GB920896A - A method of producing workpieces required to exhibit high strength at room and at elevated temperatures - Google Patents
A method of producing workpieces required to exhibit high strength at room and at elevated temperaturesInfo
- Publication number
- GB920896A GB920896A GB3722361A GB3722361A GB920896A GB 920896 A GB920896 A GB 920896A GB 3722361 A GB3722361 A GB 3722361A GB 3722361 A GB3722361 A GB 3722361A GB 920896 A GB920896 A GB 920896A
- Authority
- GB
- United Kingdom
- Prior art keywords
- workpiece
- hours
- blank
- final dimensions
- titanium
- 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
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
- Heat Treatment Of Steel (AREA)
Abstract
A method of producing a hot extrusion, drop forging or like die or tool or component stressed at high temperature and made of an alloy containing more than 50% nickel or nickel and cobalt and up to 45% chromium and at least one of the elements iron, manganese, aluminium molybdenum, tungsten, vanadium, titanium, niobium, tantalum, silicon and carbon in quantity not exceeding a total of 40% comprises the steps of successively reducing the workpiece by hot working, e.g. by forging, upsetting or pressing, to a shape exceeding the final dimensions by between 10 and 20% subjecting the workpiece to a solution heat treatment at 1,050 to 1,200 DEG C. for 1 to 10 hours, cooling the preformed workpiece directly from the said temperature to a temperature below the recrystallization point and within the range 600 DEG to 700 DEG C. and then reducing the workpiece to its final dimensions and finally subjecting the workpiece to a precipitation hardening treatment at between 650 DEG and 800 DEG C. for 10 to 20 hours. In an example, a precipitation hardenable austenitic alloy is hot worked into a disc or plate-shaped die blank having dimensions exceeding the desired final dimensions by 13.5%. The blank is solution heat treated at 1,150 DEG C. for 2 hours and then cooled to 650 DEG C. at which temperature the blank is reduced to its final dimensions by upsetting. Finally, the blank is heat treated at 700 DEG C. for 16 hours to effect the precipitation hardening. The alloys contain not more than 1% C., not more than 5% titanium and silicon, and none of said additional elements should exceed 25%. Minor quantities of nitrogen, copper and rare earth metals may be included. The alloys may contain alloying components in the following quantities:- .Chromium.Up to 30% .Molybdenum.Up to 10% .Tungsten.Up to 10% .Vanadium.Up to 5% .Titanium.Up to 5% .Niobium and tantalum.Up to 10% .Aluminium.Up to 6% .Silicon.Up to 3% .Manganese.Up to 3% .Nitrogen.Up to 0.5% .Boron.Up to 0.5% .Zirconium.Up to 0.5% .Iron.Up to 10%
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED0034549 | 1960-10-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB920896A true GB920896A (en) | 1963-03-13 |
Family
ID=7042232
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3722361A Expired GB920896A (en) | 1960-10-18 | 1961-10-17 | A method of producing workpieces required to exhibit high strength at room and at elevated temperatures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB920896A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2380420A2 (en) * | 1977-02-15 | 1978-09-08 | Dervaux Ets | Internal combustion engine valve body - is welded to its seat and is then aged |
FR2574686A1 (en) * | 1984-12-18 | 1986-06-20 | United Technologies Corp | PROCESS FOR MANUFACTURING TURBINE DISKS |
EP0260510A2 (en) * | 1986-09-15 | 1988-03-23 | General Electric Company | Thermomechanical method of forming fatigue crack resistant nickel base superalloys and product formed |
GB2270324A (en) * | 1992-09-04 | 1994-03-09 | Mtu Muenchen Gmbh | Treatment of y"- hardening nickel-based alloys |
US20140076597A1 (en) * | 2012-09-18 | 2014-03-20 | BPP Cables Ltd. | Subterranean Cable |
-
1961
- 1961-10-17 GB GB3722361A patent/GB920896A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2380420A2 (en) * | 1977-02-15 | 1978-09-08 | Dervaux Ets | Internal combustion engine valve body - is welded to its seat and is then aged |
FR2574686A1 (en) * | 1984-12-18 | 1986-06-20 | United Technologies Corp | PROCESS FOR MANUFACTURING TURBINE DISKS |
EP0260510A2 (en) * | 1986-09-15 | 1988-03-23 | General Electric Company | Thermomechanical method of forming fatigue crack resistant nickel base superalloys and product formed |
EP0260510A3 (en) * | 1986-09-15 | 1989-10-18 | General Electric Company | Thermomechanical method of forming fatigue crack resistant nickel base superalloys and product formed |
GB2270324A (en) * | 1992-09-04 | 1994-03-09 | Mtu Muenchen Gmbh | Treatment of y"- hardening nickel-based alloys |
GB2270324B (en) * | 1992-09-04 | 1996-06-26 | Mtu Muenchen Gmbh | Treatment of y"-hardening nickel-based alloys |
US20140076597A1 (en) * | 2012-09-18 | 2014-03-20 | BPP Cables Ltd. | Subterranean Cable |
US20140076606A1 (en) * | 2012-09-18 | 2014-03-20 | BPP Cables Ltd. | Subterranean Cable |
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