US3169860A - Molybdenum-hafnium alloy casting - Google Patents

Molybdenum-hafnium alloy casting Download PDF

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Publication number
US3169860A
US3169860A US191258A US19125862A US3169860A US 3169860 A US3169860 A US 3169860A US 191258 A US191258 A US 191258A US 19125862 A US19125862 A US 19125862A US 3169860 A US3169860 A US 3169860A
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molybdenum
hafnium
tungsten
carbon
content
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US191258A
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Semchyshen Marion
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Cyprus Amax Minerals Co
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American Metal Climax Inc
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C27/00Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
    • C22C27/04Alloys based on tungsten or molybdenum

Definitions

  • the present invention relates to cast molybdenum base alloys containing hafnium and which are characterized by the fact that they are capable of being worked at elevated temperatures and have unusually high strength at temperatures in the range of 1600 F. and above.
  • the alloys of the present invention contain from .02% to 12% hafnium and up to .75 carbon, preferably 01% to .04% carbon.
  • the balance consists essentially of molybdenum, except that small quantities of titanium and/ or zirconium may be present as optional ingredients.
  • titanium may be present in amounts up to but not more than 5% and zirconium in amounts up to 1%.
  • a portion of the molybdenum may be replaced by tungsten up to a total not exceeding the molybdenum present. Since even the smallest amount of oxygen is deleterious, the oxygen content of the alloys must be less than 005% and is preferably less than 002%.
  • the alloys of the present invention may be prepared by arc-melting in vacuum, preferably using a furnace of the type disclosed in United States Patent 2,656,743.
  • the preferred method of deoxidizing the melt is by adding carbon to the charge to react with any oxygen present in raw materials and in quantities which will leave the desired excess in the final casting.
  • the absolute pressure during the melting operation is preferably maintained below 50 microns of mercury.
  • a twelfth example of an alloy containing both the optional ingredients titanium and zirconium is an alloy containing .14% hafnium, 148% titanium, .077% zirconium, .02% carbon and the balance consisting essentially of molybdenum.
  • any of the above examples may have up to one-half of the molybdenum replaced by tungsten.
  • the use of larger quantities of tungsten should be avoided because of forging difiiculties.
  • the maximum hafnium content decrease proportionately from 12% to 1% as the tungsten content increases toward equality with the molybdenum.
  • the high strength of the alloys of the present invention will be apparent from the fact that the alloy of Example 1 has a tensile strength of 66,300 pounds per square inch at 1600 F the alloy of Example 3 has a tensile strength of 74,900 pounds per square inch at 1600 F.; the alloy of Example 8 has a tensile strength of 85,100 pounds per square inch at 1800 F.; and the alloy of Example 12 has a tensile strength of 85,200 pounds per square inch at 1800 F.
  • the tensile strength figures given above are all applicable to the forged alloys in a stress-relieved condition.
  • the alloys of the present invention may be forged or worked at temperatures in the neighborhood of 2300 F. or above.
  • a cast alloy containing from .02% to 12% hafnium, .01% to .75% carbon, less than 005% oxygen, not more than 5% titanium, not more than 1% zirconium, and the balance consisting essentially of a member from the group consisting of molybdenum and mixtures of molybdenum and tungsten wherein the molybdenum content is at least equal to the tungsten content.
  • a cast alloy containing from .02% to 12% hafnium, 01% to .75 carbon, less than 005% oxygen, and the balance consisting essentially of molybdenum.
  • a cast molybdenum alloy capable of being worked at elevated temperatures and containing from .02% to 12% hafnium, not more than .75 carbon, less than .005 oxygen, not more than 5% titanium and not more than 1% zirconium, the balance consisting essentially of a member from the group consisting of molybdenum and mixtures of molybdenum and tungsten wherein the molybdenum content is at least equal to the tungsten content, and the maximum hafnium content being reduced proportionately from 12% to 1% as the tungsten content increases toward equality with the molybdenum.
  • a cast molybdenum alloy capable of being worked at elevated temperatures and containing from .02% to 12% hafnium, not more than .75 carbon, less than .005 oxygen, not more than 5% titanium and not more than 1% zirconium, the balance consisting essentially of molybdenum.
  • a cast molybdenum alloy capable of being worked at elevated temperatures and containing from .02% to 12% hafnium, and .01% to .04% carbon, the balance consisting essentially of molybdenum.

Description

United States Patent the Public Claims. (Cl. 75176) This application is a continuation-in-part of applicants application Serial No. 41,766, filed July 11, 1960, now abandoned, which was a continuation-in-part of application Serial No. 760,066, filed September 10, 1958, and now abandoned.
The present invention relates to cast molybdenum base alloys containing hafnium and which are characterized by the fact that they are capable of being worked at elevated temperatures and have unusually high strength at temperatures in the range of 1600 F. and above.
The alloys of the present invention contain from .02% to 12% hafnium and up to .75 carbon, preferably 01% to .04% carbon. The balance consists essentially of molybdenum, except that small quantities of titanium and/ or zirconium may be present as optional ingredients. Thus, titanium may be present in amounts up to but not more than 5% and zirconium in amounts up to 1%. In addition, a portion of the molybdenum may be replaced by tungsten up to a total not exceeding the molybdenum present. Since even the smallest amount of oxygen is deleterious, the oxygen content of the alloys must be less than 005% and is preferably less than 002%.
The alloys of the present invention may be prepared by arc-melting in vacuum, preferably using a furnace of the type disclosed in United States Patent 2,656,743. The preferred method of deoxidizing the melt is by adding carbon to the charge to react with any oxygen present in raw materials and in quantities which will leave the desired excess in the final casting. The absolute pressure during the melting operation is preferably maintained below 50 microns of mercury.
The following are specific examples of alloys coming within the scope of the present invention:
A twelfth example of an alloy containing both the optional ingredients titanium and zirconium is an alloy containing .14% hafnium, 148% titanium, .077% zirconium, .02% carbon and the balance consisting essentially of molybdenum.
In cases where a higher melting point or slightly higher strength in a recrystallized state at temperatures above 2000 F. is desired, any of the above examples may have up to one-half of the molybdenum replaced by tungsten. In alloys such as the present, in which substantial quantities of molybdenum are employed, the use of larger quantities of tungsten should be avoided because of forging difiiculties. In addition, it is preferred that the maximum hafnium content decrease proportionately from 12% to 1% as the tungsten content increases toward equality with the molybdenum.
Patented Feb. 16, 1965 The high strength of the alloys of the present invention will be apparent from the fact that the alloy of Example 1 has a tensile strength of 66,300 pounds per square inch at 1600 F the alloy of Example 3 has a tensile strength of 74,900 pounds per square inch at 1600 F.; the alloy of Example 8 has a tensile strength of 85,100 pounds per square inch at 1800 F.; and the alloy of Example 12 has a tensile strength of 85,200 pounds per square inch at 1800 F. The tensile strength figures given above are all applicable to the forged alloys in a stress-relieved condition.
The alloys of the present invention may be forged or worked at temperatures in the neighborhood of 2300 F. or above.
All proportions given are proportions by weight.
What is claimed is:
1. A cast alloy containing from .02% to 12% hafnium, .01% to .75% carbon, less than 005% oxygen, not more than 5% titanium, not more than 1% zirconium, and the balance consisting essentially of a member from the group consisting of molybdenum and mixtures of molybdenum and tungsten wherein the molybdenum content is at least equal to the tungsten content.
2. A cast alloy containing from .02% to 12% hafnium, 01% to .75 carbon, less than 005% oxygen, and the balance consisting essentially of molybdenum.
3. A cast molybdenum alloy capable of being worked at elevated temperatures and containing from .02% to 12% hafnium, not more than .75 carbon, less than .005 oxygen, not more than 5% titanium and not more than 1% zirconium, the balance consisting essentially of a member from the group consisting of molybdenum and mixtures of molybdenum and tungsten wherein the molybdenum content is at least equal to the tungsten content, and the maximum hafnium content being reduced proportionately from 12% to 1% as the tungsten content increases toward equality with the molybdenum.
4. A cast molybdenum alloy capable of being worked at elevated temperatures and containing from .02% to 12% hafnium, not more than .75 carbon, less than .005 oxygen, not more than 5% titanium and not more than 1% zirconium, the balance consisting essentially of molybdenum.
5. A cast molybdenum alloy capable of being worked at elevated temperatures and containing from .02% to 12% hafnium, and .01% to .04% carbon, the balance consisting essentially of molybdenum.
References Cited by the Examiner Reinhold Publishing Corp., Chapman & Hall, Ltd., London, see especially Table 12.17 and Chemical Properties, pages 212-213.
DAVID L. RECK, Primary Examiner.
W. A. DOUGLAS, Examiner.

Claims (1)

1. A CAST ALLOY CONTAINING FROM .02% TO 12% HAFNIUM, .01% TO .75% CARBON, LESS THAN .005% OXYGEN, NOT MORE THAN 5% TITANIUM, NOT MORE THAN 1% ZIRCONIUM, AND THE BALANCE CONSISTING ESSENTIALLY OF A MEMBER FROM THE GROUP CONSISTING OF MOLYBDENUM AND MIXTURES OF MOLYBDENUM AND TUNGSTEN WHEREIN TH EMOLYBDENUM CONTENT IS AT LEAST EQUAL TO THE TUNGSTEN CONTENT.
US191258A 1962-04-30 1962-04-30 Molybdenum-hafnium alloy casting Expired - Lifetime US3169860A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3243291A (en) * 1963-10-29 1966-03-29 Gen Telephone & Elect High-temperature alloy
US3403009A (en) * 1964-08-10 1968-09-24 Minnesota Mining & Mfg Refractory metal structures
US3447921A (en) * 1966-12-21 1969-06-03 Gen Electric Molybdenum-base alloy
US3869635A (en) * 1972-06-28 1975-03-04 Siemens Ag Rotary anode for an x-ray tube
US4144022A (en) * 1977-04-11 1979-03-13 Amax Inc. Furnace rollers
US4165982A (en) * 1976-12-11 1979-08-28 Daido Tokushuko Kabushiki Kaisha Molybdenum base alloy having excellent high-temperature strength and a method of producing same
US4657735A (en) * 1985-10-02 1987-04-14 Amax Inc. Mo-Hf-C alloy composition
US4717538A (en) * 1986-11-28 1988-01-05 Gte Products Corporation Molybdenum-tungsten-titanium-zirconium-carbon alloy system
US4780902A (en) * 1985-07-11 1988-10-25 Schwarzkopf Development Corporation Rotary anode for X-ray tubes

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2234969A (en) * 1939-02-24 1941-03-18 Mallory & Co Inc P R Tungsten base contact
US2580273A (en) * 1947-09-25 1951-12-25 Climax Molybdenum Co Refractory metal alloy castings and methods of making same
US2678269A (en) * 1951-10-06 1954-05-11 Climax Molybdenum Co Molybdenum-titanium alloys
US2678271A (en) * 1951-10-06 1954-05-11 Climax Molybdenum Co Molybdenum-zirconium alloys
GB756012A (en) * 1951-03-30 1956-08-29 Climax Molybdenum Co Improvements in or relating to cast molybdenum base alloys
US2798808A (en) * 1953-02-02 1957-07-09 Westinghouse Electric Corp Method of introducing zirconia into tungsten powder preliminary to forming electrodes
US2960403A (en) * 1958-02-24 1960-11-15 American Metal Climax Inc Molybdenum-base alloys
US3116145A (en) * 1962-04-30 1963-12-31 American Metal Climax Inc Tungsten-hafnium alloy casting

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2234969A (en) * 1939-02-24 1941-03-18 Mallory & Co Inc P R Tungsten base contact
US2580273A (en) * 1947-09-25 1951-12-25 Climax Molybdenum Co Refractory metal alloy castings and methods of making same
GB756012A (en) * 1951-03-30 1956-08-29 Climax Molybdenum Co Improvements in or relating to cast molybdenum base alloys
US2678269A (en) * 1951-10-06 1954-05-11 Climax Molybdenum Co Molybdenum-titanium alloys
US2678271A (en) * 1951-10-06 1954-05-11 Climax Molybdenum Co Molybdenum-zirconium alloys
US2798808A (en) * 1953-02-02 1957-07-09 Westinghouse Electric Corp Method of introducing zirconia into tungsten powder preliminary to forming electrodes
US2960403A (en) * 1958-02-24 1960-11-15 American Metal Climax Inc Molybdenum-base alloys
US3116145A (en) * 1962-04-30 1963-12-31 American Metal Climax Inc Tungsten-hafnium alloy casting

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3243291A (en) * 1963-10-29 1966-03-29 Gen Telephone & Elect High-temperature alloy
US3403009A (en) * 1964-08-10 1968-09-24 Minnesota Mining & Mfg Refractory metal structures
US3447921A (en) * 1966-12-21 1969-06-03 Gen Electric Molybdenum-base alloy
US3869635A (en) * 1972-06-28 1975-03-04 Siemens Ag Rotary anode for an x-ray tube
US4165982A (en) * 1976-12-11 1979-08-28 Daido Tokushuko Kabushiki Kaisha Molybdenum base alloy having excellent high-temperature strength and a method of producing same
US4144022A (en) * 1977-04-11 1979-03-13 Amax Inc. Furnace rollers
US4780902A (en) * 1985-07-11 1988-10-25 Schwarzkopf Development Corporation Rotary anode for X-ray tubes
US4657735A (en) * 1985-10-02 1987-04-14 Amax Inc. Mo-Hf-C alloy composition
US4717538A (en) * 1986-11-28 1988-01-05 Gte Products Corporation Molybdenum-tungsten-titanium-zirconium-carbon alloy system

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