GB2462704B - A single crystal component and a method of heat treating a single crystal component - Google Patents
A single crystal component and a method of heat treating a single crystal componentInfo
- Publication number
- GB2462704B GB2462704B GB0913062A GB0913062A GB2462704B GB 2462704 B GB2462704 B GB 2462704B GB 0913062 A GB0913062 A GB 0913062A GB 0913062 A GB0913062 A GB 0913062A GB 2462704 B GB2462704 B GB 2462704B
- Authority
- GB
- United Kingdom
- Prior art keywords
- single crystal
- crystal component
- heat treating
- component
- treating
- 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 - Fee Related
Links
- 239000013078 crystal Substances 0.000 title 2
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- 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
- 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
- C30B33/00—After-treatment of single crystals or homogeneous polycrystalline material with defined structure
- C30B33/02—Heat treatment
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/607—Monocrystallinity
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13627108P | 2008-08-22 | 2008-08-22 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB0913062D0 GB0913062D0 (en) | 2009-09-02 |
| GB2462704A GB2462704A (en) | 2010-02-24 |
| GB2462704B true GB2462704B (en) | 2010-07-21 |
Family
ID=41066906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB0913062A Expired - Fee Related GB2462704B (en) | 2008-08-22 | 2009-07-28 | A single crystal component and a method of heat treating a single crystal component |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US20100043929A1 (en) |
| GB (1) | GB2462704B (en) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101595237B (en) * | 2006-12-04 | 2011-12-14 | 东北泰克诺亚奇股份有限公司 | Amorphous alloy composition |
| US8641381B2 (en) * | 2010-04-14 | 2014-02-04 | General Electric Company | System and method for reducing grain boundaries in shrouded airfoils |
| PL2615243T3 (en) * | 2012-01-11 | 2017-12-29 | MTU Aero Engines AG | Blade ring segment for a fluid flow engine and method for producing the same |
| US20180051360A1 (en) * | 2016-08-16 | 2018-02-22 | United Technologies Corporation | Formable Superalloy Single Crystal Composition |
| US11306595B2 (en) | 2018-09-14 | 2022-04-19 | Raytheon Technologies Corporation | Wrought root blade manufacture methods |
| US11199101B2 (en) | 2019-12-12 | 2021-12-14 | General Electric Company | System and method to apply multiple thermal treatments to workpiece and related turbomachine components |
| US11242588B2 (en) | 2019-12-12 | 2022-02-08 | General Electric Company | System and method to apply multiple thermal treatments to workpiece and related turbomachine components |
| CN114214510B (en) * | 2021-12-28 | 2024-02-06 | 北京钢研高纳科技股份有限公司 | Method for removing residual stress in high-temperature alloy part through vibration aging and application of method |
| CN114672882A (en) * | 2022-03-14 | 2022-06-28 | 浙江大学 | A kind of single crystal superalloy with medium temperature and high creep strength and its preparation method and application |
| CN114718655B (en) * | 2022-04-02 | 2023-08-04 | 浙江大学 | Non-uniform structure single crystal turbine blade and preparation method thereof |
| CN114813329B (en) * | 2022-04-26 | 2023-07-28 | 北京航空航天大学杭州创新研究院 | A Remaining Life Prediction Method for Nickel-based Single Crystal Superalloys Under Random Creep Loads |
| GB202213705D0 (en) * | 2022-09-20 | 2022-11-02 | Rolls Royce Plc | Method for coating a tip of an aerofoil and aerofoil |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02228444A (en) * | 1989-03-01 | 1990-09-11 | Natl Res Inst For Metals | High strength ni-base single crystal heat resisting alloy |
| RU2033467C1 (en) * | 1991-11-18 | 1995-04-20 | Институт металлофизики АН Украины | Method for treatment of monocrystalline articles from dispersed-setting materials |
| US20060207693A1 (en) * | 2001-08-30 | 2006-09-21 | Deluca Daniel P | Modified advanced high strength single crystal superalloy composition |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4921405A (en) * | 1988-11-10 | 1990-05-01 | Allied-Signal Inc. | Dual structure turbine blade |
| US5106266A (en) * | 1989-07-25 | 1992-04-21 | Allied-Signal Inc. | Dual alloy turbine blade |
| US5527402A (en) * | 1992-03-13 | 1996-06-18 | General Electric Company | Differentially heat treated process for the manufacture thereof |
| US5451142A (en) * | 1994-03-29 | 1995-09-19 | United Technologies Corporation | Turbine engine blade having a zone of fine grains of a high strength composition at the blade root surface |
| US20090317287A1 (en) * | 2008-06-24 | 2009-12-24 | Honeywell International Inc. | Single crystal nickel-based superalloy compositions, components, and manufacturing methods therefor |
-
2009
- 2009-07-28 GB GB0913062A patent/GB2462704B/en not_active Expired - Fee Related
- 2009-07-29 US US12/461,012 patent/US20100043929A1/en not_active Abandoned
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02228444A (en) * | 1989-03-01 | 1990-09-11 | Natl Res Inst For Metals | High strength ni-base single crystal heat resisting alloy |
| RU2033467C1 (en) * | 1991-11-18 | 1995-04-20 | Институт металлофизики АН Украины | Method for treatment of monocrystalline articles from dispersed-setting materials |
| US20060207693A1 (en) * | 2001-08-30 | 2006-09-21 | Deluca Daniel P | Modified advanced high strength single crystal superalloy composition |
Also Published As
| Publication number | Publication date |
|---|---|
| GB0913062D0 (en) | 2009-09-02 |
| US20100043929A1 (en) | 2010-02-25 |
| GB2462704A (en) | 2010-02-24 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20130728 |