US2104836A - Heat-resisting implement - Google Patents
Heat-resisting implement Download PDFInfo
- Publication number
- US2104836A US2104836A US89371A US8937136A US2104836A US 2104836 A US2104836 A US 2104836A US 89371 A US89371 A US 89371A US 8937136 A US8937136 A US 8937136A US 2104836 A US2104836 A US 2104836A
- Authority
- US
- United States
- Prior art keywords
- metals
- heat
- resisting
- group
- implement
- 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
- 229910052751 metal Inorganic materials 0.000 description 17
- 239000002184 metal Substances 0.000 description 17
- 229910045601 alloy Inorganic materials 0.000 description 13
- 239000000956 alloy Substances 0.000 description 13
- 150000002739 metals Chemical class 0.000 description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 10
- 229910052684 Cerium Inorganic materials 0.000 description 8
- 238000007792 addition Methods 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical group [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 7
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical group [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 6
- 239000011651 chromium Substances 0.000 description 6
- 230000000737 periodic effect Effects 0.000 description 5
- 229910000990 Ni alloy Inorganic materials 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 230000003647 oxidation Effects 0.000 description 4
- 238000007254 oxidation reaction Methods 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 3
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 229910052770 Uranium Inorganic materials 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 229910052761 rare earth metal Inorganic materials 0.000 description 3
- 150000002910 rare earth metals Chemical class 0.000 description 3
- 239000010936 titanium Substances 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- 239000010953 base metal Substances 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 239000011733 molybdenum Substances 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- WHDPTDWLEKQKKX-UHFFFAOYSA-N cobalt molybdenum Chemical compound [Co].[Co].[Mo] WHDPTDWLEKQKKX-UHFFFAOYSA-N 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- -1 iron group metals Chemical class 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000011572 manganese Substances 0.000 description 1
- PYLLWONICXJARP-UHFFFAOYSA-N manganese silicon Chemical compound [Si].[Mn] PYLLWONICXJARP-UHFFFAOYSA-N 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052720 vanadium Inorganic materials 0.000 description 1
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 1
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
Definitions
- This invention relates to heat-resisting implemeats constructed from alloys of metals or the iron group and the sixth group oi the periodic system of the elements.
- the heat resistance oi' an implement constructed irom a chrome-nickel alloy is considerably reduced by addition of titanium or also vanadium: even additions of aluminum bring about improvements of the heat resistance only under particular conditions, whereas in small quantities they have disadvantageous influences.
- titanium and aluminum are nearly related to the rare earths, it was consequently to be ex- 35 pected that the latter analogously with the former elements would behave in a similar manner, that is to say would not give rise to any increase in the heat resistance of implements made of chrome-nickel alloys. Thorough research has now shown that these rare earth metals in contradistinction to titanium and aluminum have the property of increasing to a considerable extent the heat resistance oi implements constructed from alloys oi.
- metals of the iron group and the sixth group of the periodic system of the elements e. g.. constructed from chrome-nickel alloys.
- the life of a 0.4 mm. wire in the form of a small spiral wound on a 3 mm. mandrel heated electrically to 1050* C. for alternate periods of two minutes with interposed breaks oi 2 minutes was about 120 hours.
- a similar wire made of the same alloy with an addition of 0.2% oi a metal of the cerium group or 0.2% of cerium mixed metal i. e., cerium mixed or alloyed with other metals of the rare earths had a life period oi about 200 to 280hours.
- the base metal for the heat resisting implements to which the rare earth metals are added may contain besides metals oi the sixth group or the periodic system of the elements metals of the iron group as the main constituent, namely 50 to 98% of nickel, and up to 48% of iron or iron plus cobalt, the amount of cobalt not exceeding 20% oi the final alloy.
- the percentage of the metals of the sixth group oi the periodic system of the elements namely chromium, molybdenum, tungsten and uranium may amount to 1 to 48%, the chromium contents being 1 to 30%: the amount of each 0! the metals molybdenum. tungsten and uranium should not exceed 20%.
- the alloys may further contain small additions for deoxidation or for improving the malleability such as manganese. magnesium or silicon each up to an amount of 2%, the sum of these additions not exceeding 2%.
- I claim l A high temperature oxidation resistant alloy containing .01 to 1.2% Ce, 1 to 30% Cr, the balance consisting of iron group metals.
- a high temperature oxidation resistant alloy containing .01 to 1.2% Ce, 1 to 30% Or, the balance consisting of at least one of the metals of the iron group.
- a high temperature oxidation resistant alloy containing .01 to 1.2% Ca, 1 to 30% Cr, a small but eil'ective amount up to 20% Co, the balance consisting of nickel.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
Talented Jan. 11, 1938 UNITED STATES 8.104.838 HEAT-BESISTING Werner Hessenbrueh, Hanan-on-the-Maln, Germany, assignor to iirm Reruns-Vacuumschmelze Aktiengeselischait, Hanan-on-the Main, Germany No Drawing. Original application March i, 1985, Serial No. 9,800. Divided and this application July 7, 1938, Serial No. 89,871.
March 24, 1934 4 Claims.
This application is a division of my coDending patent application Serial No. 9,806, tiled Mar. 1935.
This invention relates to heat-resisting implemeats constructed from alloys of metals or the iron group and the sixth group oi the periodic system of the elements.
The heat resistance of implements constructed from alloys of metals of the iron group and the E52 merits, e. g., constructed from chrome-nickel alloys is to be ascribed in the first place to the fact that the high chromium content in association with nickel forms a strongly adherent oxide layer which protects the remaining metal from buming. It was formerly supposed that the heat resistance of implements constructed from such alloys could be considerably improved when elements more electropositive than nickel, the oxides of which are stable above 1500 C. were added thereto. It has, however, been shown that these considerations are by no means generally ap plicable and that although certain of these electropositive elements increase the heat resistance, others on the contrary do not. Thus, for example, the heat resistance oi' an implement constructed irom a chrome-nickel alloy is considerably reduced by addition of titanium or also vanadium: even additions of aluminum bring about improvements of the heat resistance only under particular conditions, whereas in small quantities they have disadvantageous influences. Since titanium and aluminum are nearly related to the rare earths, it was consequently to be ex- 35 pected that the latter analogously with the former elements would behave in a similar manner, that is to say would not give rise to any increase in the heat resistance of implements made of chrome-nickel alloys. Thorough research has now shown that these rare earth metals in contradistinction to titanium and aluminum have the property of increasing to a considerable extent the heat resistance oi implements constructed from alloys oi. metals of the iron group and the sixth group of the periodic system of the elements. e. g.. constructed from chrome-nickel alloys. Thus, for example, the life of a 0.4 mm. wire in the form of a small spiral wound on a 3 mm. mandrel heated electrically to 1050* C. for alternate periods of two minutes with interposed breaks oi 2 minutes, was about 120 hours. A similar wire made of the same alloy with an addition of 0.2% oi a metal of the cerium group or 0.2% of cerium mixed metal i. e., cerium mixed or alloyed with other metals of the rare earths had a life period oi about 200 to 280hours. Higher percentages of cerium give a corresponding increase in improvement except that with sixth group of the periodic system 0! the elelarger additions the eiiect is not wholly proportional to the amount introduced, a content of about 0.84% of cerium or "cerium mixed metal" iving about the maximum effect a content 01' 1.2% being the upper limit coming into consideration.
The addition of metals of the rare earths required for obtaining an appreciable increasing oi the lite period of heat resisting implements such as heating wires or hands for electrically heated furnaces, structural elements or the inner parts of heating and annealing furnaces, e. g. conveying chains, supporting sheet metal, pyrometer protecting tubes 81c, need be very small, inasmuch as additions of 0.02 percent of rare earth metals to the molten base metal or a content of 0.01% in the final alloy already suillce to give a noticeable efl'ect. The base metal for the heat resisting implements to which the rare earth metals are added may contain besides metals oi the sixth group or the periodic system of the elements metals of the iron group as the main constituent, namely 50 to 98% of nickel, and up to 48% of iron or iron plus cobalt, the amount of cobalt not exceeding 20% oi the final alloy. The percentage of the metals of the sixth group oi the periodic system of the elements namely chromium, molybdenum, tungsten and uranium may amount to 1 to 48%, the chromium contents being 1 to 30%: the amount of each 0! the metals molybdenum. tungsten and uranium should not exceed 20%. When several of the elements cobalt molybdenum, tungsten and uranium are contained at the same time in the alloy, their sum should not exceed 20%. The alloys may further contain small additions for deoxidation or for improving the malleability such as manganese. magnesium or silicon each up to an amount of 2%, the sum of these additions not exceeding 2%.
I claim l. A high temperature oxidation resistant alloy containing .01 to 1.2% Ce, 1 to 30% Cr, the balance consisting of iron group metals.
2. A high temperature oxidation resistant alloy containing .01 to 1.2% Ce, 1 to 30% Or, the balance consisting of at least one of the metals of the iron group.
3. A high temperature oxidation resistant alloy containing .01 to 1.2% Ce, 1 to 30% Cr, up to 2% 01' a deoxidizer from the group consisting of manganese silicon and aluminum and the balance consisting of at least one of the metals of the iron group.
4. A high temperature oxidation resistant alloy containing .01 to 1.2% Ca, 1 to 30% Cr, a small but eil'ective amount up to 20% Co, the balance consisting of nickel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US89371A US2104836A (en) | 1935-03-07 | 1936-07-07 | Heat-resisting implement |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US9806A US2067569A (en) | 1934-03-24 | 1935-03-07 | Heat resisting implements |
| US89371A US2104836A (en) | 1935-03-07 | 1936-07-07 | Heat-resisting implement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2104836A true US2104836A (en) | 1938-01-11 |
Family
ID=26679899
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US89371A Expired - Lifetime US2104836A (en) | 1935-03-07 | 1936-07-07 | Heat-resisting implement |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2104836A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2553330A (en) * | 1950-11-07 | 1951-05-15 | Carpenter Steel Co | Hot workable alloy |
| US2838394A (en) * | 1955-01-24 | 1958-06-10 | Kanthal Ab | Nickel-chromium alloys containing rare earth metals and boron |
| DE1068023B (en) * | 1959-10-29 | |||
| US3017265A (en) * | 1959-09-25 | 1962-01-16 | Gen Electric | Oxidation resistant iron-chromium alloy |
| US3031297A (en) * | 1959-11-03 | 1962-04-24 | Gen Electric | Oxidation resistant alloy |
| US3360365A (en) * | 1964-05-12 | 1967-12-26 | Boehler & Co Ag Geb | Process of producing an alloy steel for hot-working tools |
| US3362813A (en) * | 1964-09-15 | 1968-01-09 | Carpenter Steel Co | Austenitic stainless steel alloy |
| US4128419A (en) * | 1973-03-14 | 1978-12-05 | Terekhov Kuzma I | Nickel-base alloy |
| US4155751A (en) * | 1975-12-29 | 1979-05-22 | Cabot Corporation | Weldable alloy |
-
1936
- 1936-07-07 US US89371A patent/US2104836A/en not_active Expired - Lifetime
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1068023B (en) * | 1959-10-29 | |||
| US2553330A (en) * | 1950-11-07 | 1951-05-15 | Carpenter Steel Co | Hot workable alloy |
| US2838394A (en) * | 1955-01-24 | 1958-06-10 | Kanthal Ab | Nickel-chromium alloys containing rare earth metals and boron |
| US3017265A (en) * | 1959-09-25 | 1962-01-16 | Gen Electric | Oxidation resistant iron-chromium alloy |
| US3031297A (en) * | 1959-11-03 | 1962-04-24 | Gen Electric | Oxidation resistant alloy |
| US3360365A (en) * | 1964-05-12 | 1967-12-26 | Boehler & Co Ag Geb | Process of producing an alloy steel for hot-working tools |
| US3362813A (en) * | 1964-09-15 | 1968-01-09 | Carpenter Steel Co | Austenitic stainless steel alloy |
| US4128419A (en) * | 1973-03-14 | 1978-12-05 | Terekhov Kuzma I | Nickel-base alloy |
| US4155751A (en) * | 1975-12-29 | 1979-05-22 | Cabot Corporation | Weldable alloy |
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