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USRE24243E - J x x xx - Google Patents

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USRE24243E
USRE24243E US24243DE USRE24243E US RE24243 E USRE24243 E US RE24243E US 24243D E US24243D E US 24243DE US RE24243 E USRE24243 E US RE24243E
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alloys
nickel
calcium
aluminum
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01BCABLES; CONDUCTORS; INSULATORS; SELECTION OF MATERIALS FOR THEIR CONDUCTIVE, INSULATING OR DIELECTRIC PROPERTIES
    • H01B1/00Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors
    • H01B1/02Conductors or conductive bodies characterised by the conductive materials; Selection of materials as conductors mainly consisting of metals or alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel

Definitions

  • This invention relates to alloys and more particularly to alloys for electric resistance units.
  • alloy having the property of resisting oxidation at high temperature is essential.
  • the alloys forming the subject matter of this invention are characterized by ability to resist oxidation and by a prolonged life, exceeding that of other known alloys when used under high temperature conditions. Since the introduction of nickelchromium-iron alloys as electric resistance units, many developments have occurred that have improved their resistance to oxidation. In a number of prior patents I have disclosed and claimed various alloying additions of calcium, zirconium and aluminum which greatly improve the life of heating elements. It has also been proposed to add rare earth metals, such as cerium, to nickelchromium-iron alloys to improve the life of the heating elements.
  • the present invention is, therefore, directed to the addition of small quantities of the rare earths with calcium and aluminum to nickel-chromium-iron alloys. I have found that such combination of addition elements greatly increases the period of life of nickel-chromiumiron alloys when employed under conditions where they are subjected to high temperatures.
  • the alloys forming the subject matter of the present invention may also contain small amounts of either silicon or manganese or both of these elements.
  • the rare earth metals may be added as misch metal having an approximate composition of 45 percent cerium, 30 percent lanthanum, 20 percent ytterbium and didymium.
  • the rare earth metals in the form of misch metal, I do not restrict myself to the use of this material as one or more of the rare earth metals may be added singly and its effect is of a similar nature.
  • the additions may be used to advantage with the nickel-chromium-iron alloys of which the best known examples are the alloys of 30 to 70 percent nickel, 10 to 25 percent chromium, balance iron.
  • the additions were made to the alloys consisting of substantially 35 perand aluminum as well nickel-chromium-iron cent nickel, 20 percent chromium and balance iron.
  • Rare earth metals such as misch metal, with calcium and aluminum may be added to such alloys with or without silicon.
  • the proportions of nickel in such alloys may vary from 30 to 50 percent and the chromium from 10 to 25 percent with the balance iron.
  • the quantities of such addition elements are subtracted from the iron content.
  • the final alloys will contain 30 to 50 percent nickel, 10 to 25 percent chromium, the addition elements calcium, aluminum and the rare earth metals in the percentages hereinafter stated, and the balance iron. While. the proportions of calcium, aluminum and rare earth metals may vary within certain limits, I have found that the best results are obtained when these materials are present in the final alloys within the following'limits:
  • alloys contain manganese, silicon, or carbon, they may be present within the following limits:
  • the alloys so prepared have been tested for resistance to oxidation at high temperature by a modification of the method approved by the American Society for Testing Materials Accelerated Life Test for Metallic Materials, B76-39.
  • the alloy is produced in the form of a wire, drawn to a diameter of approximately .025" and tested at a temperature of 1950 F., instead of a temperature of 2050 R, which is the temperature of the standard ASTM method for testing the 60 nickel, 15 chromium alloys.
  • the useful life in hours for wire of substantially 35 percent nickel, 20 percent chromium containing calcium, zirconium and aluminum as addition elements, balance iron, is of the order of hours.
  • the useful life of the alloys of the present invention, according to the above described test is of the order of 400 hours. Thus, the useful life is increased around 300 percent over that of the alloys containing the calcium, zirconium, aluminum group when the rare earth metals are added with calcium and aluminum in the proportions herein stated.
  • the alloys are prepared in the usual manner by placing the ingredients in a bath, heating until the alloying elements become molten and then pouring. In adding rare earth metals to a molten bath, it is necessary to add considerably larger quantities than will be found in the cast metal because they vaporize readily and pass out of the bath. In many instances, with additions of the rare earth metals only a spectrographic trace of one or more of the rare earth metals is found in the cast material. The presence of such traces, however, in combination with calcium and aluminum, greatly increases the oxidation resistance of the alloys.
  • the rare earth metals may be added in amounts suflicient to leave a residue in the cast alloys up to .2 percent but in most instances the use of such amounts is not necessary.
  • a nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .20 percent calcium, .01 to 1.0 percent aluminum, a trace to .50 percent of a rare earth metal, balance essentially iron.
  • a nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent of a rare earth metal, balance essentially iron.
  • a nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .20 percent calcium, .01 to 1.0 percent aluminum, a trace to .50 percent cerium and lanthanum, balance essentially iron.
  • a nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent cerium and lanthanum, balance essentially iron.
  • An electric resistance element consisting substantially of percent nickel, substantially 20 percent chr0- mium, .001 to .20 percent calcium, .0] to 1.0 percent aluminum, a trace to .50 percent of a rare earth metal, balance essentially iron.
  • An electric resistance element consisting substantially of 35 percent nickel, substantially 20 percent chr0- mium, 001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent of a rare earth metal, balance essentially iron.
  • An electric resistance element consisting substantially of 35 percent nickel, substantially 20 percent chr0- mium, .001 to .20 percent calcium, .01 to 1.0 percent aluminum, a trace to .50 percent cerium and lanthanum, balance essentially iron.
  • An electric resistance element consisting substantially 0f 35 percent nickel, substantially 20 percent chr0- mium, .001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent cerium and lanthanum, balance essentially iron.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Adornments (AREA)

Description

Re. 24,243 Reissued Dec. 4, 1956 ALLOYS AND ELECTRICAL RESISTANCE ELEMENTS James M. Lohr, Morristown, N. J., assignor to Driver- Harris Company, Harrison, N. J., a corporation of New Jersey 8 Claims. (Cl. 75-124) atter enclosed in heavy brackets appears in the original patent but forms no part of this reissue specification; matter printed in italics indicates the additions made by reissue.
This invention relates to alloys and more particularly to alloys for electric resistance units.
In the manufacture of electrical resistance units, an
alloy having the property of resisting oxidation at high temperature is essential. The alloys forming the subject matter of this invention are characterized by ability to resist oxidation and by a prolonged life, exceeding that of other known alloys when used under high temperature conditions. Since the introduction of nickelchromium-iron alloys as electric resistance units, many developments have occurred that have improved their resistance to oxidation. In a number of prior patents I have disclosed and claimed various alloying additions of calcium, zirconium and aluminum which greatly improve the life of heating elements. It has also been proposed to add rare earth metals, such as cerium, to nickelchromium-iron alloys to improve the life of the heating elements.
I have found that when calcium as rare earth metals are added to alloys, better results are obtained than if the calcium, zirconium, aluminum group or the rare earths are used alone. The present invention is, therefore, directed to the addition of small quantities of the rare earths with calcium and aluminum to nickel-chromium-iron alloys. I have found that such combination of addition elements greatly increases the period of life of nickel-chromiumiron alloys when employed under conditions where they are subjected to high temperatures. The alloys forming the subject matter of the present invention may also contain small amounts of either silicon or manganese or both of these elements. The rare earth metals may be added as misch metal having an approximate composition of 45 percent cerium, 30 percent lanthanum, 20 percent ytterbium and didymium. Although it is convenient to add the rare earth metals in the form of misch metal, I do not restrict myself to the use of this material as one or more of the rare earth metals may be added singly and its effect is of a similar nature. The additions may be used to advantage with the nickel-chromium-iron alloys of which the best known examples are the alloys of 30 to 70 percent nickel, 10 to 25 percent chromium, balance iron.
This application is a division of my copending application Serial No. 117,510, filed September 23, 1949, now Patent No. 2,581,420. The claims of this application are directed to alloys containing 30 to 50 percent nickel and 10 to 25 percent chromium, and more specifically to alloys containing substantially 35 percent nickel and substantially 20 percent chromium.
In the examples hereinafter described, the additions were made to the alloys consisting of substantially 35 perand aluminum as well nickel-chromium-iron cent nickel, 20 percent chromium and balance iron. Rare earth metals, such as misch metal, with calcium and aluminum may be added to such alloys with or without silicon. The proportions of nickel in such alloys may vary from 30 to 50 percent and the chromium from 10 to 25 percent with the balance iron. Employing nickelchromium-irc-n alloys of these proportions, I have added calcium, aluminum and misch metal in the quantities or amounts hereinafter mentioned.
In preparing alloys containing the addition elements above mentioned, the quantities of such addition elements are subtracted from the iron content. For example, when additions are made to base alloys containing 30 to 50 percent nickel, 10 to 25 percent chromium, the final alloys will contain 30 to 50 percent nickel, 10 to 25 percent chromium, the addition elements calcium, aluminum and the rare earth metals in the percentages hereinafter stated, and the balance iron. While. the proportions of calcium, aluminum and rare earth metals may vary within certain limits, I have found that the best results are obtained when these materials are present in the final alloys within the following'limits:
Percent Calcium .O0l.20
Aluminum .01-1.0
Rare earth metals Trace-0.50
If the alloys contain manganese, silicon, or carbon, they may be present within the following limits:
- Percent Manganese .02-4.0
Silicon .203.0
Carbon 0.25 max.
While alloys having the properties desired to a very high degree are obtained within the limits before men tioned, the preferred range of addition elements is as follows:
The alloys so prepared have been tested for resistance to oxidation at high temperature by a modification of the method approved by the American Society for Testing Materials Accelerated Life Test for Metallic Materials, B76-39. In conducting such test, the alloy is produced in the form of a wire, drawn to a diameter of approximately .025" and tested at a temperature of 1950 F., instead of a temperature of 2050 R, which is the temperature of the standard ASTM method for testing the 60 nickel, 15 chromium alloys. The useful life in hours for wire of substantially 35 percent nickel, 20 percent chromium containing calcium, zirconium and aluminum as addition elements, balance iron, is of the order of hours. The useful life of the alloys of the present invention, according to the above described test, is of the order of 400 hours. Thus, the useful life is increased around 300 percent over that of the alloys containing the calcium, zirconium, aluminum group when the rare earth metals are added with calcium and aluminum in the proportions herein stated.
The alloys are prepared in the usual manner by placing the ingredients in a bath, heating until the alloying elements become molten and then pouring. In adding rare earth metals to a molten bath, it is necessary to add considerably larger quantities than will be found in the cast metal because they vaporize readily and pass out of the bath. In many instances, with additions of the rare earth metals only a spectrographic trace of one or more of the rare earth metals is found in the cast material. The presence of such traces, however, in combination with calcium and aluminum, greatly increases the oxidation resistance of the alloys. The rare earth metals may be added in amounts suflicient to leave a residue in the cast alloys up to .2 percent but in most instances the use of such amounts is not necessary.
In the test referred to above the increase of electrical resistance at temperature with time is plotted and an increase of percent in resistance is known as the useful life. The life of the tested specimen to burn-out is known as total life.
I claim:
1. A nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .20 percent calcium, .01 to 1.0 percent aluminum, a trace to .50 percent of a rare earth metal, balance essentially iron.
2. A nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent of a rare earth metal, balance essentially iron.
3. A nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .20 percent calcium, .01 to 1.0 percent aluminum, a trace to .50 percent cerium and lanthanum, balance essentially iron.
4. A nickel-chromium-iron alloy consisting substantially of 35 percent nickel, substantially 20 percent chromium, .001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent cerium and lanthanum, balance essentially iron.
. 4 5. An electric resistance element consisting substantially of percent nickel, substantially 20 percent chr0- mium, .001 to .20 percent calcium, .0] to 1.0 percent aluminum, a trace to .50 percent of a rare earth metal, balance essentially iron.
6. An electric resistance element consisting substantially of 35 percent nickel, substantially 20 percent chr0- mium, 001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent of a rare earth metal, balance essentially iron.
7. An electric resistance element consisting substantially of 35 percent nickel, substantially 20 percent chr0- mium, .001 to .20 percent calcium, .01 to 1.0 percent aluminum, a trace to .50 percent cerium and lanthanum, balance essentially iron.
8. An electric resistance element consisting substantially 0f 35 percent nickel, substantially 20 percent chr0- mium, .001 to .07 percent calcium, .01 to .40 percent aluminum, a trace to .20 percent cerium and lanthanum, balance essentially iron.
References Cited in the file of this patent or the original patent UNITED STATES PATENTS 1,941,648 Armstrong Jan. 2, 1934 2,047,916 Lohr July 14, 1936 2,047,917 Lohr July 14, 1936 2,047,918 Lohr July 14, 1936 2,581,420 Lohr Jan. 8, 1952 FOREIGN PATENTS 488,926 Great Britain July 12, 1938
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3362813A (en) * 1964-09-15 1968-01-09 Carpenter Steel Co Austenitic stainless steel alloy
US4043838A (en) 1975-04-25 1977-08-23 Allegheny Ludlum Industries, Inc. Method of producing pitting resistant, hot-workable austenitic stainless steel
US4735771A (en) 1986-12-03 1988-04-05 Chrysler Motors Corporation Method of preparing oxidation resistant iron base alloy compositions
US4891183A (en) * 1986-12-03 1990-01-02 Chrysler Motors Corporation Method of preparing alloy compositions
US4999158A (en) * 1986-12-03 1991-03-12 Chrysler Corporation Oxidation resistant iron base alloy compositions

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3362813A (en) * 1964-09-15 1968-01-09 Carpenter Steel Co Austenitic stainless steel alloy
US4043838A (en) 1975-04-25 1977-08-23 Allegheny Ludlum Industries, Inc. Method of producing pitting resistant, hot-workable austenitic stainless steel
US4735771A (en) 1986-12-03 1988-04-05 Chrysler Motors Corporation Method of preparing oxidation resistant iron base alloy compositions
WO1989009841A1 (en) * 1986-12-03 1989-10-19 Chrysler Motors Corporation Method of preparing oxidation resistant iron base alloy compositions
US4891183A (en) * 1986-12-03 1990-01-02 Chrysler Motors Corporation Method of preparing alloy compositions
US4999158A (en) * 1986-12-03 1991-03-12 Chrysler Corporation Oxidation resistant iron base alloy compositions

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