GB1386808A - Alloy microstructure control - Google Patents
Alloy microstructure controlInfo
- Publication number
- GB1386808A GB1386808A GB1608472A GB1608472A GB1386808A GB 1386808 A GB1386808 A GB 1386808A GB 1608472 A GB1608472 A GB 1608472A GB 1608472 A GB1608472 A GB 1608472A GB 1386808 A GB1386808 A GB 1386808A
- Authority
- GB
- United Kingdom
- Prior art keywords
- inch
- alloy
- gradient
- heated
- hour
- 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
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/186—High-melting or refractory metals or alloys based thereon of zirconium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
-
- 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
-
- 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
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B1/00—Single-crystal growth directly from the solid state
- C30B1/02—Single-crystal growth directly from the solid state by thermal treatment, e.g. strain annealing
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B29/00—Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
- C30B29/10—Inorganic compounds or compositions
- C30B29/52—Alloys
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Manufacture And Refinement Of Metals (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
- Forging (AREA)
- Powder Metallurgy (AREA)
Abstract
1386808 Heat-treating high temperature alloys GENERAL ELECTRIC CO 7 April 1972 [22 July 1971] 16084/72 Headings C7A and C7N A solid state process for producing a columnar grain structure consists of treating the alloy to develop a dislocation density such that when the alloy is heated to 50% to 100% of the incipient melting temperature in degrees Rankine it will develop a grain size the largest dimension of which is at least 200 microns, and then progressively heating the alloy into that range by passing through it a temperature gradient of at least 500F/inch, the high temperature end of the gradient leading. The process is applied particularly to alloys based on Fe, Ni, Co, Ti, Cr, W or Mo, when the thermal gradient may be 500-5000F/inch advancing at 0.5-144 inches per hour. The alloy may be strengthened by oxide dispersion, precipitated γ1, or rare earth metal addition. In particular examples an alloy of 80% Ni and 20% Cr dispersion strengthened with 2 volume % of thoria was extruded at 1800-1860F and was then heated progressively to 2400-2425F by passage of a temperature gradient of 1500-2000F/inch at a rate of 0.1 inch, 0.5 inch, 5 inch, 24 inch or 72 inch/hour. Furthermore an alloy containing 15% Cr, 5% Al, 1% Nb, 1% Y, balance Fe and dispersion strengthened with 4 vol.% Al 2 O 3 was rolled at 1800F and then heated to 2425F by passage of a 1500F/ inch temperature gradient at 1 inch/hour. Suitable apparatus for carrying out the invention comprises a planar induction coil 10 and water cooled chill block through which a workpiece 20 is passed. The power supply to the coil is controlled by optical pyrometer 26. The process may be applied to turbine blades.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US16503071A | 1971-07-22 | 1971-07-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1386808A true GB1386808A (en) | 1975-03-12 |
Family
ID=22597115
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1608472A Expired GB1386808A (en) | 1971-07-22 | 1972-04-07 | Alloy microstructure control |
Country Status (7)
Country | Link |
---|---|
US (1) | US3772090A (en) |
JP (1) | JPS5335887B1 (en) |
BE (1) | BE782473A (en) |
DE (1) | DE2219275C3 (en) |
FR (1) | FR2146716A5 (en) |
GB (1) | GB1386808A (en) |
IT (1) | IT953571B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2256202A (en) * | 1991-04-24 | 1992-12-02 | Inco Alloys Int | Controlled grain size for ods iron-base alloys |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3975219A (en) * | 1975-09-02 | 1976-08-17 | United Technologies Corporation | Thermomechanical treatment for nickel base superalloys |
CA1135924A (en) * | 1978-05-04 | 1982-11-23 | Sanford Baranow | Process for enhancing the mechanical properties of oxide dispersion strengthened materials |
US4475980A (en) * | 1982-06-01 | 1984-10-09 | United Technologies Corporation | Solid state production of multiple single crystal articles |
US4481043A (en) * | 1982-12-07 | 1984-11-06 | The United States Of America As Represented By The United States Department Of Energy | Heat treatment of NiCrFe alloy to optimize resistance to intergrannular stress corrosion |
EP0115092B1 (en) * | 1983-02-01 | 1987-08-12 | BBC Brown Boveri AG | Structural element with a high corrosion and oxidation resistance made from a dispersion-hardened superalloy, and process for its manufacture |
US4617817A (en) * | 1985-02-06 | 1986-10-21 | The United States Of America As Represented By The Secretary Of The Air Force | Optimizing hot workability and controlling microstructures in difficult to process high strength and high temperature materials |
DE3669044D1 (en) * | 1985-12-19 | 1990-03-22 | Bbc Brown Boveri & Cie | METHOD FOR ZONING A METAL WORKPIECE. |
US4762679A (en) * | 1987-07-06 | 1988-08-09 | The United States Of America As Represented By The Secretary Of The Air Force | Billet conditioning technique for manufacturing powder metallurgy preforms |
EP0331360B1 (en) * | 1988-02-26 | 1994-02-02 | Hitachi, Ltd. | Method of preparing an oxide high-temperature superconducting material |
WO1990014308A1 (en) * | 1989-05-15 | 1990-11-29 | Massachusetts Institute Of Technology | Textured oxide compositions by directional oxidation |
US20070267109A1 (en) * | 2006-05-17 | 2007-11-22 | General Electric Company | High pressure turbine airfoil recovery device and method of heat treatment |
US8357328B2 (en) * | 2009-12-14 | 2013-01-22 | General Electric Company | Methods for processing nanostructured ferritic alloys, and articles produced thereby |
CN113234905B (en) * | 2021-05-10 | 2023-06-13 | 烟台大学 | High-flux preparation method and device for gradient thermal deformation and gradient thermal treatment |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE399896C (en) * | 1924-07-31 | Frederick Shand Goucher Dr | Process for the production of metal wires or threads, in particular from refractory metals | |
DE1179968B (en) * | 1962-02-21 | 1964-10-22 | Magnetfab Bonn Gmbh | Process for the production of recrystallization textures in metallic permanent magnets |
NL136758C (en) * | 1963-10-21 | 1900-01-01 | ||
GB1134492A (en) * | 1964-03-11 | 1968-11-27 | Johnson Matthey Co Ltd | Methods of improving the mechanical properties of metals and their alloys |
US3368883A (en) * | 1965-07-29 | 1968-02-13 | Du Pont | Dispersion-modified cobalt and/or nickel alloy containing anisodiametric grains |
US3388010A (en) * | 1965-07-29 | 1968-06-11 | Fansteel Metallurgical Corp | Dispersion-hardened metal sheet and process for making same |
US3540947A (en) * | 1966-10-25 | 1970-11-17 | Sadaichi Komaki | Method of manufacturing a permanent magnetic alloy |
US3677835A (en) * | 1970-10-16 | 1972-07-18 | United Aircraft Corp | Homogeneous nickel-base superalloy castings |
-
1971
- 1971-07-22 US US00165030A patent/US3772090A/en not_active Expired - Lifetime
-
1972
- 1972-03-28 IT IT22496/72A patent/IT953571B/en active
- 1972-04-07 GB GB1608472A patent/GB1386808A/en not_active Expired
- 1972-04-20 DE DE2219275A patent/DE2219275C3/en not_active Expired
- 1972-04-21 BE BE782473A patent/BE782473A/en not_active IP Right Cessation
- 1972-04-21 FR FR7214121A patent/FR2146716A5/fr not_active Expired
- 1972-04-21 JP JP3969872A patent/JPS5335887B1/ja active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2256202A (en) * | 1991-04-24 | 1992-12-02 | Inco Alloys Int | Controlled grain size for ods iron-base alloys |
GB2256202B (en) * | 1991-04-24 | 1994-08-24 | Inco Alloys Int | Controlled grain size for ods iron-base alloys |
Also Published As
Publication number | Publication date |
---|---|
DE2219275C3 (en) | 1982-02-11 |
FR2146716A5 (en) | 1973-03-02 |
BE782473A (en) | 1972-10-23 |
JPS5335887B1 (en) | 1978-09-29 |
DE2219275A1 (en) | 1973-02-01 |
DE2219275B2 (en) | 1981-06-04 |
IT953571B (en) | 1973-08-10 |
US3772090A (en) | 1973-11-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
746 | Register noted 'licences of right' (sect. 46/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |