DE58904084D1 - METAL ITEM, ESPECIALLY GAS TURBINE BLADE WITH PROTECTIVE COATING. - Google Patents
METAL ITEM, ESPECIALLY GAS TURBINE BLADE WITH PROTECTIVE COATING.Info
- Publication number
- DE58904084D1 DE58904084D1 DE8989901530T DE58904084T DE58904084D1 DE 58904084 D1 DE58904084 D1 DE 58904084D1 DE 8989901530 T DE8989901530 T DE 8989901530T DE 58904084 T DE58904084 T DE 58904084T DE 58904084 D1 DE58904084 D1 DE 58904084D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- turbine blade
- protective coating
- especially gas
- metal item
- 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
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 239000002184 metal Substances 0.000 title 1
- 239000011253 protective coating Substances 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/023—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only
Landscapes
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Coating By Spraying Or Casting (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE8989901530T DE58904084D1 (en) | 1988-02-05 | 1989-01-19 | METAL ITEM, ESPECIALLY GAS TURBINE BLADE WITH PROTECTIVE COATING. |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE3803517 | 1988-02-05 | ||
| DE8989901530T DE58904084D1 (en) | 1988-02-05 | 1989-01-19 | METAL ITEM, ESPECIALLY GAS TURBINE BLADE WITH PROTECTIVE COATING. |
| PCT/DE1989/000023 WO1989007159A1 (en) | 1988-02-05 | 1989-01-19 | Metallic object, in particular gas turbine blade with protective coating |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE58904084D1 true DE58904084D1 (en) | 1993-05-19 |
Family
ID=6346731
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE8989901530T Expired - Fee Related DE58904084D1 (en) | 1988-02-05 | 1989-01-19 | METAL ITEM, ESPECIALLY GAS TURBINE BLADE WITH PROTECTIVE COATING. |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0397731B1 (en) |
| JP (1) | JPH03503184A (en) |
| DE (1) | DE58904084D1 (en) |
| IN (1) | IN171444B (en) |
| WO (1) | WO1989007159A1 (en) |
Families Citing this family (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3370676B2 (en) * | 1994-10-14 | 2003-01-27 | シーメンス アクチエンゲゼルシヤフト | Protective layer for protecting members against corrosion, oxidation and thermal overload, and method of manufacturing the same |
| WO1996035825A1 (en) * | 1995-05-08 | 1996-11-14 | Helmut Tannenberger | Workpiece for high-temperature uses and process for producing it |
| DE59601728D1 (en) * | 1995-07-25 | 1999-05-27 | Siemens Ag | PRODUCT WITH A METAL BASE WITH COOLING CHANNELS AND THEIR PRODUCTION |
| DE19815473A1 (en) | 1998-04-07 | 1999-10-14 | Ghh Borsig Turbomaschinen Gmbh | Hot gas-carrying gas manifold of a gas turbine |
| CH695689A5 (en) * | 2001-05-23 | 2006-07-31 | Sulzer Metco Ag | A method for generating a thermally insulating layer system on a metallic substrate. |
| EP1524334A1 (en) * | 2003-10-17 | 2005-04-20 | Siemens Aktiengesellschaft | Protective coating for protecting a structural member against corrosion and oxidation at high temperatures and structural member |
| GB2421032A (en) * | 2004-12-11 | 2006-06-14 | Siemens Ind Turbomachinery Ltd | A method of protecting a component against hot corrosion |
| US20070116875A1 (en) | 2005-11-22 | 2007-05-24 | United Technologies Corporation | Strip process for superalloys |
| ATE462807T1 (en) * | 2006-08-23 | 2010-04-15 | Siemens Ag | TURBINE BLADE WITH A COATING SYSTEM |
| EP2206805A1 (en) * | 2009-01-08 | 2010-07-14 | Siemens Aktiengesellschaft | MCrAIX coating with different chrome and aluminium contents |
| EP2557201A1 (en) | 2011-08-09 | 2013-02-13 | Siemens Aktiengesellschaft | Alloy, protective coating and component |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3649225A (en) * | 1969-11-17 | 1972-03-14 | United Aircraft Corp | Composite coating for the superalloys |
| FR2207198B1 (en) * | 1972-10-23 | 1976-08-20 | Onera (Off Nat Aerospatiale) | |
| US4284688A (en) * | 1978-12-21 | 1981-08-18 | Bbc Brown, Boveri & Company Limited | Multi-layer, high-temperature corrosion protection coating |
| US4326011A (en) * | 1980-02-11 | 1982-04-20 | United Technologies Corporation | Hot corrosion resistant coatings |
-
1989
- 1989-01-19 WO PCT/DE1989/000023 patent/WO1989007159A1/en not_active Ceased
- 1989-01-19 DE DE8989901530T patent/DE58904084D1/en not_active Expired - Fee Related
- 1989-01-19 EP EP89901530A patent/EP0397731B1/en not_active Expired - Lifetime
- 1989-01-19 JP JP89501389A patent/JPH03503184A/en active Pending
- 1989-01-30 IN IN91/CAL/89A patent/IN171444B/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| JPH03503184A (en) | 1991-07-18 |
| EP0397731B1 (en) | 1993-04-14 |
| IN171444B (en) | 1992-10-17 |
| EP0397731A1 (en) | 1990-11-22 |
| WO1989007159A1 (en) | 1989-08-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| DE58908611D1 (en) | HIGH-TEMPERATURE-RESISTANT CORROSION PROTECTION COATING, IN PARTICULAR FOR GAS TURBINE COMPONENTS. | |
| DE69105712D1 (en) | Gas turbine shroud. | |
| DE69006433D1 (en) | Turbine blade. | |
| DE69205656D1 (en) | Gas turbine shroud. | |
| GB2243413B (en) | Gas turbine bladed disk. | |
| DE69204293D1 (en) | GAS TURBINE GONDOLA. | |
| DE69107148D1 (en) | Gas turbine with cooled blades. | |
| DE69018338D1 (en) | Gas turbine. | |
| DE3789514D1 (en) | Cooled gas turbine blade. | |
| DE68908676D1 (en) | Turbine blade damper and fuse. | |
| NL194342B (en) | Cooled blades for a gas turbine engine. | |
| FI896093A0 (en) | VARMLAMINERBARA, GAS OGENOMSLAEPPLIGA FLERSKIKTSFOLIER. | |
| DE68906334D1 (en) | GAS TURBINE WITH A COOLED VAN SHEET RING. | |
| NO893533D0 (en) | STRONG, MAGNESIUM-BASED ALLOY. | |
| DE58900122D1 (en) | SCISSORS, ESPECIALLY HAIRDRESSING SCISSORS. | |
| DE58907451D1 (en) | Burners, especially high speed burners. | |
| IT8522312A0 (en) | FIXING ARRANGEMENT FOR TURBINE BLADES, PARTICULARLY FOR GAS TURBINES. | |
| IT8941631A0 (en) | EQUIPMENT FOR THE PRECISE DETECTION OF TURBINE BLADE PASSAGE TIMES. | |
| NO160807C (en) | Gas turbine. | |
| DE69100652D1 (en) | Turbomachine rotor with blade attachment. | |
| DE68919829D1 (en) | GENERATOR WITH GAS TURBINE. | |
| DE68901360D1 (en) | TURBINE WITH VARIABLE STATOR GEOMETRY. | |
| DE58904084D1 (en) | METAL ITEM, ESPECIALLY GAS TURBINE BLADE WITH PROTECTIVE COATING. | |
| IT1233365B (en) | TURBINE WITH SEMI ISOLATED INLET. | |
| DE68902717D1 (en) | TURNING PLANE BLADE AND ROTOR EQUIPPED WITH IT. |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8364 | No opposition during term of opposition | ||
| 8339 | Ceased/non-payment of the annual fee |