IN165091B - - Google Patents

Info

Publication number
IN165091B
IN165091B IN855/CAL/86A IN855CA1986A IN165091B IN 165091 B IN165091 B IN 165091B IN 855CA1986 A IN855CA1986 A IN 855CA1986A IN 165091 B IN165091 B IN 165091B
Authority
IN
India
Application number
IN855/CAL/86A
Other languages
English (en)
Inventor
Bernard Becker
Helmut Maghon
Wilhelm Schulten
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Publication of IN165091B publication Critical patent/IN165091B/en

Links

Classifications

    • 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
    • F23R3/002—Wall structures

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IN855/CAL/86A 1985-12-02 1986-11-25 IN165091B (el)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3542531 1985-12-02
DE3623744 1986-07-14

Publications (1)

Publication Number Publication Date
IN165091B true IN165091B (el) 1989-08-12

Family

ID=25838380

Family Applications (1)

Application Number Title Priority Date Filing Date
IN855/CAL/86A IN165091B (el) 1985-12-02 1986-11-25

Country Status (4)

Country Link
US (1) US4749029A (el)
EP (1) EP0224817B1 (el)
DE (1) DE3664374D1 (el)
IN (1) IN165091B (el)

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JPH03504999A (ja) * 1988-06-13 1991-10-31 シーメンス、アクチエンゲゼルシヤフト 高温流体を導く構造物のための熱遮蔽装置
US5072785A (en) * 1990-06-12 1991-12-17 United Technologies Corporation Convectively cooled bolt assembly
US5113660A (en) * 1990-06-27 1992-05-19 The United States Of America As Represented By The Secretary Of The Air Force High temperature combustor liner
US5129447A (en) * 1991-05-20 1992-07-14 United Technologies Corporation Cooled bolting arrangement
US5331816A (en) * 1992-10-13 1994-07-26 United Technologies Corporation Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles
ES2117402T3 (es) * 1994-01-24 1998-08-01 Siemens Ag Procedimiento para la combustion de un combustible en aire comprimido.
DE19502730A1 (de) * 1995-01-28 1996-08-01 Abb Management Ag Keramische Auskleidung
US5755093A (en) * 1995-05-01 1998-05-26 United Technologies Corporation Forced air cooled gas turbine exhaust liner
DE19623300A1 (de) * 1996-06-11 1997-12-18 Siemens Ag Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen, mit geschichtetem Aufbau
FR2752916B1 (fr) * 1996-09-05 1998-10-02 Snecma Chemise de protection thermique pour chambre de combustion de turboreacteur
WO1998013645A1 (de) 1996-09-26 1998-04-02 Siemens Aktiengesellschaft Hitzeschildkomponente mit kühlfluidrückführung und hitzeschildanordnung für eine heissgasführende komponente
DE59706557D1 (de) * 1997-07-28 2002-04-11 Alstom Keramische Auskleidung
DE29714742U1 (de) 1997-08-18 1998-12-17 Siemens AG, 80333 München Hitzeschildkomponente mit Kühlfluidrückführung und Hitzeschildanordnung für eine heißgasführende Komponente
JP4172913B2 (ja) * 1998-03-19 2008-10-29 シーメンス アクチエンゲゼルシヤフト 燃焼器用壁セグメントおよび燃焼器
EP1006315B1 (de) 1998-11-30 2004-01-21 ALSTOM (Switzerland) Ltd Keramische Auskleidung für einen Brennraum
US6286317B1 (en) * 1998-12-18 2001-09-11 General Electric Company Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity
GB9926257D0 (en) 1999-11-06 2000-01-12 Rolls Royce Plc Wall elements for gas turbine engine combustors
DE10114619B4 (de) * 2000-03-27 2006-07-27 Cummins Inc., Columbus Belüftendes Befestigungselement
DE10036211A1 (de) * 2000-07-25 2002-02-07 Rolls Royce Deutschland Brennkammerschindel
EP1260767A1 (de) 2001-05-25 2002-11-27 Siemens Aktiengesellschaft Hitzeschildanordnung für eine Heissgas führende Komponente, insbesondere für Strukturteile von Gasturbine, sowie Verfahren zum Herstellen einer derartigen Anordnung
EP1284390A1 (de) 2001-06-27 2003-02-19 Siemens Aktiengesellschaft Hitzeschildanordnung für eine Heissgas führende Komponente, insbesondere für Strukturteile von Gasturbinen
US6711900B1 (en) * 2003-02-04 2004-03-30 Pratt & Whitney Canada Corp. Combustor liner V-band design
US7146815B2 (en) * 2003-07-31 2006-12-12 United Technologies Corporation Combustor
US7114321B2 (en) * 2003-07-31 2006-10-03 General Electric Company Thermal isolation device for liquid fuel components
EP1507116A1 (de) 2003-08-13 2005-02-16 Siemens Aktiengesellschaft Hitzeschildanordnung für eine ein Heissgas führende Komponente, insbesondere für eine Brennkammer einer Gasturbine
US7338244B2 (en) * 2004-01-13 2008-03-04 Siemens Power Generation, Inc. Attachment device for turbine combustor liner
US20080003078A1 (en) * 2006-05-02 2008-01-03 United Technologies Corporation Fastener
EP1865258A1 (de) * 2006-06-06 2007-12-12 Siemens Aktiengesellschaft Gepanzerte Maschinenkomponente und Gasturbine
GB0705458D0 (en) * 2007-03-22 2007-05-02 Rolls Royce Plc A Location ring arrangement
US8435007B2 (en) * 2008-12-29 2013-05-07 Rolls-Royce Corporation Hybrid turbomachinery component for a gas turbine engine
US8973375B2 (en) * 2008-12-31 2015-03-10 Rolls-Royce North American Technologies, Inc. Shielding for a gas turbine engine component
ES2531099T3 (es) * 2009-06-09 2015-03-10 Siemens Ag Disposición de elemento de escudo térmico y procedimiento para el montaje de un elemento de escudo térmico
GB0913580D0 (en) * 2009-08-05 2009-09-16 Rolls Royce Plc Combustor tile
CH703656A1 (de) 2010-08-27 2012-02-29 Alstom Technology Ltd Von Heissgasen durchströmbarer Gehäusekörper mit innerem Hitzeschild.
US10378775B2 (en) * 2012-03-23 2019-08-13 Pratt & Whitney Canada Corp. Combustor heat shield
US20130298564A1 (en) * 2012-05-14 2013-11-14 General Electric Company Cooling system and method for turbine system
US9243801B2 (en) * 2012-06-07 2016-01-26 United Technologies Corporation Combustor liner with improved film cooling
US9335049B2 (en) 2012-06-07 2016-05-10 United Technologies Corporation Combustor liner with reduced cooling dilution openings
US9217568B2 (en) 2012-06-07 2015-12-22 United Technologies Corporation Combustor liner with decreased liner cooling
US9239165B2 (en) 2012-06-07 2016-01-19 United Technologies Corporation Combustor liner with convergent cooling channel
DE102012213637A1 (de) * 2012-08-02 2014-02-06 Siemens Aktiengesellschaft Brennkammerkühlung
EP2711630A1 (de) 2012-09-21 2014-03-26 Siemens Aktiengesellschaft Vorrichtung zum Kühlen einer Tragstruktur eines Hitzeschildes und Hitzeschild
EP2711634A1 (de) * 2012-09-21 2014-03-26 Siemens Aktiengesellschaft Hitzeschild mit einer Tragstruktur und Verfahren zum Kühlen der Tragstruktur
US9322334B2 (en) * 2012-10-23 2016-04-26 General Electric Company Deformable mounting assembly
DE102012023297A1 (de) * 2012-11-28 2014-06-12 Rolls-Royce Deutschland Ltd & Co Kg Schindelbefestigungsanordnung einer Gasturbinenbrennkammer
ITMI20131115A1 (it) * 2013-07-03 2015-01-04 Ansaldo Energia Spa Piastrella per il rivestimento di camere di combustione, in particolare di impianti per la produzione di energia elettrica a turbina a gas, e camera di combustione comprendente detta piastrella
DE102013226490A1 (de) * 2013-12-18 2015-06-18 Rolls-Royce Deutschland Ltd & Co Kg Gekühlte Flanschverbindung eines Gasturbinentriebwerks
DE102013226488A1 (de) * 2013-12-18 2015-06-18 Rolls-Royce Deutschland Ltd & Co Kg Unterlegscheibe einer Brennkammerschindel einer Gasturbine
DE102015202097A1 (de) * 2015-02-06 2016-08-11 Siemens Aktiengesellschaft Ringbrennkammer mit Bypasssegment
US9869204B2 (en) * 2015-03-06 2018-01-16 United Technologies Corporation Integrated inner case heat shield
US10767863B2 (en) * 2015-07-22 2020-09-08 Rolls-Royce North American Technologies, Inc. Combustor tile with monolithic inserts
US10935236B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10655853B2 (en) * 2016-11-10 2020-05-19 United Technologies Corporation Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
US10830433B2 (en) * 2016-11-10 2020-11-10 Raytheon Technologies Corporation Axial non-linear interface for combustor liner panels in a gas turbine combustor
US10935235B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
DE102017212575A1 (de) * 2017-07-21 2019-01-24 Siemens Aktiengesellschaft Verfahren zur Erhöhung der Leistung einer Gasturbine
US20190112946A1 (en) * 2017-10-13 2019-04-18 United Technologies Corporation Double wall service tube with annular airflow passage
US10801469B2 (en) * 2017-11-07 2020-10-13 General Electric Company Wind blade joints with floating connectors
US11204169B2 (en) * 2019-07-19 2021-12-21 Pratt & Whitney Canada Corp. Combustor of gas turbine engine and method
US10969106B2 (en) * 2019-08-13 2021-04-06 General Electric Company Axial retention assembly for combustor components of a gas turbine engine
FR3111414B1 (fr) * 2020-06-15 2022-09-02 Safran Helicopter Engines Production par fabrication additive de pièces complexes
RU209216U1 (ru) * 2021-08-30 2022-02-07 Антон Владимирович Новиков Теплозащитный экран для камеры сгорания газовой турбины
RU209161U1 (ru) * 2021-12-01 2022-02-03 Антон Владимирович Новиков Теплозащитный экран для камеры сгорания газовой турбины

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GB647302A (en) * 1948-05-14 1950-12-13 Edgar Phillips Peregrine Improvements in or relating to linings for combustion chambers and the like
BE535497A (el) * 1954-02-26
US2938333A (en) * 1957-03-18 1960-05-31 Gen Motors Corp Combustion chamber liner construction
GB1038661A (en) * 1961-12-05 1966-08-10 Ass Elect Ind Improvements relating to metallic gas turbine combustion chambers
DE1173734B (de) * 1962-10-11 1964-07-09 Siemens Ag Brennkammer, insbesondere fuer Gasturbinen, mit einer aus feuerfesten Steinen aufgebauten Auskleidung
GB1487064A (en) * 1974-08-23 1977-09-28 Rolls Royce Wall structure for hot fluid streams
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
US4071194A (en) * 1976-10-28 1978-01-31 The United States Of America As Represented By The Secretary Of The Navy Means for cooling exhaust nozzle sidewalls
JPS5857658B2 (ja) * 1980-04-02 1983-12-21 工業技術院長 セラミツクスによる高熱曝露壁面の熱遮断構造
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
US4422300A (en) * 1981-12-14 1983-12-27 United Technologies Corporation Prestressed combustor liner for gas turbine engine

Also Published As

Publication number Publication date
EP0224817A1 (de) 1987-06-10
DE3664374D1 (en) 1989-08-17
EP0224817B1 (de) 1989-07-12
US4749029A (en) 1988-06-07

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