US2141389A - Alloy steel - Google Patents
Alloy steel Download PDFInfo
- Publication number
- US2141389A US2141389A US194880A US19488038A US2141389A US 2141389 A US2141389 A US 2141389A US 194880 A US194880 A US 194880A US 19488038 A US19488038 A US 19488038A US 2141389 A US2141389 A US 2141389A
- Authority
- US
- United States
- Prior art keywords
- chromium
- nickel
- alloy steel
- alloy
- elevated temperatures
- 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
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
- C22C38/52—Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
Definitions
- This invention comprises improvements in or relating to alloy steels exhibiting good mechanical properties at elevated temperatures.
- the present invention provides an austenitic nickel-chromium alloy steel suitable in particular as a constructional material for use at elevated temperatures, and characterized in that it contains as essential constituents a small proportion of titanium and a relatively higher proportion of cobalt.
- the invention comprises an alloy containing 20-40% nickel, 6-20% chromium, 10-30% cobalt, 1-5% titanium, up to 0.6% carbon and the remainder iron.
- the improved alloy may also embody small proportions of other elements such as manganese and silicon normally used in alloy steel production. It is also within the invention to replace part of the nickel up to say by manganese, and to replace part of the chromium up to say 3% by silicon.
- the following is an example of an alloy composition according to the invention and of the properties possessed thereby:-
- An austenitic nickel-chromium alloy steel suitable in particular as a constructional material for use at elevated temperatures and comprising about 30% nickel, 10% chromium, 20% cobalt, 2% titanium, 0.1% carbon and the remainder iron.
- a constructional aterial for use at elevated temperatures comprising an austenitic nickel-chromium alloy steel containing about 30% nickel, 10% chromium, 20% cobalt, 2% titanium, 0.1%carbon and the remainder iron, the steel being in the condition which results from heat treatment by air cooling at about 1050 C. and reheating to about 650 C., and having a yield point of about 32 tons per square inch, a maximum stress of about 60 tons per square inch and a percentage elongation of about 31.
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 Dec. 27, 1938 UNITED STATES PATENT OFFICE 2,141,389 ALLOY STEEL William Herbert signor to Thos. Firth Hatfield, Sheflield, England, as-
& John Brown Limited,
Sheffield, England, a British company 3 Claims.
This invention comprises improvements in or relating to alloy steels exhibiting good mechanical properties at elevated temperatures.
Numerous alloy combinations have been proposed for obtaining improved properties of constructional materials for use at elevated temperatures.
It is generally recognized that, as regards steels, the richer alloys of the austenitic type, containing sufficient proportions of chromium, nickel and other elements to render them for practical purposes stable in the austenitic or austenito-martensitic condition, show superior properties to ordinary alloy steels when tested in the range of temperature round about 500 C. and upwards. In this connection, the addition of tungsten for improving high temperature performance of chromium-nickel steels is well establlshed.
The present invention provides an austenitic nickel-chromium alloy steel suitable in particular as a constructional material for use at elevated temperatures, and characterized in that it contains as essential constituents a small proportion of titanium and a relatively higher proportion of cobalt.
More specifically the invention comprises an alloy containing 20-40% nickel, 6-20% chromium, 10-30% cobalt, 1-5% titanium, up to 0.6% carbon and the remainder iron.
The improved alloy may also embody small proportions of other elements such as manganese and silicon normally used in alloy steel production. It is also within the invention to replace part of the nickel up to say by manganese, and to replace part of the chromium up to say 3% by silicon. The following is an example of an alloy composition according to the invention and of the properties possessed thereby:-
Analysis Per cent 0.1 0.36 1.14 30.05 9.66 20.43 '1 2.08 Fe Remainder.
Treatment:
Air cooled 1050" C. and reheated to 650 C.
Tests at ordinary temperatures:
Yield point 32 tons/sq. in. Maximum stress 59 tons/sq. in. Elongation 31%.
Reduction of area 41%.
Tests at 600 0.-
Short time test:
(Rate of pull 0.12" per minute.) Ultimate strength 35-tons/sq. in. Long time test:
(Hatfield time-yield test) time-yield value 15.5 tons/sq. in.
I claim:
1. An austenitic nickel-chromium alloy-steel suitable in particular as a constructional material for use at elevated temperatures and comprising 20-40% nickel, 6-20'% chromium, in excess of 10% and up to 30% cobalt, 1-5% titanium, a material amount not exceeding 0.6% carbon, and the remainder iron with a minimum of 20%.
2. An austenitic nickel-chromium alloy steel suitable in particular as a constructional material for use at elevated temperatures and comprising about 30% nickel, 10% chromium, 20% cobalt, 2% titanium, 0.1% carbon and the remainder iron. v
3. A constructional aterial for use at elevated temperatures comprising an austenitic nickel-chromium alloy steel containing about 30% nickel, 10% chromium, 20% cobalt, 2% titanium, 0.1%carbon and the remainder iron, the steel being in the condition which results from heat treatment by air cooling at about 1050 C. and reheating to about 650 C., and having a yield point of about 32 tons per square inch, a maximum stress of about 60 tons per square inch and a percentage elongation of about 31.
WILLIAM HERBERT HATFIELD.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2141389X | 1937-04-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2141389A true US2141389A (en) | 1938-12-27 |
Family
ID=10899596
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US194880A Expired - Lifetime US2141389A (en) | 1937-04-19 | 1938-03-09 | Alloy steel |
Country Status (1)
Country | Link |
---|---|
US (1) | US2141389A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504453A (en) * | 1946-11-18 | 1950-04-18 | Thos Firth & John Brown Ltd | Alloy steels for use at elevated temperatures |
US2763543A (en) * | 1953-05-25 | 1956-09-18 | Nyby Bruk Ab | Restorable alloys |
US2793948A (en) * | 1954-08-27 | 1957-05-28 | Nyby Bruk Ab | Restorable fe-cr-ni alloy |
-
1938
- 1938-03-09 US US194880A patent/US2141389A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504453A (en) * | 1946-11-18 | 1950-04-18 | Thos Firth & John Brown Ltd | Alloy steels for use at elevated temperatures |
US2763543A (en) * | 1953-05-25 | 1956-09-18 | Nyby Bruk Ab | Restorable alloys |
US2793948A (en) * | 1954-08-27 | 1957-05-28 | Nyby Bruk Ab | Restorable fe-cr-ni alloy |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2590835A (en) | Alloy steels | |
US3366471A (en) | High strength alloy steel compositions and process of producing high strength steel including hot-cold working | |
US3154412A (en) | Heat-resistant high-strength stainless steel | |
US2572191A (en) | Alloy steel having high strength at elevated temperature | |
US2562854A (en) | Method of improving the high-temperature strength of austenitic steels | |
US2747989A (en) | Ferritic alloys | |
US2693413A (en) | Alloy steels | |
US2141389A (en) | Alloy steel | |
US2704250A (en) | High temperature high strength alloys | |
US3128175A (en) | Low alloy, high hardness, temper resistant steel | |
US2909425A (en) | Austenitic cr-mn-c-n steels for elevated temperature service | |
US2194178A (en) | Low alloy steel | |
US2737455A (en) | Ferritic creep-resisting steels | |
US2504453A (en) | Alloy steels for use at elevated temperatures | |
US2513935A (en) | Alloy steels | |
US2402814A (en) | Alloy steel | |
US2857266A (en) | High temperature resistant alloys | |
US2624670A (en) | Chromium steels | |
US2978319A (en) | High strength, low alloy steels | |
US3069257A (en) | Alloy steel and method | |
US2949355A (en) | High temperature alloy | |
US2815280A (en) | Alloy steel and article made therefrom | |
US2120554A (en) | Chromium steel | |
US2921849A (en) | High strength alloy steels | |
US3820981A (en) | Hardenable alloy steel |