GB201119786D0 - Methods for improving corrosion and axidation resistance to the under platform region of a gas turbine blade - Google Patents
Methods for improving corrosion and axidation resistance to the under platform region of a gas turbine bladeInfo
- Publication number
- GB201119786D0 GB201119786D0 GBGB1119786.0A GB201119786A GB201119786D0 GB 201119786 D0 GB201119786 D0 GB 201119786D0 GB 201119786 A GB201119786 A GB 201119786A GB 201119786 D0 GB201119786 D0 GB 201119786D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- axidation
- resistance
- methods
- gas turbine
- turbine blade
- 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.)
- Withdrawn
Links
- 238000005260 corrosion Methods 0.000 title 1
- 230000007797 corrosion Effects 0.000 title 1
- 238000000034 method Methods 0.000 title 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/18—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions
- C23C10/20—Solid state diffusion of only metal elements or silicon into metallic material surfaces using liquids, e.g. salt baths, liquid suspensions only one element being diffused
-
- 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
- F01D5/288—Protective coatings for blades
-
- 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
- F05D2230/00—Manufacture
- F05D2230/90—Coating; Surface treatment
-
- 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
- F05D2240/00—Components
- F05D2240/80—Platforms for stationary or moving blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2009/044838 WO2010134918A1 (en) | 2009-05-21 | 2009-05-21 | Methods for improving corrosion and oxidation resistance to the under platform region of a gas turbine blade |
Publications (2)
Publication Number | Publication Date |
---|---|
GB201119786D0 true GB201119786D0 (en) | 2011-12-28 |
GB2482460A GB2482460A (en) | 2012-02-01 |
Family
ID=41698279
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1119786.0A Withdrawn GB2482460A (en) | 2009-05-21 | 2009-05-21 | Methods for improving corrosion and oxidation resistance to the under platform region of a gas turbine blade |
Country Status (5)
Country | Link |
---|---|
JP (1) | JP2012527537A (en) |
CA (1) | CA2761697A1 (en) |
DE (1) | DE112009004789T5 (en) |
GB (1) | GB2482460A (en) |
WO (1) | WO2010134918A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2834387B1 (en) | 2012-04-03 | 2016-05-18 | MTU Aero Engines GmbH | Slurry and method for producing an aluminum diffusion layer |
EP2662529A1 (en) * | 2012-05-09 | 2013-11-13 | Siemens Aktiengesellschaft | Airfoil with PtAl bond coating and TBC, corresponding airfoil arrangement and manufacturing method |
US9435268B2 (en) * | 2014-03-24 | 2016-09-06 | General Electric Company | Methods of Si based ceramic components volatilization control in a gas turbine engine |
DE102014222024A1 (en) | 2014-10-29 | 2016-06-16 | MTU Aero Engines AG | Slip and method of making an oxidation and corrosion resistant diffusion layer |
US10053779B2 (en) | 2016-06-22 | 2018-08-21 | General Electric Company | Coating process for applying a bifurcated coating |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4310574A (en) | 1980-06-20 | 1982-01-12 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of protecting a surface with a silicon-slurry/aluminide coating |
US5795659A (en) | 1992-09-05 | 1998-08-18 | International Inc. | Aluminide-silicide coatings coated products |
JP3538106B2 (en) * | 2000-03-02 | 2004-06-14 | 株式会社東芝 | Gas turbine component reprocessing method |
US7270852B2 (en) * | 2003-08-04 | 2007-09-18 | General Electric Company | Aluminizing slurry compositions free of hexavalent chromium, and related methods and articles |
US7332024B2 (en) * | 2004-04-29 | 2008-02-19 | General Electric Company | Aluminizing composition and method for application within internal passages |
US7597934B2 (en) * | 2006-02-21 | 2009-10-06 | General Electric Company | Corrosion coating for turbine blade environmental protection |
US20080202552A1 (en) * | 2006-12-07 | 2008-08-28 | Lawrence Bernard Kool | Method for selectively removing coatings from metal substrates |
-
2009
- 2009-05-21 CA CA2761697A patent/CA2761697A1/en not_active Abandoned
- 2009-05-21 WO PCT/US2009/044838 patent/WO2010134918A1/en active Application Filing
- 2009-05-21 JP JP2012511796A patent/JP2012527537A/en active Pending
- 2009-05-21 GB GB1119786.0A patent/GB2482460A/en not_active Withdrawn
- 2009-05-21 DE DE112009004789T patent/DE112009004789T5/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2482460A (en) | 2012-02-01 |
WO2010134918A1 (en) | 2010-11-25 |
DE112009004789T5 (en) | 2012-06-21 |
CA2761697A1 (en) | 2010-11-25 |
JP2012527537A (en) | 2012-11-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2412925A4 (en) | Turbine blade and gas turbine | |
EP2372165A4 (en) | Turbine blade and gas turbine | |
EP2381069A4 (en) | Gas turbine facility | |
EP2592228A4 (en) | Turbine blade and engine component | |
GB201015028D0 (en) | Gas turbine engine | |
ZA201403162B (en) | Blade for wind turbine and method of assembly of the blade | |
GB0809759D0 (en) | Gas turbine engine | |
EP2659095A4 (en) | Gas turbine engine and cooled flowpath component therefor | |
EP2309108A4 (en) | Gas turbine | |
EP2261468A4 (en) | Gas turbine | |
EP2309109A4 (en) | Gas turbine and method of operating gas turbine | |
PL2402559T3 (en) | Turbine blade with tip shroud | |
PL2603669T3 (en) | Blade assembly and corresponding gas turbine | |
GB0903935D0 (en) | Gas turbine engine | |
EP2410125A4 (en) | Gas turbine | |
EP2519437A4 (en) | Composite gas turbine engine component | |
PL2572867T3 (en) | Method and manufacturing line for manufacturing wind turbine blades | |
GB0813483D0 (en) | Gas turbine engine nacelle | |
GB0813482D0 (en) | Gas turbine engine nacelle | |
GB201015029D0 (en) | Gas turbine engine | |
EP2559857A4 (en) | Gas turbine and turbine stationary blade for same | |
EP2103782A4 (en) | Blade structure for gas turbine | |
ZA201300874B (en) | Solar tower with integrated gas turbine | |
GB2491791B (en) | Gas turbines | |
GB201215069D0 (en) | Method for making a metal reinforcement for the blade of a turbine engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |