US2147636A - Alloy - Google Patents
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- Publication number
- US2147636A US2147636A US173596A US17359637A US2147636A US 2147636 A US2147636 A US 2147636A US 173596 A US173596 A US 173596A US 17359637 A US17359637 A US 17359637A US 2147636 A US2147636 A US 2147636A
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- US
- United States
- Prior art keywords
- alloy
- thermal treatment
- cobalt
- boron
- hardness
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/07—Alloys based on nickel or cobalt based on cobalt
Definitions
- An object of the present invention is to provide an alloy especially adapted-for use as metal cut ting tools, the cutting efliciency of which is superior to that of heretofore known high speed tools and other alloys.
- a further object is to provide an alloy which is free from or substantially free from carbon and which is readily amenable to thermal treatment by means of which the hardness, cutting efliciency resistance to deformation and other physical properties and characteristics can be accurately controlled over a comparatively wide range.
- Alloys of this invention may be used in the cast condition for certain purposes, but approximate maximum values of hardness, resistance to deformation and certain other important physical properties can be developed only through thermal treatment or through mechanical working and thermal treatment. Bodies of the alloy which have been subjected to such treatment are particularly. valuable for use as tools, dies and the like for the cutting or mechanical working of metals, as well as for many other industrial uses.
- the present alloy is particularly responsive to thermal treatment for the development of precipitation hardening and I usually prefer to subject the alloy to such thermal treatment before using it for metal cutting tools, dies, etc.
- cast bodies of the alloy may have a hardness of from to 57 on the Rockwell 0 scale and by subjecting the material to suitable 80 thermal treatment such as heating to a temperature higher than approximately 1000 C., followed by rapid quenching, the hardness can be lowered to an approximate range of from 35 to 45 Rockwell C.
- suitable 80 thermal treatment such as heating to a temperature higher than approximately 1000 C., followed by rapid quenching, the hardness can be lowered to an approximate range of from 35 to 45 Rockwell C.
- the alloy can subsequently be as subjectedto' a second thermal treatment, such.
- Bodies of .the alloy whichhave been subjected to a suitable thermal treatment are particularly resistant to abrasion at normal and elevated temperatureaand are also remarkably resistant to failure from sudden or repeated'shock and to me 15 chanical deformation. Consequently, cutting tools, dies and other articles composed of thepresent alloy retain an efiicient cutting edge or working face for unusually long periods of time.
- chromium may be used as an 25 essential component in the present alloy in an amount from 1% to 15%.
- compositions within the scope of the present invention which I have found well adapted for numerous industrial applica- 30 tions are the following: Boron 1.75%, titanium 3.60%, tungsten17%, cobalt substantially the balance; boron 2.15%, titanium 1%, molybdenum A 14%, cobalt substantially the balance; boron 2.45%, titanium 1.50%, tungsten 4%, chromium 35 14%, cobalt substantially the balance.
- An object of the present invention is to provide an alloy having high hardness. valuable metal cutting properties, etc. which is free from or substantially free from carbon and thus elim- 40 inate all of the serious disadvantages associated with carbon containing alloys or compositions intended for metal cutting tools, etc.
- I prefer to have the alloys entirely free from carbon in many instances I have found carbon present in the nature of an impurity incidental to manufacture. It is important, however, to restrict the carbon content to a maximum of about 0.15%, as I have found that the presence of to embrittle the alloy but also inhibit or retard -the desired or necessary reactions during thermal treatment. Furthermore, the presence of appreciable amounts of carbon decreases the red cutting tool.
- the preferred structure or a body of the present alloy particularly after thermal treatment, comprises at least two principal constituents; one, a relatively hard intermetallic compound of boron with one or more of the other essential components; and, two, a solid solution of two or more of the essential components which a lower degree of hardness and functions as a matrix.
- the mm of the con- .stituents. as well as ratio of particle size in any body of the alloy may be accurately controlled and flxed over a wide range by'means of thermal treatment.
- balance cobalt in the foregoing and in the following claims I intend that the alloy of the present invention comprise all of the I I 2,147,686 .hardnessof the alloy when it is used-as a metal,
- I claim: 7 A precipitation hardened alloy containing boron 0.50% to 4%, titanium 0.25% to 7%, metal selected from the group tungsten, molybdenum and uranium 2% to 30% and thebalanc'e. cobalt. 1
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cutting Tools, Boring Holders, And Turrets (AREA)
Description
Patented Feb. 2-1, 1939 ALLOY Anthony G. de Golyer, New York, N. Y.
No Drawing.
"gfiiu ation November 9, 1937, Serial No. 173, I
3 Claims. (Cl. 75-1711) The present invention relates to a new and.
useful alloy containing boron, titanium, tungsten and cobalt, ,which is characterized by being responsive to thermal treatment for the improve- 5 ment of physical properties.
An object of the present invention is to provide an alloy especially adapted-for use as metal cut ting tools, the cutting efliciency of which is superior to that of heretofore known high speed tools and other alloys. A further object is to provide an alloy which is free from or substantially free from carbon and which is readily amenable to thermal treatment by means of which the hardness, cutting efliciency resistance to deformation and other physical properties and characteristics can be accurately controlled over a comparatively wide range.
I have found through experiment that by alloying or otherwise intimately combining boron, titanium, tungsten and cobalt within the range boron 0.50% to 4%, titanium 0.25% to 7%, tung-- s'ten 2% to 30% and cobalt substantially the balance that I obtain metallic compositions which are readily responsive to thermal treatment by means of which the physical properties and characteristics can be developed and controlled. I have found that molybdenum or uranium may be used to supplant all or a portion of the tungsten of the alloy. I
Alloys of this invention may be used in the cast condition for certain purposes, but approximate maximum values of hardness, resistance to deformation and certain other important physical properties can be developed only through thermal treatment or through mechanical working and thermal treatment. Bodies of the alloy which have been subjected to such treatment are particularly. valuable for use as tools, dies and the like for the cutting or mechanical working of metals, as well as for many other industrial uses.
The present alloy is particularly responsive to thermal treatment for the development of precipitation hardening and I usually prefer to subject the alloy to such thermal treatment before using it for metal cutting tools, dies, etc. As an illustration, cast bodies of the alloy may have a hardness of from to 57 on the Rockwell 0 scale and by subjecting the material to suitable 80 thermal treatment such as heating to a temperature higher than approximately 1000 C., followed by rapid quenching, the hardness can be lowered to an approximate range of from 35 to 45 Rockwell C. The alloy can subsequently be as subjectedto' a second thermal treatment, such.
- higher percentages of this element not only act as heating to a temperature lower than 1000 C. for one hour or more, followed by cooling at a normal rate by which the hardness can be increased to from approximately 58'to '70 Rockwell C. An-important property of the alloy is that virtually all of the maximum hardness developed by thermal treatment is retained when the alloy is subjected to temperatures between 500 C. and 750 C. for long periods in various industrial operations.
Bodies of .the alloy whichhave been subjected to a suitable thermal treatment are particularly resistant to abrasion at normal and elevated temperatureaand are also remarkably resistant to failure from sudden or repeated'shock and to me 15 chanical deformation. Consequently, cutting tools, dies and other articles composed of thepresent alloy retain an efiicient cutting edge or working face for unusually long periods of time.
The more important distinctive advantages are 20 apparently due to the presence of appreciable amounts of boron in the composition, in conjunction with the other components within the percentages specified herein.
I have found that chromium may be used as an 25 essential component in the present alloy in an amount from 1% to 15%.
Specific examples of compositions within the scope of the present invention which I have found well adapted for numerous industrial applica- 30 tions are the following: Boron 1.75%, titanium 3.60%, tungsten17%, cobalt substantially the balance; boron 2.15%, titanium 1%, molybdenum A 14%, cobalt substantially the balance; boron 2.45%, titanium 1.50%, tungsten 4%, chromium 35 14%, cobalt substantially the balance.
. An object of the present invention is to provide an alloy having high hardness. valuable metal cutting properties, etc. which is free from or substantially free from carbon and thus elim- 40 inate all of the serious disadvantages associated with carbon containing alloys or compositions intended for metal cutting tools, etc. Although I prefer to have the alloys entirely free from carbon, in many instances I have found carbon present in the nature of an impurity incidental to manufacture. It is important, however, to restrict the carbon content to a maximum of about 0.15%, as I have found that the presence of to embrittle the alloy but also inhibit or retard -the desired or necessary reactions during thermal treatment. Furthermore, the presence of appreciable amounts of carbon decreases the red cutting tool.
My investigations indicate that the preferred structure or a body of the present alloy, particularly after thermal treatment, comprises at least two principal constituents; one, a relatively hard intermetallic compound of boron with one or more of the other essential components; and, two, a solid solution of two or more of the essential components which a lower degree of hardness and functions as a matrix. The mm of the con- .stituents. as well as ratio of particle size in any body of the alloy may be accurately controlled and flxed over a wide range by'means of thermal treatment. p v
a By the term balance cobalt" in the foregoing and in the following claims I intend that the alloy of the present invention comprise all of the I I 2,147,686 .hardnessof the alloy when it is used-as a metal,
essential components, other than cobalt, within 4 the limits specified herein, with -the remainder cobalt except for substantially ineffectual amounts of impurities which may be present incidental to manufacture. 5
I claim: 7 1. A precipitation hardened alloy containing boron 0.50% to 4%, titanium 0.25% to 7%, metal selected from the group tungsten, molybdenum and uranium 2% to 30% and thebalanc'e. cobalt. 1
ANTHONY G. Di: GOLYER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US173596A US2147636A (en) | 1937-11-09 | 1937-11-09 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US173596A US2147636A (en) | 1937-11-09 | 1937-11-09 | Alloy |
Publications (1)
Publication Number | Publication Date |
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US2147636A true US2147636A (en) | 1939-02-21 |
Family
ID=22632740
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US173596A Expired - Lifetime US2147636A (en) | 1937-11-09 | 1937-11-09 | Alloy |
Country Status (1)
Country | Link |
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US (1) | US2147636A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2699993A (en) * | 1951-06-29 | 1955-01-18 | Union Carbide & Carbon Corp | Welding rods for hard-facing |
US2743174A (en) * | 1946-04-25 | 1956-04-24 | John R Keeler | Uranium-titanium alloys |
-
1937
- 1937-11-09 US US173596A patent/US2147636A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2743174A (en) * | 1946-04-25 | 1956-04-24 | John R Keeler | Uranium-titanium alloys |
US2699993A (en) * | 1951-06-29 | 1955-01-18 | Union Carbide & Carbon Corp | Welding rods for hard-facing |
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