US2090044A - Alloys - Google Patents
Alloys Download PDFInfo
- Publication number
- US2090044A US2090044A US29674A US2967435A US2090044A US 2090044 A US2090044 A US 2090044A US 29674 A US29674 A US 29674A US 2967435 A US2967435 A US 2967435A US 2090044 A US2090044 A US 2090044A
- Authority
- US
- United States
- Prior art keywords
- alloys
- alloy
- beryllium
- titanium
- 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 20
- 239000000956 alloy Substances 0.000 title description 20
- 229910052790 beryllium Inorganic materials 0.000 description 8
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 6
- 229910052719 titanium Inorganic materials 0.000 description 6
- 239000010936 titanium Substances 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 5
- 229910052799 carbon Inorganic materials 0.000 description 5
- 229910052750 molybdenum Inorganic materials 0.000 description 5
- 239000011733 molybdenum Substances 0.000 description 5
- 235000016768 molybdenum Nutrition 0.000 description 5
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- 229910052804 chromium Inorganic materials 0.000 description 4
- 239000011651 chromium Substances 0.000 description 4
- 229910017052 cobalt Inorganic materials 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 4
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 3
- 239000004615 ingredient Substances 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 229910000684 Cobalt-chrome Inorganic materials 0.000 description 2
- 229910001347 Stellite Inorganic materials 0.000 description 2
- AHICWQREWHDHHF-UHFFFAOYSA-N chromium;cobalt;iron;manganese;methane;molybdenum;nickel;silicon;tungsten Chemical compound C.[Si].[Cr].[Mn].[Fe].[Co].[Ni].[Mo].[W] AHICWQREWHDHHF-UHFFFAOYSA-N 0.000 description 2
- 239000010952 cobalt-chrome Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052715 tantalum Inorganic materials 0.000 description 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 101100008049 Caenorhabditis elegans cut-5 gene Proteins 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- WAIPAZQMEIHHTJ-UHFFFAOYSA-N [Cr].[Co] Chemical compound [Cr].[Co] WAIPAZQMEIHHTJ-UHFFFAOYSA-N 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000010959 steel 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
- C22C30/00—Alloys containing less than 50% by weight of each constituent
-
- 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 prior stellite type of alloy (cobalt-chromi- 20 um basis) also incorporated one or more of additional ingredients such, for example, as tungsten and molybdenum, and sometimes nickel.
- the present invention is concerned with alloys of the cobalt chromium type, which alloysare capable of heat treatment and have material- 30 1y improved properties, such as cutting emciency. strength and toughness, although they are not brittle.
- metals such as beryllium 35 or titanium or both. I prefer also to melt and pour my improved alloys in vacuo.
- the present invention contemplates an alloy containing from about 30% to about 60.0% cobalt and from about 20% to 10 about 40% chromium. While some improvement may be effected by the beryllium or titanium even when substantial amounts of carbon are present, I prefer to reduce or even eliminate the carbon, and I have further found that the properties may very readily be appreciably improved by heat treatment. ably quenched in oil or some equivalent quenching medium, from a high temperature, and then' For example, the alloys are desir-' subsequently annealed at a temperature of from about 500 to 900 C.
- the brittleness of stellites and similar cutting alloys heretofore employed is at least in large part produced by the content of carbon, and the invention contemplates the ad- 5,
- the total amount of titanium or beryllium or both should be in the 10' neighborhood of from about .3% to about 4%]
- chromium and beryllium or titanium I also contemplate the use of tungsten, molybdenum or tantalum either individually or in combinations.
- the total content l5 of this constituent should be less than 25% of the,alloy, and it is preferable where only molybdenum and/or tantalum are employed, to keep the totalbelow about 15%.
- Nickel may also be added to the alloy, although preferably not in excess of about 10%.
- Thepreferred range of beryllium or titanium (or both combined) is from about 1% to about 2%.
- a cutting tool composed of an alloy consisting 40 of from about .3% to about 4% beryllium, molyb denum up to about 15%, and the balance a basic ingredient composed of cobalt and chromium, the former of which comprises from about 30% to about 60% of the entire alloy and the latter of which comprises from about 20% to about 40% of the entire alloy.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Materials For Medical Uses (AREA)
Description
Patented Aug. 17, 1937 UNITED STATES PATENT OFFICE 2,090,044 annoys Werner Hessenbruch, Hanau-on-the-Maln, Germany, assignor to Heraeus-Vacuumschmelze, A. G., Hanau-on-the-Main, Germany No Drawing. Application July 3, 1935, Serial No. 29,674. In Germany July 14, 1934 1 Claim. (01. 75-171) Recently there have been some sintered alloysv introduced for machining hard materials and ordinary steels. While these alloys represent an improvement over some of the former materials employed in high-speed tools, as well as an improvement over heretofore known alloys similar to the so-called stellite (built up on a cobaltchromium basis), still these prior sintered alloys have been subject to a number of disadvantages. For example, the prior alloys have been very brittle. Other types of alloys employed for cut- 5 ting tools heretofore, for example, stellites, have been open to the objection that their hardness,
especially at higher temperatures, was not sumcient.
The prior stellite type of alloy (cobalt-chromi- 20 um basis) also incorporated one or more of additional ingredients such, for example, as tungsten and molybdenum, and sometimes nickel.
These prior alloys, furthermore, had an average content of carbon from about 2% to about 4%,
5 and they were ordinarily cast and were not capable of being improved by heat treatment.
The present invention is concerned with alloys of the cobalt chromium type, which alloysare capable of heat treatment and have material- 30 1y improved properties, such as cutting emciency. strength and toughness, although they are not brittle.
An important factor in producing the improvement is the addition of metals such as beryllium 35 or titanium or both. I prefer also to melt and pour my improved alloys in vacuo.
More specifically, the present invention contemplates an alloy containing from about 30% to about 60.0% cobalt and from about 20% to 10 about 40% chromium. While some improvement may be effected by the beryllium or titanium even when substantial amounts of carbon are present, I prefer to reduce or even eliminate the carbon, and I have further found that the properties may very readily be appreciably improved by heat treatment. ably quenched in oil or some equivalent quenching medium, from a high temperature, and then' For example, the alloys are desir-' subsequently annealed at a temperature of from about 500 to 900 C. The brittleness of stellites and similar cutting alloys heretofore employed is at least in large part produced by the content of carbon, and the invention contemplates the ad- 5,
dition of titanium or beryllium and elimination of or at least reduction in the carbon content,
' in instances where it is desired to materially diminish the brittleness. The total amount of titanium or beryllium or both should be in the 10' neighborhood of from about .3% to about 4%] In addition to the cobalt, chromium and beryllium or titanium, I also contemplate the use of tungsten, molybdenum or tantalum either individually or in combinations. The total content l5 of this constituent should be less than 25% of the,alloy, and it is preferable where only molybdenum and/or tantalum are employed, to keep the totalbelow about 15%.
Nickel may also be added to the alloy, although preferably not in excess of about 10%.' v
Thepreferred range of beryllium or titanium (or both combined) is from about 1% to about 2%.
As a specific example of an alloy of the type contemplated by this invention, which alloy is tough, hard, and strong, even when heated to high temperature, I mention one containing the following ingredients in about the proportions indicated:
' Per cent Cobalt 40 Chromium 25 Tungsten- 18 Nickel 10 Molybdenum 5 I Beryllium from 1% to 2 I claim:-
A cutting tool composed of an alloy consisting 40 of from about .3% to about 4% beryllium, molyb denum up to about 15%, and the balance a basic ingredient composed of cobalt and chromium, the former of which comprises from about 30% to about 60% of the entire alloy and the latter of which comprises from about 20% to about 40% of the entire alloy.
WERNER HESSENBRUCH.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2090044X | 1934-07-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2090044A true US2090044A (en) | 1937-08-17 |
Family
ID=7984429
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US29674A Expired - Lifetime US2090044A (en) | 1934-07-14 | 1935-07-03 | Alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2090044A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2469718A (en) * | 1945-01-13 | 1949-05-10 | Vanadium Corp Of America | Alloys |
| US2805945A (en) * | 1949-01-28 | 1957-09-10 | Straumann Reinhard | Mainspring composed of nickel base alloys |
| US2841511A (en) * | 1952-09-16 | 1958-07-01 | Onera (Off Nat Aerospatiale) | Metal alloy and its manufacturing process |
| US3524775A (en) * | 1967-12-06 | 1970-08-18 | Cabot Corp | High strength cobalt-beryllium alloy and method of producing the same |
-
1935
- 1935-07-03 US US29674A patent/US2090044A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2469718A (en) * | 1945-01-13 | 1949-05-10 | Vanadium Corp Of America | Alloys |
| US2805945A (en) * | 1949-01-28 | 1957-09-10 | Straumann Reinhard | Mainspring composed of nickel base alloys |
| US2841511A (en) * | 1952-09-16 | 1958-07-01 | Onera (Off Nat Aerospatiale) | Metal alloy and its manufacturing process |
| US3524775A (en) * | 1967-12-06 | 1970-08-18 | Cabot Corp | High strength cobalt-beryllium alloy and method of producing the same |
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