US3264694A - Method of casting - Google Patents

Method of casting Download PDF

Info

Publication number
US3264694A
US3264694A US398457A US39845764A US3264694A US 3264694 A US3264694 A US 3264694A US 398457 A US398457 A US 398457A US 39845764 A US39845764 A US 39845764A US 3264694 A US3264694 A US 3264694A
Authority
US
United States
Prior art keywords
titanium
zirconia
container
metal
melting
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US398457A
Inventor
Berthold C Weber
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US797309A external-priority patent/US3049432A/en
Application filed by Individual filed Critical Individual
Priority to US398457A priority Critical patent/US3264694A/en
Application granted granted Critical
Publication of US3264694A publication Critical patent/US3264694A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B60/00Obtaining metals of atomic number 87 or higher, i.e. radioactive metals
    • C22B60/02Obtaining thorium, uranium, or other actinides
    • C22B60/0291Obtaining thorium, uranium, or other actinides obtaining thorium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B34/00Obtaining refractory metals
    • C22B34/10Obtaining titanium, zirconium or hafnium
    • C22B34/12Obtaining titanium or titanium compounds from ores or scrap by metallurgical processing; preparation of titanium compounds from other titanium compounds see C01G23/00 - C01G23/08
    • C22B34/1295Refining, melting, remelting, working up of titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B34/00Obtaining refractory metals
    • C22B34/10Obtaining titanium, zirconium or hafnium
    • C22B34/14Obtaining zirconium or hafnium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22BPRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
    • C22B34/00Obtaining refractory metals
    • C22B34/30Obtaining chromium, molybdenum or tungsten
    • C22B34/32Obtaining chromium
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B15/00Single-crystal growth by pulling from a melt, e.g. Czochralski method
    • C30B15/10Crucibles or containers for supporting the melt
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S266/00Metallurgical apparatus
    • Y10S266/905Refractory metal-extracting means

Definitions

  • This invention relates to a container for the metals titanium, zirconium, hafnium and thorium and the like, in the Group IV-A, such as of the periodic chart of the elements in Metals Handbook published in 1948 by The American Society for Metals, 7301 Euclid Avenue, Cleveland 3, Ohio, at page 22, and more particularly to an improved container made of zirconia and these metals and the containers used for melting and casting these metals.
  • the invention described herein is the fruition of work done by the inventor in the science of ceramics.
  • the objects of the present invention are to provide new and superior compositions for the fabrication of crucibles, molds and the like used in melting metals, such as those in Group IV-A of the Periodic System, without contaminating the melt or the castings taken from the molds; the provision of melting crucibles, casting molds and the like that have good thermal shock resistance; the provision of a metal modified zirconia material; the process in the metallurgy of titanium of providing an improved container for liquid titanium that is chemically inert there to and that replaces the earlier water cooled copper crucible, and that is suitable for inductance heating; the making of alloys of accurate compositions of the metals here of interest; and the like.
  • the metal titanium is of increasing importance because it is a lightweight, strong, corrosion resistant and ductile metal of high melting point. It fills a gap between aluminum alloys and stainless steel in its density, modulus of elasticity, and strength at solid state temperatures.
  • the metal titanium is particularly favored for aircraft use because of its high strength to weight ratio; its outstanding sea water and marine atmosphere corrosion resistance, which exceeds that of austenitic stainless steel and is equal to that of platinum and comparable material.
  • the desirable metallic properties of titanium are de- ICC stroyed by embrittlement in the presence of interstitial impurities such as oxygen, nitrogen and hydrogen. Hydrogen can be removed from titanium by a vacuum treatment. When titanium has dissolved oxygen and nitrogen, the oxygen and nitrogen cannot be removed from the titanium by any known method.
  • the melting of titanium without contamination has been a major problem in its fabrication. Every known crucible material is attacked to some degree by molten titanium. In skull melting, using the arc melting tech nique, a layer of titanium may be frozen against a refractory crucible to serve as an inside wall in contact with the molten titanium. Another method used with the arc melting technique employs water cooled copper crucibles with water close to the molten metal, which introduces an explosion hazard. An induction melting method is preferred.
  • the ceramic crucible that is contemplated herein does not require cooling and has material advantages over earlier crucibles that are set forth more extensively hereinafter.
  • Zirconia is one of the most refractory of the oxides.
  • the melting point of zirconia is 2680i20 C., which is about 4850 F.
  • Pure zirconia possesses monoclinic symmetry at room temperature of about 20 C, to 25 C.; and at about 1000 C. It transforms reversibly to the tetragonal crystal modification, accompanied by a large change in thermal expansion. Pure zirconia products crack badly on heating and cooling.
  • the batch preparation for making a container such as a crucible consists illustratively of the Weighing out of 93.5% ZrO and 6.45% Ti metal powder.
  • the metal powder is of the highest purity available, such as titanium in excess of 99% by weight of elemental titanium.
  • the zirconia raw material is in excess of 98.9% Z1 0
  • An illustrative available fineness of the powder is 325 mesh.
  • Crucible shapes are made by conventional methods of pressing, jiggering or slip casting. For pressing, the batch is suspended in methyl alcohol, mixed by short ball milling, pressed in a mold to shape the powdered mix, the shape is air dried at room temperature, fired in a vacuum, and then the shape is cooled in the vacuum to room temperature.
  • the preparation of a casting slip is accomplished illustratively by short ball milling the batch of 93.5% ZrO and 6.45% Ti powders mixed with one normal hydrochloric acid as deflocculent.
  • the resultant slurry of creamy consistency is then freed of air bubbles using a water pump and is checked for pH, grain size and viscosity.
  • the slip is then cast in plaster of Paris molds, using drain casting techniques common to the porcelain and clay industry.
  • the cast shape releases easily from the mold after a short drying period at room temperature.
  • the cast shape is removed from the mold, completely air dried and is heated to 100 C. for a short period.
  • the dried cast shape such as a crucible, is then fired in a vacuum of at least 5 1O mm. of mercury.
  • the composition has a wide sintering range of illustratively from 1760 to 1870 C. and above, or 3200 to 3400 F. and above.
  • the sintered piece is 'held at the sinter temperature and soaked for one hour and is then cooled to room temperature before breaking the vacuum.
  • the fired pieces are black throughout.
  • the material is hard, strong and crack-free. It has a bulk density of 5.5 g./cm. and a true specific gravity of 5.7 g./cm. It has substantially no porosity, its water absorption being about 0.1%.
  • the total shrinkage is about 20% for slip cast and 15% for pressed crucibles.
  • the zirconia containing 15 atomic percent of Ti material has an excellent thermal shock resistance.
  • Experimental crucibles were cycled rapidly several times from room temperature to 1900 C. or 3450 F. at minute periods, with no observable cracks.
  • a possible explanation for the inertness of the atomic percent titanium in zirconia composition to molten titanium is that 15 atomic percent of titanium represents the saturation point for Ti solution in ZrO at the elevated temperature, which is analogous to 15 atomic percent Zr solubility in ZrO as described in the literature. As the total amount of Ti which can dissolve in ZrO at the melting point of Ti is already in the crucible composition, the possibility of attack is thus reduced.
  • Atomic percent is defined at page 83 Olf I-Iackhs Chemical Dictionary by Julius Grant, 1946 printing, published by The Blakiston Company, Philadelphia, Pennsylvania. Zirconia-titanium solid solution at room temperature is of black color and is free from cracks.
  • the titanium By sintering titanium in a vacuum, the titanium forms a substitutional solid solution with zirconia resulting in an oxygen deficient zirconia lattice. On cooling the solution of titanium in zirconia some of the titanium comes out of solution.
  • the thermal shock resistance of the material is explained by the stress relieving nature of this metal component, in addition to an increased thermal conductivity and the high strength of the material.
  • the ceramic processes are processes of arrested reactions, in comparison with the metals processes wherein melts commonly are overheated to lower the metals viscosities for casting operations.
  • the metal charge is melted by heat transmitted through the crucible wall, which means the crucible is at a higher temperature than the charge.
  • Th reactivity of molten titanium with the crucible material increases exponentially with temperature and hence super-heating increases the reaction rate many fold.
  • the recommended heating schedule is to balance the crucible melt temperature below the metal melting point and then overheat for as short a time as possible and only as high as is actually required to obtain the proper metal viscosity condition for casting.
  • the purity of the furnace atmosphere that is essential for successful titanium melting is not as much of a problem on a laboratory scale as it is in industrial practice, as will be appreciated by designers of furnaces.
  • Induction-type melting with the possibility of reduced melting time, provides more favorable conditions than does resistance heated furnaces. If a suscepter is required, molybdenum or tungsten are preferred to graphite within the melting area for minimizing the contamination of the melt.
  • the titanium metal charge itself may be used as the suscepter, in which case a suitable backing material that is stable both in a vacuum and in contact with titanium vapor must be employed, such as prefired material of the crucible composition in granular form. The fact that zirconia becomes an electrical conductor above 1000 C. does not appear to be a problem because of the higher conductivity of the metal.
  • the charged crucible is placed in a furnace designed for either vacuum or neutral atmosphere firing. Both the crucible and the charge are first degassed by evacuating the furnace to about 2 10- mm. mercury and heating in vacua to approximately 1000 C. Soaking at this temperature for 15 minutes is adequate for the removal of practically all of the air that is absorbed in both the charge and the crucible.
  • purified helium is introduced into the furnace and the furnace temperature is gradually increased until the titanium charge is melted. After the complete melting of the titanium is observed, the power into the furnace is shut off and the helium atmosphere is maintained until the furnace and its charge have cooled to room temperature.
  • the helium preferably of grade A, is passed through a liquid nitrogen trap, a desiccant such as anhydrous calcium chloride or the like, and a 1000 C. getter furnace illustratively using a getter alloy of Zr and 35% Ti is preferred to titanium sponge for re moving the last traces of oxygen from the helium.
  • the method of casting metals selected from the group consisting of titanium, zirconium, hafnium, thorium and chromium which comprises the steps of providing a container consisting essentially of zirconia saturated with the metal to be cast in substitut-ional solid solution in said zirconia, placing a charge of the selected metal in the container, melting the metal in the container while minimizing a reaction between the melt and the container by balancing the container melt temperature below the metal melting point, preheating the melt for a minimal possible time and only as high as is required to obtain the proper viscosity of the metal for casting, and cooling the metal to room temperature.
  • the process of causing zirconium to pass between its solid and its liquid physical states in a container that is chemically inert to the zirconium by being of the compositon zirconia containing 15 atomic percent zirconium as representing the saturation point at elevated temperatures for zirconium in solution in zirconia by the steps of providing a container consisting essentially of zirconia saturated wth zirconium in :su-bstitut-ional solid solution in said zirconia, placing a charge of zirconium in the container and heating the zirconium just barely to its melting temperature, minimizing the soaking tim the molten zirconium contacts its container, and maintaining a chemically inert atmosphere around the container and the zirconium as the zirconium reverts to its solid state.

Description

Unite States ate 3,264,694 METHOD OF CASTING Berthold C. Weber, Dayton, Ohio, assignor to the United States of America as represented by the Secretary of the Air Force No Drawing. Griginal applications Mar. 4, 1959, Ser. No. 797,309, now Patent No. 3,049,432, dated Aug. 14, 1962, and Apr. 2, 1962, Ser. No. 184,610, now Patent No. 3,189,473, dated June 15, 1965. Divided and this application Sept. 22, 1964, Ser. No. 398,457
5 Claims. (Cl. 22-200) The invention described herein may be manufactured and used by and for the Government for governmental purposes, without the payment to me of my royalties thereon.
The present application is a division of the application Serial No. 184,610 filed April 2, 1962, and issued on June 15, 1965, as US. Patent No. 3,189,473, and of the parent application Serial No. 797,309 filed March 4, 1959, that issued on August 14, 1962, as US. Patent No. 3,049,432.
This invention relates to a container for the metals titanium, zirconium, hafnium and thorium and the like, in the Group IV-A, such as of the periodic chart of the elements in Metals Handbook published in 1948 by The American Society for Metals, 7301 Euclid Avenue, Cleveland 3, Ohio, at page 22, and more particularly to an improved container made of zirconia and these metals and the containers used for melting and casting these metals.
The invention described herein is the fruition of work done by the inventor in the science of ceramics.
A brief summary of the invention follows, indicating its nature and substance together with a statement of the objects of the invention commensurate and consistant with the invention as claimed and also setting out the exact nature, the operation and the essence of the invention complete with proportions and techniques that are necessary with its use. The purpose of the invention also is stipulated. The presentation is adequate for any person who is skilled in the art and science to which the invention pertains to use it without involving extensive experimentation. The best mode of carrying out the invention is presented by the citing of specific operative examples inclusive of the preparation and the use of at least one example of the invention.
The objects of the present invention are to provide new and superior compositions for the fabrication of crucibles, molds and the like used in melting metals, such as those in Group IV-A of the Periodic System, without contaminating the melt or the castings taken from the molds; the provision of melting crucibles, casting molds and the like that have good thermal shock resistance; the provision of a metal modified zirconia material; the process in the metallurgy of titanium of providing an improved container for liquid titanium that is chemically inert there to and that replaces the earlier water cooled copper crucible, and that is suitable for inductance heating; the making of alloys of accurate compositions of the metals here of interest; and the like.
The metal titanium is of increasing importance because it is a lightweight, strong, corrosion resistant and ductile metal of high melting point. It fills a gap between aluminum alloys and stainless steel in its density, modulus of elasticity, and strength at solid state temperatures. The metal titanium is particularly favored for aircraft use because of its high strength to weight ratio; its outstanding sea water and marine atmosphere corrosion resistance, which exceeds that of austenitic stainless steel and is equal to that of platinum and comparable material.
The desirable metallic properties of titanium are de- ICC stroyed by embrittlement in the presence of interstitial impurities such as oxygen, nitrogen and hydrogen. Hydrogen can be removed from titanium by a vacuum treatment. When titanium has dissolved oxygen and nitrogen, the oxygen and nitrogen cannot be removed from the titanium by any known method.
The melting of titanium without contamination has been a major problem in its fabrication. Every known crucible material is attacked to some degree by molten titanium. In skull melting, using the arc melting tech nique, a layer of titanium may be frozen against a refractory crucible to serve as an inside wall in contact with the molten titanium. Another method used with the arc melting technique employs water cooled copper crucibles with water close to the molten metal, which introduces an explosion hazard. An induction melting method is preferred. The ceramic crucible that is contemplated herein does not require cooling and has material advantages over earlier crucibles that are set forth more extensively hereinafter.
Studies of the systems Ti-O, Zr-O and some phases of the ternary system Ti-Zr-O led to the concentration on zirconia as the base constituent for crucible material. Zirconia appeared to be the most promising refractory from its free energy of formation and heat of formation. These studies led to an oxygen deficient zirconia material that is made stable thermally by reacting zirconia with titanium metal powder as a novel refractory material. Zirconium has a higher affinity for oxygen than titanium has and can take oxygen away from titanium oxide. X- ray diffraction analysis indicates that when TiO plus Zr are reacted the end products are monoclinic zirconia and an expanded titanium lattice. It is concluded that zirconium reduces titania and that zirconia is not reduced by titanium. The chemical reduction does not involve or concern the substitution of a zirconium atom by a titanium atom in the ZrO lattice.
Zirconia is one of the most refractory of the oxides. The melting point of zirconia is 2680i20 C., which is about 4850 F. Pure zirconia possesses monoclinic symmetry at room temperature of about 20 C, to 25 C.; and at about 1000 C. It transforms reversibly to the tetragonal crystal modification, accompanied by a large change in thermal expansion. Pure zirconia products crack badly on heating and cooling.
The new approach to thermally stabilizing zirconia which is chemically inert to attack by molten titanium has evolved from an investigation of the systems ZrO -TiO and ZrO -Ti, from which specially promising results were obtained from the system ZrO Ti.
Crack-free and thermal shock resistant crucible specimens, that were black in color throughout, were obtained when mixtures of titanium metal powder and pure zirconia powder were sintercd in a vacuum at temperatures that range from 1760 to 1870 C. and above, or 3200 to 3400 F. and above. An experimentally successful crucible is made of ZrO with a fifteen atomic percent titanium addition. On firing this material a substitutional solid solution of titanium in zirconia having a defect structure due to an oxygen deficiency is formed. Its inertness to molten titanium is believed to be accounted for by the low oxygen availability of the material.
Container fabrication The batch preparation for making a container such as a crucible consists illustratively of the Weighing out of 93.5% ZrO and 6.45% Ti metal powder. The metal powder is of the highest purity available, such as titanium in excess of 99% by weight of elemental titanium. The zirconia raw material is in excess of 98.9% Z1 0 An illustrative available fineness of the powder is 325 mesh. Crucible shapes are made by conventional methods of pressing, jiggering or slip casting. For pressing, the batch is suspended in methyl alcohol, mixed by short ball milling, pressed in a mold to shape the powdered mix, the shape is air dried at room temperature, fired in a vacuum, and then the shape is cooled in the vacuum to room temperature.
The preparation of a casting slip is accomplished illustratively by short ball milling the batch of 93.5% ZrO and 6.45% Ti powders mixed with one normal hydrochloric acid as deflocculent. The resultant slurry of creamy consistency is then freed of air bubbles using a water pump and is checked for pH, grain size and viscosity. The slip is then cast in plaster of Paris molds, using drain casting techniques common to the porcelain and clay industry. The cast shape releases easily from the mold after a short drying period at room temperature. The cast shape is removed from the mold, completely air dried and is heated to 100 C. for a short period.
The dried cast shape, such as a crucible, is then fired in a vacuum of at least 5 1O mm. of mercury. The composition has a wide sintering range of illustratively from 1760 to 1870 C. and above, or 3200 to 3400 F. and above. The sintered piece is 'held at the sinter temperature and soaked for one hour and is then cooled to room temperature before breaking the vacuum. The fired pieces are black throughout. The material is hard, strong and crack-free. It has a bulk density of 5.5 g./cm. and a true specific gravity of 5.7 g./cm. It has substantially no porosity, its water absorption being about 0.1%. The total shrinkage is about 20% for slip cast and 15% for pressed crucibles.
The zirconia containing 15 atomic percent of Ti material has an excellent thermal shock resistance. Experimental crucibles were cycled rapidly several times from room temperature to 1900 C. or 3450 F. at minute periods, with no observable cracks.
X-ray and microscopic studies of the material have been made without completely clarifying how zirconia and titanium combine. The room temperature X-ray analysis of the fired ZrO containing 1 5 atomic percent of Ti produces a very weak, scarcely detectable expanded titanium pattern. The principal phase in monoclinic zirconia. The weak titanium pattern, dark color of the reaction product, and its high thermal shock resistance, suggests a solid solution of titanium in zirconia, but a noticeable shift in the lattice constant of z-irconia is not observed. Elevated temperature X-ray studies indicate the usual monoclinic to tetragonal inversion of zirconia.
A possible explanation for the inertness of the atomic percent titanium in zirconia composition to molten titanium is that 15 atomic percent of titanium represents the saturation point for Ti solution in ZrO at the elevated temperature, which is analogous to 15 atomic percent Zr solubility in ZrO as described in the literature. As the total amount of Ti which can dissolve in ZrO at the melting point of Ti is already in the crucible composition, the possibility of attack is thus reduced. Atomic percent is defined at page 83 Olf I-Iackhs Chemical Dictionary by Julius Grant, 1946 printing, published by The Blakiston Company, Philadelphia, Pennsylvania. Zirconia-titanium solid solution at room temperature is of black color and is free from cracks. By sintering titanium in a vacuum, the titanium forms a substitutional solid solution with zirconia resulting in an oxygen deficient zirconia lattice. On cooling the solution of titanium in zirconia some of the titanium comes out of solution. The thermal shock resistance of the material is explained by the stress relieving nature of this metal component, in addition to an increased thermal conductivity and the high strength of the material.
Melting procedure In the melting of titanium in crucibles made of this titanium saturated zirconia material, the evaluation of the melts by Vickers hardness determinations demonstrate that there is no significant increase in hardness when the melts 4 are not superheated. The three factors which mainly influence the successful use of this crucible material as a container for molten titanium are the melting temperature, the soaking time, and the atmosphere purity.
Undue overheating of the melt must be avoided so as not to reach a final equilibrium condition between the melt and the crucible material, as is commonly required in the ceramics field to obtain optimal properties. The ceramic processes are processes of arrested reactions, in comparison with the metals processes wherein melts commonly are overheated to lower the metals viscosities for casting operations.
In the use of resistance heating the metal charge is melted by heat transmitted through the crucible wall, which means the crucible is at a higher temperature than the charge. Th reactivity of molten titanium with the crucible material increases exponentially with temperature and hence super-heating increases the reaction rate many fold. To minimize any reaction between the melt and the container material, the recommended heating schedule is to balance the crucible melt temperature below the metal melting point and then overheat for as short a time as possible and only as high as is actually required to obtain the proper metal viscosity condition for casting.
The purity of the furnace atmosphere that is essential for successful titanium melting is not as much of a problem on a laboratory scale as it is in industrial practice, as will be appreciated by designers of furnaces.
Induction-type melting with the possibility of reduced melting time, provides more favorable conditions than does resistance heated furnaces. If a suscepter is required, molybdenum or tungsten are preferred to graphite within the melting area for minimizing the contamination of the melt. The titanium metal charge itself may be used as the suscepter, in which case a suitable backing material that is stable both in a vacuum and in contact with titanium vapor must be employed, such as prefired material of the crucible composition in granular form. The fact that zirconia becomes an electrical conductor above 1000 C. does not appear to be a problem because of the higher conductivity of the metal.
For the melting of titanium the charged crucible is placed in a furnace designed for either vacuum or neutral atmosphere firing. Both the crucible and the charge are first degassed by evacuating the furnace to about 2 10- mm. mercury and heating in vacua to approximately 1000 C. Soaking at this temperature for 15 minutes is adequate for the removal of practically all of the air that is absorbed in both the charge and the crucible.
Following the degassing of the furnace and its charge, purified helium is introduced into the furnace and the furnace temperature is gradually increased until the titanium charge is melted. After the complete melting of the titanium is observed, the power into the furnace is shut off and the helium atmosphere is maintained until the furnace and its charge have cooled to room temperature.
It is of utmost importance that a satisfactory furnace atmosphere is maintained, with the vacuum above 5 1O* mm. of mercury during the degassing stage of the firing and with an extremely pure helium gas atmosphere during the later stage of the melting operation. Leakage in the helium system can best be avoided by using an all glass purification train. The helium, preferably of grade A, is passed through a liquid nitrogen trap, a desiccant such as anhydrous calcium chloride or the like, and a 1000 C. getter furnace illustratively using a getter alloy of Zr and 35% Ti is preferred to titanium sponge for re moving the last traces of oxygen from the helium.
While the crucible material composed of ZrO with an addition of Ti was successfully used to melt titanium without contamination, the basic principle derived from the research which led to the invent-ion can be applied also to synthesize container materials for melting other reactive metals, not only zirconium, hafnium and thorium, which are sister or analogous metals to titanium and zirconium 5 according to the Mendelejetf classification of elements, belonging to Group IV-A of the Periodic Table, but also chromium and other refractory metals having a melting point below approximately 2500" C. or 4530 F. In each case the individual metal to be melted is added to zirconia and containers formed from these compositions are fired in vacua to result in an oxygen deficient metal modified zirconia material. The name metal modified oxide (MMO) has been coined for this new class of materials.
Successful melting experiments have already been con ducted, in addition to titanium, with zirconium and chromium in containers composed of Zr plus 15 atomic percent of Zr and ZrO plus 15 atomic percent of Cr respectively. In the case of chromium-modified-zirconia it is necessary to change the firing conditions because of the volatility of chromium in vacua. These crucibles of chromium-modified-zirconia, therefore, have to be fired in a helium or argon atmosphere at atmospheric pressure.
The process and the products that are disclosed herein are submitted as experimentally confirmed improvements in the melting and in the casting of the Group IV-A metals and similar highly reactive metals of high melting points, such as Cr, Th and the like, and comparable modifications may be made therein without departing from the spirit and the scope of this invention as defined in the claims appended hereto.
I claim:
1, The method of casting metals selected from the group consisting of titanium, zirconium, hafnium, thorium and chromium which comprises the steps of providing a container consisting essentially of zirconia saturated with the metal to be cast in substitut-ional solid solution in said zirconia, placing a charge of the selected metal in the container, melting the metal in the container while minimizing a reaction between the melt and the container by balancing the container melt temperature below the metal melting point, preheating the melt for a minimal possible time and only as high as is required to obtain the proper viscosity of the metal for casting, and cooling the metal to room temperature.
2. The method of casting defined by claim 1 under an inert atmosphere.
3. The process of causing titanium to pass between its solid and its liquid physical states in a container that is chemically inert to the titanium by being of the composi tion zirconia containing 15 atomic percent titanium as representing the saturation point at elevated temperatures for titanium in solution in zirconia, by the steps of providing a container consisting essentially of zirconia saturated with titanium in substitutional solid solution in said zirconia, placing a charge of titanium in the container, and heating the titanium just barely to its melting temperature, minimizing the melting and the soaking time of the melt in the container, and maintaining a chemically inert atmosphere around both the container and the molten titanium.
4. The process of causing chromium to pass between its solid and its liquid physical states in a container that is chemically inert to the chromium by the container being of the composition zirconia fully saturated at elevated temperatures with chromium, by the steps of providing a container consisting essentially of zirconia saturated with chromium in substitutional solid solution in said zirconia, placing a charge of chromium in the container and heating the chromium just barely to its melting temperature in the container, minimizing the melting and soaking time the chromium melt contacts its container, and maintaining a chemically inert atmosphere around the container and the molten chromium.
5. The process of causing zirconium to pass between its solid and its liquid physical states in a container that is chemically inert to the zirconium by being of the compositon zirconia containing 15 atomic percent zirconium as representing the saturation point at elevated temperatures for zirconium in solution in zirconia, by the steps of providing a container consisting essentially of zirconia saturated wth zirconium in :su-bstitut-ional solid solution in said zirconia, placing a charge of zirconium in the container and heating the zirconium just barely to its melting temperature, minimizing the soaking tim the molten zirconium contacts its container, and maintaining a chemically inert atmosphere around the container and the zirconium as the zirconium reverts to its solid state.
References Cited by the Examiner UNITED STATES PATENTS 1,790,918 2/1931 Hauser 10639 2,205,854 6/1940 Kroll -84 2,684,297 7/1954 Urban 75-96 2,694,646 11/1954 Wagner et al 186-57 I. SPENCER OVERI-IOLSER, Primary Examiner.
MARCUS U. LYONS, Examiner.
E. MAR, Assistant Examiner.

Claims (1)

1. THE METHOD OF CASTING METALS SELECTED FROM THE GROUP CONSISTING OF TITANIUM, ZIRCONIUM, HAFNIUM, THORIUM AND CHROMIUM WHICH COMPRISES THE STEPS OF PROVIDNG A CONTAINER CONSISTING ESSENTIALLY OF ZIRCONIA SATURATED WITH THE METAL TO BE CAST IN SUBSTITUTIONAL SOLID SOLUTION IN SAID ZIRCONIA, PLACING A CHARGE OF THE SELECTED METAL IN THE CONTAINER, MELTING THE METAL IN THE CONTAINER WHILE MINMIZING A REACTION BETWEEN THE MELT AND THE CONTAINER BY BALANCING THE CONTAINER MELT TEMPERATURE BELOW THE METAL MELTING POINT, PREHEATING THE MELT FOR A MINIMAL POSSIBLE TIME AND ONLY AS HIGH AS IS REQUIRED TO OBTAIN THE PROPER VISCOSITY OF THE METAL FOR CASTING, AND COOLING THE METAL TO ROOM TEMPERATURE.
US398457A 1959-03-04 1964-09-22 Method of casting Expired - Lifetime US3264694A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US398457A US3264694A (en) 1959-03-04 1964-09-22 Method of casting

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US797309A US3049432A (en) 1959-03-04 1959-03-04 Crucible and refractory material therefor
US398457A US3264694A (en) 1959-03-04 1964-09-22 Method of casting

Publications (1)

Publication Number Publication Date
US3264694A true US3264694A (en) 1966-08-09

Family

ID=27016261

Family Applications (1)

Application Number Title Priority Date Filing Date
US398457A Expired - Lifetime US3264694A (en) 1959-03-04 1964-09-22 Method of casting

Country Status (1)

Country Link
US (1) US3264694A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3398923A (en) * 1964-11-20 1968-08-27 Schwarzkopf Dev Company Shaped bodies with high temperature strength and corrosion resistance against moltenmetals particularly molten iron and steels
US3414046A (en) * 1964-12-10 1968-12-03 Schwarzkopf Dev Company Mold structures for continuously casting an elongated metal body of desired cross-section
US5525560A (en) * 1992-09-21 1996-06-11 Matsushita Electric Works, Ltd. Zirconia based composite material and method of manufacturing the same product
US5641719A (en) * 1995-05-09 1997-06-24 Flex Products, Inc. Mixed oxide high index optical coating material and method

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1790918A (en) * 1931-02-03 Max hatjser
US2205854A (en) * 1937-07-10 1940-06-25 Kroll Wilhelm Method for manufacturing titanium and alloys thereof
US2684297A (en) * 1951-08-04 1954-07-20 Nat Lead Co Process for melting highly reactive metals
US2694646A (en) * 1949-07-19 1954-11-16 Zirconium Corp Of America Zirconia compositions

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1790918A (en) * 1931-02-03 Max hatjser
US2205854A (en) * 1937-07-10 1940-06-25 Kroll Wilhelm Method for manufacturing titanium and alloys thereof
US2694646A (en) * 1949-07-19 1954-11-16 Zirconium Corp Of America Zirconia compositions
US2684297A (en) * 1951-08-04 1954-07-20 Nat Lead Co Process for melting highly reactive metals

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3398923A (en) * 1964-11-20 1968-08-27 Schwarzkopf Dev Company Shaped bodies with high temperature strength and corrosion resistance against moltenmetals particularly molten iron and steels
US3414046A (en) * 1964-12-10 1968-12-03 Schwarzkopf Dev Company Mold structures for continuously casting an elongated metal body of desired cross-section
US5525560A (en) * 1992-09-21 1996-06-11 Matsushita Electric Works, Ltd. Zirconia based composite material and method of manufacturing the same product
US5641719A (en) * 1995-05-09 1997-06-24 Flex Products, Inc. Mixed oxide high index optical coating material and method
US5989626A (en) * 1995-05-09 1999-11-23 Flex Products, Inc. Mixed oxide high index optical coating material and method

Similar Documents

Publication Publication Date Title
Long et al. Aluminum Nitride, a Refractory for Aluminum to 2000° C.
US3108887A (en) Refractory articles and method of making same
Brewer et al. A study of the refractory borides
US2548897A (en) Process for melting hafnium, zirconium, and titanium metals
US3758662A (en) In carbonaceous mold forming dense carbide articles from molten refractory metal contained
US3049432A (en) Crucible and refractory material therefor
Weber et al. Ceramic crucible for melting titanium
Kalish et al. Densification mechanisms in high‐pressure hot‐pressing of HfB2
US3879210A (en) Fused-cast refractory
Yanagihara et al. Isothermal and Cyclic Oxidation of Mo (Si1− x, Alx) 2 up to 2048 K
EP0261063B1 (en) Method for producing self-supporting ceramic bodies with graded properties
US3264694A (en) Method of casting
Aneziris et al. Fine grained Mg–PSZ ceramics with titania and alumina or spinel additions for near net shape steel processing
Hong et al. Nonisothermal gravimetric investigation on kinetics of reduction of magnesia by aluminum
US4244743A (en) Sulfur containing refractory for resisting reactive molten metals
US3189473A (en) Method of making a container
US3011982A (en) Refractory and method of making the same
US4382997A (en) Spinel surfaced objects
Yu et al. Slag corrosion resistance of Al4SiC4
Ritland et al. Alumina‐Copper Composites by Vapor Phase Sintering
Handwerker et al. Formation of alumina-chromia-chromium composites by a partial reduction reaction
Brace et al. Preparation and Properties of Titanium-Base Alloys
JPS6236087A (en) Granular sic-dispersed metal silicon heat-resistant material
US3340078A (en) Fused refractory castings
US4735922A (en) Porous refractory hard metal compositions and method of forming same