US1833723A - Alloy - Google Patents
Alloy Download PDFInfo
- Publication number
- US1833723A US1833723A US644058A US64405823A US1833723A US 1833723 A US1833723 A US 1833723A US 644058 A US644058 A US 644058A US 64405823 A US64405823 A US 64405823A US 1833723 A US1833723 A US 1833723A
- Authority
- US
- United States
- Prior art keywords
- alloy
- aluminum
- chromium
- iron
- furnace
- 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
- 229910045601 alloy Inorganic materials 0.000 title description 26
- 239000000956 alloy Substances 0.000 title description 26
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 16
- 229910052782 aluminium Inorganic materials 0.000 description 14
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 13
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 8
- 239000011651 chromium Substances 0.000 description 8
- 229910052742 iron Inorganic materials 0.000 description 8
- 229910001610 cryolite Inorganic materials 0.000 description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- 238000007670 refining Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 3
- 229910052710 silicon Inorganic materials 0.000 description 3
- 239000010703 silicon Substances 0.000 description 3
- 239000002893 slag Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 2
- 239000005864 Sulphur Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910052698 phosphorus Inorganic materials 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 235000008733 Citrus aurantifolia Nutrition 0.000 description 1
- 229910001209 Low-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
- 235000011941 Tilia x europaea Nutrition 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910052770 Uranium Inorganic materials 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000004571 lime Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium 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
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
Description
Patented Nov. 24, 1931 UNITED STATES PATENT OFFICE WILLIAM E. BUDER,
OF SCHENTECTADY, NEW YORK, ASSIG-NOR TO GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
ALLOY No Drawing. Application filed June 7,
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 in 'air without excessive oxidation.
More specifically my invention relates to electric resistance heating alloys and to alloys which may be cast to form various articles required to withstand high temperatures.
In carrying out my invention 1 provide an alloy having an iron, base and containing from 15 to 35f/ of chromium and from 5 to 12% of aluminum. Preferably I use 25% of chromium, and of aluminum,- the re- 15 mainder consisting substantially of iron.
For the purpose of improving the physi cal quality of the alloy, about 1% of a suit-1 able grain refining and purifying element may be added in making the alloy, such as titanium, zirconium, molybdenum, uranium,
all or a large portion of it may go off withvanadium or the like, although this is not absolutely necessary. The alloy mayand probably Will' not contain the percentage of grain refining element added to the mixture, since the slag.
This alloy may be forged or drawn into wire and has the other characteristics essential to a satisfactory resistance heating conductor such as durability or the property of withstanding high temperatureswithout ex ces'sive oxidation, sufficient resistivity to generate the required amount of heat when a current is passed through it, and a zero temperw caturecoefficient of resistance throughout its "ohms per mil foot, and the durability also increases, while the ductility becomes less. The temperature coeflicient of resistance is 1923. Serial No. 644,058.
practically zero throughout the ranges of the various elements given, and the alloy shows very little oxidation when run for long periods at temperatures above 1000 0.] The composition ofthe alloy actually used would therefore 'be determined by the relativeimportance of cost of the materials, resistivity, durability, and mechanical quality.
The metal forming the base of the alloy may be ordinary low carbon steel or even commercial iron. A steel containing .02% or less of carbon, .04% "or less of sulphur, or less of phosphorus and 0.15% or less of. silicon is satisfactory for my purpose.
In making the alloy it is preferable to use an electric furnace, since this furnace lends itself more readily to the cpntrolling of an alloy. The furnaceshould preferably have a basic lining since i 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 is objectionable. When the aluminum is not added in the furnace but is added in the ladle, the basic lining becomes less important.
The iron and chromium are melted in the furnace and then tapped on to the aluminum, which has been preheated to a molten condition in the ladle. Care should be taken to have the iron and chromium.mi-xture thor-' oughly deoxidized before adding' it to the aluminum. It is preferable to have the carbon as low as possible in case thematerial used runs a little higher than approximately .01% in carbon, the carbon should be reduced in the furnace before making the alloy. This appliesalso to the elements phosphorus and sulphur.. None of the furnace slag should be allowed to come into contact with the alloy after the aluminum has been added. The molten aluminum and also the alloy after. the addition of. the aluminum should be kept covered with a special-slag of cryolite or a cryolite lime mixture to protect the-aluminum from oxidation. Cryolite is used because of its solubility for aluminum oxide. Care should be takento have the metal in the furnace just hot enough to pour cleanly from the ladle but not superheated. The cooler it is when cast the better the grain obtained. When castingthe alloy eve precaution should be taken to prevent oxi ation. This ay be done by filling the molds beforehand ith a non-oxidizing 'gassuch as nitrogen ',-:or carbon dioxide,- or bygdusting the molds lightly bug thoroughly ith cryolite to dissolve the oxide film forme between the ladle and the mold. This revents the formation of cold-shutsand-su sequent c'racks'dueito' them. The cryolite method'is' preferredto the gas method.
While'I have described a specific embodiment of my invention inaccordance with the provisions ofth patent statutes, it' should be gunderstood thatI do'not'limit my invention thereto, since various modificaions thereof will suggest themselves. to those skilled in the art without departing from the -,spirit of my invention, the scope of which is set forth in the annexed claims. What I claim asg-newvandidesire ,to secure by Letters Patent ojfthe United States'is 1. A heat resisting alloy containing ap- 1 proximately .of,chromium,,and 10% of aluminum, the'rem'ainder consisting of ironand not more than 1%ofa gram refining element. 7
2. A heat resisting alloy having an iron, aozbase and containing approximately 25% of chromium and 1 Q% 0f aluminum, there-2 mainder consisting of an appreciable amount but not more-than 1%,of a grain refining.
element.
= '35; 3. .A heat resisting alloy having an iron base and containing approximately 25% of {chromium and 10% of aluminum, the remainder consisting of-an appreciable amount but not' ;more than 1%;0fi-titanium; -v 1 4o 4.-A resistor containing about'25% chromium, about 10% aluminum and about 65% iron, said alloy having a substantially zero temperature'coeificient of resistance throughout its normal operating range.
5 3 In witness ,Whereof, I have hereunto set my hand this 6th day of June, 1923. p
' WILLIAM'E; RUDER.
60 vii
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US644058A US1833723A (en) | 1923-06-07 | 1923-06-07 | Alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US644058A US1833723A (en) | 1923-06-07 | 1923-06-07 | Alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
US1833723A true US1833723A (en) | 1931-11-24 |
Family
ID=24583278
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US644058A Expired - Lifetime US1833723A (en) | 1923-06-07 | 1923-06-07 | Alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US1833723A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2533736A (en) * | 1946-05-11 | 1950-12-12 | Driver Harris Co | Electric resistance element and method of heat-treatment |
US3026197A (en) * | 1959-02-20 | 1962-03-20 | Westinghouse Electric Corp | Grain-refined aluminum-iron alloys |
US3171737A (en) * | 1961-04-28 | 1965-03-02 | Hoskins Mfg Company | Electrical resistance alloy |
US3859079A (en) * | 1972-08-09 | 1975-01-07 | Bethlehem Steel Corp | High temperature oxidation resistant alloy |
DE3520473A1 (en) * | 1984-06-08 | 1986-01-02 | Kyocera Corp., Kyoto | IMPLANTATION ALLOY OF FE-CR-AL TYPE FOR MEDICAL TREATMENT AND METHOD FOR PRODUCING SUCH AN ALLOY |
-
1923
- 1923-06-07 US US644058A patent/US1833723A/en not_active Expired - Lifetime
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2533736A (en) * | 1946-05-11 | 1950-12-12 | Driver Harris Co | Electric resistance element and method of heat-treatment |
US3026197A (en) * | 1959-02-20 | 1962-03-20 | Westinghouse Electric Corp | Grain-refined aluminum-iron alloys |
US3171737A (en) * | 1961-04-28 | 1965-03-02 | Hoskins Mfg Company | Electrical resistance alloy |
US3859079A (en) * | 1972-08-09 | 1975-01-07 | Bethlehem Steel Corp | High temperature oxidation resistant alloy |
DE3520473A1 (en) * | 1984-06-08 | 1986-01-02 | Kyocera Corp., Kyoto | IMPLANTATION ALLOY OF FE-CR-AL TYPE FOR MEDICAL TREATMENT AND METHOD FOR PRODUCING SUCH AN ALLOY |
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