US3049432A - Crucible and refractory material therefor - Google Patents

Crucible and refractory material therefor Download PDF

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US3049432A
US3049432A US797309A US79730959A US3049432A US 3049432 A US3049432 A US 3049432A US 797309 A US797309 A US 797309A US 79730959 A US79730959 A US 79730959A US 3049432 A US3049432 A US 3049432A
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titanium
zirconia
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metal
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    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B35/00Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
    • C04B35/01Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
    • C04B35/48Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on zirconium or hafnium oxides, zirconates, zircon or hafnates

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  • This invention relates to the metals titanium, zirconium, hafnium and thorium and the like, in the group IVA such as of the periodic chart of the elements in Metals Handbook, published in 1948 by The American Society of Metals, 7301 Euclid Avenue, Cleveland 3, Ohio, at page 22, and more particularly to a improved container made of zirconia and these metals and the container used for melting and casting these metals and illustrative-1y to an improved process in the metallurgy of titanium.
  • 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 in group IVA 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 thereto and that replaces the earlier water cooled copper crucible, and that is suitable for inductance or resistance heating; 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 3,049,432 Patented Aug. 14, 1962 ICC elasticity, and strength at intermediate temperatures.
  • the metal titanium is particularly favored for aircraft use because or" 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 destroyed by embrittlement in the presence of interstitial impurities such as oxygen, nitrogen and hydrogen. Hydrogen can be removed by titanium by a vacuum treatment. When titanium has dissolved oxygen and nitrogen, they 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 technique, 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 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; and at about 1000 C. it transforms reversibly to tetragonal crystal modification, accompanied by a large change in thermal expansion. Pure zirconia products crack badly on heating and cooling.
  • Crucible Fabrication as titanium in excess of 99% by weight of elemental titanium.
  • the zirconia raw material is in excess of 98.9% Z10
  • An illustrative available fineness of the powder is 325 mesh.
  • Crucible shapes are made by conventional methods of pressing, iiggering or slip casting. For pressing, the batch is suspended in methyl alcohol, mixed by short ball milling and then is dried at room temperature.
  • the preparation of a casting slip is accomplished illustratively by short ball milling the batch with one normal hydrochloric acid as defiocculent.
  • 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, is removed from the mold, completely air dried and is heated to 100 C. for a short period.
  • the dried crucibles are then fired in a vacuum of at least 5X10 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 soaked for one hour and 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.
  • 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.
  • 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.
  • the ceramic processes are processes of arrested reactions, in comparison with the metals processes wherein melts commonly are overheated to lower 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.
  • the 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 scheuie is to balance the crucible melt temperature below the metal melting point and then overheat as short a time as possible and only as high as is actually required to obtain the proper viscosity condition for casting.
  • the purity of the furnace atmosphere essential for successful titanium melting is not so 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 provide more favorable conditions than does resistance heated furnaces. If a susceptor is required molybdenum or tungsten are preferred to graphite.
  • the titanium metal charge itself may be used as the susceptor, 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.
  • zirconia becomes an electrical conduotor 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 furrnace to about 2X10- mm. mercury and heating in vacuo 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 65% Zr and 35% Ti as being preferred to titanium sponge for removing the last traces of oxygen from the helium.
  • composition of matter that consists of zirconia that has a defect lattice structure due to an oxygen deficiency and which zirconia is fully saturated with the addi- 6 tion of a metal selected from the group consisting of zirconium, titanium, hafnium, thorium and chromium and said metal being in substitutional solid solution in said zirconia.
  • composition of matter that consists of zirconia that has a defect lattice structure due to an oxygen deficiency and which zirconia is fully saturated with titanium in substitutional solid solution in said zirconia.
  • a crack-free and thermal shock resistant crucible that consists of zirconia that has a defect lattice structure due to an oxygen deficiency and which Zirconia is fully saturated with a metal selected from the group consisting of zirconium, titanium, hafnium, thorium and chromium, said metal being in substitutional solid solution in said zirconia.
  • a crack free and thermal shock resistant crucible consisting of zirconia that has a defect lattice structure due to an oxygen deficiency, which zirconia is fully saturated with titanium in substitutional solid solution in the zircoma.

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  • Engineering & Computer Science (AREA)
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Description

United States Patent l 3,049,432 CRUCIBLE AND REFRACTORY MATERIAL THEREFOR Berthold C. Weber, Dayton, Ohio, assignor to the United States of America as represented by the Secretary of the Air Force No Drawing. Filed Mar. 4, 1959, Ser. No. 797,309 4 Claims. (Cl. 106-57) (Granted under Title 35, US. Code (1952), see. 266) The invention described herein may be manufactured and used by and for the Government for governmental purposes, without the payment to me of any royalties thereon.
This invention relates to the metals titanium, zirconium, hafnium and thorium and the like, in the group IVA such as of the periodic chart of the elements in Metals Handbook, published in 1948 by The American Society of Metals, 7301 Euclid Avenue, Cleveland 3, Ohio, at page 22, and more particularly to a improved container made of zirconia and these metals and the container used for melting and casting these metals and illustrative-1y to an improved process in the metallurgy of titanium.
As a background for imparting a clear understanding of the present invention as claimed reference is made to the Berthold C. Weber and Philip S. Hessinger application Serial Number 369,259, filed July 20, 1953, now abandoned, for patent on a Container Material and Melting Technique for Melting Reactive Metals, and Berthold C. Weber application Serial Number 434,092, filed June 2, 1954, now abandoned, for patent on an Oxygen Deficient Zirconia Container. The present application is a continuation in part of said application Serial No. 434,092 that has resulted from the summation of experimental work done on the same subject matter during the time interval. This application is copending with both of the above applications Serial Numbers 369,259 and 434,092. Further study of the materials described in the earlier applications and the mechanism of their synthesis have revealed inaccuracies and important improvements in both the materials and the methods here of interest.
A brief summary of the invention follows, indicating its nature and substance together with a statement of the objects of the invention commensurate and consistent 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 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 in group IVA 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 thereto and that replaces the earlier water cooled copper crucible, and that is suitable for inductance or resistance heating; 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 3,049,432 Patented Aug. 14, 1962 ICC elasticity, and strength at intermediate temperatures. The metal titanium is particularly favored for aircraft use because or" 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 destroyed by embrittlement in the presence of interstitial impurities such as oxygen, nitrogen and hydrogen. Hydrogen can be removed by titanium by a vacuum treatment. When titanium has dissolved oxygen and nitrogen, they 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 technique, 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 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, ZrO and some phases of the ternary system Ti--ZrO 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 Z00 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; and at about 1000 C. it transforms reversibly to 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 ZrOg-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 sintered 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.
Crucible Fabrication as titanium in excess of 99% by weight of elemental titanium. The zirconia raw material is in excess of 98.9% Z10 An illustrative available fineness of the powder is 325 mesh. Crucible shapes are made by conventional methods of pressing, iiggering or slip casting. For pressing, the batch is suspended in methyl alcohol, mixed by short ball milling and then is dried at room temperature.
The preparation of a casting slip is accomplished illustratively by short ball milling the batch with one normal hydrochloric acid as defiocculent. 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, is removed from the mold, completely air dried and is heated to 100 C. for a short period.
The dried crucibles are then fired in a vacuum of at least 5X10 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 soaked for one hour and 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 ZrC- containing atomic percent of Ti produces a very weak, scarcely detectable expanded titanium pattern. The principal phase is 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 zirconia is not observed. Elevated temperature X-ray studies indicate the usual monoclinic to tctragonal inversion of zirconia.
A possible explanation for the inertness of the 15 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.
Despite the absence of conclusive evidence for a zirconia-titanium solid solution at room temperature, the black color of the fired material and the freedom from cracks indicate that some modification of zirconia occurs.
It is assumed therefore, that by sintering in a vacuum titanium forms a substitutional solid solution with zirconia resulting in an oxygen deficient zirconia lattice. On cooling 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.
M clting Procedure In the melting of titanium in crucibles of this material the evaluation of the melts by Vickers hardness determinations demonstrate that there is no significant increase in hardness when the melts 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 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. The 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 scheuie is to balance the crucible melt temperature below the metal melting point and then overheat as short a time as possible and only as high as is actually required to obtain the proper viscosity condition for casting.
The purity of the furnace atmosphere essential for successful titanium melting is not so 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 provide more favorable conditions than does resistance heated furnaces. If a susceptor is required molybdenum or tungsten are preferred to graphite. The titanium metal charge itself may be used as the susceptor, 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 conduotor 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 furrnace to about 2X10- mm. mercury and heating in vacuo 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 be maintained, with the vacuum better than 5 l0 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 65% Zr and 35% Ti as being preferred to titanium sponge for removing the last traces of oxygen from the helium.
While the crucible material composed of ZrO with addition of Ti was successfully used to melt titanium without contamination, the basic principle derived from the research which led to the invention 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 under the Mendeleerf classification of elements, belonging to group IVA 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 vacuo 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 conducted, in addition to titanium, with zirconium and chromium in containers composed of ZrO plus 15 at% Zr and ZrO plus 15 at% Cr respectively. In the case of chromium-modified-zirconia it is necessary to change the firing conditions because of the volatility of chromium in vacuo. These crucibles 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 group IVA 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 composition of matter that consists of zirconia that has a defect lattice structure due to an oxygen deficiency and which zirconia is fully saturated with the addi- 6 tion of a metal selected from the group consisting of zirconium, titanium, hafnium, thorium and chromium and said metal being in substitutional solid solution in said zirconia.
2. The composition of matter that consists of zirconia that has a defect lattice structure due to an oxygen deficiency and which zirconia is fully saturated with titanium in substitutional solid solution in said zirconia.
3. A crack-free and thermal shock resistant crucible that consists of zirconia that has a defect lattice structure due to an oxygen deficiency and which Zirconia is fully saturated with a metal selected from the group consisting of zirconium, titanium, hafnium, thorium and chromium, said metal being in substitutional solid solution in said zirconia.
4. A crack free and thermal shock resistant crucible consisting of zirconia that has a defect lattice structure due to an oxygen deficiency, which zirconia is fully saturated with titanium in substitutional solid solution in the zircoma.
References Cited in the file of this patent UNITED STATES PATENTS 1,518,818 Reitz Dec. 9, 1924 2,205,854 Kroll June 25, 1940 2,684,297 Urban July 20, 1954 UNITED STATES PATENT OFFICE CERTIFICATE OF CORRECTION Patent No. 3,049,432 August 14, 1962 Berthold C. Weber e above numbered pat- It is hereby certified that error appears in th ould read as ent requiring correction and that the said Letters Patent sh corrected below.
ior "by", first occurrence, read Column 2, line 10, from line 43, for "Z00 read- ZrOg column 4, line 42, for"furrnace" read furnace Signed and sealed this 12th day of February, 1963,
(SEAL) Attcst:
ERNEST w. SWIDER DAVID LADD Attesting Officer Commissioner of Patents

Claims (1)

1. THE COMPOSITION OF MATTER THAT CONSISTS OF ZIRCONIA THAT HAS A DEFECT LATTICE STRUCTURE DUE TO AN OXYGEN DEFICIENCY AND WHICH ZIRCONIA IS FULLY SATURATED WITH THE ADDITION OF A METAL SELECTED FROM THE GROUP CONSISTING OF ZIRCONIUM, TITANIUM, HAFNIUM, THORIUM AND CHROMIUM AND SAID METAL BEING IN SUBSTANTIONAL SOLID SOLUTION IN SAID ZIRCONIA.
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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3219466A (en) * 1962-03-19 1965-11-23 Gibbons Dudley Ltd Method of producing ceramic articles and the articles produced by this method
US3410716A (en) * 1965-04-01 1968-11-12 Trw Inc Coating of refractory metals with metal modified oxides
US3753745A (en) * 1970-06-04 1973-08-21 Nippon Tungsten Zirconium oxide series spraying material
US3771997A (en) * 1967-08-02 1973-11-13 Foseco Int Titanium oxides in electroslag processes
US3890140A (en) * 1973-05-10 1975-06-17 Us Energy Aluminum titanate crucible for molten uranium
US4091970A (en) * 1976-05-20 1978-05-30 Toshiba Kikai Kabushiki Kaisha Pump with porus ceramic tube
US4856576A (en) * 1988-09-02 1989-08-15 Teledyne Industries, Inc. Zirconium-containing coating composition
US4916022A (en) * 1988-11-03 1990-04-10 Allied-Signal Inc. Titania doped ceramic thermal barrier coatings
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
US20080292791A1 (en) * 2007-04-30 2008-11-27 General Electric Company Methods for making reinforced refractory crucibles for melting titanium alloys
US20100025395A1 (en) * 2008-07-29 2010-02-04 Ivoclar Vivadent Ag Apparatus for the heating of molding, in particular dental-ceramic moldings
US20120144959A1 (en) * 2009-07-01 2012-06-14 Precious Metals Recovery Pty Ltd Smelting method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1518818A (en) * 1916-11-22 1924-12-09 Rietz Eduard Graphite crucible
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1518818A (en) * 1916-11-22 1924-12-09 Rietz Eduard Graphite crucible
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

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3219466A (en) * 1962-03-19 1965-11-23 Gibbons Dudley Ltd Method of producing ceramic articles and the articles produced by this method
US3410716A (en) * 1965-04-01 1968-11-12 Trw Inc Coating of refractory metals with metal modified oxides
US3771997A (en) * 1967-08-02 1973-11-13 Foseco Int Titanium oxides in electroslag processes
US3753745A (en) * 1970-06-04 1973-08-21 Nippon Tungsten Zirconium oxide series spraying material
US3890140A (en) * 1973-05-10 1975-06-17 Us Energy Aluminum titanate crucible for molten uranium
US4091970A (en) * 1976-05-20 1978-05-30 Toshiba Kikai Kabushiki Kaisha Pump with porus ceramic tube
US4856576A (en) * 1988-09-02 1989-08-15 Teledyne Industries, Inc. Zirconium-containing coating composition
US4916022A (en) * 1988-11-03 1990-04-10 Allied-Signal Inc. Titania doped ceramic thermal barrier coatings
US5525560A (en) * 1992-09-21 1996-06-11 Matsushita Electric Works, Ltd. Zirconia based composite material and method of manufacturing the same product
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