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US2665474A - Highly refractory molybdenum alloys - Google Patents

Highly refractory molybdenum alloys Download PDF

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US2665474A
US2665474A US150541A US15054150A US2665474A US 2665474 A US2665474 A US 2665474A US 150541 A US150541 A US 150541A US 15054150 A US15054150 A US 15054150A US 2665474 A US2665474 A US 2665474A
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silicon
molybdenum
alloys
alloy
bodies
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US150541A
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Edward A Beidler
Ivor E Campbell
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Fansteel Inc
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Fansteel Inc
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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
    • C04B35/515Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
    • C04B35/58Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides
    • C04B35/58085Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on silicides
    • C04B35/58092Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on borides, nitrides, i.e. nitrides, oxynitrides, carbonitrides or oxycarbonitrides or silicides based on silicides based on refractory metal silicides
    • 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
    • Y10S239/00Fluid sprinkling, spraying, and diffusing
    • Y10S239/19Nozzle materials
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12486Laterally noncoextensive components [e.g., embedded, etc.]
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12674Ge- or Si-base component
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • Y10T428/12826Group VIB metal-base component
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • Y10T428/12826Group VIB metal-base component
    • Y10T428/12833Alternative to or next to each other
    • 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
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/13Hollow or container type article [e.g., tube, vase, etc.]

Definitions

  • This invention relates to solid, dense molybdenum alloy bodies having high strengths and a high resistance to oxidation, to thermal shock, to erosion of hot gases and to deformation at elevated temperatures.
  • the refractory metal molybdenum has highly desirable properties and characteristics for many purposes and retains its normal mechanical properties at elevated temperatures. Molybdenum, for example, is very desirable for use in electric furnace heating elements, however, it is subject to oxidation at elevated temperatures and oxygen is excluded by maintaining a flow of hydrogen over the heated resistance element.
  • the principal purpose of the present invention is to provide solid bodies formed of certain molybdenum alloys which bodies possess the aforementioned characteristics and properties at elevated temperatures.
  • Another purpose of this invention is to provide solid bodies of irregular configuration formed of certain molybdenum alloys.
  • Fig. 1 is a cross-sectional view of a nozzle :formed of the alloys of this invention.
  • Fig. 2 is a cross-sectional view of a large body formed of the alloys of thisinvention and including a reinforcing core.
  • the present invention contemplates the production of solid bodies formed of molybdenumsilicon alloys or intermetallic compounds, the silicon content of thealloys varying in the molec ularra'tio of silicon to molybdenum of from about 1:1 to about 3:1. This ratio corresponds .toallcys or intermetallic compounds of molybdenum and silicon containing from about 22% to about 47% silicon.
  • the alloy or compound corresponding to a molecular ratio of silicon to molybdenum of about 2:1 or containing about 37% silicon appears to provide the most satisfactory bodies.
  • These alloys of intermetallic compounds may be formed by any desired method.
  • One convenient method includes mixing molybdenum powder and silicon powder in the desired proportions in accordance with powder metallurgy practice. The mixture is then pressed into briquets and the briquets heated slowly to a temperature of about 1050 C. to about 1100 C: A rapid exothermic reaction occurs and continues to a temperature of about 1450 C. The rate of reaction and completeness of the reaction may be regulated by a control of the particle size of the molybdenum and silicon powders. The mass, after it is cooled, is quite porous and brittle and may be employed directly or may be converted into a granular or powder form.
  • the alloy or intermetallic compound so produced is melted as by heating in an arc-melting furnace or may be placed in a suitable crucible and heated by induction.
  • the molybdenum-silicon alloys are quite reactive with many of the usual refractory materials employed for lining crucibles and furnaces at the temperatures required to render the alloys sufiiciently fluid to permit pouring and casting. Thus, magnesia and beryllia are not satisfactory.
  • Graphite apparently reacts with the molybdenum-silicon alloys to a sufiicient extent so that the alloys when melted in contact with graphite become somewhat viscous.
  • the alloys react sufficiently with graphite so that although they are heated in contact with graphite to temperatures as high as about 2200 0., the molten alloys do not possess sufficient fluidity to permit satisfactory casting.
  • zirconia stabilized with calcium oxide is satisfactory as furnace and crucible linings and for the manufacture of crucibles.
  • the alloys may be cast in molds formed of graphite or zirconia. Since the alloys are generally cast at temperatures above 1800 C., the
  • molds are preheated to a temperature of between- 500 C. and 1000 C. before the molten alloy is poured into the mold to avoid chilling the hot mass too rapidly.
  • graphite molds are less desirable because the higher heat conductivity of graphite results in an undesired rapid cooling.
  • the cast bodies of the molybdenum-silicon alloys are somewhat brittle, particularly those cast in graphite molds due to the rapid cooling which results because of the high heat conductivity of graphite.
  • the brittleness may be reduced by vacuum annealing, for example by heating the cast bodies in a vacuum to a temperature of about 1100 C. for 20 to 24 hours. During this vacuum annealing it is observed that gases are released from the bodies.
  • the cast bodies have a density of about 6.2 grams per cubic centimeter and a compressive strength of about 100,000 pounds-per square inch at room temperature.
  • the bodies retain a high strength at elevated temperatures.
  • the bodies are extremely resistant to thermal shock, for example, the body may be rapidly heated to red heat by the use of a oxyacetylene torch and immediately quenched in water without exhibiting cracks. The body may be subjected to several such cycles without exhibiting cracks and because of the extremely high resistance to oxidation will exhibit no signs of surface oxidation.
  • the element may be formed from a cast rod of any desired diameter and length or may consist of a cast grid. Because of the highcompressivestrength, ood electrical contact with the element may be obtained by means of. suitable clamps.
  • nozzles,- jets, and vanes intended for uses where they will be subjected to high velocity gases, such as erosive gases of combustion, must possess high resistance to oxidation and the erosive action'of gases of combustion and must also be highly resistant .2 thermal shock.
  • Such elements may be advantageously formed'by casting the desired: body from the molybdenum-silicon alloys as described hereintofore.
  • a nozzle l having a longitudinally extending aperture 2 may be formed by casting the allow in a graphite mold having a suitable core for forming the aperture.
  • the cast body For some bodies, particularly larger sized bodies, it may be desirable to increase the strength of the cast body. This may be readily attained by reinforcing the cast body with molybdenum or tungsten shapes.
  • the molybdenum or tungsten core or shape is supported in the mold in a conventional manner and the molten molybdenum-silicon alloy cast about the core.
  • rods of molybdenum-silicon alloy may be employed to position the core within the mold cavity.
  • the-finished body consists of the core 3 about which the alloy 4 has been cast. It is or may consist of spaced plates, the details being dependent upon the particular shape of the fin- ..ished body.
  • a dense'body of high strength and high resistance to oxidation, to erosion of gases, to thermal shock and to deformation at temperatures above about 1200 0. consisting of a substantially non-porous cast body of a molybdenum-silicon alloy, the alloy containing from about 22.5% to about 47% silicon.
  • An electrical heating element consisting of a substantially non-porous cast body of a molybdenum-silicon alloy, the alloy containing from about 22.5% to about 47% silicon.
  • An electrical heating element consisting of a substantially non-porous cast body of a molybdenum-silicon alloy, the alloy containing about 37% silicon.
  • a nozzle for 'erosivegases of combustion consisting of a substantially non-porous cast tubular body of a molybdenum-silicon alloy, the
  • alloy containing from about 22.5% to about 47% silicon.
  • a nozzle for erosive gases of combustion consisting of a substantially non-porous cast tubular body ofa molybdenum-silicon alloy, the alloy containing about 37% silicon.
  • a dense body of high'strength and high resistance to oxidation, to erosion Of gases,' to'therma1 shock. and to deformation at temperatures above about 1200 C. said dense body comprising a core selected from the class consisting of tungsten and molybdenum encased in a substantially nonporous casting of a molybdenum-silicon alloy, the alloy containing from about 22.5% to about 47% silicon.
  • a dense body of 'high strength and high resistance to oxidation, to erosion of gases, to thermal'shock and to deformation at temperatures above about 1200 0. said dense body comprising asubstanq tially non-porous cast body of a molybdenumsilicon alloy, the alloy containing from about 22.5% to about 47% silicon, and a reinforcing core embedded in said cast body.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Furnace Details (AREA)

Description

Jan. 12, 1954 A. BEIDLER ET AL 2,665,474
HIGHLY REFRACTORY MOLYBDENUM ALLOYS Filed March 18, 1950 Fly. 1
EDWARD A. E/DLER I l/OR E CAMPBELL I N V EN TORS.
Patented Jan. 12;, 1954 UNETED HIGHLY REFRACTORY MOLYBDENUM ALLOYS York Application March 18, 1950, Serial No. 150,541
8 Claims.
This invention relates to solid, dense molybdenum alloy bodies having high strengths and a high resistance to oxidation, to thermal shock, to erosion of hot gases and to deformation at elevated temperatures.
The refractory metal molybdenum, has highly desirable properties and characteristics for many purposes and retains its normal mechanical properties at elevated temperatures. Molybdenum, for example, is very desirable for use in electric furnace heating elements, however, it is subject to oxidation at elevated temperatures and oxygen is excluded by maintaining a flow of hydrogen over the heated resistance element.
In the copending application of Campbell et al., Serial No. 150,398, filed March 18, 1950, entitled Highly Refractory Bodies, there is described and claimed a molybdenum body protected against oxidation at elevated temperatures by the provision of an integral coating or skin composed of molybdenum-silicon alloys. For some purposes, difl'iculties are encountered in producing a relatively thick and uniform alloy coating on the molybdenum to provide this integral protective skin. These difiiculties are encountered particularly in the production of bodies of irregular configuration and complex sections.
The principal purpose of the present invention is to provide solid bodies formed of certain molybdenum alloys which bodies possess the aforementioned characteristics and properties at elevated temperatures.
Another purpose of this invention is to provide solid bodies of irregular configuration formed of certain molybdenum alloys.
Other objects and advantages of this invention 'will become apparent from the following descrip- .tion and claims.
In the drawings:
Fig. 1 is a cross-sectional view of a nozzle :formed of the alloys of this invention.
Fig. 2 is a cross-sectional view of a large body formed of the alloys of thisinvention and including a reinforcing core.
The present invention contemplates the production of solid bodies formed of molybdenumsilicon alloys or intermetallic compounds, the silicon content of thealloys varying in the molec ularra'tio of silicon to molybdenum of from about 1:1 to about 3:1. This ratio corresponds .toallcys or intermetallic compounds of molybdenum and silicon containing from about 22% to about 47% silicon. The alloy or compound corresponding to a molecular ratio of silicon to molybdenum of about 2:1 or containing about 37% silicon appears to provide the most satisfactory bodies.
These alloys of intermetallic compounds may be formed by any desired method. One convenient method includes mixing molybdenum powder and silicon powder in the desired proportions in accordance with powder metallurgy practice. The mixture is then pressed into briquets and the briquets heated slowly to a temperature of about 1050 C. to about 1100 C: A rapid exothermic reaction occurs and continues to a temperature of about 1450 C. The rate of reaction and completeness of the reaction may be regulated by a control of the particle size of the molybdenum and silicon powders. The mass, after it is cooled, is quite porous and brittle and may be employed directly or may be converted into a granular or powder form.
The alloy or intermetallic compound so produced is melted as by heating in an arc-melting furnace or may be placed in a suitable crucible and heated by induction. The molybdenum-silicon alloys are quite reactive with many of the usual refractory materials employed for lining crucibles and furnaces at the temperatures required to render the alloys sufiiciently fluid to permit pouring and casting. Thus, magnesia and beryllia are not satisfactory. Graphite apparently reacts with the molybdenum-silicon alloys to a sufiicient extent so that the alloys when melted in contact with graphite become somewhat viscous. The alloys react sufficiently with graphite so that although they are heated in contact with graphite to temperatures as high as about 2200 0., the molten alloys do not possess sufficient fluidity to permit satisfactory casting. We have found that zirconia stabilized with calcium oxide is satisfactory as furnace and crucible linings and for the manufacture of crucibles.
The alloys may be cast in molds formed of graphite or zirconia. Since the alloys are generally cast at temperatures above 1800 C., the
molds are preheated to a temperature of between- 500 C. and 1000 C. before the molten alloy is poured into the mold to avoid chilling the hot mass too rapidly. In some instances, particularly in forming bodies having relatively thin sections, graphite molds are less desirable because the higher heat conductivity of graphite results in an undesired rapid cooling.
We have found that when the alloys are melted there is an ebullition of gas, and this ebullition appears to continue until the alloy begins to solidify. Castings thus produced are porous and the degrees of porosity appears to vary inversely with the maximum temperature of the melt prior to pouring and with the period of time the material has been maintained in a molten condition. We have discovered that by heating the molten mass to a higher temperature for a brief period or by maintaining themassmolten for a prolonged period, the ebullition may be brought farther towards completion so as to provide substantially non-porous cast bodies. During the ebullition, the alloys appear to lose silicon and it may be necessary in some, instances to add silicon so as to insure the desired silicon content in the finished cast bodies.
The cast bodies of the molybdenum-silicon alloys are somewhat brittle, particularly those cast in graphite molds due to the rapid cooling which results because of the high heat conductivity of graphite. The brittleness may be reduced by vacuum annealing, for example by heating the cast bodies in a vacuum to a temperature of about 1100 C. for 20 to 24 hours. During this vacuum annealing it is observed that gases are released from the bodies.
The cast bodies have a density of about 6.2 grams per cubic centimeter and a compressive strength of about 100,000 pounds-per square inch at room temperature. The bodies retain a high strength at elevated temperatures. The bodies are extremely resistant to thermal shock, for example, the body may be rapidly heated to red heat by the use of a oxyacetylene torch and immediately quenched in water without exhibiting cracks. The body may be subjected to several such cycles without exhibiting cracks and because of the extremely high resistance to oxidation will exhibit no signs of surface oxidation. I
temperatures and the bodies are extremely resistant to deformation at high temperatures.
Electrical heating elements must posses a high resistance to thermal shock, a high resistance "to oxidation and must have a fairly highelectrical conductivity. Cast bodies of molybdenumsilicon alloys are particularly advantageous as such heating elements becauseof their exceedingly high resistance'to oxidation. The element may be formed from a cast rod of any desired diameter and length or may consist of a cast grid. Because of the highcompressivestrength, ood electrical contact with the element may be obtained by means of. suitable clamps.
As is well known, various types of nozzles,- jets, and vanes intended for uses where they will be subjected to high velocity gases, such as erosive gases of combustion, must possess high resistance to oxidation and the erosive action'of gases of combustion and must also be highly resistant .2 thermal shock. Such elements may be advantageously formed'by casting the desired: body from the molybdenum-silicon alloys as described hereintofore. As' illustrated in"Fig.'l, a nozzle l having a longitudinally extending aperture 2 may be formed by casting the allow in a graphite mold having a suitable core for forming the aperture.
For some bodies, particularly larger sized bodies, it may be desirable to increase the strength of the cast body. This may be readily attained by reinforcing the cast body with molybdenum or tungsten shapes. In the production of such bodies, the molybdenum or tungsten core or shape is supported in the mold in a conventional manner and the molten molybdenum-silicon alloy cast about the core. In order to prevent contamination of the'alloy, rods of molybdenum-silicon alloy may be employed to position the core within the mold cavity. As shown in Fig.2, the-finished body consists of the core 3 about which the alloy 4 has been cast. It is or may consist of spaced plates, the details being dependent upon the particular shape of the fin- ..ished body.
It is to be understood that the foregoing description is intended to be illustrative of our invention and "the specific examples included are set forth for purposes of illustration rather than as limitations of the invention.
We claim:
1. As an articleof manufacture, a dense'body of high strength and high resistance to oxidation, to erosion of gases, to thermal shock and to deformation at temperatures above about 1200 0., consisting of a substantially non-porous cast body of a molybdenum-silicon alloy, the alloy containing from about 22.5% to about 47% silicon.
2. As an article of manufacturea dense body of high strength and high resistance to oxidation, to erosion-of gases, to thermal shock and to deformation at temperatures above about 1200 0., consisting of a substantially nonporous cast body of a molybdenum-silicon alloy, the
alloy containing about 37% silicon.
3. An electrical heating element consisting of a substantially non-porous cast body of a molybdenum-silicon alloy, the alloy containing from about 22.5% to about 47% silicon.
4. An electrical heating element consisting of a substantially non-porous cast body of a molybdenum-silicon alloy, the alloy containing about 37% silicon.
5. A nozzle for 'erosivegases of combustion consisting of a substantially non-porous cast tubular body of a molybdenum-silicon alloy, the
alloy containing from about 22.5% to about 47% silicon.
6. A nozzle for erosive gases of combustion consisting of a substantially non-porous cast tubular body ofa molybdenum-silicon alloy, the alloy containing about 37% silicon.
7. Asan article of manufacture, a dense body of high'strength and high resistance to oxidation, to erosion Of gases,' to'therma1 shock. and to deformation at temperatures above about 1200 C., said dense body comprisinga core selected from the class consisting of tungsten and molybdenum encased in a substantially nonporous casting of a molybdenum-silicon alloy, the alloy containing from about 22.5% to about 47% silicon.
8. As an article of manufacture, a dense body of 'high strength and high resistance to oxidation, to erosion of gases, to thermal'shock and to deformation at temperatures above about 1200 0., said dense body comprising asubstanq tially non-porous cast body of a molybdenumsilicon alloy, the alloy containing from about 22.5% to about 47% silicon, and a reinforcing core embedded in said cast body.
References Cited in the file Of this patent UNITED STATES PATENTS Number 6 FOREIGN PATENTS Number Country Date EDWARD BEIDLER- 294,267 Germany Sept. 25, 1916 IVOR CAMPBELL 435,754 Great Britain Sept. 23, 1935 OTHER REFERENCES Hansen: Aufbau der Zweistoffleigerungen, 1936; page 912.
Name Date Kelley June 25, 1929 w g f??? gfig August 1944 Marshall Apr. 12, 1932 pages 8 up Linz July 1, 1942 Briney Nov. 25, 1952

Claims (1)

1. AS AN ARTICLE OF MANUFACTURE, A DENSE BODY OF HIGH STRENGTH AND HIGH RESISTANCE TO OXIDATION, TO EROSION OF GASES, TO THERMAL SHOCK AND TO DEFORMATION AT A TEMPERATURES ABOVE ABOUT 1200* C., CONSISTING OF A SUBSTANTIALLY NON-POROUS CAST BODY OF A MOLYBDENUM-SILICON ALLOY, THE ALLOY CONTAINING FROM ABOUT 22.5% TO ABOUT 47% SILICON.
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2745928A (en) * 1952-10-06 1956-05-15 American Electro Metal Corp Heater bodies and their production
US2770029A (en) * 1952-06-02 1956-11-13 Norton Co Composite electrical resistor
US2779580A (en) * 1954-07-26 1957-01-29 Schwarzkopf Dev Co High temperature furnaces and their production
US2779579A (en) * 1954-07-26 1957-01-29 Schwarzkopf Dev Co Conveyor for high temperature furnaces
US2831242A (en) * 1953-03-25 1958-04-22 Schwarzkopf Dev Co Sintered electric resistance heating element
US2839292A (en) * 1954-08-09 1958-06-17 Harry T Bellamy Refractory reservoir for aluminum
US2982619A (en) * 1957-04-12 1961-05-02 Roger A Long Metallic compounds for use in hightemperature applications
US3038817A (en) * 1958-08-13 1962-06-12 Crucible Steel Co America Self-healing coatings for refractory metals and method for applying the same
DE1135262B (en) * 1954-03-01 1962-08-23 Boehler & Co Ag Geb Process for the production of wear-resistant surfaces on workpieces from non-magnetizable steels
US3090686A (en) * 1958-02-19 1963-05-21 Nachtman John Simon Recovery of metal by use of lead
US3097795A (en) * 1960-11-01 1963-07-16 Parker Hannifin Corp Spill type fuel injection nozzle
US3297487A (en) * 1964-10-16 1967-01-10 Du Pont Fuel cell
US5595616A (en) * 1993-12-21 1997-01-21 United Technologies Corporation Method for enhancing the oxidation resistance of a molybdenum alloy, and a method of making a molybdenum alloy
US6715701B1 (en) * 1998-01-15 2004-04-06 Nitinol Technologies, Inc. Liquid jet nozzle

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE294267C (en) *
US1718563A (en) * 1925-04-17 1929-06-25 Gen Electric Treatment of metals
US1853370A (en) * 1927-12-27 1932-04-12 Technimet Company Formation of silicon alloy coatings
GB435754A (en) * 1932-12-21 1935-09-23 Ver Edelstahl Ag Improvements in or relating to the production of carbides, carbonitrides, nitrides, borides, silicides and titanides
US2290194A (en) * 1940-08-13 1942-07-21 Climax Molybdenum Co Process of producing molybdenum containing alloys
US2619406A (en) * 1949-04-27 1952-11-25 Union Carbide & Carbon Corp Method for the solid phase production of a disilicide

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE294267C (en) *
US1718563A (en) * 1925-04-17 1929-06-25 Gen Electric Treatment of metals
US1853370A (en) * 1927-12-27 1932-04-12 Technimet Company Formation of silicon alloy coatings
GB435754A (en) * 1932-12-21 1935-09-23 Ver Edelstahl Ag Improvements in or relating to the production of carbides, carbonitrides, nitrides, borides, silicides and titanides
US2290194A (en) * 1940-08-13 1942-07-21 Climax Molybdenum Co Process of producing molybdenum containing alloys
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Cited By (15)

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US2770029A (en) * 1952-06-02 1956-11-13 Norton Co Composite electrical resistor
US2745928A (en) * 1952-10-06 1956-05-15 American Electro Metal Corp Heater bodies and their production
US2831242A (en) * 1953-03-25 1958-04-22 Schwarzkopf Dev Co Sintered electric resistance heating element
DE1135262B (en) * 1954-03-01 1962-08-23 Boehler & Co Ag Geb Process for the production of wear-resistant surfaces on workpieces from non-magnetizable steels
US2779580A (en) * 1954-07-26 1957-01-29 Schwarzkopf Dev Co High temperature furnaces and their production
US2779579A (en) * 1954-07-26 1957-01-29 Schwarzkopf Dev Co Conveyor for high temperature furnaces
US2839292A (en) * 1954-08-09 1958-06-17 Harry T Bellamy Refractory reservoir for aluminum
US2982619A (en) * 1957-04-12 1961-05-02 Roger A Long Metallic compounds for use in hightemperature applications
US3090686A (en) * 1958-02-19 1963-05-21 Nachtman John Simon Recovery of metal by use of lead
US3038817A (en) * 1958-08-13 1962-06-12 Crucible Steel Co America Self-healing coatings for refractory metals and method for applying the same
US3097795A (en) * 1960-11-01 1963-07-16 Parker Hannifin Corp Spill type fuel injection nozzle
US3297487A (en) * 1964-10-16 1967-01-10 Du Pont Fuel cell
US5595616A (en) * 1993-12-21 1997-01-21 United Technologies Corporation Method for enhancing the oxidation resistance of a molybdenum alloy, and a method of making a molybdenum alloy
US5693156A (en) * 1993-12-21 1997-12-02 United Technologies Corporation Oxidation resistant molybdenum alloy
US6715701B1 (en) * 1998-01-15 2004-04-06 Nitinol Technologies, Inc. Liquid jet nozzle

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