US2126749A - Alloy - Google Patents
Alloy Download PDFInfo
- Publication number
- US2126749A US2126749A US143469A US14346937A US2126749A US 2126749 A US2126749 A US 2126749A US 143469 A US143469 A US 143469A US 14346937 A US14346937 A US 14346937A US 2126749 A US2126749 A US 2126749A
- Authority
- US
- United States
- Prior art keywords
- alloy
- thermal treatment
- hardness
- boron
- cobalt
- 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
Links
- 229910045601 alloy Inorganic materials 0.000 title description 25
- 239000000956 alloy Substances 0.000 title description 25
- 238000007669 thermal treatment Methods 0.000 description 13
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 10
- 229910052796 boron Inorganic materials 0.000 description 10
- 229910017052 cobalt Inorganic materials 0.000 description 10
- 239000010941 cobalt Substances 0.000 description 10
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 8
- 239000011651 chromium Substances 0.000 description 8
- 238000005520 cutting process Methods 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 7
- 229910052799 carbon Inorganic materials 0.000 description 7
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 229910052726 zirconium Inorganic materials 0.000 description 6
- 230000000704 physical effect Effects 0.000 description 5
- 239000000470 constituent Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229910001315 Tool steel Inorganic materials 0.000 description 1
- 238000003483 aging Methods 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
Classifications
-
- 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
- the present invention relates to a new and useful alloy containing boron, zirconium, chromium and cobalt, which is characterized by being responsive to thermal treatment for the 5' improvement of physical properties.
- An object of the present invention is to provide an alloy especially adapted for use as metal cutting tools, the cutting efficiency of which is superior to that of heretofore known high speed Y tools and other alloys.
- a further object is to provide analloy which is free from, or substanlo tially free from, carbon, and which is readily amenable to thermal treatment by means of which the hardness, cutting efliciency 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 approximatemaximum values of hardness, resistance to impact 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,
- cast bodies of this alloy may have a hardness of from 52 to 58 on the Rockwell C scale and by subjecting the material to suitable thermal treatment, such as heating to a tem- 1o perature higher than approximately 1000" C., followed by rapid quenching, the hardness may be lowered to an approximate range of from'36' to .44 Rockwell C.
- suitable thermal treatment such as heating to a tem- 1o perature higher than approximately 1000" C., followed by rapid quenching, the hardness may be lowered to an approximate range of from'36' to .44 Rockwell C.
- the alloy can subsequently be subjected to a second thermal treatment, such 15 as heating to a temperature lower than 1000 C. for a period of one hour or more, followed by cooling at a normal rate, by which the hardness can be increased to from approximately 58 to 66 Rockwell C. valuable for many industrial uses.
- compositions within the 40 scope of the present invention which I have found well adapted for numerous industrial applications are of the following: boron 1.75%, zlrconium 4.75%, chromium.7.50 cobalt substantially the balance; boron 1.95%, zirconium 45 0.75%, chromium 15%, cobalt substantially the balance;. boron 2.30%, zirconium 2%, chromium 12%, cobalt substantially the balance.
- An objective of the present invention is to provide an alloy having high hardness, advanta- 60 geous metal cutting properties, etc., which is free from, or substantially free from, carbon, and thus eliminate all of the serious disadvantages associated with carbon containing alloys or compositions intended for metal cutting tools, etc.
- the alloy is 20 though 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 0! about 0.15%, as I have found that the presence of higher percentages of this element not only embrittle the alloy, but also inhibit or retard the desired or necessary reactions during thermal treatment. The presence of appreciable amounts of carbon decreases the red hardness of the alloy; 1-. e., hardness at temperatures oi approximately 550 C. and higher.
- the preferred structure of a body of the present alloy comprises at least two-principal constituents; one, a relatively hard lntermetallicj compound of boron with one or more of the other essential components; and,
- the ratio of the constituents as well as the ratio oi particle size in any particular body or the alloy may be accurately controlled and fixed over a wide range I by means of thermal treatment or mechanical working and thermal treatment.
- the alloy of the present invention comprises boron, zirconium,
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
Description
Patented Aug. 16, 1938 PATENT OFFICE ALLOY Anthony de Golyer, New York, N. Y.
No Drawing. Application May 19, 1937, Serial No. 143,469 v 1 Claim.
The present invention relates to a new and useful alloy containing boron, zirconium, chromium and cobalt, which is characterized by being responsive to thermal treatment for the 5' improvement of physical properties. This application is a continuation in part of my copending application Serial No. 721,771 filed April 21, 1934.
An object of the present invention is to provide an alloy especially adapted for use as metal cutting tools, the cutting efficiency of which is superior to that of heretofore known high speed Y tools and other alloys. A further object is to provide analloy which is free from, or substanlo tially free from, carbon, and which is readily amenable to thermal treatment by means of which the hardness, cutting efliciency 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, zirconium, chromium and cobalt within the range of boron 0.50% to 4%, zirconium 0.25% to 5%, chromium 1% to 17% 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.
Alloys of this invention may be used in the cast condition for certain purposes, but approximatemaximum values of hardness, resistance to impact 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,
40 and the like for the-cutting .or mechanical working of metals, as well as for many other industrial uses.
Numerous metallic compositions have heretofore been proposed as improvements on the known types of high speed tool steel, but all of such proposed compositions have disadvantages which render them unsuitable for general application as metal cutting or forming tools. One
disadvantage of such compositions is that nonev treatment for the development of precipitation hardening, often referred to as age hardening.
I prefer to subject the alloy to thermal treatment before using it for metal cutting tools,'dies, etc. 7 I have found that both the cast and forged mate- 5 rials are responsive to thermal treatment. As an illustration, cast bodies of this alloy may have a hardness of from 52 to 58 on the Rockwell C scale and by subjecting the material to suitable thermal treatment, such as heating to a tem- 1o perature higher than approximately 1000" C., followed by rapid quenching, the hardness may be lowered to an approximate range of from'36' to .44 Rockwell C. The alloy can subsequently be subjected to a second thermal treatment, such 15 as heating to a temperature lower than 1000 C. for a period of one hour or more, followed by cooling at a normal rate, by which the hardness can be increased to from approximately 58 to 66 Rockwell C. valuable for many industrial uses.
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 and 2a The more important distinctive advantages 5 are apparently due to the presence. of appreciable amounts of boron in the composition, in conjunction with the other components, within the percentages specified herein.
Specific examples of composition within the 40 scope of the present invention which I have found well adapted for numerous industrial applications are of the following: boron 1.75%, zlrconium 4.75%, chromium.7.50 cobalt substantially the balance; boron 1.95%, zirconium 45 0.75%, chromium 15%, cobalt substantially the balance;. boron 2.30%, zirconium 2%, chromium 12%, cobalt substantially the balance.
An objective of the present invention is to provide an alloy having high hardness, advanta- 60 geous metal cutting properties, etc., which is free from, or substantially free from, carbon, and thus eliminate all of the serious disadvantages associated with carbon containing alloys or compositions intended for metal cutting tools, etc. Al-
'In the latter condition the alloy is 20 though 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 0! about 0.15%, as I have found that the presence of higher percentages of this element not only embrittle the alloy, but also inhibit or retard the desired or necessary reactions during thermal treatment. The presence of appreciable amounts of carbon decreases the red hardness of the alloy; 1-. e., hardness at temperatures oi approximately 550 C. and higher.
My investigations indicate that the preferred structure of a body of the present alloy, particularly after thermal treatment, comprises at least two-principal constituents; one, a relatively hard lntermetallicj compound of boron with one or more of the other essential components; and,
two, a solid solution of two or more or the essentlal components which has a lower degree of hardness and functions as a matrix. The ratio of the constituents as well as the ratio oi particle size in any particular body or the alloy may be accurately controlled and fixed over a wide range I by means of thermal treatment or mechanical working and thermal treatment.
By reason of the combined advantageous physical properties and-characteristics'possessed by the alloy 01' the present invention, tools and other articles composed oi! this alloy may be operated eiliciently and economically under conditions which are impossible or uneconomical with tools, etc., composed of heretofore ,khow'n alloys or metallic compositions.
By the term the balance substantially cobalt" or the "balance cobalt" in the foregoing and in the following claim, I intend that the alloy of the present invention comprises boron, zirconium,
and chromium within the percentaae limits specified, with the remainder cobalt, except for inei'iectual amounts of impurities which may be present incidental to manufacture.
I claim:
' A precipitation hardened. alloy containing boron 0.50% .to 4%, zirconium-0.25% to--5%, chromium 1% to 17%, the balance cobalt.
ANTHONY G. or GOLYER.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US143469A US2126749A (en) | 1937-05-19 | 1937-05-19 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US143469A US2126749A (en) | 1937-05-19 | 1937-05-19 | Alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2126749A true US2126749A (en) | 1938-08-16 |
Family
ID=22504223
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US143469A Expired - Lifetime US2126749A (en) | 1937-05-19 | 1937-05-19 | Alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US2126749A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2983602A (en) * | 1957-09-24 | 1961-05-09 | Armour Res Found | Cobalt alloys |
US3362816A (en) * | 1963-06-22 | 1968-01-09 | Fed Republic Of Germany | Cobalt alloy |
-
1937
- 1937-05-19 US US143469A patent/US2126749A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2983602A (en) * | 1957-09-24 | 1961-05-09 | Armour Res Found | Cobalt alloys |
US3362816A (en) * | 1963-06-22 | 1968-01-09 | Fed Republic Of Germany | Cobalt alloy |
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