US2005431A - Alloy - Google Patents
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- Publication number
- US2005431A US2005431A US748084A US74808434A US2005431A US 2005431 A US2005431 A US 2005431A US 748084 A US748084 A US 748084A US 74808434 A US74808434 A US 74808434A US 2005431 A US2005431 A US 2005431A
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- US
- United States
- Prior art keywords
- nickel
- chromium
- percent
- alloys
- alloy
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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
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/058—Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
Definitions
- This invention relates to alloys and more par ticularly to alloys for electrical resistance units.
- 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 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 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 20 parts of 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. and iron in nickel-chromiumiron alloys is 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.
- the quantities of the additional elements are subtracted from the nickel content; as for example, when calcium, zirconium and aluminum are added to an alloy containing 15 to 25 percent chromium and the balance nickel, the final alloy .will contain 15 to 25 percent chromium, calcium, zirconium and aluminum in the percentages herein stated and the balance nickel.”
- the proportions of calcium, zirconium and aluminum may vary within certain limits. I have found that best results are obtained when 5 these metals are present in the nickel-chromium or nickel-chromium-iron alloy within the following limits:
- 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.
- 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 5 ty-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 ac.- complished by means of an interrupter.
- nickel-chromium alloys is meant to include alloys of nickel and. chromium and is also'intended to include alloys formed of nickel, chromium and iron.
- the alloys referred to herein small amounts of phosphorous and. sulphur may be present as impurities.
- the nickel may also contain about 1 percent of cobalt.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Conductive Materials (AREA)
Description
, oxidation at high temperatures is essential.
'atenied June 18, 1935 REUE JUL 2? l i NlTED STATES ALLOY RElSSUED James M. Lohr, Morristown, N. I... assignor to Driver-Harris Company, Harrison, N. .1, a. corporation of New Jersey No Drawing. Application October 12, 1934,
lul. 211943 Serial No. 748,084
2 Claims.
This invention relates to alloys and more par ticularly to alloys for electrical resistance units.
In the manufacture of electrical resistance units, an'alloy having the property of resisting 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 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 20 parts of 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-chromiumiron alloys is 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.
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, zirconium and aluminum are added to an alloy containing 15 to 25 percent chromium and the balance nickel, the final alloy .will contain 15 to 25 percent chromium, calcium, zirconium and aluminum in the percentages herein stated and the balance nickel."
The proportions of calcium, zirconium and aluminum may vary within certain limits. I have found that best results are obtained when 5 these metals are present in the nickel-chromium or nickel-chromium-iron alloy within the following limits:
The preferred portions of the alloying-agents are as follows: 2
Percent Calcium .03 H Zirconium .25 Aluminum .0'7- .38 Manganese 0.05-1.0 25 Silicon 0.40-1.0
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 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 40 613. The method is substantially as follows:
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 5 ty-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 ac.- complished by means of an interrupter.
In testing the alloys of my invention according to the above described method a reference sample composed of percent nickel and 20 percent chromium and no alloy additions having an approximate life of hours was used. This value is considered as 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 No. Go Zr Al useful life will be noted that the useful life of such samples is from 575 percent to 795 percent of the 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 aluminum therefore greatly increases the useful life of the alloy for electrical resistance purposes where the wire is exposed to a high temperature.
4 In the claims the phrase nickel-chromium alloys is meant to include alloys of nickel and. chromium and is also'intended to include alloys formed of nickel, chromium and iron.
In the alloys referred to herein, small amounts of phosphorous and. sulphur may be present as impurities. The nickel may also contain about 1 percent of cobalt.
I claim:
1. A nickle-ehromium alloy containing 15 to 25 per cent chromium, .01 to .20 percent calcium, .01 to .50 percent zirconium and .01 to 1 percent aluminum, balance nickel. I r
2. A nickel-chromium alloy containing 15 to 25 percent chromium, substantially .03 percent cal- 1 cium, substantially .20 percent zirconium and from .07 to .38 percent aluminum, balance nickel.
JAMES M. LOHR.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US748084A US2005431A (en) | 1934-10-12 | 1934-10-12 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US748084A US2005431A (en) | 1934-10-12 | 1934-10-12 | Alloy |
Publications (1)
Publication Number | Publication Date |
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US2005431A true US2005431A (en) | 1935-06-18 |
Family
ID=25007933
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US748084A Expired - Lifetime US2005431A (en) | 1934-10-12 | 1934-10-12 | Alloy |
Country Status (1)
Country | Link |
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US (1) | US2005431A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2581420A (en) * | 1949-09-23 | 1952-01-08 | Driver Harris Co | Alloys |
US2687956A (en) * | 1951-12-28 | 1954-08-31 | Driver Harris Co | Alloy |
-
1934
- 1934-10-12 US US748084A patent/US2005431A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2581420A (en) * | 1949-09-23 | 1952-01-08 | Driver Harris Co | Alloys |
US2687956A (en) * | 1951-12-28 | 1954-08-31 | Driver Harris Co | Alloy |
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