US1572996A - Alloy - Google Patents
Alloy Download PDFInfo
- Publication number
- US1572996A US1572996A US429544A US42954420A US1572996A US 1572996 A US1572996 A US 1572996A US 429544 A US429544 A US 429544A US 42954420 A US42954420 A US 42954420A US 1572996 A US1572996 A US 1572996A
- Authority
- US
- United States
- Prior art keywords
- per cent
- alloy
- tungsten
- chromium
- manganese
- 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 15
- 239000000956 alloy Substances 0.000 title description 15
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 239000011651 chromium Substances 0.000 description 8
- 239000011572 manganese Substances 0.000 description 8
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 8
- 239000010937 tungsten Substances 0.000 description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 7
- 229910052748 manganese Inorganic materials 0.000 description 7
- 229910052721 tungsten Inorganic materials 0.000 description 7
- 229910052804 chromium Inorganic materials 0.000 description 6
- 229910052759 nickel Inorganic materials 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
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 229910017052 cobalt Inorganic materials 0.000 description 3
- 239000010941 cobalt Substances 0.000 description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 229910052720 vanadium Inorganic materials 0.000 description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 3
- QGZKDVFQNNGYKY-UHFFFAOYSA-N Ammonia Chemical compound N QGZKDVFQNNGYKY-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000003786 synthesis reaction Methods 0.000 description 2
- 239000010936 titanium Substances 0.000 description 2
- 229910052719 titanium Inorganic materials 0.000 description 2
- 101100087530 Caenorhabditis elegans rom-1 gene Proteins 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- 229910000640 Fe alloy Inorganic materials 0.000 description 1
- 101100305983 Mus musculus Rom1 gene Proteins 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910001080 W alloy Inorganic materials 0.000 description 1
- 229910021529 ammonia Inorganic materials 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- WHHGLZMJPXIBIX-UHFFFAOYSA-N decabromodiphenyl ether Chemical compound BrC1=C(Br)C(Br)=C(Br)C(Br)=C1OC1=C(Br)C(Br)=C(Br)C(Br)=C1Br WHHGLZMJPXIBIX-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- PSGAAPLEWMOORI-PEINSRQWSA-N medroxyprogesterone acetate Chemical compound C([C@@]12C)CC(=O)C=C1[C@@H](C)C[C@@H]1[C@@H]2CC[C@]2(C)[C@@](OC(C)=O)(C(C)=O)CC[C@H]21 PSGAAPLEWMOORI-PEINSRQWSA-N 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance 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
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
Definitions
- This invention has for object improvements in the alloy resisting oxidationwhich is described in my application filed Dec. 9, 1918, Ser. No. 265,985, primarily with a view of adapting the alloy to the particular conditions which are necessitated by manufacture on a large scale in a metallurgical appa ratus such as the Martin furnace. end the limiting content of carbon and manganese originally prescribed has been extended and according to this invention the carbon may -be carried to 1 per cent, and the manganese to 5 per cent.
- the alloy retains its specific properties when the llmiting content of nickel and chromium is more extended than that prescribed in the said ap plication.
- the proportions fixed in the said application were to 70 per cent; by the present invention they may be 50 to 80 per cent; for the chromium, instead of 10 to 15 per cent, the proportions may be 8 to 25 per cent.
- the proportions of tungsten and molybdenum. may be lowered respectively to 0.5 per cent and 0.2 er cent so as to increase notably the capacity for being forged, without. which the alloy ceases to possess the properties indicated.
- the alloy which is thebasis of the pres ent invention contains essentially iron, a.
- the typical alloy comprises: 1
- the maximum content for manganese and minimum and maximum for nickel and chromium are carried respectively to 5 per cent, 50 per cent, and 80 per cent, and 8 per cent,
- composition there are certain-modifications of composition. possible without bringing about important modifications of quality; thus for 0.5 to 8 per cent of tungsten may be substituted 0.2 to 5 per cent of molybdenum, or
- these two metals may be'added together, sayto the extent of 0.2 to 8 per cent, of the total.
- This extension of content in tungsten and molybdenum over that indicated in the aforesaid application is owing to the experience that these metals are eflicient even in small proportion for imparting resistance to corrosion.
- the properties may be further improved,
- the alloy in which have a mean value may have a tensile strength the various elements of to kilos per square mm. with an elastic limit of 20 to 30 kilos and a coefficient .of elongation 'of 40 percent at a temperature of 800 0., the values indicated in the aforesaid application, while being totally devoid of brittleness.
- the content of tungsten or molybdenum or their mixture falls to the neighbourhood of'the lower limit indicated, the facility with which thcalloy can-be forged is notably.
- That alloy of iron, chromium, nickel, tungsten and manganese comprising nickel to 80 percent, chromium 8 to 25 percent,
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
Patented Feb.l6, 19 26 .5
UNITED STATES PA'l'E-NT OFFICE 2mm exam, on runs, amen, ASSIGNOR 'ro socm'rfi AnonYmE on oouiunmnx. rounoumnnuw & DECA'ZEVILLE, or PARIS, FRANCE.
ALLOY.
No Drawing.
; '84 Rue de Lille, Paris, Seine,-France, have application or as described herein; these 3 molybdenum, cobalt, vanadium and tita-.
invented new and useful Improvements in Alloys, which is fully set forth in the fol:
lowing specification. I
This invention has for object improvements in the alloy resisting oxidationwhich is described in my application filed Dec. 9, 1918, Ser. No. 265,985, primarily with a view of adapting the alloy to the particular conditions which are necessitated by manufacture on a large scale in a metallurgical appa ratus such as the Martin furnace. end the limiting content of carbon and manganese originally prescribed has been extended and according to this invention the carbon may -be carried to 1 per cent, and the manganese to 5 per cent.
Moreover, it has now been found, as the result of new experiments, that the alloy retains its specific properties when the llmiting content of nickel and chromium is more extended than that prescribed in the said ap plication. For the nickel the proportions fixed in the said application were to 70 per cent; by the present invention they may be 50 to 80 per cent; for the chromium, instead of 10 to 15 per cent, the proportions may be 8 to 25 per cent. Soalso, the proportions of tungsten and molybdenum.may be lowered respectively to 0.5 per cent and 0.2 er cent so as to increase notably the capacity for being forged, without. which the alloy ceases to possess the properties indicated. I
It has further been found that these alloys 'havea certain number of-industrial applications, whether made as described in the said have not been mentioned in the said application.
The alloy which is thebasis of the pres ent invention contains essentially iron, a.
high content of nickel, chromium, tungsten, manganese. It may include as accessories nium. It is easy to make in large uantities and is adapted tobe cast, forge rolled,
To this Application filed. December 9, 1920. Serial No. 429,544.
drawn and worked. 'The typical alloy comprises: 1
. Per cent.
, Nickel 50 to 80 Chromium 8 to 25 Tungsten 0.5 to 8 Manganese 1 to 5 Carbon 0.3 to 1 Iron The rest Example of composition: Ni: 65, Cr: 12, W: 1.5, Mn: 3, C: 0.5, iron: the rest.
. The maximum content for manganese and minimum and maximum for nickel and chromium are carried respectively to 5 per cent, 50 per cent, and 80 per cent, and 8 per cent,
and 25 per cent, in order to agree with the necessities of working, the yields and the nature of the added materials used in the Martin furnace. The presence of the manganese is-essential to ensure perfect homogeneity of the metal .as well as a satisfactory capacity for forging.
There are certain-modifications of composition. possible without bringing about important modifications of quality; thus for 0.5 to 8 per cent of tungsten may be substituted 0.2 to 5 per cent of molybdenum, or
these two metals may be'added together, sayto the extent of 0.2 to 8 per cent, of the total. This extension of content in tungsten and molybdenum over that indicated in the aforesaid application is owing to the experience that these metals are eflicient even in small proportion for imparting resistance to corrosion.
The properties may be further improved,
while facilitating the manufacture, by adding to the alloy above defined 0.2 to 1 per cent of vanadium, or 0.1 to 0.2 per cent of titanium, or 0.1 to 1 per cent of a mixture of vanadium and titanium. So also 0 to 10 per cent of cobalt may be added with a view.
of improving the mechanical strength of the alloy. The proportions of. the added elements indicated are added at. the cost of the content of iron.
The alloy in which have a mean value, such as the example indicated above, may have a tensile strength the various elements of to kilos per square mm. with an elastic limit of 20 to 30 kilos and a coefficient .of elongation 'of 40 percent at a temperature of 800 0., the values indicated in the aforesaid application, while being totally devoid of brittleness. When the content of tungsten or molybdenum or their mixture falls to the neighbourhood of'the lower limit indicated, the facility with which thcalloy can-be forged is notably.
increased, in the sense that this operation may be'performed, with less precaution and within the limits of temperature more extended; on the contrary, the fi ures indicated for the tensile strength an "the elastic limit at 800 0., while being incomparably higher than those of all steels or special alloys, are susceptible to a diminution of 5 to 10 kilos or square mm. respectively without sensi ly modifying the coefiicient of elongation.
i The following are industrial applicationsof the alloys forming the subject matter of the aforesaid application and .of' this invention: a
, Manufacture of apparatus used in chemical industry for synthetic reactions; in particular those used for the synthesis of ammonia (notably when these apparatus prising also rom 1 to 10 claves for synthesis, for chemical reactions,
at high temperatures, suc as or recuperation of'heat, burner nozzles, in-
jector nozzles ogerating in a su erheated surrounding, or ifiusing ,or liquids of corrosive km Having thus. described the nature of the said invention and the best means I know of carrying the same into practical effect, I-cl-aim: u
1. That alloy of iron, chromium, nickel, tungsten and manganesecomprising nickel to 80 percent, chromium 8 to 25 percent,
tungsten 0.5 to 8 percent, manganese 1 '5 percent, and carbon 0.3 to 1 percent.-
2. An allo as set forth in claim 1 comrcent of cobalt. have signed this PIERRE GIRIN.
' In testimony whereof specification.
gases. an VEPOHIS'
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US429544A US1572996A (en) | 1920-12-09 | 1920-12-09 | Alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US429544A US1572996A (en) | 1920-12-09 | 1920-12-09 | Alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1572996A true US1572996A (en) | 1926-02-16 |
Family
ID=23703712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US429544A Expired - Lifetime US1572996A (en) | 1920-12-09 | 1920-12-09 | Alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1572996A (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2458502A (en) * | 1944-06-30 | 1949-01-11 | Coast Metals Inc | Structural element for high temperature service use |
| US2475642A (en) * | 1944-09-29 | 1949-07-12 | Westinghouse Electric Corp | Mechanical element which is to be subjected to high temperatures |
| US2503608A (en) * | 1949-03-17 | 1950-04-11 | Thompson Prod Inc | Weldable nickel base alloy |
| US2540107A (en) * | 1946-09-04 | 1951-02-06 | Blaw Knox Co | High-temperature alloys |
| US2631095A (en) * | 1950-02-21 | 1953-03-10 | Cons Car Heating Co Inc | Alloy adapted for prosthetic articles |
| US2661285A (en) * | 1950-02-25 | 1953-12-01 | Gorschalki Max | Nonferrous alloy |
| US2681276A (en) * | 1950-07-20 | 1954-06-15 | Esterbrook Pen Co | Pen nib alloy |
| US2747993A (en) * | 1951-12-26 | 1956-05-29 | Gen Electric | High temperature nickel-base alloy |
| US2783144A (en) * | 1954-12-15 | 1957-02-26 | Crucible Steel Company | Hard facing alloy |
| US2958598A (en) * | 1957-01-18 | 1960-11-01 | Int Nickel Co | Sparking plug electrodes |
| US3607250A (en) * | 1970-01-12 | 1971-09-21 | Blaw Knox | High-temperature alloys and articles |
| US4331741A (en) * | 1979-05-21 | 1982-05-25 | The International Nickel Co., Inc. | Nickel-base hard facing alloy |
-
1920
- 1920-12-09 US US429544A patent/US1572996A/en not_active Expired - Lifetime
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2458502A (en) * | 1944-06-30 | 1949-01-11 | Coast Metals Inc | Structural element for high temperature service use |
| US2475642A (en) * | 1944-09-29 | 1949-07-12 | Westinghouse Electric Corp | Mechanical element which is to be subjected to high temperatures |
| US2540107A (en) * | 1946-09-04 | 1951-02-06 | Blaw Knox Co | High-temperature alloys |
| US2503608A (en) * | 1949-03-17 | 1950-04-11 | Thompson Prod Inc | Weldable nickel base alloy |
| US2631095A (en) * | 1950-02-21 | 1953-03-10 | Cons Car Heating Co Inc | Alloy adapted for prosthetic articles |
| US2661285A (en) * | 1950-02-25 | 1953-12-01 | Gorschalki Max | Nonferrous alloy |
| US2681276A (en) * | 1950-07-20 | 1954-06-15 | Esterbrook Pen Co | Pen nib alloy |
| US2747993A (en) * | 1951-12-26 | 1956-05-29 | Gen Electric | High temperature nickel-base alloy |
| US2783144A (en) * | 1954-12-15 | 1957-02-26 | Crucible Steel Company | Hard facing alloy |
| US2958598A (en) * | 1957-01-18 | 1960-11-01 | Int Nickel Co | Sparking plug electrodes |
| US3607250A (en) * | 1970-01-12 | 1971-09-21 | Blaw Knox | High-temperature alloys and articles |
| US4331741A (en) * | 1979-05-21 | 1982-05-25 | The International Nickel Co., Inc. | Nickel-base hard facing alloy |
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