UA41485C2 - Gas-turbine unit with body of combustion chamber the inner side of which is covered with massif ceramic bricks - Google Patents
Gas-turbine unit with body of combustion chamber the inner side of which is covered with massif ceramic bricksInfo
- Publication number
- UA41485C2 UA41485C2 UA99074363A UA99074363A UA41485C2 UA 41485 C2 UA41485 C2 UA 41485C2 UA 99074363 A UA99074363 A UA 99074363A UA 99074363 A UA99074363 A UA 99074363A UA 41485 C2 UA41485 C2 UA 41485C2
- Authority
- UA
- Ukraine
- Prior art keywords
- covered
- gas
- combustion chamber
- turbine unit
- massif
- Prior art date
Links
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
- F01D5/288—Protective coatings for blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Ceramic Engineering (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Solid-Fuel Combustion (AREA)
Abstract
This invention relates to gas-turbine unit with body of combustion chamber the inner side of which is covered with ceramic bricks. Gas-turbine unit with body of combustion chamber the inner side of which is covered with massif ceramic bricks, with rotor equipped with working blades and body equipped with guide blades, at that at least first blades have at the side turned to the turbine ceramic heat-insulation layer, at that to the surface of ceramic bricks coating is applied.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19704976A DE19704976C2 (en) | 1997-01-29 | 1997-01-29 | Gas turbine system with a combustion chamber casing lined with ceramic stones |
PCT/DE1998/000324 WO1998034068A1 (en) | 1997-01-29 | 1998-01-29 | Gas turbine installation with a ceramic-covered combustion chamber housing |
Publications (1)
Publication Number | Publication Date |
---|---|
UA41485C2 true UA41485C2 (en) | 2001-09-17 |
Family
ID=7819815
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UA99074363A UA41485C2 (en) | 1997-01-29 | 1998-01-29 | Gas-turbine unit with body of combustion chamber the inner side of which is covered with massif ceramic bricks |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0960308B1 (en) |
JP (1) | JP4294736B2 (en) |
DE (2) | DE19704976C2 (en) |
RU (1) | RU2178530C2 (en) |
UA (1) | UA41485C2 (en) |
WO (1) | WO1998034068A1 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1072573A1 (en) | 1999-07-30 | 2001-01-31 | Siemens Aktiengesellschaft | Method of making a refractory body and ceramic combustion chamber stone |
PL200773B1 (en) * | 2003-04-18 | 2009-02-27 | System Spo & Lstrok Ka Akcyjna | Method for applying anticorrosive coating on furnace waterwalls |
US20100285415A1 (en) * | 2007-11-23 | 2010-11-11 | Boettcher Andreas | Burner Element and Burner Having Aluminum Oxide Coating and Method for Coating a Burner Element |
EP2169311A1 (en) * | 2008-09-29 | 2010-03-31 | Siemens Aktiengesellschaft | Material mixture for producing a fire-retardant material, fire-retardant moulding body and method for its manufacture |
EP2233835A1 (en) * | 2009-03-23 | 2010-09-29 | Siemens Aktiengesellschaft | Combustion chamber brazed with ceramic inserts |
ITMI20111519A1 (en) | 2011-08-08 | 2013-02-09 | Ansaldo Energia Spa | TILE OF CERAMIC MATERIAL FOR THE COATING OF COMBUSTION CHAMBERS, IN PARTICULAR OF GAS TURBINES, AND ITS RELATED MANUFACTURING METHOD |
RU2554690C1 (en) * | 2014-07-01 | 2015-06-27 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения"(АО"ВПК"НПО машиностроения") | Cruise missile engine combustion chamber |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL69245C (en) * | 1946-01-09 | |||
US2763919A (en) * | 1950-07-28 | 1956-09-25 | Thompson Prod Inc | Coated refractory body |
US4159357A (en) * | 1975-03-13 | 1979-06-26 | Motoren- Und Turbinen-Union Munchen Gmbh | Process for surface treating parts made of ceramic material |
DE2630247A1 (en) * | 1976-07-06 | 1978-01-19 | Daimler Benz Ag | Exhaust gas pipe for internal combustion engines - lined with thermal insulation so gas has high temp. when it meets purificn. catalyst |
DE3446649A1 (en) * | 1984-12-20 | 1986-06-26 | G + H Montage Gmbh, 6700 Ludwigshafen | Lining for high-temperature gas turbines |
DE3638658C1 (en) * | 1986-11-12 | 1988-04-21 | Daimler Benz Ag | Heat-insulating lining for a gas turbine |
AU2211488A (en) * | 1987-10-01 | 1989-04-06 | Gte Laboratories Incorporated | Oxidation resistant, high temperature thermal cyling resistant coatings on silicon-based substrates and process for the production thereof |
US5169674A (en) * | 1990-10-23 | 1992-12-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method of applying a thermal barrier coating system to a substrate |
US5391404A (en) * | 1993-03-15 | 1995-02-21 | The United States Of America As Represented By The National Aeronautics And Space Administration | Plasma sprayed mullite coatings on silicon-base ceramics |
DE4343319A1 (en) * | 1993-12-18 | 1995-06-22 | Abb Patent Gmbh | Combustion chamber with a ceramic lining |
JP4245661B2 (en) * | 1995-06-26 | 2009-03-25 | ゼネラル・エレクトリック・カンパニイ | Thermal barrier coating composite protected by multiple coatings |
-
1997
- 1997-01-29 DE DE19704976A patent/DE19704976C2/en not_active Expired - Lifetime
-
1998
- 1998-01-29 UA UA99074363A patent/UA41485C2/en unknown
- 1998-01-29 DE DE59802328T patent/DE59802328D1/en not_active Expired - Lifetime
- 1998-01-29 JP JP53245998A patent/JP4294736B2/en not_active Expired - Lifetime
- 1998-01-29 EP EP98909340A patent/EP0960308B1/en not_active Expired - Lifetime
- 1998-01-29 WO PCT/DE1998/000324 patent/WO1998034068A1/en active IP Right Grant
- 1998-01-29 RU RU99118768/06A patent/RU2178530C2/en active
Also Published As
Publication number | Publication date |
---|---|
DE59802328D1 (en) | 2002-01-17 |
WO1998034068A1 (en) | 1998-08-06 |
EP0960308B1 (en) | 2001-12-05 |
DE19704976C2 (en) | 1999-02-25 |
EP0960308A1 (en) | 1999-12-01 |
JP4294736B2 (en) | 2009-07-15 |
DE19704976A1 (en) | 1998-07-30 |
RU2178530C2 (en) | 2002-01-20 |
JP2001509874A (en) | 2001-07-24 |
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