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 bricks

Info

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
Application number
UA99074363A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Андреас НАЙДЕЛЬ
Клаус РАШКЕ
Original Assignee
Сіменс Акцієнгезельшафт
Сименс Акциенгезельшафт
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Сіменс Акцієнгезельшафт, Сименс Акциенгезельшафт filed Critical Сіменс Акцієнгезельшафт
Publication of UA41485C2 publication Critical patent/UA41485C2/en

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.
UA99074363A 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 UA41485C2 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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

Similar Documents

Publication Publication Date Title
GB2317005B (en) Gas turbine engine combustion chamber with thermal protective lining
CA2189641A1 (en) Bearing support housing
GB2327467B (en) Gas or steam turbine blade
CA2301775A1 (en) Method of manufacturing a diamond-silicon carbide-silicon composite and a composite produced by this method
BG105542A (en) Reduction in the noise produced by a rotor blade of a wind turbine
ZA997089B (en) Gas turbine power augmentation.
WO2000048429A3 (en) Infrared heater and components thereof
GB9904221D0 (en) Gas turbine engine bearing arrangement
DE69816291D1 (en) THICKER WITH LASER SEGMENTED CERAMIC HEAT SHIELD FOR THE RIFLE RING OF TURBINES
SG83157A1 (en) Laser shock peened gas turbine engine seal teeth
UA41485C2 (en) Gas-turbine unit with body of combustion chamber the inner side of which is covered with massif ceramic bricks
AU2471700A (en) Gas turbine engine
BR9916032B1 (en) ceramic lighter, method of using a polycrystalline thickened hot surface ceramic lighter.
DE69828224D1 (en) GAS TURBINE CHAMBER WITH STEAM COOLING
BR9915412A (en) Engine valve assembly
UA73042C2 (en) Ramjet air-jet engine
GB2345943B (en) Precision crowning of blade attachments in gas turbines
GB9825504D0 (en) An engine
EG22526A (en) Combustion chamber for gas turbine
WO1998053850A3 (en) Compositions and means for the treatment of burns and other cutaneous traumas
DE59806717D1 (en) Ceramic lining of a combustion chamber
BR9916138A (en) Brick made of refractory material, and use of it
SE8200221L (en) HARD COVER CHAIN
RU99118768A (en) GAS TURBINE INSTALLATION WITH FACED CERAMIC STONES COMBUSTION CHAMBER HOUSING
CA2239571A1 (en) An improved strain relief main shaft assembly