminum ingots, and/or selectively added electrolytic copper, and 1/3 of the zinc ingots at a bottom of a furnace, stirring evenly after all materials are melted, adding the remaining zinc ingots, and using a bell to press the magnesium ingot to the bottom of the furnace at about 540°C after the materials are all melted, after the magnesium ingot is melted, adding selectively a refiner, adding a purifying agent for purifying after the refiner is fully reacted, then removing residue and gas, allowing a product to stand after a composition test is qualified, and casting boat-shaped ingots after slagging and taking out of the furnace, wherein the refiner is a salt refiner containing a titanium salt or a boron salt or a composite of both, and is not an intermediate alloy containing RE or Zr or B.
  • Preferably, the amount of Mg in the alloy is 0.005-0.015 wt%. Preferably, the amount of Cu in the zinc alloy is 0.5-1.0 wt%. Preferably the alloy does not contain Zr, Sb, Cr, Mn, Ti, Bi, Se, Ni and the like, except that these elements are present as impurities in the zinc alloy each with an amount of less than 0.001 wt%.
  • Using the refiner of the present application can achieve the refining effect of the master alloy while ensuring good polishing performance. The problem of polishing hardpoints caused by the use of intermediate alloy containing RE or Zr or B can be avoided. Thus the mirror polishing contour requirements can be met.
  • In the zinc alloy of the present application, aluminum is the main alloy element, which functions to prevent the oxidation of zinc liquid, improve the surface quality of the casting, reduce the brittleness of the casting, and reduce the corrosion of zinc to the iron crucible. In addition, the addition of aluminum can also modify the grains and improve the strength and hardness of the alloy. The Al amount of the present application is 3.9-4.1 wt%. When the Al amount is less than 3.5 wt%, the fluidity of the alloy becomes poor, and the casting molding defect rate increases.
  • Adding magnesium to the zinc alloy of the present application can significantly reduce the intergranular corrosion tendency of the alloy and improve the corrosion resistance of the alloy. This is also the meaning of the initial addition of magnesium. The addition of magnesium by those skilled in the art is generally controlled at 0.03-0.06%. This amount is not high in the entire alloy system. Therefore, those skilled in the art usually do not pay attention to the influence of this amount. In the initial development of the present application, the inventors did not actually pay attention to the influence of this element, and mainly considered the influence of other main elements on alloy properties. However, it was found that the control of other elements could not solve the defect of hot cracking. In an accidental experiment, the inventor added an insufficient amount of magnesium and found that no hot cracking defect occurred. Therefore, the inventor began to study the influence of magnesium on zinc alloys. It was found that magnesium can not only modify the crystal grains and increase the strength of the alloy but more unexpectedly, by controlling the amount of magnesium, the defects of hot cracks can be significantly overcome. In the present application, the amount of Mg is controlled at 0.005~0.018 wt%. When the amount of Mg is less than 0.005 wt%, the alloy has poor corrosion resistance and reduced dimensional stability. When the amount of Mg is higher than 0.018 wt%, the alloy has an obvious hot cracking tendency and decreased plasticity.
  • The selective addition of a small amount of copper to the zinc alloy of the present application can improve the fluidity of the alloy and increase the strength of the alloy, and also help to improve the hot crack resistance of the alloy. The amount of Cu amount added is controlled at 0.2-1.0 wt%. On the one hand, a higher Cu amount increases the cost of raw materials. On the other hand, as the Cu amount increases, although the strength of the alloy increases, it increases the intergranular corrosion tendency of the alloy.
  • When the elements Zr, Sb, Cr, Mn, Ti, Bi, and Se in the present application exist as impurities, the amount of any single element is less than 0.001 wt%. This is of great significance for ensuring the high-quality polishing performance of the alloy and reducing the tendency of forming cracks and intergranular corrosion.
  • Compared with the prior art, the zinc alloy of the present application has at least the following beneficial effects:
  • The zinc alloy produced by the method of the present application has a significant thermal crack resistance effect. Compared with the commonly used ZAMAK3 and ZAMAK5 alloys, the thermal crack defect rate can be reduced by more than 50%, and the abnormal processing time of the product can be reduced, thereby effectively increasing the production capacity and improving the market competitiveness of the product.
  • The zinc alloy resulting from the method of the present application has significant thermal crack resistance and polishability, and excellent electroplating performance. The alloy can meet the high surface quality requirements of castings, and is suitable for die-casting production of components of plumbing and bathroom accessories, small hardware accessories, electronic appliances, toys, and the like, and is especially suitable for cast products prone to hot cracks.
  • DETAILED DESCRIPTION OF EMBODIMENTS
  • The present application will be further described in detail below in conjunction with specific embodiments and drawings.
  • Example
  • The compositions of the alloys of the present application and the comparative alloys are shown in Table 1.
  • The alloy of the present application and the comparative alloy are prepared according to the following steps: weighing zinc ingots, aluminum ingots, magnesium ingots and selectively electrolytic copper according to the composition of the zinc alloy; adding the aluminum ingots, and selectively electrolytic copper, and 1/3 of the zinc ingots at the bottom of a furnace, stirring evenly after all materials are melted, adding the remaining zinc ingots, and using a bell to press the magnesium ingot to the bottom of the furnace at about 540°C after the materials are all melted, after the magnesium ingot is melted, selectively adding a refiner; which may be titanium salt, adding a purifying agent for purifying after the refiner is fully reacted, then removing residue and gas, allowing a product to stand after a composition test is qualified and casting after slagging and taking out of the furnace.
  • The alloy of the present application is a boat-shaped ingot for remelting.
  • Performance testing of the alloy of the present application and the comparative alloy is carried out. The specific performance testing items and basis are as follows:
  • 1. Casting performance
  • The flow length of the melt is measured using a spiral specimen commonly used in casting alloys, and the fluidity of the alloy is evaluated, which is used to evaluate the casting performance of alloys 1-8 of the present application and comparative alloys 1-6. All samples are cast by hand, and the casting temperature is 420°C±2°C. The results are shown in Table 2.
  • 2. Resistance to hot crack of the product
  • The same mold, the same die-casting machine, the same die-casting parameters, the same operator are used to die cast the alloy 1-8 of the present application and the comparative alloy 1-6 to form the same product, with a die-casting temperature of 420°C±10°C. The defective rates regarding die-casting cracks are shown in Table 2.
  • 3. Polishing performance
  • The castings are polished separately, and then observed with naked eyes. If there are no hard spots, the result is excellent and indicated by "O"; if the total number of hard spots is more than 3, and the diameter of each hard spot is less than 0.5 mm (0.01969 inch), the result is bad and indicated by "×." The results are shown in Table 2. Example alloys 1,2 and 4 fall outside the scope of protection. Table 1 The composition of the alloys of the present application and the comparative alloys (wt%)
    Example Al Mg Cu Other elements Refiner Zn
    Alloys of the present application 1 3.50 0.005 added the remainder
    2 3.70 0.01 the remainder
    3 3.90 0.007 the remainder
    4 4.30 0.01 the remainder
    5 4.1 0.015 0.2 the remainder
    6 3.90 0.008 0.5 the remainder
    7 4.05 0.01 0.7 the remainder
    8 3.98 0.01 1.0 added the remainder
    Comparative alloy 1 ZAMAK 3 4.05 0.03 not added the remainder
    Comparative alloy 2 ZAMAK 5 3.98 0.05 0.7 not added the remainder
    Comparative alloy 3 4.08 0.04 Zr:0.04 not added the remainder
    Comparative alloy 4 4.12 0.05 0.8 Ti:0.03 not added the remainder
    Comparative alloy 5 3.95 0.06 Mn:0.5 not added the remainder
    Bi:0.2
    Comparative alloy 6 4.20 0.03 Sb:0.03 not added the remainder
    Table 2 Performances of the alloys of the present application and comparative alloys
    Example Casting performance Polishing performance Resistance to hot crack /hot crack defective rate
    flow length /mm
    Alloys of the present application 1 240 ○ 5%
    2 255 ○ 8%
    3 262 ○ 2%
    4 280 ○ 5%
    5 257 ○ 3%
    6 268 ○ 2.5%
    7 259 ○ 3%
    8 276 ○ 1%
    Comparati ve alloys 1 (ZAMAK3) 251 ○ 100%
    2 (ZAMAK5) 243 ○ 90%
    3 238 × 85%
    4 240 × 80%
    5 228 ○ 90%
    6 234 ○ 75%
  • According to the performance test results in Table 2, it can be seen that as a casting alloy, the alloy of the present application has fluidity equivalent to that of ZAMAK3 and ZAMAK5 zinc alloys, but its resistance to hot cracking is significantly better than that of ZAMAK3 and ZAMAK5. The polishing performance of alloys 1- 8 of the present application is better than that of comparative alloys 3 and 4. Among them, alloys 3, 5, 6, 7, and 8 of the present application have the best comprehensive properties such as crack resistance and polishing performance relatively. Alloys 3 and 8 of the present application which have an added refiner have better crack resistance. The crack resistance of comparative alloys 1-6 is not as good as that of the alloy of the present application. The crack resistance of comparative alloys 3-4 is relatively good, but the polishing performance thereof is poor, and thus they are not suitable for application to exterior parts of a bathroom with high polishing requirements.
  • In summary, the alloy resulting from the method of the present application has good casting properties, excellent crack resistance, excellent polishing, and electroplating properties, and is suitable for die-casting and gravity casting to produce components of plumbing, sanitary ware, hardware accessories, electronic appliances, toys, and the like, especially suitable for casting products prone to forming cracks.
  • The above-mentioned embodiments are used to explain the present application, not to limit the present application.

Claims (4)

  1. A method for producing a zinc alloy with excellent crack resistance, containing
    Al at an amount of 3.9-4.1 wt%,
    Mg at an amount of 0.005-0.018 wt%,
    optionally Cu at an amount of 0.2-1.0 wt%,
    the remainder of the alloy being Zn and unavoidable impurities,
    comprising the following steps: weighing zinc ingots, aluminum ingots, magnesium ingots and/or selectively added electrolytic copper according to the composition of the zinc alloy; adding the aluminum ingots, and/or selectively added electrolytic copper, and 1/3 of the zinc ingots at a bottom of a furnace, stirring evenly after all materials are melted, adding the remaining zinc ingots, and using a bell to press the magnesium ingot to the bottom of the furnace at about 540°C after the materials are all melted, after the magnesium ingot is melted, adding selectively a refiner, adding a purifying agent for purifying after the refiner is fully reacted, then removing residue and gas, allowing a product to stand after a composition test is qualified, and casting boat-shaped ingots after slagging and taking out of the furnace, wherein the refiner is a salt refiner containing a titanium salt or a boron salt or a composite of both, and is not an intermediate alloy containing RE or Zr or B.
  2. The method according to claim 1, wherein the amount of Mg in the zinc alloy is 0.005-0.015 wt%.
  3. The method according to claim 1 or 2, wherein the amount of Cu in the zinc alloy is 0.5-1.0 wt%.
  4. The method according to claim 1, wherein the alloy does not contain Zr, Sb, Cr, Mn, Ti, Bi, Se, Ni and the like, except that these elements are present as impurities in the zinc alloy each with an amount of less than 0.001 wt%.
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