US2665474A - Highly refractory molybdenum alloys - Google Patents
Highly refractory molybdenum alloys Download PDFInfo
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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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- 229910001182 Mo alloy Inorganic materials 0.000 title description 6
- 229910052710 silicon Inorganic materials 0.000 claims description 18
- 239000010703 silicon Substances 0.000 claims description 18
- 229910000676 Si alloy Inorganic materials 0.000 claims description 15
- GALOTNBSUVEISR-UHFFFAOYSA-N molybdenum;silicon Chemical compound [Mo]#[Si] GALOTNBSUVEISR-UHFFFAOYSA-N 0.000 claims description 15
- 239000007789 gas Substances 0.000 claims description 12
- 230000003647 oxidation Effects 0.000 claims description 12
- 238000007254 oxidation reaction Methods 0.000 claims description 12
- 230000035939 shock Effects 0.000 claims description 9
- 230000003628 erosive effect Effects 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 229910045601 alloy Inorganic materials 0.000 description 29
- 239000000956 alloy Substances 0.000 description 29
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 18
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 12
- 229910052750 molybdenum Inorganic materials 0.000 description 11
- 239000011733 molybdenum Substances 0.000 description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 10
- 229910002804 graphite Inorganic materials 0.000 description 10
- 239000010439 graphite Substances 0.000 description 10
- 238000010438 heat treatment Methods 0.000 description 8
- 238000005266 casting Methods 0.000 description 6
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 4
- 229910000765 intermetallic Inorganic materials 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- LTPBRCUWZOMYOC-UHFFFAOYSA-N Beryllium oxide Chemical compound O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 description 2
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical compound [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 2
- 238000000137 annealing Methods 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 230000001747 exhibiting effect Effects 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000011863 silicon-based powder Substances 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 description 1
- 239000000292 calcium oxide Substances 0.000 description 1
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- QFXZANXYUCUTQH-UHFFFAOYSA-N ethynol Chemical group OC#C QFXZANXYUCUTQH-UHFFFAOYSA-N 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000010301 surface-oxidation reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped 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
- C04B35/58—Shaped 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
- C04B35/58085—Shaped 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
- C04B35/58092—Shaped 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
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S239/00—Fluid sprinkling, spraying, and diffusing
- Y10S239/19—Nozzle materials
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12674—Ge- or Si-base component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
- Y10T428/12826—Group VIB metal-base component
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12806—Refractory [Group IVB, VB, or VIB] metal-base component
- Y10T428/12826—Group VIB metal-base component
- Y10T428/12833—Alternative to or next to each other
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow 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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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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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US150541A US2665474A (en) | 1950-03-18 | 1950-03-18 | Highly refractory molybdenum alloys |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US150541A US2665474A (en) | 1950-03-18 | 1950-03-18 | Highly refractory molybdenum alloys |
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| Publication Number | Publication Date |
|---|---|
| US2665474A true US2665474A (en) | 1954-01-12 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US150541A Expired - Lifetime US2665474A (en) | 1950-03-18 | 1950-03-18 | Highly refractory molybdenum alloys |
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| US (1) | US2665474A (en) |
Cited By (14)
| 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)
| 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 |
-
1950
- 1950-03-18 US US150541A patent/US2665474A/en not_active Expired - Lifetime
Patent Citations (6)
| 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 |
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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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