US1633826A - Alloy - Google Patents

Alloy Download PDF

Info

Publication number
US1633826A
US1633826A US644057A US64405723A US1633826A US 1633826 A US1633826 A US 1633826A US 644057 A US644057 A US 644057A US 64405723 A US64405723 A US 64405723A US 1633826 A US1633826 A US 1633826A
Authority
US
United States
Prior art keywords
alloy
aluminum
nickel
percent
chromium
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
Application number
US644057A
Inventor
William E Ruder
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US644057A priority Critical patent/US1633826A/en
Application granted granted Critical
Publication of US1633826A publication Critical patent/US1633826A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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

  • My invention relates to alloys and has for its object the provision of an alloy which is heat resisting or capable of withstanding high temperatures without excessive oxida- I tion.
  • my invention relates to alloys which may be cast to form various articles required to withstand high temperatures, such as annealing boxes, furnace structures, etc., and also to electric resistance heating alloys.
  • the furnace should preferably have a basic lin-' ing since if an acid lining were used a certain amount of silicon in the lining would be reduced by the aluminum and enter into the alloy. Even a small percentage of silicon in the alloy would be obiectionable.
  • the basic lining becomes less important.
  • the iron and nickel andchromium are melted in the furnace and then tapped on to the aluminum which has been preheated to a molten condition in the ladle.
  • the titanium and manganese are also added in the furnace. Care should be taken to have the iron nickel. chromium mixture thoroughly physical characteristics of the alloy, aldeoxidized before adding it to the aluminum. It 1s preferable to have the carbon as low as though this is not absolutely necessary.
  • the alloy may not and preferably will not conpossible and in case the material used runs tain the percentage of purifying and grain a little higher than approximately .01 perrefining material added to the mixture since cent of carbon. the carbon should be reduced all .ora large portion of it may go ofi with in the furnace before making the alloy.
  • This the slag Preferably. I use 30 percent of applies also to the elements phosphorus and nickel. 8 percent of 1 1 nd 10 persulphur. None of the furnace slag should so cent of chromium. the remainder consisting be allowed to come into contact with the alsubstantially of iron. loy after the aluminum .has been added.
  • Cryolite is used because of its may also be forged, rolled 0r drawn into SOlUbIlIty for aluminum oxide. Care should wire. Its drawing properties'are impro d be taken to have the metal in the furnace by the addition of the manganese, and prefillst h en ugh o pour cleanly from the erebly a small amount of the manganese ladle. The cooler it is when cast the better should remain in the alloy. It has a resistthe .l ne
  • the alloy shows very little oxidation when, run for long periods at temperatures above 1000 degrees C.
  • the metal forming the base of the alloy 50 may be ordinary low carbon steel or even commercial iron.
  • cryolite method is preferred to the gas method.
  • a heat resisting alloy having an iron base and containing approximately 30% of nickel, 8% of aluminum and 10%of chromium.
  • a heat resisting alloy having aniron base and containing, approximately 30% of nickel, 8% of aluminum, 10% chromium, and 1%of titanium.
  • a heat resisting alloy having an iron base and containing, approximately 30% of nickel, 8% of aluminum, 10% of chromium,

Description

Patented June 28, 1027.
UNITED STATES PATENT- OFFICE.
OF SCHENECTADY, NEW YORK, ASSIGNOR TO GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK. 4
WILLIAM E. RUDER,
ALLOY.
Io Drawing. Application filed June 7,1923, Serial No. 644,057. Renewed April 29, 1927.
My invention relates to alloys and has for its object the provision of an alloy which is heat resisting or capable of withstanding high temperatures without excessive oxida- I tion.
More specifically my invention relates to alloys which may be cast to form various articles required to withstand high temperatures, such as annealing boxes, furnace structures, etc., and also to electric resistance heating alloys.
I have found that an alloy having an iron base and containing from to percent of nickel, 7 to 9 percent of aluminum, and 7 to 15 percent of chromium forms avery satisfactory material for castings required to. withstand high temperatures. About 1 percent each of a suitable purifying and grain refining material, such as titanium, manganese, or both, may and preferably is added for the purpose of improving the and .15 percent of silicon is satisfactory for my purpose.
In making the alloy it is preferable to use an electric furnace since it lends itself more readily to the controlling of the alloy. The furnace should preferably have a basic lin-' ing since if an acid lining were used a certain amount of silicon in the lining would be reduced by the aluminum and enter into the alloy. Even a small percentage of silicon in the alloy would be obiectionable. When the aluminum is not added in the furnace but is added in the ladle the basic lining becomes less important.
The iron and nickel andchromium are melted in the furnace and then tapped on to the aluminum which has been preheated to a molten condition in the ladle. The titanium and manganese are also added in the furnace. Care should be taken to have the iron nickel. chromium mixture thoroughly physical characteristics of the alloy, aldeoxidized before adding it to the aluminum. It 1s preferable to have the carbon as low as though this is not absolutely necessary. The alloy may not and preferably will not conpossible and in case the material used runs tain the percentage of purifying and grain a little higher than approximately .01 perrefining material added to the mixture since cent of carbon. the carbon should be reduced all .ora large portion of it may go ofi with in the furnace before making the alloy. This the slag. Preferably. I use 30 percent of applies also to the elements phosphorus and nickel. 8 percent of 1 1 nd 10 persulphur. None of the furnace slag should so cent of chromium. the remainder consisting be allowed to come into contact with the alsubstantially of iron. loy after the aluminum .has been added. An alloy made up of the various metals The molten aluminum and also the alloy in the percentage ranges given is extremely after the addition of the aluminum should tough and is very readily cast. It may be be kept covered with a special slag of cryolite machined and hence is particularly suitable 01 a cryollte lime mixture to protect it from for castings requiring machining. The alloy Oxidat on. Cryolite is used because of its may also be forged, rolled 0r drawn into SOlUbIlIty for aluminum oxide. Care should wire. Its drawing properties'are impro d be taken to have the metal in the furnace by the addition of the manganese, and prefillst h en ugh o pour cleanly from the erebly a small amount of the manganese ladle. The cooler it is when cast the better should remain in the alloy. It has a resistthe .l ne
ance of approximately 850 ohms per mil. foot and a low temperature coefficient of resistanc e so that it is particularly adapted 45 for use as an electrical resistance heating element. The alloy shows very little oxidation when, run for long periods at temperatures above 1000 degrees C.
The metal forming the base of the alloy 50 may be ordinary low carbon steel or even commercial iron. A steel containing .02 percent or le'ss'of carbon, .04 percent or less of sulphur, .03 percent or less of phosphorus,
When casting the alloy every precaution should be taken to prevent oxidation. This may be done by filling the molds beforehand with a non-oxidizing gas, such as nitrogen or carbon dioxide, or by dusting the molds lightly but thoroughly with cryolite to dissolve the oxide film formed between the ladle and the mold. This prevents the formation of cold shuts and subsequent cracks due to them. The cryolite method is preferred to the gas method.
While I have described a specific embodiment of my invention in accordance with the provisionsgof the patent statutes, it should be understood that I do not limit my invention thereto, since various modifications thereof W111 suggest themselves to those '40 to 60% iron, 25% or more of nickel and smaller amounts but at least 7% each of aluminum and chromium.
251.;A heat resisting alloy havingan iron base and containing from 25 to 40% of nickel, from 7 to 9% of aluminum and from 7 to 15% of chromium.
3. Aheat resisting alloy containing 50% or more of iron, 25% or more of. nickel and 7% or more each of aluminum and chromium. I
4. A heat resisting alloy having an iron base and containing approximately 30% of nickel, 8% of aluminum and 10%of chromium.
5. A heat resisting alloy having aniron base and containing, approximately 30% of nickel, 8% of aluminum, 10% chromium, and 1%of titanium.
6. A heat resisting alloy having an iron base and containing, approximately 30% of nickel, 8% of aluminum, 10% of chromium,
1%;of titanium, and 1% of manganese.
In witness whereof, I have hereunto set my hand this 6th day of June, 1923.
WHJLIAM E. RUDER.
US644057A 1923-06-07 1923-06-07 Alloy Expired - Lifetime US1633826A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US644057A US1633826A (en) 1923-06-07 1923-06-07 Alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US644057A US1633826A (en) 1923-06-07 1923-06-07 Alloy

Publications (1)

Publication Number Publication Date
US1633826A true US1633826A (en) 1927-06-28

Family

ID=24583271

Family Applications (1)

Application Number Title Priority Date Filing Date
US644057A Expired - Lifetime US1633826A (en) 1923-06-07 1923-06-07 Alloy

Country Status (1)

Country Link
US (1) US1633826A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2688535A (en) * 1949-11-07 1954-09-07 Madaras Corp Metallurgical process

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2688535A (en) * 1949-11-07 1954-09-07 Madaras Corp Metallurgical process

Similar Documents

Publication Publication Date Title
US1928747A (en) Nonferrous alloy
US1556776A (en) Material for resisting oxidation at high temperatures
US2287888A (en) Manganese-base alloys
US2253502A (en) Malleable iron
US2189198A (en) Copper-titanium alloy
US1633826A (en) Alloy
US1833723A (en) Alloy
JPS6158541B2 (en)
US1641752A (en) Oxidation-resisting material
US2310094A (en) Electrical resistance element
US2022686A (en) Aluminum alloy casting and method of making the same
US2173254A (en) Copper alloy
JPS6241302B2 (en)
US2240064A (en) Alloy for metal to glass seals
US2050387A (en) Method of making stable invar
US935863A (en) Alloy and process for its production.
US1612642A (en) Method of adding aluminum to aluminum-containing alloys
US1538360A (en) Malleable noncorrodible alloy
US2240063A (en) Alloys for metal to glass seals
US2059555A (en) Alloys
US1389133A (en) Heat-resisting alloy
US1633805A (en) Heat-resisting alloy
US2046380A (en) Copper base alloys
US1396276A (en) Process for improving ferrous metals
US2432149A (en) Heat resistant nickel alloys