US2909429A - Highly wear-resistant zinc base alloy and method of making same - Google Patents

Highly wear-resistant zinc base alloy and method of making same Download PDF

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US2909429A
US2909429A US520149A US52014955A US2909429A US 2909429 A US2909429 A US 2909429A US 520149 A US520149 A US 520149A US 52014955 A US52014955 A US 52014955A US 2909429 A US2909429 A US 2909429A
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alloy
manganese
zirconium
iron
zinc
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Robert F Thomson
James C Holzwarth
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Motors Liquidation Co
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Motors Liquidation Co
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C18/00Alloys based on zinc
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C20/00Alloys based on cadmium

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  • Zinc base alloys "commercially used today for drawing dies-and similar purposes usually possess inadequate wear properties for many requirements. it is therefore a principal objectof the present invention to overcome this deficiency by providing a zinc base alloy characterized by greatly increased .wear properties, high resistance to fracture, good, castability and homogeneity. his a further object of thi'sinvention to provide a drawing. die formed of an inexpensive zinc base alloy which possesses high wear resistance, a low melting point .and uniform shrinkage. I v
  • a small amount of magnesium also may be advantageously included in the alloy, In this type of zinc base alloy the and copper j are added to increase the'tensile strength and hardness and to reduce the solidification temperature of the alloy.
  • Magnesium is 9 preferably includedin the alloy to overcomethe corrosive influence. of any impurities. which maybe present in the alloy. It tliere'fore .promotes dimensional stability and prevents a decrease in the strength of the alloy on aging.
  • the resultant material is a longfwearing, generally homogenous alloy having'good castability properties.
  • the wear resistance of a zinc base: alloy may be improved by the inclusion of dispersed, hard particles .of nickel-titanium in the alloy.
  • iron-zirconiumma'nganes'ealloys do not contain any relatively critical nickel andhence'are preferred in theevent of a nickel shortage because of a national emergency or for other teristic of this alloy permits the exact size of castings to be predetermined with precision, eliminating the necessity for extensive use of profiling machines.
  • the subject alloy is ideally suited for use as a drawing die material since the processing of dies formed of this alloy is comparatively simple, requiring a minimum of equipment and labor. Cost is further reduced by the fact that this alloy can be remelted many times, permitting the material in obsolete dies to be almost entirely recovered. 7
  • this zinc base alloy can be cast and the diversity of forms into which, the molten alloy will flow make it a very desirable material for a variety of purposes. Furthermore, finished castings of'this alloy can be produced comparatively quickly, making them available for production use within a relatively short time.
  • the high Wear resistance of the final zinc base alloy is due to the presence of the dispersed, hard particles ofironzirconium-manganese alloy in the softer matrix. These particlesdo not readily float or settle 'out of the Zinc-rich melt since they have a specific gravity which closely approximates that of the melt, provided the iron content is not excessive.
  • the present invention provides an alloy. which has proper particle distribution, as Well as optimum particle size, resulting in physical characteristics wlll ich satisfy all requirements for an outstanding tool a 0y.
  • a desirable zinc base drawing die alloy which possesses exceptional wear resistance is one consisting essentially of about 2% to 5% aluminum, 0.5% to 5% copper, 1% to 3% hard particles of iron-zirconium-manganese and the balance substantially all zinc.
  • the inclusion of approximately v0.02% to 0.3% magnesium' is beneficial to reduce the corrosive tendencies of impurities such as lead, cadmium and It will be understood, of course, that the zinc base alloy also may contain small amounts of silicon and other elements as incidental impurities.
  • a zinc base alloy containing at least approximately zinc has its wear resistance appreciably improved by the presence of the aforementioned hard iron-zirconiummanganese particles. It will be understood, however, that the term zinc base alloy, as used herein, is intended to encompass those alloys in which zinc is the major constituent and preferably constitutes at least 50% of the alloy.
  • Wear resistance is a function of both the size and distribution of the hard iron-zirconium-manganese particles. Since particle size and distribution are dependent on such factors as metal viscosity, solidification rates and methods of alloying, this invention also provides a preferred procedure for preparing the zinc base In the case of a drawing die it is desirable to produce maximum wear resistance without causing scoring of the part being drawn.
  • the iron-zirconium-manganese alloy can be initially prepared by melting together the three individual constituents- Commercially pure zirconium and manganese may be conveniently employed. Theresultant pre-alloy also may contain small quantities of other metals, such as aluminum, silicon, chromium, magnesium and nickel. Normally the maximum amounts of these latter metals would not exceed approximately 5% aluminum, 2% silicon, 1% chromium, 1% magnesium and 0.5% nickel. These exact percentages of the minor constituents are not critical in most instances, however, and are listed as examples only.
  • iron-zirconium-manganese pre-alloy does not readily dissolve in the zinc-rich metal, it is preferred to introduce these hard particles by means of an intermediate alloy or hardener containing copper.
  • an intermediate alloy or hardener containing copper When the iron-zirconium-manganese is added to molten copper, it is transformed substantially into the molten state.
  • this hardener is preferably added to the zinc in the solid state.
  • the copper base intermediate alloy Since it is desirable to cast the copper base intermediate alloy in shapes in which the copperrich matrix will dissolve most readily in the molten zincrich alloy, it is preferred to form castings having a high ratio of surface area to volume, such as flat plates orthin sheets. Generally the formed iron-zirconium-manganese particles have diameters in the order of about 0.001 inch. If the particles are much smaller than this, the wear resistance of the final zinc base alloy is not increased the desired extent.
  • the copper or copper-rich matrix is dissolved, leaving the relatively insoluble network of ironzirconium-manganese suspended in the zinc as Wearresistant particles of appropriate size. Agitation of the zinc-rich melt causes these particles to become generally uniformly dispersed through the melt, and the particles remain so dispersed in the solidified zinc base casting.
  • the preferred drawing die alloy composition may be obtained by melting substantially pure zinc and, after elevating the temperature of the molten zinc to between about 950 F. and 1075 F., dissolving therein the appropriate amount of aluminum. This addition of aluminum retards drossing of the zinc at higher temperatures arid, if a cast iron melting pot is employed, it inhibits attack of the pot by the zinc-rich melt. After further raising the temperature of the melt to between approximately 1100 F. and 1300 F., the copper-iron-zirconium-man r 4 the bath. When the magnesium is dissolved, the final alloy may be cast to shape in suitable molds.
  • the aluminum can be introduced into the melt either before or after addition of the intermediate alloy, the above alloying sequence has been found to be most satisfactory. Alternatively, a portion of this aluminum may be added prior to the introduction of the intermediate alloy and the remaining aluminum added after this alloy addition.
  • the ironzirconium-manganese alloy have a density which approximates that of the zinc-rich melt in order to prevent flotation or segregation of the iron-zirconium-manganese particles.
  • the density of zinc at its melting point is 6.92 grams per cc., and the addition of about 4% aluminum and 3.25% copper changes the density of the resultant alloy to slightly over 6.9 grams per cc. Therefore, in order to obtain proper distribution of the iron-zirconiummanganese particles, it is desirable to form these particles of an alloy having a specific gravity of about 6.5 to 7.5 grams per cc. The density of iron-is 7.87 grams per cc.
  • an ironzirconium-manganese alloy consisting essentially of 50% iron, 25% zirconium and 25% manganese provides excel lent results.
  • Such an alloy has a calculated density of about 7.43 grams per cc., which is slightly higher than the specific gravity of the aforementioned zinc-rich melt.
  • the densities of zirconium and manganese permit the reduction or substantial elimination of iron in the pre-alloy insofar as the density requirement is concerned.
  • an alloy of 50% manganese and 50% zirconium has a calculated density of approximately 6.87 grams per cc. and is sulficiently dense so that the particles thereof will not present a serious floatation problem.
  • the present invention in its broader aspects is intended to encompass the use of zirconium-manganese particles as well as ironzirconium-manganese particles.
  • the pre-alloy preferably contains at least 30% iron, and the iron may constitute as much a's approximately 70% of the iron-zirconium-manganese alloy.
  • the wear resistance of a zinc base alloy may be substantially improved with an iron-zirconium-manganese pre-alloy comprising approximately 20% to 35% zirconium, 20% to 35 manganese and the balance iron.
  • an iron-zirconium-manganese pre-alloy comprising approximately 20% to 35% zirconium, 20% to 35 manganese and the balance iron.
  • Such a pre-alloy produces particles of optimum size and density. In some instances, however, the pre-alloy may contain as little as 15% or as much as 55% zirconium, and the manganese content likewise may vary from about 15% to 55%.
  • the iron-zirconium-manganese pre-alloy is mixed with the molten copper, usually at a temperature of 2200 F. to 2700 F., it is preferred to form an intermediate alloy containing approximately 55% to copper. If this alloy has a copper content less than 55 it is difiicult to place the copper-rich matrix of the copper-iron-zircomum-manganese intermediate alloy in solution in the zincrich melt. Therefore, a copper base alloy comprising about 3% to 20% zirconium, 3% to 20% manganese, 5% to 35 iron and the balance copper is appropriate for use in carrying out the present invention. In order to provide a zinc base alloy with approximately 0.5% to 4% iron-zirconium-manganese particles, the intermediate alloy normally constitutes about 1% to.9% of the final alloy, depending on the compositionof the pre-alloy,
  • the alloying procedure employed in forming the hardener is of importance in achieving optimum, results.
  • the iron-zirconium-manganese pre-alloy may be compounded by melting together the proper amounts of these elements, preferably ata temperature of approximately 2900 F. to 3100 F.
  • zirconium is a rather readily oxidizable and nitridable element
  • a wear test using this apparatus was conducted in which the specimen load was increased during a fivehour period from zero load and automatically adjusted to produce a constant frictional load rather than a constant load normal to the wheel.
  • This test included a ten minute run-in period in which only the weight of the specimen being tested and its holder bore against the wheel, a period of 1% hours to load the specimen to 500 pounds, a 30 minute period at500 pounds to establish the frictional characteristics, and the balance of the five hours run with this established value of friction maintained constant. After each test any loosely adher ing, deformed metal and burrs were removed from the Wear test sample, and loss in weight values were used in comparing the wear resistance of the specimens.
  • the zinc base alloy specimens formed from a zinc base alloy consisting essentially of 3.25% copper, 4% aluminum, 0.1% magnesium and the balance zinc showed an average Weight loss of 0.4764 gram.
  • a zinc base die alloy specimen of similar composition but containing the afore mentioned preferred amounts of the iron-zirconiummanganese particles lost an average of only approximate- 1y 0.0248 gram.
  • the results of this test show how greatly the presence of dispersed particles of the hard iron-zirconium-manganese alloy'increases the wear resistance of zinc base alloys.
  • a zinc base alloy characterized by high wear resistance consisting essentially of at least approximately zinc and about 1 to 3% of iron-zirconiurn-manganese particles dispersed throughout the alloy, said particles comprising approximately 30% to 70% iron, 15 to 55% zirconium and 15 to 55 manganese.
  • An alloy comprising approximately 2% to 5% aluminum, 0.5 to 5% copper, 0.5 to 4% hard particles of iron-zirconium-manganese alloyof which the zirconium and manganese each constitutes 15% to 55 and the balance substantially all zinc.
  • a highly wear-resistant zinc base alloy consisting essentially of about 2% to 5% aluminum, 0.5% to 5% copper, 0.02% to 0.3% magnesium, 0.5 to 4%. particles of iron-zirconium-manganese alloy and the balance zinc plus incidental impurities, said particles comprising approximately 30% to 70% iron, 15 to 55% zirconium and 15 to 55% manganese.
  • a casting alloy consisting essentially of about 3% to 5% aluminum, 2% to 3.5% copper, 0.05% to. 0.2% magnesium, approximately 1% to 3% hard iron-zircomum-manganese particles, and the balance substantially all zinc and incidental impurities, said par-ticles comprising approximately 30% to 70% iron, 15% to 55% zirconium and 15 to 55 manganese.
  • a zinc base alloy characterized by outstanding wear resistance and comprising approximately 2% to 5% aluminum, 0.5 to 5% copper, 0.2% to 2% iron, 0.15% to 1% zirconium, 0.15 to 1% manganese and the balance substantially all zinc plus incidental impurities, a substantial proportion of said iron, zirconium and manganese being present in the form of particles of iron-zirconium-manganese dispersed throughout said zinc base alloy.
  • An alloy consisting essentially of about 3% to 5% aluminum, 2% to 3.5% copper, 0.05% to 0.2% magnesium, 0.2% to 2% iron, 0.15% to 1% zirconium, 0.15% to 1% manganese and 87% to 93% zinc, a substantial proportion of said iron, zirconium and manganese being combined in the form of hard particles of iron-zirconium? manganese alloy.
  • a method of increasing the wear resistance of a zinc base alloy which comprises adding to a zinc-rich melt a pre-alloy constituting 0.5% to 4% of the final iron, and consisting essentially of about 30% to 70% iron, 15 to 55 zirconium and 15% to 55% manganese.
  • a method of preparing a highly wear-resistant zinc base alloy comprising adding to a zinc-rich melt a pre-alloy having a network of ironzirconium-manganese in a coppenrich matrix, said network comprising approximately 30% to 70% iron, to 55% zirconium and 15% to 55% manganese, said pre-alloy being added in an amount sufficient to cause the said iron-zirconium-manganese to constitute approximately 0.5% to 4% of the final alloy.
  • a wear-resistant zinc base alloy comprising dissolving in a zinc-rich melt a pre-alloy consisting essentially of about 5% to 35% iron, 3% to zirconium, 3% to 20% manganese and the balance substantially all copper, said prealloy being added in an amount sufficient to produce an iron-zirconium-manganese content in the final alloy of approximately 0.5 to 4%.
  • a process of forming a wear-resistant zinc base casting alloy which consists of melting commercially pure zinc, dissolving therein at a temperature of approximately 950 F. to 1075 F. a quantity of aluminum equal to 2% to 5% of the final alloy and a pre-alloy consisting essentially of about 55% to 90% copper, 5% to 35% iron, 3% to 20% zirconium and 3% to 20% manganese, said pre-alloy being added in an amount such that the sum of the iron, zirconium and manganese contents thereof constitute approximately 0.5% to 4% of the final zinc base alloy, and thereafter fiuxing the melt to remove objectionable oxides.
  • a process of forming a wear-resistant zinc base casting alloy which consists of melting commercially pure zinc, dissolving therein at a temperature of approximately 950 F. to 1075" F. a quantity of aluminum equal to about 2% to 5% of the final alloy, raising the temperature of the resultant zinc-rich meltto between approximately 1100" F. and 1300 F., thereafter adding to said melt a pre-alloy consisting of copper, iron, zi-rconium and manganese, the composition of said prealloy being such that the final alloy contains 2% to 5% aluminum, 0.5% to 5% copper, 0.2% to 2% iron, 0.15% to 1% zirconium and 0.15% to 1% manganese, lowering the temperature of the zinc-rich melt to about 900 F. to 950 F., fiuxing said melt to remove objectionable oxides, and subsequently dissolving in the melt an amount of magnesium equal to 0.02% to 0.3% of the final alloy.
  • a zinc base alloy characterized by high wear, resistance comprising at least 85% zinc, minor proportions of aluminum and copper, and approximately 0.5% to 4% hard iron-zirconium-manganese particles generally uniformly dispersed throughout said alloy, said particles consisting essentially of about 15%.to zirconium, 15% to 55% manganese and the balance substantially all 11'011.
  • a method of increasing the Wear resistance of a zinc base alloy which comprises adding to a zinc-rich melt comprising at least 85 zinc a pre-alloy containing an amount of zirconium-manganese effective to form in the resultant zinc base alloy, upon solidification thereof, about 0.5 to 4% dispersed, hard particles having a specific gravity of approximately 6.5 to 7.5 grams per cubic centimeter and containing at least 15 zirconium and at least 15% manganese.
  • a method of increasing the wear resistance of a zinc base alloy which comprises adding to a zinc-rich melt a pre-alloy containing iron-zirconium-manganese which forms in the resultant zinc base alloy, upon solidification thereof, an amount of dispersed, hard particles of iron-zirconium-manganese equal to approximately 0.5% to 4% of said zinc base alloy, said hard particles consisting essentially of about 30% to iron, 15 to 55% zirconium and 15% to 55% manganese.

Description

.Unitcd State P o 2,909,429 ,7 HIGHLY WEAR-RESISTANT ziNc BASE ALLOY AND METHOD OF MAKING SAME,
Robert F. Thomson, Grosse Pointe Woods, and James C. Holzwarth Birmingham, Mich., assignors to General Motors Corporation, Detroit, Mich.,,a corporation of Delaware 7 No Drawing. Application July 5, 1955 Serial No. 520,149
16 Claims. c1. 75-178) 2,909,429 Patented Oct. 20, 1959 ICC zinc-rich melt in the form of a copper base intermediate ing kettle being required. The uniform shrinkage characand a process forproducing such an alloy. More particularly, the invention pertains to an alloy of this type which is characterized by outstanding wear resistance properties due to the presenceof hard particles of an iron-zirconiummanganese alloy. v i
Zinc base alloys "commercially used today for drawing dies-and similar purposes usually possess inadequate wear properties for many requirements. it is therefore a principal objectof the present invention to overcome this deficiency by providing a zinc base alloy characterized by greatly increased .wear properties, high resistance to fracture, good, castability and homogeneity. his a further object of thi'sinvention to provide a drawing. die formed of an inexpensive zinc base alloy which possesses high wear resistance, a low melting point .and uniform shrinkage. I v
, Theseand other objects and advantages are attained in accordance with-the present invention with a zinc base alloy containing a small amount of dispersed particles of iron-zirconium-manganese alloy. These particles contain hard intermetallic compounds or phases of manganese-zirconium whichare primarily responsible for the outstanding wear resistance of the zinc base alloy; v
'In particular, we have found that a zinc base alloy which contains small amounts of copper and aluminum,
as well 55.1116, aforementioned hard particles of iron zirconium-manganese, ,isfespeciallysuitable for use as a 3' drawing die. A small amount of magnesium also may be advantageously included in the alloy, In this type of zinc base alloy the and copper j are added to increase the'tensile strength and hardness and to reduce the solidification temperature of the alloy. Magnesium is 9 preferably includedin the alloy to overcomethe corrosive influence. of any impurities. which maybe present in the alloy. It tliere'fore .promotes dimensional stability and prevents a decrease in the strength of the alloy on aging.
The resultant material is a longfwearing, generally homogenous alloy having'good castability properties. 7
i 'As disclosed in co-pending patent application Serial No. l78,34'5,file'd August 8, 1950,,lin the name of James Q. Holzwarth, new Patent'No. 2,720,459, patented October 11,1955, the wear resistance of a zinc base: alloy may be improved by the inclusion of dispersed, hard particles .of nickel-titanium in the alloy. However, iron-zirconiumma'nganes'ealloys do not contain any relatively critical nickel andhence'are preferred in theevent of a nickel shortage because of a national emergency or for other teristic of this alloy permits the exact size of castings to be predetermined with precision, eliminating the necessity for extensive use of profiling machines. Accordingly, the subject alloy is ideally suited for use as a drawing die material since the processing of dies formed of this alloy is comparatively simple, requiring a minimum of equipment and labor. Cost is further reduced by the fact that this alloy can be remelted many times, permitting the material in obsolete dies to be almost entirely recovered. 7
In addition, the facility with which this zinc base alloy can be cast and the diversity of forms into which, the molten alloy will flow make it a very desirable material for a variety of purposes. Furthermore, finished castings of'this alloy can be produced comparatively quickly, making them available for production use within a relatively short time.
The high Wear resistance of the final zinc base alloy is due to the presence of the dispersed, hard particles ofironzirconium-manganese alloy in the softer matrix. These particlesdo not readily float or settle 'out of the Zinc-rich melt since they have a specific gravity which closely approximates that of the melt, provided the iron content is not excessive. Hence the present invention provides an alloy. which has proper particle distribution, as Well as optimum particle size, resulting in physical characteristics wlll ich satisfy all requirements for an outstanding tool a 0y.
Commercially satisfactory results may be obtained in accordance with our invention with a final zi-nc base alloy containing approximately 1% to 3% by weight of hard particles of iron-zirconium-manganese alloy. However, the iron-zirconium-manganese particles maybe present in amounts as large as about 4% by ,weight, and in some instances a noticeable improvement in Wear resistance results when these particles constitute as little as about 0.5% of the zinc base alloy. If the alloy contains more than approximately 4% of these particles, the castability of the alloy is impaired audits cost becomes excessive. Hence, a desirable zinc base drawing die alloy which possesses exceptional wear resistance is one consisting essentially of about 2% to 5% aluminum, 0.5% to 5% copper, 1% to 3% hard particles of iron-zirconium-manganese and the balance substantially all zinc. The inclusion of approximately v0.02% to 0.3% magnesium'is beneficial to reduce the corrosive tendencies of impurities such as lead, cadmium and It will be understood, of course, that the zinc base alloy also may contain small amounts of silicon and other elements as incidental impurities.
Thus it can be seen that in accordance with our invention a zinc base alloy containing at least approximately zinc has its wear resistance appreciably improved by the presence of the aforementioned hard iron-zirconiummanganese particles. It will be understood, however, that the term zinc base alloy, as used herein, is intended to encompass those alloys in which zinc is the major constituent and preferably constitutes at least 50% of the alloy.
More specifically, we have obtained outstanding wear characteristics in a cast alloy consisting essentially of 87% to 93% zinc, 3% to 5% aluminum, 2% to 3.5% copper, 0.05% to 0.2% magnesium, and 1% to 3% ironzirconiuIn-manganese alloy in the form of dispersed hard particles, An alloy consisting of approximately 4% aluminum, 0.15% magnesium, 3.25% copper, 1.5% ironzirconium-manganese and the balance zinc plus incidental alloy.
impurities appears to possess optimum castability and wear resistance properties.
Wear resistance, of course, *is a function of both the size and distribution of the hard iron-zirconium-manganese particles. Since particle size and distribution are dependent on such factors as metal viscosity, solidification rates and methods of alloying, this invention also provides a preferred procedure for preparing the zinc base In the case of a drawing die it is desirable to produce maximum wear resistance without causing scoring of the part being drawn.
The iron-zirconium-manganese alloy can be initially prepared by melting together the three individual constituents- Commercially pure zirconium and manganese may be conveniently employed. Theresultant pre-alloy also may contain small quantities of other metals, such as aluminum, silicon, chromium, magnesium and nickel. Normally the maximum amounts of these latter metals would not exceed approximately 5% aluminum, 2% silicon, 1% chromium, 1% magnesium and 0.5% nickel. These exact percentages of the minor constituents are not critical in most instances, however, and are listed as examples only.
Inasmuch as the iron-zirconium-manganese pre-alloy does not readily dissolve in the zinc-rich metal, it is preferred to introduce these hard particles by means of an intermediate alloy or hardener containing copper. When the iron-zirconium-manganese is added to molten copper, it is transformed substantially into the molten state. During solidification of the intermediate alloy, there appears to be a decrease in the solubility of the iron-zirconiummanganese alloy in the copper, and this alloy is therefore preferentially isolated as a network in the copper-rich matrix. In order to form long-wearing particles of suitable size, this hardener is preferably added to the zinc in the solid state. Since it is desirable to cast the copper base intermediate alloy in shapes in which the copperrich matrix will dissolve most readily in the molten zincrich alloy, it is preferred to form castings having a high ratio of surface area to volume, such as flat plates orthin sheets. Generally the formed iron-zirconium-manganese particles have diameters in the order of about 0.001 inch. If the particles are much smaller than this, the wear resistance of the final zinc base alloy is not increased the desired extent.
Upon introduction of the intermediate alloy to the zinc-rich melt, the copper or copper-rich matrix is dissolved, leaving the relatively insoluble network of ironzirconium-manganese suspended in the zinc as Wearresistant particles of appropriate size. Agitation of the zinc-rich melt causes these particles to become generally uniformly dispersed through the melt, and the particles remain so dispersed in the solidified zinc base casting.
The preferred drawing die alloy composition may be obtained by melting substantially pure zinc and, after elevating the temperature of the molten zinc to between about 950 F. and 1075 F., dissolving therein the appropriate amount of aluminum. This addition of aluminum retards drossing of the zinc at higher temperatures arid, if a cast iron melting pot is employed, it inhibits attack of the pot by the zinc-rich melt. After further raising the temperature of the melt to between approximately 1100 F. and 1300 F., the copper-iron-zirconium-man r 4 the bath. When the magnesium is dissolved, the final alloy may be cast to shape in suitable molds.
Although the aluminum can be introduced into the melt either before or after addition of the intermediate alloy, the above alloying sequence has been found to be most satisfactory. Alternatively, a portion of this aluminum may be added prior to the introduction of the intermediate alloy and the remaining aluminum added after this alloy addition.
As hereinbefore explained, it is desirable that the ironzirconium-manganese alloy have a density which approximates that of the zinc-rich melt in order to prevent flotation or segregation of the iron-zirconium-manganese particles. The density of zinc at its melting point is 6.92 grams per cc., and the addition of about 4% aluminum and 3.25% copper changes the density of the resultant alloy to slightly over 6.9 grams per cc. Therefore, in order to obtain proper distribution of the iron-zirconiummanganese particles, it is desirable to form these particles of an alloy having a specific gravity of about 6.5 to 7.5 grams per cc. The density of iron-is 7.87 grams per cc. and the density of manganese is 7.2 grams per cc., while the density of commercially available zirconium is about 6.5 grams per cc. Hence, we have found that an ironzirconium-manganese alloy consisting essentially of 50% iron, 25% zirconium and 25% manganese provides excel lent results. Such an alloy has a calculated density of about 7.43 grams per cc., which is slightly higher than the specific gravity of the aforementioned zinc-rich melt.
It will be noted, however, that the densities of zirconium and manganese permit the reduction or substantial elimination of iron in the pre-alloy insofar as the density requirement is concerned. For example, an alloy of 50% manganese and 50% zirconium has a calculated density of approximately 6.87 grams per cc. and is sulficiently dense so that the particles thereof will not present a serious floatation problem. Hence, the present invention in its broader aspects is intended to encompass the use of zirconium-manganese particles as well as ironzirconium-manganese particles. Generally, however, it is much preferred to include iron in the pre-alloy since this reduces the cost of the resultant material to an appreciable extent and conserves the use of relatively scarce manganese and zirconium. Thus, the pre-alloy preferably contains at least 30% iron, and the iron may constitute as much a's approximately 70% of the iron-zirconium-manganese alloy.
We prefer to have a ratio of zirconium to manganese in the iron-zirconium-manganese alloy of about 1 to 1, but an appreciable variation in the relative amounts of these three constituents is permissible. Thus we have found that the wear resistance of a zinc base alloy may be substantially improved with an iron-zirconium-manganese pre-alloy comprising approximately 20% to 35% zirconium, 20% to 35 manganese and the balance iron. Such a pre-alloy produces particles of optimum size and density. In some instances, however, the pre-alloy may contain as little as 15% or as much as 55% zirconium, and the manganese content likewise may vary from about 15% to 55%.
When the iron-zirconium-manganese pre-alloy is mixed with the molten copper, usually at a temperature of 2200 F. to 2700 F., it is preferred to form an intermediate alloy containing approximately 55% to copper. If this alloy has a copper content less than 55 it is difiicult to place the copper-rich matrix of the copper-iron-zircomum-manganese intermediate alloy in solution in the zincrich melt. Therefore, a copper base alloy comprising about 3% to 20% zirconium, 3% to 20% manganese, 5% to 35 iron and the balance copper is appropriate for use in carrying out the present invention. In order to provide a zinc base alloy with approximately 0.5% to 4% iron-zirconium-manganese particles, the intermediate alloy normally constitutes about 1% to.9% of the final alloy, depending on the compositionof the pre-alloy,
,af A r 4 although 3% to 6. 5% is preferredPWheri such an intermediate alloy is added to' a zinc-rich melt, it should introduce into the final alloy approximately 0.2% to 2% iron, 0.15% to 1% zirconium and 0.15% to 1% manganese in the form of iron-zirconium-manganese particles and about 0.5% to 5% copper which is not combined with these particles.
Since the hard particles result principally from the combination of zirconium and manganese and are formed during the preparation of the pre-alloy, the alloying procedure employed in forming the hardener is of importance in achieving optimum, results. Accordingly, the iron-zirconium-manganese pre-alloy may be compounded by melting together the proper amounts of these elements, preferably ata temperature of approximately 2900 F. to 3100 F. Inasmuch as zirconium is a rather readily oxidizable and nitridable element, it is desirable to use an inert gas as the melting atmosphere. We have obtained most satisfactory melting and high zirconium recovery using an induction furnace under an argon atmosphere.
It will be noted that it is necessary to form'particles of manganese-zirconium or iron-zirconium-manganese in order to obtain high wear and score resistance in accordance with the invention. Merely adding the iron, zir conium and manganese separately to the zinc-rich melt, even if these constituents are introduced in the aforementioned preferred proportions, does not form these hard particles or provide the necessary wear resistance. It is the alloy of iron, zirconium and manganese, rather than the individual elements, which contributes the desirable properties of wear and score resistance to the final zinc base alloy.
Wear tests were conducted to compare zinc base alloys formed in accordance with our invention withthe same material devoid of iron-zirconium-manganese particles. Samples 1 /8 inch wide and 42 inch high were prepared from the cast zinc base alloys to be tested, and each specimen was machined at one edge to prepare a inch by 1 /8 inch rubbing surface. The specimens were next successively locked in a fixture of a Wear test machine and placed in contact with a rotating smoothsurfaced wheel of low carbon steel having a face width of one inch. Increased wear resistance was measured by decreased weight loss in grams.
A wear test using this apparatus was conducted in which the specimen load was increased during a fivehour period from zero load and automatically adjusted to produce a constant frictional load rather than a constant load normal to the wheel. This test included a ten minute run-in period in which only the weight of the specimen being tested and its holder bore against the wheel, a period of 1% hours to load the specimen to 500 pounds, a 30 minute period at500 pounds to establish the frictional characteristics, and the balance of the five hours run with this established value of friction maintained constant. After each test any loosely adher ing, deformed metal and burrs were removed from the Wear test sample, and loss in weight values were used in comparing the wear resistance of the specimens.
At the end of the test period the zinc base alloy specimens formed from a zinc base alloy consisting essentially of 3.25% copper, 4% aluminum, 0.1% magnesium and the balance zinc showed an average Weight loss of 0.4764 gram. On the other hand, a zinc base die alloy specimen of similar composition but containing the afore mentioned preferred amounts of the iron-zirconiummanganese particles lost an average of only approximate- 1y 0.0248 gram. The results of this test show how greatly the presence of dispersed particles of the hard iron-zirconium-manganese alloy'increases the wear resistance of zinc base alloys.
Although the final alloy formed has been described as particularly suitable as a drawing die material, it also may be employed to considerable advantage in other 6 applications in which high wear resistance, good castabil ity, uniformity of properties throughout a cast section, good machinability, and anti-score properties are es importance. i
While we have set forthherein specific examples of zinc base alloys possessing high wear resistance characteristics due to the presence of hard particles of manganese-zirconium or iron-zirconium-manganese, it is not intended to restrict the invention to any specific zinc base alloy. We believe that we are the firstto discover the value of adding these particles to zinc base alloys generally, and the invention is not to be restricted except as defined in the following claims. 3 i
We claim: i V
1. A zinc base alloy characterized by high wear recomprising approximately 30% to 70% iron, 15% to 55% zirconium and 15% to 55 manganese.
3. A zinc base alloy characterized by high wear resistance consisting essentially of at least approximately zinc and about 1 to 3% of iron-zirconiurn-manganese particles dispersed throughout the alloy, said particles comprising approximately 30% to 70% iron, 15 to 55% zirconium and 15 to 55 manganese.
4. An alloy comprising approximately 2% to 5% aluminum, 0.5 to 5% copper, 0.5 to 4% hard particles of iron-zirconium-manganese alloyof which the zirconium and manganese each constitutes 15% to 55 and the balance substantially all zinc.
5. A highly wear-resistant zinc base alloy consisting essentially of about 2% to 5% aluminum, 0.5% to 5% copper, 0.02% to 0.3% magnesium, 0.5 to 4%. particles of iron-zirconium-manganese alloy and the balance zinc plus incidental impurities, said particles comprising approximately 30% to 70% iron, 15 to 55% zirconium and 15 to 55% manganese.
6. A casting alloy consisting essentially of about 3% to 5% aluminum, 2% to 3.5% copper, 0.05% to. 0.2% magnesium, approximately 1% to 3% hard iron-zircomum-manganese particles, and the balance substantially all zinc and incidental impurities, said par-ticles comprising approximately 30% to 70% iron, 15% to 55% zirconium and 15 to 55 manganese.
7. A zinc base alloy characterized by outstanding wear resistance and comprising approximately 2% to 5% aluminum, 0.5 to 5% copper, 0.2% to 2% iron, 0.15% to 1% zirconium, 0.15 to 1% manganese and the balance substantially all zinc plus incidental impurities, a substantial proportion of said iron, zirconium and manganese being present in the form of particles of iron-zirconium-manganese dispersed throughout said zinc base alloy.
'8. An alloy consisting essentially of about 3% to 5% aluminum, 2% to 3.5% copper, 0.05% to 0.2% magnesium, 0.2% to 2% iron, 0.15% to 1% zirconium, 0.15% to 1% manganese and 87% to 93% zinc, a substantial proportion of said iron, zirconium and manganese being combined in the form of hard particles of iron-zirconium? manganese alloy.
9. A method of increasing the wear resistance of a zinc base alloy which comprises adding to a zinc-rich melt a pre-alloy constituting 0.5% to 4% of the final iron, and consisting essentially of about 30% to 70% iron, 15 to 55 zirconium and 15% to 55% manganese.
10. In a method of preparing a highly wear-resistant zinc base alloy, the step which comprises adding to a zinc-rich melt a pre-alloy having a network of ironzirconium-manganese in a coppenrich matrix, said network comprising approximately 30% to 70% iron, to 55% zirconium and 15% to 55% manganese, said pre-alloy being added in an amount sufficient to cause the said iron-zirconium-manganese to constitute approximately 0.5% to 4% of the final alloy.
11. In a process of forming a wear-resistant zinc base alloy, the step which comprises dissolving in a zinc-rich melt a pre-alloy consisting essentially of about 5% to 35% iron, 3% to zirconium, 3% to 20% manganese and the balance substantially all copper, said prealloy being added in an amount sufficient to produce an iron-zirconium-manganese content in the final alloy of approximately 0.5 to 4%.
12. A process of forming a wear-resistant zinc base casting alloy which consists of melting commercially pure zinc, dissolving therein at a temperature of approximately 950 F. to 1075 F. a quantity of aluminum equal to 2% to 5% of the final alloy and a pre-alloy consisting essentially of about 55% to 90% copper, 5% to 35% iron, 3% to 20% zirconium and 3% to 20% manganese, said pre-alloy being added in an amount such that the sum of the iron, zirconium and manganese contents thereof constitute approximately 0.5% to 4% of the final zinc base alloy, and thereafter fiuxing the melt to remove objectionable oxides.
13. A process of forming a wear-resistant zinc base casting alloy which consists of melting commercially pure zinc, dissolving therein at a temperature of approximately 950 F. to 1075" F. a quantity of aluminum equal to about 2% to 5% of the final alloy, raising the temperature of the resultant zinc-rich meltto between approximately 1100" F. and 1300 F., thereafter adding to said melt a pre-alloy consisting of copper, iron, zi-rconium and manganese, the composition of said prealloy being such that the final alloy contains 2% to 5% aluminum, 0.5% to 5% copper, 0.2% to 2% iron, 0.15% to 1% zirconium and 0.15% to 1% manganese, lowering the temperature of the zinc-rich melt to about 900 F. to 950 F., fiuxing said melt to remove objectionable oxides, and subsequently dissolving in the melt an amount of magnesium equal to 0.02% to 0.3% of the final alloy.
14. A zinc base alloy characterized by high wear, resistance comprising at least 85% zinc, minor proportions of aluminum and copper, and approximately 0.5% to 4% hard iron-zirconium-manganese particles generally uniformly dispersed throughout said alloy, said particles consisting essentially of about 15%.to zirconium, 15% to 55% manganese and the balance substantially all 11'011.
15. A method of increasing the Wear resistance of a zinc base alloy which comprises adding to a zinc-rich melt comprising at least 85 zinc a pre-alloy containing an amount of zirconium-manganese effective to form in the resultant zinc base alloy, upon solidification thereof, about 0.5 to 4% dispersed, hard particles having a specific gravity of approximately 6.5 to 7.5 grams per cubic centimeter and containing at least 15 zirconium and at least 15% manganese.
16. A method of increasing the wear resistance of a zinc base alloy which comprises adding to a zinc-rich melt a pre-alloy containing iron-zirconium-manganese which forms in the resultant zinc base alloy, upon solidification thereof, an amount of dispersed, hard particles of iron-zirconium-manganese equal to approximately 0.5% to 4% of said zinc base alloy, said hard particles consisting essentially of about 30% to iron, 15 to 55% zirconium and 15% to 55% manganese.
References Cited in the file of this patent UNITED STATES PATENTS 2,048,288 Pierce et a1. July 21, 1936 2,372,546 Bunn Mar. 27, 1945 2,504,935 Morris Apr. 18, 1950 2,641,540 Mohling et al. June 9, 1953 2,747,989 Kirkby et al. May 29, 1956 2,795,501 Kelly June 11, 1957 FOREIGN PATENTS 296,780 Germany Mar. 13, 1915 OTHER REFERENCES Zirconium and Zirconium Alloys (published by ASM), Cleveland, Ohio (1953), pages 283-290 relied on.
entra.
KARL H; AXLINE UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No, 2,909,429
Robert F., Thomson et al.
October 20, 1959 It is hereby certified that error appears in the printed specificationof the above numbered patent requiring cor rection and that the said Letters Patent should read as cor rected below.
I Column 3, line 25 for "metal" read melt ---g column 6, line 7O for "iron" read alloy Signed and sealed this 16th day of August 1960:.
(SEAL) Attest:
ROBERT c. WATSON M tes ting Officer Commissioner of Patents

Claims (1)

1. A ZINC BASE ALLOY CHARACTERIZED BY HIGH WEAR RESISTANCE COMPRISING AT LEAST 85% ZINC AND ABOUT 0.5% TO 4% DISPERSED, HARD PARTICLES OF AN ALLOY CONTAINING AT LEAST 15% MANGANESE AND AT LEAST 15% ZIRCONIUM, SAID PARTICLES HAVING A SPECIFIC GRAVITY OF ABOUT 6.5 TO 7.5 GRAMS PER CUBIC CENTIMETER.
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US724891A US2883280A (en) 1955-07-05 1958-03-31 Ferrous base alloy

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3254993A (en) * 1963-03-18 1966-06-07 Ball Brothers Co Inc Zinc alloy and method of making same
US5945066A (en) * 1997-11-20 1999-08-31 Griffin; James D. Zinc-copper based alloy and castings made therefrom

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE296780C (en) *
US2048288A (en) * 1929-03-18 1936-07-21 New Jersey Zinc Co Zinc base alloy
US2372546A (en) * 1943-09-09 1945-03-27 Revere Copper & Brass Inc Zinc base alloy
US2504935A (en) * 1945-11-14 1950-04-18 Bridgeport Brass Co Copper base alloy and conductor and manufacture thereof
US2641540A (en) * 1951-07-19 1953-06-09 Allegheny Ludlum Steel Ferrous base chromium-nickel-titanium alloy
US2747989A (en) * 1952-05-28 1956-05-29 Firth Vickers Stainless Steels Ltd Ferritic alloys
US2795501A (en) * 1955-01-28 1957-06-11 Westinghouse Electric Corp Copper base alloys

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE296780C (en) *
US2048288A (en) * 1929-03-18 1936-07-21 New Jersey Zinc Co Zinc base alloy
US2372546A (en) * 1943-09-09 1945-03-27 Revere Copper & Brass Inc Zinc base alloy
US2504935A (en) * 1945-11-14 1950-04-18 Bridgeport Brass Co Copper base alloy and conductor and manufacture thereof
US2641540A (en) * 1951-07-19 1953-06-09 Allegheny Ludlum Steel Ferrous base chromium-nickel-titanium alloy
US2747989A (en) * 1952-05-28 1956-05-29 Firth Vickers Stainless Steels Ltd Ferritic alloys
US2795501A (en) * 1955-01-28 1957-06-11 Westinghouse Electric Corp Copper base alloys

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3254993A (en) * 1963-03-18 1966-06-07 Ball Brothers Co Inc Zinc alloy and method of making same
US5945066A (en) * 1997-11-20 1999-08-31 Griffin; James D. Zinc-copper based alloy and castings made therefrom

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