US2097178A - Alloy - Google Patents
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- Publication number
- US2097178A US2097178A US96997A US9699736A US2097178A US 2097178 A US2097178 A US 2097178A US 96997 A US96997 A US 96997A US 9699736 A US9699736 A US 9699736A US 2097178 A US2097178 A US 2097178A
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- United States
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- alloy
- hardness
- thermal treatment
- cutting
- nickel
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Classifications
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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
Description
Patented Oct. 26,1937
UNITED STATES PATENT OFFICE No Drawing. Application August 20, 1936,
Serial No. 96,997 i 3 Claims. (01. 148-321) The present invention relates to a new and useful alloy and relates particularly to an alloy containingboron, tungsten and nickel, which is characterized by being responsive to thermal 5 treatment for the improvement of physical properties. M An object of the present invention is to provide an alloy especially adapted for use as metal cutting tools, the cutting efliciency of which is 10 superior to that of present known high speed steels 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, tensile strength, cutting efliciency and other physical properties and characteristics may be accurately controlled over a comparatively wide range.
I have found through experiment that by al- 2 loying or otherwise intimately combining boron, tungsten and nickel within the range of boron 0.50% to 2.75%, tungsten 5% to and nickel .substantially the balance, that I obtain metallic compositions which possess in combination me.-
5 terially improved physicalproperties compared to those of heretofore known alloysor compositions intended for the cutting orworking of metals. p I
'Alloys of this invention may be used in the 3 cast condition but approximate. maximum values of hardness, resistance to impact and, certain other important physical properties. can be developed only through thermal treatment, or
- through mechanical working and subsequent thermal treatment. Bodies of the alloys which have been subjected to such treatment are particularly valuable for use as tools, dies and the likefor the cutting or mechanical working of metals.-
Numerous-metallic compositions have heretofore been proposed as improvement on the generally known 18-4-1 type of tungsten-chromium-vanadium high speed tool steel, and while many of such compositions possess: greater hardness than such steel, all of them have disadvantages which render them unsuitable for general application as metal cutting or forming tools.
' 1 Compositions containing principally carbides of tungsten, molybdenum or tantalum .bonded with a relatively soft matrix metal have a high degree of hardness, but are extremely brittle. Cast compodtions of the types heretofore proposed require the presence of at least 1.50% carbon to qualify as metal cutting tools and, as is'well. known, such alloys are-not only brittle, but, are so sensitive to various operatingconditions as to greatly restrict the scope of usefulness. One of the greatest disadvantages of such heretofore proposed compositions is that none of them are responsive to thermal treatment for regulation of physical properties, and 5 consequently physical properties-'and character- 'istics are governed entirely by the chemical composition of the sintered or cast material.
My alloy may be usedin the as-cast condition, or it may be forged or otherwise mechanically l0 worked. I have found that both the cast and forged material are amenable to thermal treatment. For example, cast bodies of this alloy may have a hardness of from 50 to on the Rockwell C. scale and .by subjecting the .mate- 15 rial to suitable thermal treatment, such as quenching from a temperature higher than approximately 1000 C., the hardness may be. owered to an approximate range of from 40 to 4'7 Rockwell C. In this condition the bodies may 20 be ground, shaped or formed, asdesired. The alloy may subsequently be submitted to a second thermal treatment, such as heating to a temperatur of less than 1000 C. for a period of one hour or more, by which the hardness may 25 be increased to from approximately 60 to Rockwell C. In the latter condition the alloy' is especially valuable for the cutting or mechanical working of a large number of metals and alloys, as well as numerous non-metallic materials. An 30 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 elevated temperatures, e. g. such as are generated in the tip of a tool cutting 5 metal at high speed. Although the alloy has a high degree of hardness and resistance abrasion by hot metal chips, especially after thermal treatment, it is remarkably resistant to failure from sudden or repeated shock. Therefore, 40
' tools 'made of the present alloy retain an eflicient cutting edge for longer-periods than other tools.
The more important distinctive and valuable advantages are, apparently, due to the presence of appreciable amounts of boronin the compo-' 5 sition, in conjunction with the other component elements within the percentages specified herein.
I have found that molybdenum may be used to supplant all or a portion of the tungstenoi' the 50 present alloy. Likewise, uranium may be vused in place of either timgsten or molybdenum.
Specific examples of compositions within the scope of the present invention which I have found -well adapted for metal cutting tools, dies 55 and. the like are the following: boron 1.20%,
tungsten 14%, nickel balance; boron 2.10%, tung-- sten 19.50%, nickel balance; boron 1.65%, molybdenum 13%, nickel balance; boron 1.70%, tungsten 5%, molybdenum nickel balance.
An objective of the present invention is to provide alloys having high hardness, high resistance to shock and impact, advantageous metal cutting properties, etc., which are free from or substantially free from carbon, and thus eliminate all of the serious disadvantages associated with carbon containing non-ferrous alloys or compositions intended for metal cutting tools. Although I prefer to have the alloys of this'invention entirely free from carbon, in many instances I have found carbon present in the nature of an impurity incidental to manufacture. It is important to restrict the amount of carbon so present to a maximum of about 0.15%, as I have found that the presence of higher percentages of this element make the alloy extremely brittle and subject to failure during cutting operations, and also inhibits the desired and necessary reactions during thermal treatment. Furthermore, the presence of appreciable amounts of carbon decreases the red hardness of the alloy, i. e. hardness at temperatures of approximately 550 C. and higher.
By reason of the fact that the elements forming the essential components of the alloy of the present invention invariably are contaminated with other elements when produced in commercial quantities, the alloys of my invention usually contain insignificant amounts of one or more elements in the nature of impurities incidental to manufacture. The amount of such impurities should be restricted to percentages which are not efiective on the physical properties or characteristics of the alloy, nor on the physical reactions during thermal treatment. I have found that the amount of any one of such incidental impurities should be restricted to percentages not exceeding 1%, and in many instances to materially lower percentages. The presence of larger amounts of such impurities, particularly silicon and aluminum, materially decreases the" resistance of the alloy to failure under shock and impact during cutting operations, and, further, inhibits the desired physical reactions during thermal treatsecond. a solid solution of two or more of the essential components which has a lower degree of hardness and functions as a matrix. In some instances the structure will contain a third constituent in the nature of an eutectoid. The ratio of the constituents and the ratio of particle size in any particular body of the alloy may be accurately controlled and fixed over a wide range by means of thermal treatment, or mechanical working and subsequent thermal treatment.
By reason of the combined advantageous physicalproperties possessed by the alloy of the present invention, tools and other articles composed of this alloy may be operated efilciently and economically under conditions which are impossible or uneconomical with tools or articles composed of heretofore known alloys or metallic compositions. I
I By the term "the balance substantially nicke in the foregoing andin the following claims. I intend that the alloy of the present invention comprises boron and metal of the group tungsten, molybdenum and uranium within the percentage limits specified, with the remainder nickel except for ineffective amounts of impurities which may be present incidental to manufacture.
I claim:
1. An age hardened alloy containing boron 0.50% to 2.75%, metal from the group tungsten, molybdenum and uranium 5% to 25%, the balance substantially nickel.
2. An age hardened alloy containing boron 0.50% to 2.75%, tungsten 5% to 25%, the balance substantially nickel.
3. An age hardened alloy containing boron 0.50% to 2.75%, molybdenum 5% to 25%, the
balance substantially nickel.
ANTHONY G. DE GOLYER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US96997A US2097178A (en) | 1936-08-20 | 1936-08-20 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US96997A US2097178A (en) | 1936-08-20 | 1936-08-20 | Alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2097178A true US2097178A (en) | 1937-10-26 |
Family
ID=22260157
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US96997A Expired - Lifetime US2097178A (en) | 1936-08-20 | 1936-08-20 | Alloy |
Country Status (1)
Country | Link |
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US (1) | US2097178A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2442163A (en) * | 1943-08-31 | 1948-05-25 | Eitel Mccullough Inc | Cathode structure |
US3057422A (en) * | 1962-10-09 | Toll highway recorder system | ||
US3620718A (en) * | 1970-08-28 | 1971-11-16 | Nasa | Nickel base alloy |
-
1936
- 1936-08-20 US US96997A patent/US2097178A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3057422A (en) * | 1962-10-09 | Toll highway recorder system | ||
US2442163A (en) * | 1943-08-31 | 1948-05-25 | Eitel Mccullough Inc | Cathode structure |
US3620718A (en) * | 1970-08-28 | 1971-11-16 | Nasa | Nickel base alloy |
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