GB2463304B - A method for the manufacture of monocrystalline blades - Google Patents
A method for the manufacture of monocrystalline bladesInfo
- Publication number
- GB2463304B GB2463304B GB8227301A GB8227301A GB2463304B GB 2463304 B GB2463304 B GB 2463304B GB 8227301 A GB8227301 A GB 8227301A GB 8227301 A GB8227301 A GB 8227301A GB 2463304 B GB2463304 B GB 2463304B
- Authority
- GB
- United Kingdom
- Prior art keywords
- manufacture
- monocrystalline blades
- monocrystalline
- blades
- 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
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
Classifications
-
- 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
- C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
- C30B11/14—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method characterised by the seed, e.g. its crystallographic orientation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
- B22D27/045—Directionally solidified castings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/20—Measures not previously mentioned for influencing the grain structure or texture; Selection of compositions therefor
-
- 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
- C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
-
- 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)
- Crystallography & Structural Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8118071A FR2734187A1 (en) | 1981-09-25 | 1981-09-25 | Casting and directional solidification. of a cluster of turbine rotor vanes |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8227301D0 GB8227301D0 (en) | 2009-09-16 |
GB2463304A GB2463304A (en) | 2010-03-17 |
GB2463304B true GB2463304B (en) | 2010-09-29 |
Family
ID=9262451
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8227301A Expired - Lifetime GB2463304B (en) | 1981-09-25 | 1982-09-24 | A method for the manufacture of monocrystalline blades |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE3235359C1 (en) |
FR (1) | FR2734187A1 (en) |
GB (1) | GB2463304B (en) |
IT (1) | IT8223391A0 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2734189B1 (en) * | 1989-05-24 | 1997-07-18 | Snecma | DEVICE FOR SELECTING A GRAIN OF CRYSTALLIZATION FOR SINGLE CRYSTAL PIECES IN FOUNDRY |
CN1317095C (en) * | 2004-02-25 | 2007-05-23 | 中国科学院金属研究所 | Crystalloid laminae composited from single crystal and directional column crystal and preparing method |
FR3004366B1 (en) * | 2013-04-10 | 2021-04-30 | Snecma | MONOCRISTALLINE FOUNDRY MOLD |
CN109648065B (en) * | 2019-02-01 | 2020-08-21 | 中国科学院金属研究所 | Method for evaluating recrystallization forming tendency of single crystal superalloy |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1263401A (en) * | 1969-03-13 | 1972-02-09 | United Aircraft Corp | Double oriented single crystal castings |
GB1280055A (en) * | 1969-03-13 | 1972-07-05 | United Aircraft Corp | Double-oriented single crystal castings |
GB2030233A (en) * | 1978-09-16 | 1980-04-02 | Rolls Royce | Gas turbine engine blade |
GB2030069A (en) * | 1978-09-18 | 1980-04-02 | Howmet Turbine Components | Mould for directional solidified single crystal castings and method for preparing same |
GB2037200A (en) * | 1978-12-13 | 1980-07-09 | United Technologies Corp | Epitaxial solidification |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1481366A (en) * | 1965-05-27 | 1967-05-19 | United Aircraft Corp | Improvements to foundry parts and method and device for manufacturing these parts |
US3625275A (en) * | 1969-03-13 | 1971-12-07 | United Aircraft Corp | Apparatus and method for single-crystal casting |
BE737493A (en) * | 1969-08-14 | 1970-01-16 | Monocrystalline turbine blade envelope mould | |
BE795953A (en) * | 1973-02-26 | 1973-08-27 | Petrov Dmitry A | Monocrystalline metal products mfr - in a two cavity mould |
US4292010A (en) * | 1978-09-16 | 1981-09-29 | Rolls-Royce Limited | Cambered blade or vane for a gas turbine engine |
-
1981
- 1981-09-25 FR FR8118071A patent/FR2734187A1/en active Pending
-
1982
- 1982-09-23 IT IT8223391A patent/IT8223391A0/en unknown
- 1982-09-24 GB GB8227301A patent/GB2463304B/en not_active Expired - Lifetime
- 1982-09-24 DE DE3235359A patent/DE3235359C1/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1263401A (en) * | 1969-03-13 | 1972-02-09 | United Aircraft Corp | Double oriented single crystal castings |
GB1280055A (en) * | 1969-03-13 | 1972-07-05 | United Aircraft Corp | Double-oriented single crystal castings |
GB2030233A (en) * | 1978-09-16 | 1980-04-02 | Rolls Royce | Gas turbine engine blade |
GB2030069A (en) * | 1978-09-18 | 1980-04-02 | Howmet Turbine Components | Mould for directional solidified single crystal castings and method for preparing same |
GB2037200A (en) * | 1978-12-13 | 1980-07-09 | United Technologies Corp | Epitaxial solidification |
Also Published As
Publication number | Publication date |
---|---|
DE3235359C1 (en) | 1997-01-30 |
GB8227301D0 (en) | 2009-09-16 |
GB2463304A (en) | 2010-03-17 |
IT8223391A0 (en) | 1982-09-23 |
FR2734187A1 (en) | 1996-11-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PE20 | Patent expired after termination of 20 years |
Expiry date: 20020923 |