US2503608A - Weldable nickel base alloy - Google Patents
Weldable nickel base alloy Download PDFInfo
- Publication number
- US2503608A US2503608A US82000A US8200049A US2503608A US 2503608 A US2503608 A US 2503608A US 82000 A US82000 A US 82000A US 8200049 A US8200049 A US 8200049A US 2503608 A US2503608 A US 2503608A
- Authority
- US
- United States
- Prior art keywords
- alloy
- alloys
- molybdenum
- base alloy
- nickel
- 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 claims description 43
- 239000000956 alloy Substances 0.000 title claims description 43
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title description 22
- 229910052759 nickel Inorganic materials 0.000 title description 11
- 239000000203 mixture Substances 0.000 claims description 10
- 238000002485 combustion reaction Methods 0.000 claims description 9
- 239000000446 fuel Substances 0.000 claims description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 28
- 229910052750 molybdenum Inorganic materials 0.000 description 16
- 239000011733 molybdenum Substances 0.000 description 16
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 15
- 229910052742 iron Inorganic materials 0.000 description 13
- 238000005260 corrosion Methods 0.000 description 11
- 230000007797 corrosion Effects 0.000 description 11
- 229910000464 lead oxide Inorganic materials 0.000 description 11
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 10
- YEXPOXQUZXUXJW-UHFFFAOYSA-N oxolead Chemical compound [Pb]=O YEXPOXQUZXUXJW-UHFFFAOYSA-N 0.000 description 10
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 9
- 229910052804 chromium Inorganic materials 0.000 description 9
- 239000011651 chromium Substances 0.000 description 9
- 230000001590 oxidative effect Effects 0.000 description 9
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 9
- 229910052721 tungsten Inorganic materials 0.000 description 9
- 239000010937 tungsten Substances 0.000 description 9
- 229910052726 zirconium Inorganic materials 0.000 description 9
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 8
- 229910052791 calcium Inorganic materials 0.000 description 8
- 239000011575 calcium Substances 0.000 description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 7
- 229910052799 carbon Inorganic materials 0.000 description 7
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 6
- 229910052710 silicon Inorganic materials 0.000 description 6
- 239000010703 silicon Substances 0.000 description 6
- 229910018487 Ni—Cr Inorganic materials 0.000 description 2
- 239000000788 chromium alloy Substances 0.000 description 2
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910000623 nickel–chromium alloy Inorganic materials 0.000 description 2
- MRMOZBOQVYRSEM-UHFFFAOYSA-N tetraethyllead Chemical compound CC[Pb](CC)(CC)CC MRMOZBOQVYRSEM-UHFFFAOYSA-N 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 101100296544 Caenorhabditis elegans pbo-5 gene Proteins 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 229910000604 Ferrochrome Inorganic materials 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- PXHVJJICTQNCMI-LZFNBGRKSA-N nickel-65 Chemical compound [65Ni] PXHVJJICTQNCMI-LZFNBGRKSA-N 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000004576 sand Substances 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%
Definitions
- the present invention relates to alloys suitable for use at high temperatures in highly corrosive atmospheres such as are produced by lead oxide.
- the invention relates to a nickel base alloy containing molybdenum and which is suitable for facing valves and valve seats and has good weldability characteristics, high hot strength and corrosion resistance, and a wide tolerance for iron.
- nickel base alloys containing substantial proportions of chromium, together with smaller amounts of tungsten, are suitable for use under conditions where a corrosive deposit of lead oxide is present, as around-the exhaust ports of internal combustion engines utilizing fuels containing tetraethyl lead. Whilethe nickel-chromium alloys containing tungsten show good corrosion-resistance properties under oxidizingconditions where protective oxide films are formed, the corrosion resistance of these alloys decreases considerably when the oxygen content of the atmosphere is reduced to a point when the oxide films are not formed. Since exhaust gases are non-oxidizing, these known alloys are deficient for exhaust valve usage. A further disadvantage of this type of alloy is the fact that weldability characteristics are not particularly good, so that it is diflicult to puddle the alloy onto the face of the exhaust valve or other structural element which is to be used in the corrosive atmosphere.
- the present invention now provides an alloy containing molybdenum in place of tungsten which will withstand lead oxide corrosion in either non-oxidizing or oxidizing atmospheres, and especially in non-oxidizing atmospheres such ,as the exhaust gases of engines having leaded gasolines.
- the alloy of the present invention also hasexcellent welding characteristics imparted thereto by the incorporation of controlled amounts ofcalcium and zirconium. Further, this molybdenumcontaining nickel base alloy exhibits better hot hardness characteristics, especially in the higher carbon ranges, than the tungsten-containing alloy.
- an excellent corrosion-resistant alloy having good hardness properties at high temperatures may be prepared from a nickel-chromium base alloy containing relatively smaller proportions of molybdenum and capable of being appreciably idiluted-with'iron.
- the molybdenum content :of' such alloy compositions causes a, totally unexpected and remarkable increase in hothardness characteristics of the alloy, as compared with similaralloys' containing tungsten instead of molybdenum.
- molybdenum-containing alloys 4 have excellent lead oxide corrosionresistance. These characteristics are very pronouncedinnickel-chro- --mium-iron alloys which contain relatively high percentages ofcarbon in the rangefromabout 15%toabout'2.5%.
- a further advantage of the use of-molybdenum in place of tungsten in the above-mentioned type of alloy is the fact that the alloy exhibits a higher tolerance for iron than does the tungsten-containing material. Thus, a higher percentage of iron may be'included in the composition without decreasing the corrosion-resistance properties.
- the alloy compositions of the present invention preferably also contain specific small amounts of calcium and zirconium. Further, the silicon content of the alloy is carefully held below a definite maximum value. The presence of calcium and zirconium in minor specified concentrations controls the ..weldability of the product. Alloys of'this nature tend to give a gaseous weld, and this effect is substantially inhibited byv the addition of .certainminor proportions of calcium and zirconium. In this respect,.-it is also important to keep the silicon content as loW as possible, since silicon lowers the corrosion resistance of the alloy.
- the present alloys contain no cobalt. Y
- the latter element has been found to adversely affect the ability of nickel-chromium alloys to withstand-lead oxide corrosion.
- the alloys of the present invention have the following composition, the percentages being Percentages by weight:
- the alloys of this invention are especially useful in structural elements which, in use, are subject to high temperature, abrasion and wear in highly corrosive atmospheres such as are formed by burning leaded gasoline. These structural elements are preferably stabilized and hardened by heat treatment.
- each of the alloys contained from .001% to .06% calcium, from .001% to .06% zirconium, and less than .'75% silicon.
- the iron tolerance of the present alloys is of considerable importance in that various ferrochrome alloys may be used as the source of chromium and iron in the composition, thus decreasing the cost of the preparation of these alloys from that necessary where pure chromium metal is used.
- the corrosion resistance of the samples was measured in a standard lead oxide corrosion test the corrosive effects of lead oxide, especially at elevated temperatures.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Preventing Corrosion Or Incrustation Of Metals (AREA)
Description
Patented Apr. 11, 1950 "WELDABLE NICKEL BASE ALLOY :Robert T. Banistenschesterland, Ohio, assignor to Thompson Products, Inc 'Qleveland, Ohio,
a corporation of Ohio N Drawing, Application March-17, 1949, Serial No. 82,000
'2 Claims.
The present invention relates to alloys suitable for use at high temperatures in highly corrosive atmospheres such as are produced by lead oxide.
More particularly, the invention relates to a nickel base alloy containing molybdenum and which is suitable for facing valves and valve seats and has good weldability characteristics, high hot strength and corrosion resistance, and a wide tolerance for iron.
It has previously beensuggested that certain nickel base alloys, containing substantial proportions of chromium, together with smaller amounts of tungsten, are suitable for use under conditions where a corrosive deposit of lead oxide is present, as around-the exhaust ports of internal combustion engines utilizing fuels containing tetraethyl lead. Whilethe nickel-chromium alloys containing tungsten show good corrosion-resistance properties under oxidizingconditions where protective oxide films are formed, the corrosion resistance of these alloys decreases considerably when the oxygen content of the atmosphere is reduced to a point when the oxide films are not formed. Since exhaust gases are non-oxidizing, these known alloys are deficient for exhaust valve usage. A further disadvantage of this type of alloy is the fact that weldability characteristics are not particularly good, so that it is diflicult to puddle the alloy onto the face of the exhaust valve or other structural element which is to be used in the corrosive atmosphere.
The present invention now provides an alloy containing molybdenum in place of tungsten which will withstand lead oxide corrosion in either non-oxidizing or oxidizing atmospheres, and especially in non-oxidizing atmospheres such ,as the exhaust gases of engines having leaded gasolines. The alloy of the present invention also hasexcellent welding characteristics imparted thereto by the incorporation of controlled amounts ofcalcium and zirconium. Further, this molybdenumcontaining nickel base alloy exhibits better hot hardness characteristics, especially in the higher carbon ranges, than the tungsten-containing alloy.
It is therefore an object of the present invention to provide an alloy which has the ability to withstand the deleterious effects of lead oxide corrosion in non-oxidizing atmospheres and which exhibits good hardness properties at ele-.
pro ide a n ke ase a l n ain n sub n a un s o r m mand m d num and, c
taming minor amounts of calcium and zirconium to impart good weldability characteristics thereto and to increase the corrosion-resistance properties thereof.
1 have now discovered that an excellent corrosion-resistant alloy having good hardness properties at high temperatures may be prepared from a nickel-chromium base alloy containing relatively smaller proportions of molybdenum and capable of being appreciably idiluted-with'iron. The molybdenum content :of' such alloy compositions causes a, totally unexpected and remarkable increase in hothardness characteristics of the alloy, as compared with similaralloys' containing tungsten instead of molybdenum. In addition, such molybdenum-containing alloys 4 have excellent lead oxide corrosionresistance. These characteristics are very pronouncedinnickel-chro- --mium-iron alloys which contain relatively high percentages ofcarbon in the rangefromabout 15%toabout'2.5%.
A further advantage of the use of-molybdenum in place of tungsten in the above-mentioned type of alloy is the fact that the alloy exhibits a higher tolerance for iron than does the tungsten-containing material. Thus, a higher percentage of iron may be'included in the composition without decreasing the corrosion-resistance properties.
In addition to the chromium, nickel, molybdenum, carbon and iron, the alloy compositions of the present invention preferably also contain specific small amounts of calcium and zirconium. Further, the silicon content of the alloy is carefully held below a definite maximum value. The presence of calcium and zirconium in minor specified concentrations controls the ..weldability of the product. Alloys of'this nature tend to give a gaseous weld, and this effect is substantially inhibited byv the addition of .certainminor proportions of calcium and zirconium. In this respect,.-it is also important to keep the silicon content as loW as possible, since silicon lowers the corrosion resistance of the alloy.
In addition, the present alloys contain no cobalt. Y The latter element has been found to adversely affect the ability of nickel-chromium alloys to withstand-lead oxide corrosion.
The alloys of the present invention have the following composition, the percentages being Percentages by weight:
Per cent Nickel -65 Chromium 20-30 Molybdenum 6-15 Carb n ,--.-,----.sl m An especially preferred alloy within the above range is the following:
Per cent Nickel 53 Chromium 25 Molybdenum 9 Carbon 1.75 Calcium .03 maximum Zirconium .03 maximum Iron 10.5
of preferential oxides of molybdenum and chromium which protect the surfaces of the body against further oxidation.
The alloys of this invention are especially useful in structural elements which, in use, are subject to high temperature, abrasion and wear in highly corrosive atmospheres such as are formed by burning leaded gasoline. These structural elements are preferably stabilized and hardened by heat treatment.
The following table illustrates the distinct advantages of using molybdenum in place of tungsten in nickel-chromium base alloy compositions. In addition to the elements listed in the analyses below, each of the alloys contained from .001% to .06% calcium, from .001% to .06% zirconium, and less than .'75% silicon.
4 wherein the alloys are packed in lead oxide and heated for one hour at 1675 F., both in air and in a non-oxidizing atmosphere.
The above results clearly indicate that the molybdenum-containing alloys of the present invention are superior generally to those containing tungsten with respect to their ability to withstand corrosion by lead oxide and also with respect to their hardness at elevated temperatures. The efiect is very apparent at relatively high carbon contents, above about 1.5% carbon.
To show the exceptional tolerance for iron dilution possessed by the alloys of this invention, a heat was prepared containing 25% chromium, 53% nickel, 9% molybdenum, 1.75% carbon, .02% calcium, .02% zirconium, 50% silicon, and 10.5% iron. This alloy showed a lead oxide corrosion loss of 4.7 grams per square decimeter in air and 4.2 grams in a non-oxidizing atmosphere. The Brinell hardness number at room temperature was 331, and at 1400 F. the hardness number was 255. This heat compared very favorably to heat I above, which contained only 3.5% iron. The welding characteristics of the alloy containing 10.5% iron were found to be excellent.
The iron tolerance of the present alloys is of considerable importance in that various ferrochrome alloys may be used as the source of chromium and iron in the composition, thus decreasing the cost of the preparation of these alloys from that necessary where pure chromium metal is used.
From the foregoing, it will be apparent that I have herein provided alloy compositions which are especially adapted for use in structural elements which must be capable of withstanding Pbo 5 12 Brinell Hardg /Sq ness No. Melt No. Or N1 M0 0 Fe Non- In Room oxidizing 1400 F. Au- Atmosphere Temp Pbo fg Brinell Hardg [Sq ness No. Me]
Na 01' N1 W 0 Fe Non- I Room oxidizing 1400 F. Atmosphere Temp Each of the samples was sand cast, stabilized at 1650 F. for one hour, heat-treated at 1400 F. for about twenty-four hours, and thereafter air-cooled.
The corrosion resistance of the samples was measured in a standard lead oxide corrosion test the corrosive effects of lead oxide, especially at elevated temperatures.
I claim as my invention:
1. A readily weldable nickel-base alloy adapted to withstand the combustion of a leaded fuel in a combustion engine and suitable for use in exhaust valves for internal combustion engines, having the following composition by weight:
Per cent Chromium 20-30 Nickel 45-65 Molybdenum 6-15 Carbon 1.5-2.5 Calcium .001.06 Zirconium .001.06 Silicon Less than 0.75 Iron Balance 2. A readily weldable nickel base alloy adapted to withstand the combustion of a leaded fuel in a combustion engine and suitable for use as valve facing material, having the following composition by weight:
Per cent Chromium 25 Nickel 53 Molybdenum 9 The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,540,928 Clement June 9, 1925 1,572,996 Girin -1 Feb. 16, 1926 2,019,687 Lohr 1 Nov. 5, 1935 2,299,871 Baird Oct. 27, 1942 2,392,821 Kreag Jan. 15, 1946 2,400,255 Pfeil May 14, 1946
Claims (1)
1. A READILY WELDABLE NICKEL-BASE ALLOY ADAPTED TO WITHSTAND THE COMBUSTION OF A LEADED FUEL IN A COMBUSTION ENGINE AND SUITABLE FOR USE IN EXHAUST VALVES FOR INTERNAL COMBUSTION ENGINES, HAVING THE FOLLOWING COMPOSITION BY WEIGHT:
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US82000A US2503608A (en) | 1949-03-17 | 1949-03-17 | Weldable nickel base alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US82000A US2503608A (en) | 1949-03-17 | 1949-03-17 | Weldable nickel base alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2503608A true US2503608A (en) | 1950-04-11 |
Family
ID=22167765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US82000A Expired - Lifetime US2503608A (en) | 1949-03-17 | 1949-03-17 | Weldable nickel base alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2503608A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2703277A (en) * | 1952-06-12 | 1955-03-01 | Union Carbide & Carbon Corp | Nickel-base alloy for high temperature service |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1540928A (en) * | 1917-12-17 | 1925-06-09 | William H Smith | Acid-resisting alloy |
| US1572996A (en) * | 1920-12-09 | 1926-02-16 | Commentry Fourchambault & Deca | Alloy |
| US2019687A (en) * | 1935-06-14 | 1935-11-05 | Driver Harris Co | Alloy |
| US2299871A (en) * | 1941-03-31 | 1942-10-27 | Crobalt Inc | Cutting metal alloy |
| US2392821A (en) * | 1944-01-22 | 1946-01-15 | Haynes Sellite Company | Metal-working tool |
| US2400255A (en) * | 1941-05-27 | 1946-05-14 | Int Nickel Co | Electric resistance elements and the like |
-
1949
- 1949-03-17 US US82000A patent/US2503608A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1540928A (en) * | 1917-12-17 | 1925-06-09 | William H Smith | Acid-resisting alloy |
| US1572996A (en) * | 1920-12-09 | 1926-02-16 | Commentry Fourchambault & Deca | Alloy |
| US2019687A (en) * | 1935-06-14 | 1935-11-05 | Driver Harris Co | Alloy |
| US2299871A (en) * | 1941-03-31 | 1942-10-27 | Crobalt Inc | Cutting metal alloy |
| US2400255A (en) * | 1941-05-27 | 1946-05-14 | Int Nickel Co | Electric resistance elements and the like |
| US2392821A (en) * | 1944-01-22 | 1946-01-15 | Haynes Sellite Company | Metal-working tool |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2703277A (en) * | 1952-06-12 | 1955-03-01 | Union Carbide & Carbon Corp | Nickel-base alloy for high temperature service |
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