US2976192A - Process for improving the quality of copper-zirconium alloy castings - Google Patents
Process for improving the quality of copper-zirconium alloy castings Download PDFInfo
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- 238000005266 casting Methods 0.000 title claims description 67
- 238000000034 method Methods 0.000 title claims description 19
- XTYUEDCPRIMJNG-UHFFFAOYSA-N copper zirconium Chemical compound [Cu].[Zr] XTYUEDCPRIMJNG-UHFFFAOYSA-N 0.000 title description 13
- 229910001093 Zr alloy Inorganic materials 0.000 title description 12
- 229910045601 alloy Inorganic materials 0.000 claims description 42
- 239000000956 alloy Substances 0.000 claims description 42
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims description 28
- 229910052726 zirconium Inorganic materials 0.000 claims description 28
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 25
- 229910052802 copper Inorganic materials 0.000 claims description 25
- 239000010949 copper Substances 0.000 claims description 25
- 238000010583 slow cooling Methods 0.000 claims description 23
- 238000001816 cooling Methods 0.000 claims description 12
- 238000001556 precipitation Methods 0.000 claims description 6
- 230000001681 protective effect Effects 0.000 claims description 5
- 239000007787 solid Substances 0.000 claims description 5
- 238000010587 phase diagram Methods 0.000 claims description 3
- 230000000750 progressive effect Effects 0.000 claims 1
- 238000000265 homogenisation Methods 0.000 description 10
- 238000005336 cracking Methods 0.000 description 7
- 239000013078 crystal Substances 0.000 description 6
- 239000000463 material Substances 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 238000005275 alloying Methods 0.000 description 4
- 239000010439 graphite Substances 0.000 description 4
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 229910002091 carbon monoxide Inorganic materials 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 238000009413 insulation Methods 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000007669 thermal treatment Methods 0.000 description 2
- QORWJWZARLRLPR-UHFFFAOYSA-H tricalcium bis(phosphate) Chemical compound [Ca+2].[Ca+2].[Ca+2].[O-]P([O-])([O-])=O.[O-]P([O-])([O-])=O QORWJWZARLRLPR-UHFFFAOYSA-H 0.000 description 2
- 239000010455 vermiculite Substances 0.000 description 2
- 229910052902 vermiculite Inorganic materials 0.000 description 2
- 235000019354 vermiculite Nutrition 0.000 description 2
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- 235000008733 Citrus aurantifolia Nutrition 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 235000002918 Fraxinus excelsior Nutrition 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 235000011941 Tilia x europaea Nutrition 0.000 description 1
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- 239000002956 ash Substances 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910002056 binary alloy Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
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- 230000006735 deficit Effects 0.000 description 1
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- 229910052742 iron Inorganic materials 0.000 description 1
- 239000004571 lime Substances 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- 235000012245 magnesium oxide Nutrition 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
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- 239000000126 substance Substances 0.000 description 1
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Images
Classifications
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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
- C22F1/08—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
Definitions
- This invention relates to improvements in the thermal treatment of castings and relates more particularly to a process for the treatment of freshly poured castings made of copper and containing preferably within the maximum solid solubility limit of zirconium in said copper.
- the invention is useful for eliminating or greatly reducing the occurrence of intercrystalline cracking which has been heretofore encountered particularly in connection with the making of relatively large castings such as ingots, billets, bars, cakes and the like.
- Castings of most copper alloys are generally considered as being relatively free from residual stresses. However, some stresses are set up during solidlication and subsequent cooling and, in some instances, these may be sufciently high to cause intercrystalline cracks, primarily near the center line of the casting and occasionally on the casting surface. In the case of certain copper-base alloys, particularly where constituents present have either a low solubility in the alloy or a freezing point that differs appreciably from the major phase or phases, the occurrence of segregation is not uncommon. Usually a homogenizing treatment of the metal is essential or desirable before subjecting such material to working.
- 1t is therefore a principal object of this invention to provide an improved process for casting copper-zirconium alloys whereby the internal stresses are relieved tothe extent practically necessary for completely eliminating the occurrence of intercrystalline cracking notwithstanding the size or mass of the casting being produced.
- Another object of this invention is to provide an im-l proved process for the thermal treatment of freshly pouredA
- Fig. 2 is an enlarged schematic representation of the ⁇ alloy structure showing undissolved second phase accumulated in the crystal boundary region; Y
- Fig. 3 similarly illustrates the crystal boundary region with the residual second phase completely dissolved within the matrix material; and fj Fig 4 represents the cast structure upon further cooling .to temperatures below the solvus line wherein precipi- ⁇ .tation of the second phase is seen to be uniformly distributed throughout the entire casting, p Y
- oxygen-free copper refers to a high purity copper which has been substantially freed of its oxygen content by any of the known methods4 ⁇ commonly employed for :the purpose before'addition of the alloying substance thereto.
- copper which has been produced in a reducing atmosphere such as OFHC brand copper is particularly suitable for making the copper-zirconium alloys in accordance with the proc? ess herein disclosed
- copper prepared in -an inert atmos-V phere, a vacuum or in accordance with any other of the conventional practices used for making oxygen-free copper is included within the meaning of the term.
- the in: vention is also applicable to copper-zirconium alloys made with chemically deoxidized copper wherein the copper is freed of its oxygen content by the addition of small ⁇ amounts of a deoxidizer such as phosphorus, lithium and the like.
- the maximum solid solubility of zirconiumiin,initially ⁇ oxygen-free copper is seen from Fig. l to-beclosefto 0.15% by weight at about 980 C.
- the amount of zirconium in the alloy may be varied generally between 0.01- to ⁇ 0r.l'5% or thereabouts with about 0.13% being preferred for production of alloys which are particularly suitable for most electrical and electronic applications of the alloy. Where maximum resistance to softening at velevated temperatures'V is desired, the amount of zirconium is increased accordingly.
- the preliminary steps involved in making the aforesaid alloys are carried out by melting the copper using a protective atmosphere such as carbon monoxide. After heating the oxygen-free copper or oxygen-freed copper preferably to about 1170-1200 C., a sufficient quantity of zirconium either as metal, sponge, master alloy or in any other form suitable for use in making the alloy is added to provide the desired zirconium content in the alloy. At the alloying stage, it is desirable to maintain a protective atmosphere of an inert gas such as argon in place of a reducing gas under which the copper is generally melted. Following an alloying period of about 2 to 5 minutes during which time the melt is stirred with a graphite plunger, the alloy is ready for casting within 5 to 10 minutes thereafter.
- a protective atmosphere such as carbon monoxide.
- the preferred casting temperatures are between 1150 and 1225 C. in connection with the use of either bottom pouring or lip pouring procedures which are equally satisfactory. Bone ash and silicone mold dressings are satisfactory for use in casting copperzirconium alloys of the type referred to herein.
- the freshly poured alloy casting of desired zirconium content is maintained at a suciently high temperature for a prolonged period of time to permit maximum dissolution of the zirconium in the copper upon soliditication of the casting.
- This may be readily accomplished by avoiding conditions conducive to rapid cooling of the casting following solidication thereof.
- it has been found essential to maintain the freshly poured solidied casting within a temperature range preferably between about 850 and 1000 C.
- This treatment coupled with further controlled slow cooling of the alloy at an average rate not exceeding 180 C. per hour starting at not lower than about 850 C. and continued until the casting reaches a temperature of about 400 C. and preferably closer to 300 C. has been found to be both critical and essential to the reliable production of sound castings. Thereafter, the casting may be quenched in accordance with conventional practices.
- the aforesaid controlled slow cooling of the casting after effective homogenization thereof requires a minimum period of at least 21A. hours to eect lowering of the temperature from about 850 to 400 C. or thereabouts.
- a slow cooling cycle of from 3 to 5 hours or even longer especially in the case of the relatively large size castings containing more than 0.1% zirconium.
- sound castings in all instances are assured with the use of controlled slow cooling cycles such that the average cooling rate within the designated range of temperature actually falls between 100 and 160 C. per hour.
- the critical slow cooling is satisfactorily accomplished by stripping the sufficiently solidified casting from the mold while still hot and immediately burying the same in vermiculite, ashes, lime, magnesia or any other suitable insulating material capable of preventing heat losses at an excessive rate.
- the same purposes namely, obtaining substantially complete homogenization while minimizing shrink stresses in the casting to the extent that virtually no intergranular cracking is encountered may be alternatively etected by the use of molds adapted to provide the prerequisite temperature control through the use of insulation, radiation shields and the like or the use of furnaces wherein the temperature can be properly controlled to provide the desired cooling rate.
- the stripping procedure with the controlled slow cooling being effected by the provision of adequate insulation around the casting being started above at least 850 C. as previously stated, and preferably above 880 C. and somewhat higher in the case of the relatively high zirconium content alloys. It should be readily apparent from the foregoing that the longer the holding time at temperatures within or close to the alpha solid solution temperature range for any particular alloy composition after sufficient solidiiication thereof, the more efficiently and effectively is the required homogenized condition achieved.
- the subsequent slow cooling was varied to the extent that from 21/2 to 12 hours was required to lower the temperature to 400 C. or thereabouts after which the castings were quenched. Some of the surface roughness caused by contacting the hot casting with vermieulite is removed by water quenching the alloy.
- the improvement comprising the steps of maintaining the cast molten alloy immediately following solidiication thereof for from teu to thirty minutes at a temperature above 880 C. and thereafter subjecting the casting to controlled slow cooling down to at least 400 C. at an average rate below 180 C. per hour.
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- Crystallography & Structural Chemistry (AREA)
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Description
March 21, 1961 M 1 SAARlvlRTA TAL 2,976,192
PROCESS FOR IMPROVING THE QUALITY OF' COPPER-ZIRCONIUM ALLOY CASTINGS Filed July 1, 1959 ATTORN @dice Patented Mar. 21, 1961 PROCESS FOR IMPROVING THE QUALITY OF COPPER-ZIRCONIUM ALLOY CASTINGS Matti J. Saarivirta, Plainfield, Archibald A. K. Booth, Jr., Elizabeth, and John J. Burgmeister, New Brunswick, NJ., assignors to American Metal Climax, Inc., New York, N.Y., a corporation of New York Filed July 1, 1959, Ser. No. 824,343
5 Claims. (Cl. 148-3) This invention relates to improvements in the thermal treatment of castings and relates more particularly to a process for the treatment of freshly poured castings made of copper and containing preferably within the maximum solid solubility limit of zirconium in said copper. The invention is useful for eliminating or greatly reducing the occurrence of intercrystalline cracking which has been heretofore encountered particularly in connection with the making of relatively large castings such as ingots, billets, bars, cakes and the like.
Castings of most copper alloys are generally considered as being relatively free from residual stresses. However, some stresses are set up during solidlication and subsequent cooling and, in some instances, these may be sufciently high to cause intercrystalline cracks, primarily near the center line of the casting and occasionally on the casting surface. In the case of certain copper-base alloys, particularly where constituents present have either a low solubility in the alloy or a freezing point that differs appreciably from the major phase or phases, the occurrence of segregation is not uncommon. Usually a homogenizing treatment of the metal is essential or desirable before subjecting such material to working.
ln 'the case of copper-zirconium alloys made preferably with initially oxygen-free copper and containing up to the maximum solid solubility of zirconium, which alloys are described in detail in U.S. Patent No. 2,842,438, little or no diiliculty is encountered in the making of relatively small size castings using conventional casting procedures utilizing, for example, a water-cooled mold. It has been found, however, that the making of sound castings of relatively large size as is commonly required in commercial practice presents a serious problem in that the formation of intercrystalline cracks becomes extremely difficult to avoid. With the occurrence of intercrystalline cracking in the cast condition, the resulting casting becomes highly susceptible to failure particularly during hot work-Y ing of the material. This, of course, imposes a serious limitation on the widespread use of the alloy notwithstanding the excellent combination of properties possessed by the material notably with respect to resistance to softening at elevated temperatures and good electrical conductivity among other highly desirable properties.
Onceintercrystalline cracking in the cast condition occurs, subsequent processing of the casting to eect homogenization within the cast structure as by solution heat treatment of the alloy is of little or no benefit concerning the aforesaid susceptibility of the material to failure upon hot working. Hot topping applied in accordance with conventional practices has also proven ineective with respect to intercrystalline. Although it has been long recognized that for some copper base materials slow cooling which may be achieved in various ways as by using a heated mold or a well insulated mold is beneiicial for producing improved casting soundness and good surface nishes, the conventional slow cooling cycles requiring generally under two hours have been found to provide no satisfactory solution of the problem in the case of copper-zirconium alloys. With the use of such slow cooling cycles in the case of some copper-base alloys, internal stresses may be minimized but frequently such treatment adversely all'ects the mechanical properties. For this reason slowcooling is generally avoided whenever possible in the making of copper-base alloys.v
It has now been discovered that when copper-zirconium alloys of the type herein designated are subjected to relatively prolonged slow cooling to provide ample time'for substantially complete homogenization of the zirconium in the copper and to enable gradual cooling of the alloy over an appreciably longer period of time than heretofore provided in the so-called slow cooling processes;
the castings made thereby are practically entirely free` of intercrystalline cracks regardless of the size of the casting. It has been further found that notwithstanding the use of a substantially prolonged cooling cy'cle, thereis, surprisingly enough, no impairment with respect .toA any of the mechanical properties of the alloy.
1t is therefore a principal object of this invention to provide an improved process for casting copper-zirconium alloys whereby the internal stresses are relieved tothe extent practically necessary for completely eliminating the occurrence of intercrystalline cracking notwithstanding the size or mass of the casting being produced.
Another object of this invention is to provide an im-l proved process for the thermal treatment of freshly pouredA Fig. 2 is an enlarged schematic representation of the` alloy structure showing undissolved second phase accumulated in the crystal boundary region; Y
Fig. 3 similarly illustrates the crystal boundary region with the residual second phase completely dissolved within the matrix material; and fj Fig 4 represents the cast structure upon further cooling .to temperatures below the solvus line wherein precipi-` .tation of the second phase is seen to be uniformly distributed throughout the entire casting, p Y
As used hereinthe term initially oxygen-free copper refers to a high purity copper which has been substantially freed of its oxygen content by any of the known methods4` commonly employed for :the purpose before'addition of the alloying substance thereto. Although copper which has been produced in a reducing atmosphere such as OFHC brand copper is particularly suitable for making the copper-zirconium alloys in accordance with the proc? ess herein disclosed, copper prepared in -an inert atmos-V phere, a vacuum or in accordance with any other of the conventional practices used for making oxygen-free copper is included within the meaning of the term. The in: vention is also applicable to copper-zirconium alloys made with chemically deoxidized copper wherein the copper is freed of its oxygen content by the addition of small` amounts of a deoxidizer such as phosphorus, lithium and the like.
The maximum solid solubility of zirconiumiin,initially` oxygen-free copper is seen from Fig. l to-beclosefto 0.15% by weight at about 980 C. Depending upon the properties desired, the amount of zirconium in the alloy may be varied generally between 0.01- to`0r.l'5% or thereabouts with about 0.13% being preferred for production of alloys which are particularly suitable for most electrical and electronic applications of the alloy. Where maximum resistance to softening at velevated temperatures'V is desired, the amount of zirconium is increased accordingly.
The preliminary steps involved in making the aforesaid alloys are carried out by melting the copper using a protective atmosphere such as carbon monoxide. After heating the oxygen-free copper or oxygen-freed copper preferably to about 1170-1200 C., a sufficient quantity of zirconium either as metal, sponge, master alloy or in any other form suitable for use in making the alloy is added to provide the desired zirconium content in the alloy. At the alloying stage, it is desirable to maintain a protective atmosphere of an inert gas such as argon in place of a reducing gas under which the copper is generally melted. Following an alloying period of about 2 to 5 minutes during which time the melt is stirred with a graphite plunger, the alloy is ready for casting within 5 to 10 minutes thereafter. The preferred casting temperatures are between 1150 and 1225 C. in connection with the use of either bottom pouring or lip pouring procedures which are equally satisfactory. Bone ash and silicone mold dressings are satisfactory for use in casting copperzirconium alloys of the type referred to herein.
For improving the quality of the copper-zirconium alloy castings in accordance with the present invention, the freshly poured alloy casting of desired zirconium content is maintained at a suciently high temperature for a prolonged period of time to permit maximum dissolution of the zirconium in the copper upon soliditication of the casting. This may be readily accomplished by avoiding conditions conducive to rapid cooling of the casting following solidication thereof. To obtain virtually complete homogenization of the alloy thereby avoiding the presence of any appreciable residual phase in the crystal boundaries as depicted in Fig. 2, it has been found essential to maintain the freshly poured solidied casting Within a temperature range preferably between about 850 and 1000 C. for a minimum period of to 15 minutes and preferably for about 15 to 30 minutes or even longer depending upon the size of the casting and the zirconium content of the alloy. This treatment coupled with further controlled slow cooling of the alloy at an average rate not exceeding 180 C. per hour starting at not lower than about 850 C. and continued until the casting reaches a temperature of about 400 C. and preferably closer to 300 C. has been found to be both critical and essential to the reliable production of sound castings. Thereafter, the casting may be quenched in accordance with conventional practices.
Time-wise, the aforesaid controlled slow cooling of the casting after effective homogenization thereof requires a minimum period of at least 21A. hours to eect lowering of the temperature from about 850 to 400 C. or thereabouts. Experience has shown, however, that it is generally advantageous to employ a slow cooling cycle of from 3 to 5 hours or even longer especially in the case of the relatively large size castings containing more than 0.1% zirconium. Generally speaking,sound castings in all instances are assured with the use of controlled slow cooling cycles such that the average cooling rate within the designated range of temperature actually falls between 100 and 160 C. per hour.
It will be readily apparent from the phase diagram ofthe copper-rich binary alloy system (Fig. 1) that the aforesaid homogenization can be more readily achieved within the alpha temperature range (between the solidus and solvus lines) at the relatively low zirconium concentrations of the alloy than at the higher zirconium con tent values. For this reason, Iit is important that the alloys containing more than 0.10% zirconium be kept at elevated temperatures somewhat above 900 C. and preferably about 950 C. for as long as possible and for at least l5 to 30 minutes, or even a longer period of time as previously stated. This ensures practically cornplete homogenization although the desired diffusion leading to the completely homogenized state schematically depicted in Fig. 3 apparently proceeds toward completion though at a much slower rate at temperatures below the solvus line. Such continued slow cooling controlled to provide a cooling rate of below C. afterl substant-ially complete homogenization of the alloy results in minimizing shrinkage stresses while effecting precipitation of the second phase uniformly within the crystals as schematically illustrated in Fig. 4. The latter obviously occurs only at temperatures below the solvus line and at a sufficiently high zirconium content to render the alloy precipitation hardenable.
In practice, the critical slow cooling is satisfactorily accomplished by stripping the sufficiently solidified casting from the mold while still hot and immediately burying the same in vermiculite, ashes, lime, magnesia or any other suitable insulating material capable of preventing heat losses at an excessive rate. The same purposes, namely, obtaining substantially complete homogenization while minimizing shrink stresses in the casting to the extent that virtually no intergranular cracking is encountered may be alternatively etected by the use of molds adapted to provide the prerequisite temperature control through the use of insulation, radiation shields and the like or the use of furnaces wherein the temperature can be properly controlled to provide the desired cooling rate. In commercial practice, however, it is preferred to use the stripping procedure with the controlled slow cooling being effected by the provision of adequate insulation around the casting being started above at least 850 C. as previously stated, and preferably above 880 C. and somewhat higher in the case of the relatively high zirconium content alloys. It should be readily apparent from the foregoing that the longer the holding time at temperatures within or close to the alpha solid solution temperature range for any particular alloy composition after sufficient solidiiication thereof, the more efficiently and effectively is the required homogenized condition achieved.
Parallel or tapered well molds of steel and cast iron treated with bone ash mold wash have proven satisfactory for use in the process herein described but in commercial practice graphite molds are preferred. No difculty was experienced in stripping castings from either type of mold at temperatures as high as 900 to 1030 C.
Numerous castings were made using either lip or bottom pouring methods, said castings consisting of 6, 8 and 10 inch diameter billets ranging in weight from 300 to 1000 pounds. In making 8" billets weighing 300 pounds, for example, the melts of initially oxygen-free copper were made using a graphite Crucible in a 300 pound capacity induction furnace. Alloying was achieved in some instances by the addition of a master alloy consisting of 30% zirconium, balance copper; other melts were successfully made using zirconium platelets. The melts maintained under a protective atmosphere of argon, nitrogen or carbon monoxide were cast into steel, iron and also graphite molds with either parallel sides or tapered sides (1/5" taper per foot). Castings containing 0.005, 0.03, 0.08, 0.10, 0.13, 0.14, and 0.15% zirconium were perfectly sound in every instance where immediately upon soliditication of the casting (at the temperature indicated by the solidus line in Fig. l) sulhcient time was allowed for effective homogenization following which controlled slow cooling was used. The same proved true in the case of the 1000 pound billets. The procedure used consisted of maintaining the solidified casting for from 10 to 30 minutes and generally from 15 to 25 minutes `at above 850 C. and, in the case of the castings containing 0.08% or more zirconium, above 900 C. after which the castings were removed from the mold and insulated in vermiculite. The subsequent slow cooling was varied to the extent that from 21/2 to 12 hours was required to lower the temperature to 400 C. or thereabouts after which the castings were quenched. Some of the surface roughness caused by contacting the hot casting with vermieulite is removed by water quenching the alloy.
Although castings of the alloy containing generally below 0.05% zirconium were not extremely susceptible to cracking in the absence of one or both of the above precautions, an appreciable number of such castings were nevertheless sub-standard as to their quality due to the presence of some intergranular cracking. With castings of a zirconium content above 0.08%, however, the results proved unfavorable in nearly all instances in that unsound castings were consistently obtained when (a) initial cooling of the solidified casting to about 850 C. or somewhat higher from the soliditication temperature which is generally over l000 C. was permitted to occur in less than l minutes, and (b) less than a 2%: hour minimum period was allowed for the subsequent slow cooling of the casting down to a temperature of at least 400 C. That both expedients are essential especially where the zirconium content exceeds 0.08% is illustrated by the failure of prolonged hornogenization treatment in the absence of the subsequent slow cooling to produce sound castings. Experience has also shown that the aforesaid subsequent controlled slow cooling is not particularly beneficial where the prior homogenization of the alloy at the elevated temperatures is circumvented by allowing the initially solidied casting to cool to below 900-850 C. too rapidly.
It will be seen from the foregoing that the production of sound castings of copper-zirconium alloys requires avoidance of any processing conditions which fail to substantially completely homogenize the yalloy since subsequent shrinkage stresses normally encountered in the relatively large-sized castings invariably cause `cracking at the zirconium-rich phase which freezes out last at the grain boundaries. Only by providing sufficient time for the alloy to become completely homogenized and thereby freeing the crystal boundaries from the second phase and improving cohesion between the crystals particularly near the center region of the casting and by the utilization of continued slow cooling under controlled conditions to prevent excessive shrinkage stresses has it been found possible to produce completely sound relatively large sized castings of this extremely useful alloy.
-Having thus described this invention, it will be apparent to those skilled in the art that other modifications are possible. It should therefore be understood that within the scope of the appended claims, this invention may be practiced otherwise than as specifically described.
We claim:
1. In a process for making sound castings of a precipitation hardenable copper-zirconium alloy, the improvement comprising the steps of maintaining the cast molten alloy immediately following solidication thereof at a temperature above 850 C. for at least ten minutes and thereafter controlling the cooling of the casting down to a temperature of at least 400 C. to provide an average cooling rate below 180 C. per hour. l
2. In a process for making sound castings of a precipitation hardenable alloy containing between 0.08 and `0.15 by weight zirconium with the balance being oxygenfree copper, the improvement comprising the steps of maintaining the cast molten alloy immediately following solidiication thereof for from teu to thirty minutes at a temperature above 880 C. and thereafter subjecting the casting to controlled slow cooling down to at least 400 C. at an average rate below 180 C. per hour.
3. The process of claim 2 wherein the controlled slow cooling is at an average rate between and 160 C. per hour.
4. The process of claim 2 wherein the casting is quenched following the controlled slow cooling thereof down to at least 400 C.
5. The process for making sound castings of a precipitation hardenable alloy made with initially oxygen-free copper containing withinthe maximum solid solubility limit of zirconium, comprising the steps of casting the molten alloy under a protective atmosphere, homogenizing the cast solidified alloy for at least 10 minutes at a temperature above the solvus line in the phase diagram of Figure l of the accompanying drawing for any par-- References Cited in the tile of this patent UNITED STATES PATENTS Klement July 9, 1957 Saarivirta et al. July 8, 1958
Claims (1)
- 5. THE PROCESS FOR MAKING SOUND CASTINGS OF THE PRECIPITATION HARDENABLE ALLOY MADE WITH INITALLY OXYTEN-FREE COPPER CONTAINING WITHIN THE MAXIMUM SOLID SOLUBILITY LIMIT OF ZIRCONIUM, COMPRISING THE STEPS OF CASTING THE MOLTEN ALLOY UNDER A PROTECTIVE ATOMSPHERE, HOMOGENIZING THE CAST SOLIDFIED ALLOY FRO AT LEAST 10 MINUTES AT A TEMPERATURE ABOVE THE SOLVUS LINE IN THE PHASE DIAGRAM OF FIGURE 1 OF THE ACCOMPANYING DRAWING FOR ANY PARTICULAR ZIRCONIUM CONTENT AND THEREAFTER SLOW COOLING THE SUBSTANTIALLY COMPLETELY HOMOGENIZED CASTING FROM A TEMPERATURE OF AT LEAST 850*C. SUCH THAT A PROGRESSIVE COOLING THEREOF DOWN TO 400 TO 300*C. REQUIRES A MINIMUM PERIOD OF AT LEAST TWO AND ONE-HALF HOURS.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US824343A US2976192A (en) | 1959-07-01 | 1959-07-01 | Process for improving the quality of copper-zirconium alloy castings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US824343A US2976192A (en) | 1959-07-01 | 1959-07-01 | Process for improving the quality of copper-zirconium alloy castings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2976192A true US2976192A (en) | 1961-03-21 |
Family
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US824343A Expired - Lifetime US2976192A (en) | 1959-07-01 | 1959-07-01 | Process for improving the quality of copper-zirconium alloy castings |
Country Status (1)
| Country | Link |
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| US (1) | US2976192A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3228805A (en) * | 1962-09-17 | 1966-01-11 | Texas Instruments Inc | Method of producing homogeneous thermoelectric alloy slugs |
| US4436600A (en) | 1982-03-25 | 1984-03-13 | Nippon Mining Co., Ltd. | Method for treatment of copper anodes to be electrorefined |
| US4474614A (en) * | 1983-02-14 | 1984-10-02 | Atlantic Richfield Company | Impurity segregation in copper by controlled cooling treatment |
| WO1994012786A1 (en) * | 1992-12-01 | 1994-06-09 | Hydro-Petro Technology, Inc. | Cast alloy article and method of making |
| US5451273A (en) * | 1992-12-01 | 1995-09-19 | Hydro-Petro Technology, Inc. | Cast alloy article and method of making and fuel filter |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2798826A (en) * | 1956-05-09 | 1957-07-09 | Ampco Metal Inc | Method of heat treating nickel bearing aluminum bronze alloys |
| US2842438A (en) * | 1956-08-02 | 1958-07-08 | American Metal Climax Inc | Copper-zirconium alloys |
-
1959
- 1959-07-01 US US824343A patent/US2976192A/en not_active Expired - Lifetime
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2798826A (en) * | 1956-05-09 | 1957-07-09 | Ampco Metal Inc | Method of heat treating nickel bearing aluminum bronze alloys |
| US2842438A (en) * | 1956-08-02 | 1958-07-08 | American Metal Climax Inc | Copper-zirconium alloys |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3228805A (en) * | 1962-09-17 | 1966-01-11 | Texas Instruments Inc | Method of producing homogeneous thermoelectric alloy slugs |
| US4436600A (en) | 1982-03-25 | 1984-03-13 | Nippon Mining Co., Ltd. | Method for treatment of copper anodes to be electrorefined |
| US4474614A (en) * | 1983-02-14 | 1984-10-02 | Atlantic Richfield Company | Impurity segregation in copper by controlled cooling treatment |
| WO1994012786A1 (en) * | 1992-12-01 | 1994-06-09 | Hydro-Petro Technology, Inc. | Cast alloy article and method of making |
| US5451273A (en) * | 1992-12-01 | 1995-09-19 | Hydro-Petro Technology, Inc. | Cast alloy article and method of making and fuel filter |
| WO1996019658A1 (en) * | 1994-12-21 | 1996-06-27 | Hydro-Petro Technology, Inc. | Cast alloy article and method of making and fuel filter |
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