US2235232A - Metal alloy - Google Patents
Metal alloy Download PDFInfo
- Publication number
- US2235232A US2235232A US247949A US24794938A US2235232A US 2235232 A US2235232 A US 2235232A US 247949 A US247949 A US 247949A US 24794938 A US24794938 A US 24794938A US 2235232 A US2235232 A US 2235232A
- Authority
- US
- United States
- Prior art keywords
- alloy
- tungsten
- zirconium
- cobalt
- cutting
- 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
- 229910001092 metal group alloy Inorganic materials 0.000 title description 3
- 229910045601 alloy Inorganic materials 0.000 description 22
- 239000000956 alloy Substances 0.000 description 22
- 238000005520 cutting process Methods 0.000 description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 9
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 9
- 239000010941 cobalt Substances 0.000 description 9
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 9
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 9
- 229910052721 tungsten Inorganic materials 0.000 description 9
- 239000010937 tungsten Substances 0.000 description 9
- 229910052726 zirconium Inorganic materials 0.000 description 9
- 239000011651 chromium Substances 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 7
- 229910017052 cobalt Inorganic materials 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 238000005242 forging Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 150000002739 metals Chemical class 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 229910000531 Co alloy Inorganic materials 0.000 description 2
- 229910001080 W alloy Inorganic materials 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- 229910000677 High-carbon steel Inorganic materials 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229910001928 zirconium oxide Inorganic materials 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
- This invention relates to ametal alloy particularly designed for use in the manufacture of articles such as tools and cutting implements wherein are'required the qualities of hardness, toughness and elasticity, tOEether with the capacity of taking and retaining a sharp cutting edge.
- the alloy of my invention has greatly increased toughness and resistance to-shock over 1 the average chrome, cobalt and tungsten alloys in general use as cutting tools.
- I preferably use proficient, capable of maintaining a temperature of 3500 degrees Fahrenheit, and my method differs mainly from the method in common use, inthat by the use of zirconium I am able to obtain a very fine grained structure.
- chromium, cobalt and tungsten are placed in a. crucible and melted at a high heat between 3000 and 3500 degrees Fahrenheit, preferably about 3400 degrees Fahrenheit.
- the chromium and cobalt with a melting point of less than 3000 degrees Fahrenheit will have melted but the tungsten with a melting point of approximately 6150 degrees Fahrenheit will not have melted, but will have been dissolved and 55 taken into solution by the matrix of the other a high frequency electric transformer and crutwo metals, namely chromium and cobalt.
- approximately 3400 degrees Fahrenheit has been reached I introduce the zirconium in a closed container, so that it may be immediately immersed in the 5 molten bath without eXDOsure to the atmosphere.
- the molten bath is then held in this temperature-for a period of from twenty to thirty minutes, or longer, before pouring into molds and casting into the shapes desired.
- zirconium By the addition of zirconium the oxides'of the metal formed in melting the alloy are reduced and zirconium oxide is formed. This is a very minute particle. These oxides are scattered throughout the alloy. 0n cooling, when the grains start forming, a separate grain starts with each one of these particles as a nuclei.
- the size of the grain in the alloy can be controlled, and what is more important, the amount of tungsten that is thrown out will be thoroughly distributed throughout the mass, and will not exist in large concen- 40 trated plates as it is when no obstructing and oxidizing agent is used.
- I have produced an alloy consisting of of chromium, 47% of cobalt, 15% of tungsten, with 3% of zirconium added to the bath at the proper time and under the proper conditions as hereinbefore described, that not only retains its hardness and cutting edge at all cutting temperatures, but also has the added quality of cutting at exceptionally high speed, and being able to resist sudden shock without shattering.
- Lathe tools made of my alloy when used to turn down high carbon chrome-nickel-molybdenum steel forgings have enabled the lathe operator to increase the R. P. M. of his lathe fully faster than that permissible when using other tools, and at the same time taking deeper cuts and feeds.
- a metal alloy consisting of zirconium, 1 to 10%, and the balance to make of chromium, cobalt and tungsten in the proportions based on the total mass, chromium 25 to 40%, 20 cobalt 40 to 60%, tungsten 10 to 20%.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
Description
Patented Mar. 18, 1941 2,235,232 METAL ALLOY Lewis A. McElroy, Erie, Pa., a'ssignor to 'The Macollte Company, Millcreek Township, Erie County, Pa., a corporation of Pennsylvania No Drawing. Application December 2'7, 1938, Serial No. 247,949
1 Claim.
This invention relates to ametal alloy particularly designed for use in the manufacture of articles such as tools and cutting implements wherein are'required the qualities of hardness, toughness and elasticity, tOEether with the capacity of taking and retaining a sharp cutting edge.
The alloy of my invention has greatly increased toughness and resistance to-shock over 1 the average chrome, cobalt and tungsten alloys in general use as cutting tools.
An alloy of tungsten, chromium and cobalt has for years been used as a cutting alloy. This shows valuable qualities of red shortness or the" i ability to retain its hardness even at red heat. It is also very hard, but quite brittle and will not stand shock. This limits somewhat its use as a metal cutting alloy as the tool will shatter when it receives a sudden shock as it often does 1 when turning down rough out-of-round forgings where the tool contacts the metal only in spots as the forging revolves in the lathe.
To counteract this brittleness molybdenum is sometimes added to the alloy. This metal being softer and more ductile, has the eifect of toughening the alloy, but at the same time, due to its qualities it reduces thehardness of the alloy with the resultant effect that its cutting qualities are impmred.
By a new method I am able to counteract this brittleness and at the same time retain the hardness and other valuable qualities of the original alloy. I accomplish this by the addition of .varying percentages of zirconium having deoxidizing properties, and especially valuable in enabling me to obtain the desired properties in the alloy of my invention.
In carrying out my invention I preferably use cible, capable of maintaining a temperature of 3500 degrees Fahrenheit, and my method differs mainly from the method in common use, inthat by the use of zirconium I am able to obtain a very fine grained structure. v
To accomplish this, certain percentages of chromium, cobalt and tungsten are placed in a. crucible and melted at a high heat between 3000 and 3500 degrees Fahrenheit, preferably about 3400 degrees Fahrenheit. The chromium and cobalt with a melting point of less than 3000 degrees Fahrenheit will have melted but the tungsten with a melting point of approximately 6150 degrees Fahrenheit will not have melted, but will have been dissolved and 55 taken into solution by the matrix of the other a high frequency electric transformer and crutwo metals, namely chromium and cobalt. When the desired temperature, approximately 3400 degrees Fahrenheit has been reached I introduce the zirconium in a closed container, so that it may be immediately immersed in the 5 molten bath without eXDOsure to the atmosphere.
The molten bath is then held in this temperature-for a period of from twenty to thirty minutes, or longer, before pouring into molds and casting into the shapes desired.
Without the obstructing and deoxidizing agent present, when the alloy cools, the grains grow to large size and the tungsten is thrown out of solution on the grain borders. Because of this large grain size, the amount of tungsten collecting between the grains is large and the adhesion of the grains to each other is weakened, causing brittleness of the alloy.
By the addition of zirconium the oxides'of the metal formed in melting the alloy are reduced and zirconium oxide is formed. This is a very minute particle. These oxides are scattered throughout the alloy. 0n cooling, when the grains start forming, a separate grain starts with each one of these particles as a nuclei.
Consequently with so many grains starting to form at once their size is quite small when they come in contact with each other and their growth is stopped. Whereas, without the presence of an. obstructing and deoxldizing agent,
.there are only a few nuclei for the grains tov start on, and only a small number of grains forming. Therefore, they grow to large size before coming in contact with each other and. their F growth is stopped. Thus it is that by the amount of zirconium used the size of the grain in the alloy can be controlled, and what is more important, the amount of tungsten that is thrown out will be thoroughly distributed throughout the mass, and will not exist in large concen- 40 trated plates as it is when no obstructing and oxidizing agent is used.
Thus, by changing my method of producing the alloy from the simple one of just remelting 1 the metals desired in the alloy, to that whereby these metals are subject to the obstructing and deoxidizing effects of zirconium, after the melt.- i ing has taken place, melted at a temperature of over 3000 degrees Fahrenheit, holding it at that temperature for a period of from twenty to 9 thirty minutes, orlonger, I am able to control the structure and grain refinement of the mass so that the resultant cutting qualities of the alloy are far superior to that obtained in the past.
As an example: I have produced an alloy consisting of of chromium, 47% of cobalt, 15% of tungsten, with 3% of zirconium added to the bath at the proper time and under the proper conditions as hereinbefore described, that not only retains its hardness and cutting edge at all cutting temperatures, but also has the added quality of cutting at exceptionally high speed, and being able to resist sudden shock without shattering.
Lathe tools made of my alloy, when used to turn down high carbon chrome-nickel-molybdenum steel forgings have enabled the lathe operator to increase the R. P. M. of his lathe fully faster than that permissible when using other tools, and at the same time taking deeper cuts and feeds.
As a specificv example: A certain machining turn down a similar forging, the tool speed was increased from 30 feet per minute to feet per minute with the result that the operation was completed in nine hours.
Depending upon the particular purpose for 5 which the alloy is to be used, I vary the percentages of the ingredients of my alloy.
I have secured good results using 32% of chromium, 50% of cobalt, 15% of tungsten with 3% of zirconium added as hereinbefore described. 10
On a high carbon steel shaft 12 inches in diameter, turned down with a tool made of my alloy, the tool traveled 30 inches on the shaft in live minutes, or at the rate of 226 feet per minute.
What I claim as new is:
A metal alloy consisting of zirconium, 1 to 10%, and the balance to make of chromium, cobalt and tungsten in the proportions based on the total mass, chromium 25 to 40%, 20 cobalt 40 to 60%, tungsten 10 to 20%.
. t L. A. McELROY.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US247949A US2235232A (en) | 1938-12-27 | 1938-12-27 | Metal alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US247949A US2235232A (en) | 1938-12-27 | 1938-12-27 | Metal alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2235232A true US2235232A (en) | 1941-03-18 |
Family
ID=22937016
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US247949A Expired - Lifetime US2235232A (en) | 1938-12-27 | 1938-12-27 | Metal alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2235232A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2801165A (en) * | 1955-09-30 | 1957-07-30 | Coast Metals Inc | Cobalt-base alloys |
-
1938
- 1938-12-27 US US247949A patent/US2235232A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2801165A (en) * | 1955-09-30 | 1957-07-30 | Coast Metals Inc | Cobalt-base alloys |
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