US2818338A - Titanium alloys - Google Patents

Titanium alloys Download PDF

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Publication number
US2818338A
US2818338A US644434A US64443457A US2818338A US 2818338 A US2818338 A US 2818338A US 644434 A US644434 A US 644434A US 64443457 A US64443457 A US 64443457A US 2818338 A US2818338 A US 2818338A
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United States
Prior art keywords
titanium
alloys
silicon
carbon
tungsten
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US644434A
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Earl F Swazy
Richard H Freyer
Lee S Busch
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RMI Co
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RMI Co
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium

Definitions

  • This invention relates generally to alloys of titanium and has particular reference to alloys consisting of titanium, carbon and silicon, alone,-or in combination with another element, to form a quaternary alloy with titanium predominating.
  • This application is a divisional application of Serial No. 382,183, filed September 4, 1953, now Patent No. 2,786,756, dated March26, 1957, which in turn is a division of application Serial No. 138,516, filed January 13, 1950, now Patent No. 2,661,286, dated December 1, 1953.
  • An object of the present invention is to provide wrought, ductile alloys of titanium.
  • Another object of the present invention is to provide a wrought, ductile alloy of titanium, carbon and silicon.
  • Still another object of the invention is to provide quaternary alloys of titanium.
  • Yet another object of the invention is to provide alloys of titanium consisting of titanium, carbon and silicon having greater resistance to oxidation at elevated temperatures than pure titanium and exhibiting good hardness characteristics thereof.
  • Another object of the invention is to provide an alloy of titanium consisting of titanium, carbon and silicon and any one of the following elements: aluminum, copper, vanadium, chromium, boron, tungsten and iron.
  • Yet another object of the invention contemplates a method of preparing quaternary alloys of titanium consisting of the ternary alloys of carbon, silicon and titanium, to which is added an element from the group; aluminum, copper, chromium, vanadium, boron, tungsten or iron.
  • the invention in another of its aspects, relates to the novel features and principles teaching the objects of the invention and to the novel principles employed herein whether or not these features and principles may be used in said object or in said field.
  • alloys of titanium, silicon and carbon with titanium predominating as a ternary alloy, or as an alloy to which may be added another element such as aluminum, chromium, copper, vanadium, boron, tungsten or iron provide a resistance to oxidation at elevated temperatures greater than that of pure titanium.
  • Such alloys provide ductile, strong alloys of titanium and exhibit good corrosion resistance and high hardness characteristics at elevated temperatures.
  • These alloys are usually manufactured by melting and casting in a graphite retort under an inert or neutral atmosphere; for example, argon, or in a vacuum. Further, the alloys may also be prepared by powder metallurgy methods.
  • alloys containing .1% to silicon, .2% to 2% carbon with the balance titanium, as compared to pure titanium, are characterized by having a higher tensile strength, equivalent ductility, slightly higher electrical resistivity, much better resistance to oxidation at elevated temperatures and high hardness at temperatures up to 600 C. Further they may be hot or cold worked by the usual methods known to the art.
  • alloys are characterized by a unique response to heat treatment. Upon quenching from 1000 C these alloys do not harden appreciably (most alloys of; titanium which contain metals forming stable carbides doharden on quenching). However, as. the tensile strength is lowered to 113,500 p. s. i., the elonga- In' the as forged condition, the hardness at 600 C. increases from 0 Rockwell A to 32 Rockwell A when quenched. These changes are apparently caused by the presence of large amount of B titanium (body centered cubic) which is not transformed to a on fast cooling from 1000 C.
  • Alloys of titanium, tungsten, silicon and carbon have also been fabricated exhibiting substantially the same qualities as the other alloys depending upon the base ternary alloy of titanium, carbon and silicon.
  • the element tungsten is added to the basealloy above.
  • These alloys, utilizing tungsten, may be similarly manufactured as previously described and also may be prepared according. to powder metallurgy methods.
  • a preferred method consists of mixing tungsten and silicon in massive or powder form with titanium in sponge or powder form and melting and casting in graphite.
  • the source of the carbon is the crucible or retort so the amount is easily controlled by varying the time the charge is molten.
  • the alloys are preferably forged in air at temperatures between 800 C. and 900 C. but may be hot or cold worked by the usual methods known to the art.
  • the alloys of titanium, carbon, silicon and tungsten, here described, may be made containing small but significant amounts of tungsten, silicon and carbon: that is, up to 10% tungsten; up to 5% silicon; and up to 2% carbon; the balance being titanium.
  • the lower limit therefor is 0.1% tungsten; 0.1% silicon; 0.1% carbon; and the balance titanium.
  • a practical range of composition is 0.5% to 5% tungsten; 0.5% to 3% silicon; 0.3% to 0.7% carbon; and the balance titanium.
  • Alloy table depicting the con- Ii, per- Si, por- 0, per- Alloy cent cent cent and (1) Ti, Si, o 99. 7-88 0.1-io 0.2-2 (7) Ti, S1, C W 99. 7-83 1-5 l-Z 0. 1l0% sist of up to 10% silicon; up to 2% carbon; and up to 10% tungsten; the remainder being substantially all titanium. 7

Description

United States Patent 2,818,338 TITANIUM ALLOYS Earl F. Swazy, Richard; H. Freyer, and' Lee S.';Busch, Indianapolis, -Ind., assignors, by mesne assignments, to .Mallory-Sharon Titanium Corporation, Indianapolis, ,.Ind., a corporation of Delaware No Drawing. -Applicatiou September 4, 1953, SerialNo.
382,183, now Patent No. 2,786,756, datedxMarch -26, 1957, which is a division of appl cation SerialNo. 138,516, January 13,1950, now Patent No. -2',61-, 2 86, dated December 1, 1953. Divided and this application February 15, 1957, Serial No. 644,434
3 Claims. (Cl. 75175.5)
This invention relates generally to alloys of titanium and has particular reference to alloys consisting of titanium, carbon and silicon, alone,-or in combination with another element, to form a quaternary alloy with titanium predominating. This application is a divisional application of Serial No. 382,183, filed September 4, 1953, now Patent No. 2,786,756, dated March26, 1957, which in turn is a division of application Serial No. 138,516, filed January 13, 1950, now Patent No. 2,661,286, dated December 1, 1953.
An object of the present invention, therefore, is to provide wrought, ductile alloys of titanium.
Another object of the present invention is to provide a wrought, ductile alloy of titanium, carbon and silicon.
Still another object of the invention is to provide quaternary alloys of titanium.
Yet another object of the invention is to provide alloys of titanium consisting of titanium, carbon and silicon having greater resistance to oxidation at elevated temperatures than pure titanium and exhibiting good hardness characteristics thereof.
Another object of the invention is to provide an alloy of titanium consisting of titanium, carbon and silicon and any one of the following elements: aluminum, copper, vanadium, chromium, boron, tungsten and iron.
Yet another object of the invention contemplates a method of preparing quaternary alloys of titanium consisting of the ternary alloys of carbon, silicon and titanium, to which is added an element from the group; aluminum, copper, chromium, vanadium, boron, tungsten or iron.
The invention, in another of its aspects, relates to the novel features and principles teaching the objects of the invention and to the novel principles employed herein whether or not these features and principles may be used in said object or in said field.
It is found that alloys of titanium, silicon and carbon with titanium predominating as a ternary alloy, or as an alloy to which may be added another element such as aluminum, chromium, copper, vanadium, boron, tungsten or iron provide a resistance to oxidation at elevated temperatures greater than that of pure titanium. Such alloys provide ductile, strong alloys of titanium and exhibit good corrosion resistance and high hardness characteristics at elevated temperatures. These alloys are usually manufactured by melting and casting in a graphite retort under an inert or neutral atmosphere; for example, argon, or in a vacuum. Further, the alloys may also be prepared by powder metallurgy methods. Thus, as an example, alloys containing .1% to silicon, .2% to 2% carbon with the balance titanium, as compared to pure titanium, are characterized by having a higher tensile strength, equivalent ductility, slightly higher electrical resistivity, much better resistance to oxidation at elevated temperatures and high hardness at temperatures up to 600 C. Further they may be hot or cold worked by the usual methods known to the art.
tion increases to 16.5%.
2,818,338 Ratented Dec. 31 1957 ICC AS a further x mp h e ran al oy. madeby. m xin silicon powderand titanium powder or sponge, and melting and casting in graphite in argon gas, contained 0.992% silicon, ..47%- carbon, with the--balance--titanium. This alloy had the; fo1lowing =proper ties as hot forgedto. 80%
-reduction in area (equivalent'properties of titanium containing .477% carbon only are included for comparison).
Moreover, alloys,,such as above, are characterized by a unique response to heat treatment. Upon quenching from 1000 C these alloys do not harden appreciably (most alloys of; titanium which contain metals forming stable carbides doharden on quenching). However, as. the tensile strength is lowered to 113,500 p. s. i., the elonga- In' the as forged condition, the hardness at 600 C. increases from 0 Rockwell A to 32 Rockwell A when quenched. These changes are apparently caused by the presence of large amount of B titanium (body centered cubic) which is not transformed to a on fast cooling from 1000 C.
Again, in resistance to scaling tests at 900 C., an alloy containing .992% silicon was three times as effective as that for titanium containing .47% carbon. The results revealed a 536% increase in weight for the silicon alloy and 1.89% for the titanium alloy containing carbon only.
Alloys of titanium, tungsten, silicon and carbon have also been fabricated exhibiting substantially the same qualities as the other alloys depending upon the base ternary alloy of titanium, carbon and silicon. In this case the element tungsten is added to the basealloy above. These alloys, utilizing tungsten, may be similarly manufactured as previously described and also may be prepared according. to powder metallurgy methods.
For example, a preferred method consists of mixing tungsten and silicon in massive or powder form with titanium in sponge or powder form and melting and casting in graphite. Again, the source of the carbon is the crucible or retort so the amount is easily controlled by varying the time the charge is molten. The alloys are preferably forged in air at temperatures between 800 C. and 900 C. but may be hot or cold worked by the usual methods known to the art.
The alloys of titanium, carbon, silicon and tungsten, here described, may be made containing small but significant amounts of tungsten, silicon and carbon: that is, up to 10% tungsten; up to 5% silicon; and up to 2% carbon; the balance being titanium. The lower limit therefor is 0.1% tungsten; 0.1% silicon; 0.1% carbon; and the balance titanium. A practical range of composition is 0.5% to 5% tungsten; 0.5% to 3% silicon; 0.3% to 0.7% carbon; and the balance titanium.
Alloys thus prepared have the following minimum properties:
As Quenched As Hot from 600 Forged O. to
Ultimate Tensile Strength ..p. s. i 120, 000 135, 000 Elongation in perceut 7 3 ..-..-p. s. L- 15x10 18Xl0 0 Electrical Resistivity ohm-cm.. 7tl 10- X 10- The following chart is useful in stituents of the above described alloys.
Alloy table depicting the con- Ii, per- Si, por- 0, per- Alloy cent cent cent and (1) Ti, Si, o 99. 7-88 0.1-io 0.2-2 (7) Ti, S1, C W 99. 7-83 1-5 l-Z 0. 1l0% sist of up to 10% silicon; up to 2% carbon; and up to 10% tungsten; the remainder being substantially all titanium. 7
While the present invention as to its objects is merely illustrative and not exhaustive in scope and since many widely different embodiments of the invention may be made without departing from the scope thereof, it is intended that all matter contained in the above description be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. Alloys containing from 0.1% to 10% tungsten, from 0.1% to 5% silicon, from 0.1% to 2% carbon and the balance being substantially all titanium.
2. Alloys containing from 0.1% to 10% tungsten, from 0.1% to 5% silicon, from 0.1% to 2% carbon and the balance being substantially all titanium, said alloys being quench hardenable and susceptible tothe mechanism of thermal precipitation treatment.
3. Alloys of titanium as in claim 2 having the following minimum properties:
No references cited.

Claims (1)

1. ALLOYS CONTAINING FROM 0.1% TO 10% TUNGSTEN, FROM 0.1% TO 5% SILICON, FROM 0.1% TO 2% CARBON AND THE BALANCE BEING SUBSTANTIALLY ALL TITANIUM.
US644434A 1957-02-15 1957-02-15 Titanium alloys Expired - Lifetime US2818338A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5696619A (en) * 1995-02-27 1997-12-09 Texas Instruments Incorporated Micromechanical device having an improved beam

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5696619A (en) * 1995-02-27 1997-12-09 Texas Instruments Incorporated Micromechanical device having an improved beam

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