DE59802328D1 - GAS TURBINE SYSTEM WITH A COMBUSTION HOUSING LINED WITH CERAMIC STONES - Google Patents
GAS TURBINE SYSTEM WITH A COMBUSTION HOUSING LINED WITH CERAMIC STONESInfo
- Publication number
- DE59802328D1 DE59802328D1 DE59802328T DE59802328T DE59802328D1 DE 59802328 D1 DE59802328 D1 DE 59802328D1 DE 59802328 T DE59802328 T DE 59802328T DE 59802328 T DE59802328 T DE 59802328T DE 59802328 D1 DE59802328 D1 DE 59802328D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- turbine system
- combustion housing
- ceramic stones
- housing lined
- 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 - Lifetime
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)
- Ceramic Engineering (AREA)
- Combustion & Propulsion (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Solid-Fuel Combustion (AREA)
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 |
---|---|
DE59802328D1 true DE59802328D1 (en) | 2002-01-17 |
Family
ID=7819815
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19704976A Expired - Lifetime DE19704976C2 (en) | 1997-01-29 | 1997-01-29 | Gas turbine system with a combustion chamber casing lined with ceramic stones |
DE59802328T Expired - Lifetime DE59802328D1 (en) | 1997-01-29 | 1998-01-29 | GAS TURBINE SYSTEM WITH A COMBUSTION HOUSING LINED WITH CERAMIC STONES |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19704976A Expired - Lifetime DE19704976C2 (en) | 1997-01-29 | 1997-01-29 | Gas turbine system with a combustion chamber casing lined with ceramic stones |
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 |
CH690582A5 (en) * | 1995-06-26 | 2000-10-31 | Gen Electric | Composite material protected by multiple trains Over thermal barrier coating. |
-
1997
- 1997-01-29 DE DE19704976A patent/DE19704976C2/en not_active Expired - Lifetime
-
1998
- 1998-01-29 RU RU99118768/06A patent/RU2178530C2/en active
- 1998-01-29 UA UA99074363A patent/UA41485C2/en unknown
- 1998-01-29 JP JP53245998A patent/JP4294736B2/en not_active Expired - Lifetime
- 1998-01-29 WO PCT/DE1998/000324 patent/WO1998034068A1/en active IP Right Grant
- 1998-01-29 DE DE59802328T patent/DE59802328D1/en not_active Expired - Lifetime
- 1998-01-29 EP EP98909340A patent/EP0960308B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE19704976C2 (en) | 1999-02-25 |
EP0960308B1 (en) | 2001-12-05 |
JP4294736B2 (en) | 2009-07-15 |
UA41485C2 (en) | 2001-09-17 |
RU2178530C2 (en) | 2002-01-20 |
WO1998034068A1 (en) | 1998-08-06 |
EP0960308A1 (en) | 1999-12-01 |
JP2001509874A (en) | 2001-07-24 |
DE19704976A1 (en) | 1998-07-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |