RU2007119212A - METHOD FOR APPLYING COMBINED HEAT PROTECTIVE COATING TO THE TURBINES OF TURBINES OF GTE - Google Patents
METHOD FOR APPLYING COMBINED HEAT PROTECTIVE COATING TO THE TURBINES OF TURBINES OF GTE Download PDFInfo
- Publication number
- RU2007119212A RU2007119212A RU2007119212/02A RU2007119212A RU2007119212A RU 2007119212 A RU2007119212 A RU 2007119212A RU 2007119212/02 A RU2007119212/02 A RU 2007119212/02A RU 2007119212 A RU2007119212 A RU 2007119212A RU 2007119212 A RU2007119212 A RU 2007119212A
- Authority
- RU
- Russia
- Prior art keywords
- turbines
- zro
- blades
- combined heat
- gte
- Prior art date
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007119212/02A RU2349679C1 (en) | 2007-05-23 | 2007-05-23 | Method of combination heat-resistant coating on turbine blades of gas-turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2007119212/02A RU2349679C1 (en) | 2007-05-23 | 2007-05-23 | Method of combination heat-resistant coating on turbine blades of gas-turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2007119212A true RU2007119212A (en) | 2008-11-27 |
RU2349679C1 RU2349679C1 (en) | 2009-03-20 |
Family
ID=40545272
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2007119212/02A RU2349679C1 (en) | 2007-05-23 | 2007-05-23 | Method of combination heat-resistant coating on turbine blades of gas-turbine engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2349679C1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2469129C1 (en) * | 2011-04-01 | 2012-12-10 | Общество с ограниченной ответственностью Научно-производственное предприятие "Защита-Юг" (ООО НПП "Защита-Юг") | Application method of combined thermal protective coating to part from heat-resistant alloys |
RU2755131C1 (en) * | 2020-10-20 | 2021-09-13 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Краснодарское высшее военное авиационное училище летчиков имени Героя Советского Союза А.К. Серова" | Method for applying combined heat-resistant coating to turbine blades of gte |
-
2007
- 2007-05-23 RU RU2007119212/02A patent/RU2349679C1/en active
Also Published As
Publication number | Publication date |
---|---|
RU2349679C1 (en) | 2009-03-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2009119821A (en) | CERAMIC COATING SYSTEM CREATING A THERMAL BARRIER WITH TWO CERAMIC LAYERS | |
CN101479398B (en) | Method for protecting components against hot corrosion and the protective components | |
JP2007262447A (en) | Oxidation-resistant film and its deposition method, thermal barrier coating, heat-resistant member, and gas turbine | |
GB2469762B (en) | Method for improving resistance to CMAS infiltration | |
RU2008121855A (en) | METHOD FOR APPLYING A GAS TURBINE SHOVEL AND SHOVEL | |
EP2149623A3 (en) | Thermal barrier coatings and methods of producing same | |
RU2012143608A (en) | METHOD FOR OBTAINING HEAT BARRIER PROTECTION AND MULTILAYER COATING, WAY TO FORM THE HEAT BARRIER | |
MX2009008250A (en) | Compositions for topical application comprising a peroxide and retinoid. | |
US20070122658A1 (en) | Mischmetal oxide tbc | |
EA201001516A1 (en) | GLAZING COATED WITH THIN LAYERS | |
EP3068921B1 (en) | Compressor blade with erosion resistant hard material coating | |
RU2009144424A (en) | HEAT PROTECTIVE COVERING FOR TURBINE SHOVELS AND METHOD FOR ITS PRODUCTION | |
JP6365969B2 (en) | Thermal barrier coating material, turbine member having the same, and thermal barrier coating method | |
JP2015518085A5 (en) | ||
CN104451675B (en) | Preparation method of ceramic sealing coating with high thermal shock resistance | |
RU2007119212A (en) | METHOD FOR APPLYING COMBINED HEAT PROTECTIVE COATING TO THE TURBINES OF TURBINES OF GTE | |
JP2012112043A (en) | Vanadium resistant coating system | |
JP5656528B2 (en) | High temperature resistant member and gas turbine | |
JP5657048B2 (en) | High temperature resistant member and gas turbine | |
RU2009135494A (en) | METHOD FOR FORMING HEAT PROTECTIVE COATING | |
RU2010115735A (en) | METHOD FOR PRODUCING HEAT-RESISTANT COATING ON GAS TURBINE BLADES | |
RU2011153506A (en) | METHOD FOR PRODUCING METAL-CERAMIC COATINGS ON THE DENTAL SURFACE | |
WO2016076305A1 (en) | Heat shielding coating and turbine member | |
RU88389U1 (en) | GASOTURBINE ENGINE TURBIN SHOWER WITH HEAT-RESISTANT COATING | |
RU2004117227A (en) | METHOD FOR APPLYING COMBINED HEAT-RESISTANT COATING TO TURBINE BLADES |