US1483298A - Alloy comprising iron, nickel, chromium, molybdenum - Google Patents
Alloy comprising iron, nickel, chromium, molybdenum Download PDFInfo
- Publication number
- US1483298A US1483298A US535044A US53504422A US1483298A US 1483298 A US1483298 A US 1483298A US 535044 A US535044 A US 535044A US 53504422 A US53504422 A US 53504422A US 1483298 A US1483298 A US 1483298A
- Authority
- US
- United States
- Prior art keywords
- alloy
- nickel
- iron
- chromium
- molybdenum
- 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
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 title description 6
- 229910045601 alloy Inorganic materials 0.000 title description 6
- 239000000956 alloy Substances 0.000 title description 6
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 title description 4
- 239000011651 chromium Substances 0.000 title description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 title description 3
- 229910052804 chromium Inorganic materials 0.000 title description 3
- 229910052742 iron Inorganic materials 0.000 title description 3
- 239000011733 molybdenum Substances 0.000 title description 3
- 229910052759 nickel Inorganic materials 0.000 title description 3
- 229910052750 molybdenum Inorganic materials 0.000 title description 2
- 239000007789 gas Substances 0.000 description 5
- 239000000126 substance Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910000640 Fe alloy Inorganic materials 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- -1 60 to 70 er cent Chemical compound 0.000 description 1
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 229910000599 Cr alloy Inorganic materials 0.000 description 1
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 1
- 229910000997 High-speed steel Inorganic materials 0.000 description 1
- 229910001182 Mo alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 239000013043 chemical agent Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000008034 disappearance Effects 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- PXHVJJICTQNCMI-OUBTZVSYSA-N nickel-60 atom Chemical compound [60Ni] PXHVJJICTQNCMI-OUBTZVSYSA-N 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten 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
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
Definitions
- France have invented new and useful is ralsed from 400 to 500 C. and the hard 'ness conferred by a suitable tempering disappears at the same time as the reheating annuls the action of the treatment.
- the high speed steels certainly preserve their hardness at a temperature higher than the other steels, and after they have been tempered possess a high resistance, even up to a red heat, but besides the drawbacks 2 which result from their fragility and difficulties of a practical nature due to the extremely high temperature of their treatment, they do not present the desired stability when the temperature exceeds 600; in fact, not 30 only an accidental excess of temperature beyond the regulated value, but even prolonged ex osure to this temperature produce a gradua disappearance of the initial hardness and a progressive diminution of resistance. Fi- 5 nally, they are very oxidizable.
- the present application which is a divi- 4 sion of my apphcation, Serial No. 265,985, filed December 9, 1918, concerns an alloy of iron, nickel, chromium and molybdenum, and including, perhaps, tungsten or vanadium, cobalt and titanium, easy to obtain in large quantities and capable of being moulded, or otherwise, forged, rolled, wire drawn, worked, without difliculty, possessing at the tem erature of 800 a resistance almost equivalent to that of cold iron, non-fragile,
- the alloy may contain, for example:
- compositions may fer on the alloy of iron and nickel a very high resistance when heated: I can obtain easily 25 to 35 kgs. per sq. mm. with an elastic limit of 20 to 30 kgs. and a coeflicient of elongation of 40 per cent at a temperature of 800, while still preserving a total absence of fragility. These additional elements also render the alloy extremely resistant to the attack of acid vapours, as well as of hot oxidizing and moist gases.
- This alloy is certainly very suitable for the manufacture of gas turbines or for receptacles, employed in chemical industry, for reactions which take place at high temperathre and at high pressure and which produce corrosive gases or other substances.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Testing Resistance To Weather, Investigating Materials By Mechanical Methods (AREA)
Description
Patented Feb. 12, 1924.
UNITED STATES PATENT OFFICE.
PIERRE GIRIN, OF PARIS, FRANCE, ASSIGNOR TO SOCIETEANONYME DE COMMENTRY, FOURCHAMBAULT & DECAZEVILLE, OF PARIS, FRANCE.
ALLOY COMPRISING IRON, NICKEL, CHROMIUM, MOLYBDENUM.
No Drawing. Original application filed December 9, 1918, Serial No. 265,985. Divided and this application filed February 8,
To all whom it may concern:
Be it known that I, PIERRE GIRIN, a citi-' zen of France, and a resident of Paris,
France, have invented new and useful is ralsed from 400 to 500 C. and the hard 'ness conferred by a suitable tempering disappears at the same time as the reheating annuls the action of the treatment.
The high speed steels certainly preserve their hardness at a temperature higher than the other steels, and after they have been tempered possess a high resistance, even up to a red heat, but besides the drawbacks 2 which result from their fragility and difficulties of a practical nature due to the extremely high temperature of their treatment, they do not present the desired stability when the temperature exceeds 600; in fact, not 30 only an accidental excess of temperature beyond the regulated value, but even prolonged ex osure to this temperature produce a gradua disappearance of the initial hardness and a progressive diminution of resistance. Fi- 5 nally, they are very oxidizable.
In addition, the invention of gas motors, gas turbines and other thermal machines intended to act above the temperature of red heat, and the discovery of chemical synthetic 60 processes using at the same time high temperatures and high pressures, render the realization of a metal possessing certain qualities at' high temperature extremely desirable.
The present application, which is a divi- 4 sion of my apphcation, Serial No. 265,985, filed December 9, 1918, concerns an alloy of iron, nickel, chromium and molybdenum, and including, perhaps, tungsten or vanadium, cobalt and titanium, easy to obtain in large quantities and capable of being moulded, or otherwise, forged, rolled, wire drawn, worked, without difliculty, possessing at the tem erature of 800 a resistance almost equivalent to that of cold iron, non-fragile,
1922. Serial No. 535,044.
practically inoxidizable at high temperatures, even in a very oxidizing temperature, and at the same time possessing properties which are strictly reversible; by this term I understand that the properties at. a given temperature depend solely on that temperature and in no way on the preceding temperatures that havebeen obtained, nor on an exposure more or less long to the temperature used. The alloy may contain, for example:
Per cent. Nickel 60 to 70 Chromium 10 to Molybdenum 1 to 3 Manganese 1 to 2 Carbon 0.3 to 0.6
Iron forming the remainder.
Certain variations in the composition may fer on the alloy of iron and nickel a very high resistance when heated: I can obtain easily 25 to 35 kgs. per sq. mm. with an elastic limit of 20 to 30 kgs. and a coeflicient of elongation of 40 per cent at a temperature of 800, while still preserving a total absence of fragility. These additional elements also render the alloy extremely resistant to the attack of acid vapours, as well as of hot oxidizing and moist gases. This chemical unalterability is of the greatest importance for all applications, since it not only ensures the metal against corrosion, but also ensures the preservation of the initial mechanical properties, in contra-distinction to that whichtakes place with carbon steels which, when heated for a long time in an atmosphere rich in hydrogen, finally become decarburized and lose their solidity.
This alloy is certainly very suitable for the manufacture of gas turbines or for receptacles, employed in chemical industry, for reactions which take place at high temperathre and at high pressure and which produce corrosive gases or other substances.
Having thus described the nature of the said inventionand the best means I know of a carrying the same into practical vefiect, I
claim:
A high nickel ferrous alloy containing nickel, 60 to 70 er cent, chromium, 10 to 15 per cent, molyb enum, 1 to 3 per cent, manganese 1 t0 2 per cent and carbon, 0.3 to 0.6 per cent, such alloy having at elevated temperatures great mechanical resistance to chemical agents and susceptible of retaining indefinitely its initial properties, notwithstanding prolonged service.
In testimony whereof I have signed this specification.
PIERRE GIRIN.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US535044A US1483298A (en) | 1918-12-09 | 1922-02-08 | Alloy comprising iron, nickel, chromium, molybdenum |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US265985A US1504338A (en) | 1918-12-09 | 1918-12-09 | Alloy comprising iron, nickel, chromium, tungsten, or molybdenum |
| US535044A US1483298A (en) | 1918-12-09 | 1922-02-08 | Alloy comprising iron, nickel, chromium, molybdenum |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1483298A true US1483298A (en) | 1924-02-12 |
Family
ID=26951535
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US535044A Expired - Lifetime US1483298A (en) | 1918-12-09 | 1922-02-08 | Alloy comprising iron, nickel, chromium, molybdenum |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1483298A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2471476A (en) * | 1945-01-20 | 1949-05-31 | Kinetic Chemicals Inc | Process and apparatus for transmitting energy |
| US3223818A (en) * | 1961-04-27 | 1965-12-14 | Smith Corp A O | Method of welding |
| US5092737A (en) * | 1989-02-10 | 1992-03-03 | Rolls-Royce Plc | Blade tip clearance control arrangement for a gas turbine |
-
1922
- 1922-02-08 US US535044A patent/US1483298A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2471476A (en) * | 1945-01-20 | 1949-05-31 | Kinetic Chemicals Inc | Process and apparatus for transmitting energy |
| US3223818A (en) * | 1961-04-27 | 1965-12-14 | Smith Corp A O | Method of welding |
| US5092737A (en) * | 1989-02-10 | 1992-03-03 | Rolls-Royce Plc | Blade tip clearance control arrangement for a gas turbine |
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