US2402814A - Alloy steel - Google Patents
Alloy steel Download PDFInfo
- Publication number
- US2402814A US2402814A US437912A US43791242A US2402814A US 2402814 A US2402814 A US 2402814A US 437912 A US437912 A US 437912A US 43791242 A US43791242 A US 43791242A US 2402814 A US2402814 A US 2402814A
- Authority
- US
- United States
- Prior art keywords
- alloy steel
- temperatures
- titanium
- remainder
- 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
- 229910000851 Alloy steel Inorganic materials 0.000 title description 12
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 17
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 17
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 9
- 239000011651 chromium Substances 0.000 description 9
- 239000000470 constituent Substances 0.000 description 9
- 239000010949 copper Substances 0.000 description 9
- 229910052719 titanium Inorganic materials 0.000 description 9
- 239000010936 titanium Substances 0.000 description 9
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 8
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 8
- 229910052799 carbon Inorganic materials 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 8
- 229910052802 copper Inorganic materials 0.000 description 8
- 229910052742 iron Inorganic materials 0.000 description 8
- 229910052750 molybdenum Inorganic materials 0.000 description 8
- 239000011733 molybdenum Substances 0.000 description 8
- 229910052759 nickel Inorganic materials 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 229910052748 manganese Inorganic materials 0.000 description 4
- 239000011572 manganese Substances 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 239000013043 chemical agent Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
Definitions
- This invention relates to alloy steel and an important object is to provide an alloy steel adapted for the manufacture of mechanical parts which are to operate under stress at temperatures up to 800 C. and require to have high creep resistance under such working conditions.
- the term mechanical parts is to be regarded as comprehensive and includes such objects as power plant, components or units thereof, and apparatus generally intended for operation in a range of temperature extending up to 800 C., and subjected during such operation to considerable stress.
- the invention is based on the discovery that alloy steels containing carbon, nickel, chromium, molybdenum, copper and titanium in certain critical percentages possess creep resistance values, at temperatures up to 800 C., which have hitherto been regarded as unattainable.
- composition is as follows:
- the alloy may also contain silicon up to 2%, manganese up to 2% and vanadium up to 1%.
- the steel of this example possesses abnormally high creep resistance at elevated temperatures and is therefore essentially suitable for use in the manufacture according to the invention.
- the iabrication oi apparatus required to operate under stress at high temperatures that is up to 800 C., from an alloy steel comprising carbon up to 1.5%, nickel 15-25%, chromium 12- 4 20%, molybdenum 24%, copper 24%, titanium 0.25-2% and the remainder iron.
- a mechanical part required to operate under stress at high temperatures that is, up to 800 C., and having high creep resistance under such conditions, said part consisting oi alloy steel comprising carbon up to 1.5%, nickel 15-25%, chromium 12-20%, molybdenum 2-6%, copper 2-6%, titanium 0.25-2% and the remainder iron.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Description
Patented June 25, 1946 ALLOY STEEL William Herbert Hatfield, Shemeld, England, assignor to Firth-Vickers Stainless Steels Limited, Shemeld, England, a British company No Drawing. Application April 6, 1942, Serial No. 437,912. In Great Britain April 7, 1941 This invention relates to alloy steel and an important object is to provide an alloy steel adapted for the manufacture of mechanical parts which are to operate under stress at temperatures up to 800 C. and require to have high creep resistance under such working conditions. The term mechanical parts" is to be regarded as comprehensive and includes such objects as power plant, components or units thereof, and apparatus generally intended for operation in a range of temperature extending up to 800 C., and subjected during such operation to considerable stress.
The invention is based on the discovery that alloy steels containing carbon, nickel, chromium, molybdenum, copper and titanium in certain critical percentages possess creep resistance values, at temperatures up to 800 C., which have hitherto been regarded as unattainable.
Alloy steels containing the constituents above recited, but with much wider ranges prescribed for the permissible percentages of such constituents have been claimed to possess resistance to acids and other chemical agents and also to oxidation, scaling and corrosion at high temperatures, but it will be appreciated that the property of resistance to corrosion and scaling is by no means allied to, or to be confused with, resistance to creep.
According to this invention mechanical parts required for operation at temperatures up to 800 C., whilst subjected to considerable stress, are manufactured from steels lying within the following range of composition:
this characteristic which is essential to the invention it is to be emphasized that the above limits of proportion of the several constituents of the alloy are critical. Furthermore, importance is to be attached to the inclusion of titanium as an essential constituent.
The preferred range of composition is as follows:
Per cent C Up to 0.3 Ni 16.0 to 18.0 Cr 12.0 to 16.0 Mo 3.0 to 4.5 Cu 3.0 to 4.5 TL 0.25 to 1.0
' Fe Remainder 8 Claims. (Cl. 75-125) The alloy may also contain silicon up to 2%, manganese up to 2% and vanadium up to 1%.
Example Time yield 400 0. 500 0. 600 0. 700 0. 8G? C.
Tons/sq. in 18. 5 l5 0. 5 2
From the above figures it will be seen that the steel of this example possesses abnormally high creep resistance at elevated temperatures and is therefore essentially suitable for use in the manufacture according to the invention.
I claim:
1. Alloy steel possessing high creep resistance when applied for the manufacture of mechanical parts to be operated under stress at temperatures up to 800 0., comprising the following constituents and critical percentages: Carbon up to 1.5%, nickel 15.0 to 25.0%, chromium 12.0 to 20.0%, molybdenum 2.0 to 6.0%, copper 2.0 to 6.0%, titanium 0.25 to 2.0% and iron the remainder.
2. Alloy steel possessing high creep resistance when applied for the manufacture of mechanical parts to be operated under stress at temperatures up to 800 0., comprising the following constituents and critical percentages: carbon up to 0.3%, nickel 16.0 to 18.0%, chromium 12.0 to 16.0%, molybdenum 3.0 to 4.5%, copper 3.0 to 4.5%, titanium 0.25 to 1.0%, and iron the remainder.
3. Alloy steel possessing high creep resistance when applied for the manufacture of mechanical parts to be operated under stress at temperatures up to 800 0., comprising the following constituents and critical percentages: carbon up to 1.5%, silicon up to 2.0%, manganese up to 2.0%, nickel 15.0 to 25.0%, chromium 12.0 to 20.0%, molybdenum 2.0 to 6.0%, copper 2.0 to 6.0%, titanium 0.25 to 2.0%, and iron the remainder.
4. Alloy steel possessing high creep resistance when applied for the manufacture of mechanical parts to be operated under stress at temperatures up to 800 0., comprising the following constituents and critical percentages: carbon up to 0.3%, silicon up to 2.0%, manganese up to 2.0%, nickel 16.0 to 18.0%, chromium 12.0 to 16.0%, molybdenum 3.0 to 4.5%, copper 3.0 to 4.5%, titanium 0.25 to 1.0%, and iron the remainder.
5. Alloy steel possessing high creep resistance when applied for the manufacture of mechanical parts to be operated under stress at temperatures up to 800 0., comprising the following constituents and critical percentages: carbon 0.08%, silicon 0.28%. manganese 0.24%, nickel 16.93%, chromium 13.87%, molybdenum 4.31%, copper 4.47%, titanium 0.51% and iron the remainder.
6. Alloy steel according to claim 1 and containing vanadium up to 1.0% displacing an equivalent percentage of iron remainder.
7. The iabrication oi apparatus required to operate under stress at high temperatures, that is up to 800 C., from an alloy steel comprising carbon up to 1.5%, nickel 15-25%, chromium 12- 4 20%, molybdenum 24%, copper 24%, titanium 0.25-2% and the remainder iron.
8. A mechanical part required to operate under stress at high temperatures, that is, up to 800 C., and having high creep resistance under such conditions, said part consisting oi alloy steel comprising carbon up to 1.5%, nickel 15-25%, chromium 12-20%, molybdenum 2-6%, copper 2-6%, titanium 0.25-2% and the remainder iron.
WILLIAM HERBERT HATFIELD.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2402814X | 1941-04-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2402814A true US2402814A (en) | 1946-06-25 |
Family
ID=10905921
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US437912A Expired - Lifetime US2402814A (en) | 1941-04-07 | 1942-04-06 | Alloy steel |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2402814A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2447897A (en) * | 1946-05-23 | 1948-08-24 | Armco Steel Corp | High-temperature stainless steel |
| US2528497A (en) * | 1946-10-23 | 1950-11-07 | Armco Steel Corp | Alloy steel |
| US2540509A (en) * | 1947-10-14 | 1951-02-06 | Armco Steel Corp | High-temperature stainless steel |
| US2556373A (en) * | 1949-08-23 | 1951-06-12 | Thos Firth & John Brown Ltd | Alloy steels for use at elevated temperatures |
| US2633420A (en) * | 1949-10-21 | 1953-03-31 | Spitz Karl | Alloy irons and steels |
| US2891858A (en) * | 1955-09-28 | 1959-06-23 | Carpenter Steel Co | Single phase austenitic alloy steel |
| US3357868A (en) * | 1964-11-17 | 1967-12-12 | Armco Steel Corp | Stainless steel and method |
| FR2467888A1 (en) * | 1979-10-22 | 1981-04-30 | Japan Atomic Energy Res Inst | AUSTENITIC ALLOY BASED ON IRON REINFORCED SOLID SOLUTION |
-
1942
- 1942-04-06 US US437912A patent/US2402814A/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2447897A (en) * | 1946-05-23 | 1948-08-24 | Armco Steel Corp | High-temperature stainless steel |
| US2528497A (en) * | 1946-10-23 | 1950-11-07 | Armco Steel Corp | Alloy steel |
| US2540509A (en) * | 1947-10-14 | 1951-02-06 | Armco Steel Corp | High-temperature stainless steel |
| US2556373A (en) * | 1949-08-23 | 1951-06-12 | Thos Firth & John Brown Ltd | Alloy steels for use at elevated temperatures |
| US2633420A (en) * | 1949-10-21 | 1953-03-31 | Spitz Karl | Alloy irons and steels |
| US2891858A (en) * | 1955-09-28 | 1959-06-23 | Carpenter Steel Co | Single phase austenitic alloy steel |
| US3357868A (en) * | 1964-11-17 | 1967-12-12 | Armco Steel Corp | Stainless steel and method |
| FR2467888A1 (en) * | 1979-10-22 | 1981-04-30 | Japan Atomic Energy Res Inst | AUSTENITIC ALLOY BASED ON IRON REINFORCED SOLID SOLUTION |
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