US2067569A - Heat resisting implements - Google Patents
Heat resisting implements Download PDFInfo
- Publication number
- US2067569A US2067569A US9806A US980635A US2067569A US 2067569 A US2067569 A US 2067569A US 9806 A US9806 A US 9806A US 980635 A US980635 A US 980635A US 2067569 A US2067569 A US 2067569A
- Authority
- US
- United States
- Prior art keywords
- implements
- metals
- elements
- nickel
- heat resisting
- 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 18
- 239000002184 metal Substances 0.000 description 18
- 150000002739 metals Chemical class 0.000 description 14
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical group [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 11
- 229910045601 alloy Inorganic materials 0.000 description 9
- 239000000956 alloy Substances 0.000 description 9
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 9
- 229910017052 cobalt Inorganic materials 0.000 description 9
- 239000010941 cobalt Substances 0.000 description 9
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000007792 addition Methods 0.000 description 8
- 229910052684 Cerium Inorganic materials 0.000 description 7
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 7
- 229910000990 Ni alloy Inorganic materials 0.000 description 7
- 229910052804 chromium Inorganic materials 0.000 description 7
- 239000011651 chromium Substances 0.000 description 7
- 230000000737 periodic effect Effects 0.000 description 6
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 5
- 229910052750 molybdenum Inorganic materials 0.000 description 5
- 239000011733 molybdenum Substances 0.000 description 5
- 229910052759 nickel Inorganic materials 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 3
- 229910052770 Uranium Inorganic materials 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 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
- 239000010953 base metal Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 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
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/053—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 30% but less than 40%
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Treatment Of Steel In Its Molten State (AREA)
Description
Patented Jan. 12, 1937 HEAT RE SISTING IMPLEMENTS Werner Hessenbruch, Hanau-omthe-Main, Ger
many, assignmto firm Heraeus-Vacuumschmelze Aktiengesellschaft, Hanau-on-the- Main, Germany No Drawing. Application March "l, 1935; Serial No. 9,806. In Germany March 24, 1934- 1 4 Claims.
This invention relates to heat-resisting implements constructed from alloys of metals of the iron group and the sixth group of the periodic system of the elements.
5 The heat resistance of implements constructed from alloys of metals of the iron group and the sixth group of the periodic system of the elements, e. g. constructed from chrome-nickel alloys is to be ascribed in the first place to thefact that the high chromium content in. association with nickel forms a strongly adherent oxide layer which protects the remaining metal from burning. 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 applicable and that although certain of these electropositive elements increase the heat resistance, others on the contrary do not. Thus, for example, the heat resistance of an implement constructed from a chrome-nickel alloy is con- 35 siderably 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 in- 30 fluences. Since titanium and aluminum are nearly related to the rare earths, it was consequently to be expect-ed that the latter analogously with the former elements would behave in a similar manner, that is to say would not give rise 35 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 con- 4 siderable extent the heat resistance of implements constructed from alloys of metals of the iron group and the sixth group of the periodic system ofthe 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 of 2 minutes, was about 120 hours. A similar wire made of the 50 same alloy with an addition of- 0.2% of cerium or-0.2% of cerium mixed metal 1. e. cerium mixed or alloyed with other metals of the rare earths had a life period of about 200 to 280 hours. Higher percentages of cerium give a 55 corresponding increase in improvement except that with larger additions the efiect is not wholly proportional to the amount introduced, a content of about 0.8-1% of cerium or cerium mixed metal giving about the maximum efiect a content of 1.2% being the upper limit coming into 5 consideration.
The additions of metals of the rare earths required for obtaining an appreciable increasing of the .life period of heat resisting implements such as heating wires or bands for electrically 1o heated furnaces, construction elements of the inner partsof heating and annealing furnaces,
e. g. conveying chains, supporting sheet metal, pyrometer protecting tubes &c, need be very small, inasmuch as additions of 0.02 percent of 15 rare earth metals to the molten base metal or a content of 0.01% in the final alloy already suflice to give a noticeable effect. The base metal for the heat resisting implements to which the rare earth metals are added may contain 20 besides metals of the sixth group of 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% of the final alloy. The percentage of the metals of the sixth group of the periodic system of the elements namely chromium, molybdenum, tungsten and uranium may amount to 1 to 48%, the chromium contents being 1- to the amount of each of the metals molydenum, tungsten and uranium should not exceed 20%. When several of the elements cobalt, molybdenum, tungsten and uranium are contained at the same time in V the alloy, their sum should not exceed 20%. The alloys may further contain small additions for deoxidatlon 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:
1. As an article of manufacture and trade a heat resisting implement constructed of a chromium-nickel alloy comprising main and auxiliary elements, the main elements consisting of from to 98 p. ct. of nickel, from 1 to 30 p. ct. of chromium, from 9.01 to 1.2% of metals of the cerium group, from a small but efiective amount to 20% of cobalt, the auxiliary elements consisting of from a small but effective amount to 20 0 p. ct. of metals of the sixth group of the periodic system, besides chromium, and the sum .of the cobalt and the last-named metals amounting to 20% at most.
2. As an article of manufacture and trade a named metals amounting to at most.
3. As an article of manufacture and trade a heat resisting implement constructed of a chromium-nickel alloy comprising main elements and an auxiliary element, the main elements consisting of from 50 to 98 p. ct. of nickel, from 1 to p. ct. of chromium, from 0.01 to 1.2% of metals of the cerium group, from a small but eflective amount to 20% of cobalt, the auxiliary element being molybdenum. from a small but effective amount to 20% and the sum oi cobalt and molybdenum amounting to 20% at most.
4. As an article of manufacture and trade a heat resisting implement constructed of a chromium-nickel alloy comprising main elements and an auxiliary element, the-main element consisting of from to 98 p. ct. of nickel, from 1 to 30 p. ct. chromium, from 0.01 to.1.2% of cerium, from a small but effective amount to.20% of cobalt, the auxiliary element being molybdenum from a small but effective amount to 20% and the sum of cobalt and molybdeum amounting to 20% at most.
. WERNER HESSENBRUCH.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US89371A US2104836A (en) | 1935-03-07 | 1936-07-07 | Heat-resisting implement |
| US89373A US2104835A (en) | 1935-03-07 | 1936-07-07 | Heat-resisting implement |
| US89372A US2075718A (en) | 1935-03-07 | 1936-07-07 | Heat-resisting implement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2067569X | 1934-03-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2067569A true US2067569A (en) | 1937-01-12 |
Family
ID=7983401
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US9806A Expired - Lifetime US2067569A (en) | 1934-03-24 | 1935-03-07 | Heat resisting implements |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2067569A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2153962A5 (en) * | 1971-09-13 | 1973-05-04 | Cabot Corp | |
| US3787202A (en) * | 1970-11-18 | 1974-01-22 | Cyclops Corp | High temperature chromium-nickel alloy |
| US4043810A (en) * | 1971-09-13 | 1977-08-23 | Cabot Corporation | Cast thermally stable high temperature nickel-base alloys and casting made therefrom |
-
1935
- 1935-03-07 US US9806A patent/US2067569A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3787202A (en) * | 1970-11-18 | 1974-01-22 | Cyclops Corp | High temperature chromium-nickel alloy |
| FR2153962A5 (en) * | 1971-09-13 | 1973-05-04 | Cabot Corp | |
| US4043810A (en) * | 1971-09-13 | 1977-08-23 | Cabot Corporation | Cast thermally stable high temperature nickel-base alloys and casting made therefrom |
| US4118223A (en) * | 1971-09-13 | 1978-10-03 | Cabot Corporation | Thermally stable high-temperature nickel-base alloys |
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