US2005433A - Alloy - Google Patents
Alloy Download PDFInfo
- Publication number
- US2005433A US2005433A US360A US36035A US2005433A US 2005433 A US2005433 A US 2005433A US 360 A US360 A US 360A US 36035 A US36035 A US 36035A US 2005433 A US2005433 A US 2005433A
- Authority
- US
- United States
- Prior art keywords
- percent
- nickel
- chromium
- alloy
- alloys
- 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
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
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
Definitions
- This invention relates to alloys and more particularly to alloys for electrical resistance units.
- an alloy having the property of resisting 5 oxidation at high temperatures is essential.
- alloys forming the subject matter of my invention are characterized by the ability to resist oxidation and by a prolonged life, exceeding that of other known alloys, when used under high i temperature conditions.
- nickel-chromium and nickel-chromiumiron alloys having the ability to resist oxidation at high temperatures are known, their period of usefulness in service is often not as long as desired. I have found that the addition of small quantities of calcium, zirconium and aluminum to such nickel-chromium alloys greatly increases their period of life when employed under conditions where they are subjected to high temperatures.
- the alloys forming the subject matter of the present application may also contain small quantities of either silicon or manganese or both of these elements.
- nickel-chromium alloys most generally used in the art consists of 80 parts of nickel and parts of i0 chromium and I find it advantageous to add the other metals mentioned above to nickelchromium alloys of substantially these proportions.
- the proportions of nickel and chromium in the alloy may be varied.
- the chromium content may be from 15 to 25 percent and the balance nickel.
- nickel-chromium-iron alloys is 60 percent nickel, 10 to 15 percent chromium and the balance iron and I find it advantageous to employ substantially these proportions of those ingredients, adding the calcium and zirconium. These proportions may also be varied, the nickel, however, forming the major part of the alloy, and the nickel-chromium content being such that the alloy will have the characteristics of a non-ferrous alloy. Thus, I may employ from 10 percent to 18 percent chromium, 17 to 30 percent iron and the balance 5o nickel.
- the quantities of the additional elements are subtracted from the nickel content, as for example, when calcium, zircomum and aluminum are added to an alloy con- Percent Calcium .01- .20 I Zirconium .01- .50 Aluminum .o1-1.o'0
- manganese or silicon are employed, they may be used within the following limits:
- the preferred proportions of the alloying agents are the following:
- Nickel-chromium and nickel-chromium-iron alloys containing the above ingredients within the proportions given have been found by tests to have a greatly increased period of life when exposed to high temperatures. For the purpose of 35 determining the life of such alloys at high temperatures I have tested them by the method of test outlined in Tentative accelerated life test for metallic materials for electrical heating of the American Society for Testing Materials described in vol. 29 of the Proceedings of the Thirty-Second Annual Meeting of the American Society for Testing Materials beginning on page 613. The method is substantially as folows:
- a sample of the wire to be tested free from kinks, approximately twelve inches long and of about .025" diameter, is mounted vertically on the test board, the upper end being held in position by means of a suitable binding post.
- a 10 gram weight is attached to the lower end of the specimen.
- a short piece of wire is attached to the 10 gram weight and projects downward into a cup of mercury where it may move freely up and down.
- a rheostat' and an interrupter are connected in series with the specimen to the' power supply.
- the test is run on constant temperature at a standard temperature chosen for the alloy under consideration for the first twenty-four hours. Thereafter it is run on constant voltage to the burnout.
- the life in hours up to a 10 percent increase in resistance is known as useful life'while the life to the burnout is known as total life.
- the power is on two minutes and off two minutes. This is accomplished by means of an interrupter.
- the alloys referred to herein small amounts of phosphorus and sulphur may be present as impurities.
- the nickel may also contain about 1 percent of cobalt.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
Description
Patented June 18, 1935 UNITED STATES- PATENT OFFICE RElSSUED Driver-Harris Company, Harrison, N. J., a corporation of New Jersey No Drawing. Application January 4, 1935,
JUL 2.? 1943 Serial No. 360
3 Claims.
This invention relates to alloys and more particularly to alloys for electrical resistance units. In the manufacture of electrical resistance units, an alloy having the property of resisting 5 oxidation at high temperatures is essential. The
alloys forming the subject matter of my invention are characterized by the ability to resist oxidation and by a prolonged life, exceeding that of other known alloys, when used under high i temperature conditions.
While nickel-chromium and nickel-chromiumiron alloys having the ability to resist oxidation at high temperatures are known, their period of usefulness in service is often not as long as desired. I have found that the addition of small quantities of calcium, zirconium and aluminum to such nickel-chromium alloys greatly increases their period of life when employed under conditions where they are subjected to high temperatures. The alloys forming the subject matter of the present application may also contain small quantities of either silicon or manganese or both of these elements.
In carrying out my invention I add small quantities of calcium, zirconium and aluminum,
with or without silicon or manganese to nickelchromium or nickel-chromium-iron alloys. The nickel-chromium alloy most generally used in the art consists of 80 parts of nickel and parts of i0 chromium and I find it advantageous to add the other metals mentioned above to nickelchromium alloys of substantially these proportions. The proportions of nickel and chromium in the alloy may be varied. Thus the chromium content may be from 15 to 25 percent and the balance nickel.
Likewise the most generally used proportions of nickel, chromium and iron in nickel-chromium-iron alloys is 60 percent nickel, 10 to 15 percent chromium and the balance iron and I find it advantageous to employ substantially these proportions of those ingredients, adding the calcium and zirconium. These proportions may also be varied, the nickel, however, forming the major part of the alloy, and the nickel-chromium content being such that the alloy will have the characteristics of a non-ferrous alloy. Thus, I may employ from 10 percent to 18 percent chromium, 17 to 30 percent iron and the balance 5o nickel.
In preparing alloys containing the additional elements enumerated, the quantities of the additional elements are subtracted from the nickel content, as for example, when calcium, zircomum and aluminum are added to an alloy con- Percent Calcium .01- .20 I Zirconium .01- .50 Aluminum .o1-1.o'0
If manganese or silicon are employed, they may be used within the following limits:
Percent Manganese 0.022.0 Silicon 0.20-2.0
The preferred proportions of the alloying agents are the following:
Percent 25 Calcium .03 Zirconium ,25 Aluminum ()7 38 Manganese 0.05-1.0 Silicon 0.40-1.0 30
Nickel-chromium and nickel-chromium-iron alloys containing the above ingredients within the proportions given have been found by tests to have a greatly increased period of life when exposed to high temperatures. For the purpose of 35 determining the life of such alloys at high temperatures I have tested them by the method of test outlined in Tentative accelerated life test for metallic materials for electrical heating of the American Society for Testing Materials described in vol. 29 of the Proceedings of the Thirty-Second Annual Meeting of the American Society for Testing Materials beginning on page 613. The method is substantially as folows:
A sample of the wire to be tested, free from kinks, approximately twelve inches long and of about .025" diameter, is mounted vertically on the test board, the upper end being held in position by means of a suitable binding post. A 10 gram weight is attached to the lower end of the specimen. A short piece of wire is attached to the 10 gram weight and projects downward into a cup of mercury where it may move freely up and down. A rheostat' and an interrupter are connected in series with the specimen to the' power supply. The test is run on constant temperature at a standard temperature chosen for the alloy under consideration for the first twenty-four hours. Thereafter it is run on constant voltage to the burnout. The life in hours up to a 10 percent increase in resistance is known as useful life'while the life to the burnout is known as total life. Throughout the test the power is on two minutes and off two minutes. This is accomplished by means of an interrupter.
In testing the alloys of my invention according to the above described method a reference sample composed of 80 percent nickel and 20 percent chromium and no alloy additions having an approximate life of 90 hours was used. This value is considered as 100 percent and the useful life of the samples tested is determined in corresponding percentage values. In the following table the results obtained with samples containing calcium, zirconium and aluminum are given:
Percent useful life No. Ca Zr Al .standard sample. when calcium, zirconium or aluminum alone was added to a nickel-chromium alloy of the same composition, the useful life was in all cases less than 200 percent. The use of calcium, zirconium and aluminumtherefore greatly increases the useful life of the alloy for electrical resistance purposes where the wire is exposed to a high temperature.
This application is a continuation in part of my copending application Serial No. 748,084, filed October 12, 1934, and the claims herein are directed to a nickel-chromium-iron alloy contain ing calcium, zirconium and aluminum.
In the alloys referred to herein, small amounts of phosphorus and sulphur may be present as impurities. The nickel may also contain about 1 percent of cobalt.
I claim:
1. A nickel-chromium-iron alloy containing to percent chromium, to percent iron,
.01 to .20 percent calcium, .01 to .50 percent zir-- conium and .01 to 1.0 percent aluminum, balance nickel.
2. A nickel-chromium-iron alloy containing 10 to 15 percent chromium, 25 to 30 percent iron, substantially .03 percent calcium, substantially .20 percent zirconium and from .07 to .38 percent aluminum, balance nickel.
3. A nickel-chromium-iron alloy containing 10 to 18 percent chromium, 17 to 30 percent iron, .01 to .20 percent calcium, .01 to .50 percent zirconium and .01 to .10 percent aluminum, balance nickel.
JAMES M. LOHR.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US360A US2005433A (en) | 1935-01-04 | 1935-01-04 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US360A US2005433A (en) | 1935-01-04 | 1935-01-04 | Alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US2005433A true US2005433A (en) | 1935-06-18 |
Family
ID=21691188
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US360A Expired - Lifetime US2005433A (en) | 1935-01-04 | 1935-01-04 | Alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US2005433A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2515184A (en) * | 1941-01-13 | 1950-07-18 | Int Nickel Co | Age hardenable nickel alloys |
US2542266A (en) * | 1946-10-07 | 1951-02-20 | Int Nickel Co | Heat and creep resisting nickel alloy castings |
US2687956A (en) * | 1951-12-28 | 1954-08-31 | Driver Harris Co | Alloy |
-
1935
- 1935-01-04 US US360A patent/US2005433A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2515184A (en) * | 1941-01-13 | 1950-07-18 | Int Nickel Co | Age hardenable nickel alloys |
US2542266A (en) * | 1946-10-07 | 1951-02-20 | Int Nickel Co | Heat and creep resisting nickel alloy castings |
US2687956A (en) * | 1951-12-28 | 1954-08-31 | Driver Harris Co | Alloy |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Jaumot Jr et al. | Order-disorder and cold-work phenomena in Cu Pd alloys | |
JPH06184679A (en) | Copper alloy for electrical parts | |
US2460590A (en) | Electric resistance element and method of heat-treatment | |
US2940845A (en) | Columbium-titanium base oxidationresistant alloys | |
US2005433A (en) | Alloy | |
US2051562A (en) | Alloys | |
US2047916A (en) | Alloy | |
US2019688A (en) | Alloy | |
US2005431A (en) | Alloy | |
US2019687A (en) | Alloy | |
US2005430A (en) | Alloy | |
US2696544A (en) | Electric resistance alloy | |
USRE22356E (en) | Allot | |
US2047918A (en) | Alloy | |
US2581420A (en) | Alloys | |
USRE24242E (en) | Alloys and electrical resistance | |
US2019686A (en) | Alloy | |
US2063513A (en) | Alloy | |
US2005432A (en) | Alloy | |
US2687954A (en) | Alloy | |
USRE22357E (en) | Alloy | |
US3416917A (en) | Superconductor quaternary alloys with high current capacities and high critical field values | |
US2047917A (en) | Alloy | |
US2187379A (en) | Alloy | |
US2533736A (en) | Electric resistance element and method of heat-treatment |