EP2075506A3 - Brennkammerauskleidung - Google Patents

Brennkammerauskleidung Download PDF

Info

Publication number
EP2075506A3
EP2075506A3 EP08021918.1A EP08021918A EP2075506A3 EP 2075506 A3 EP2075506 A3 EP 2075506A3 EP 08021918 A EP08021918 A EP 08021918A EP 2075506 A3 EP2075506 A3 EP 2075506A3
Authority
EP
European Patent Office
Prior art keywords
reaction chamber
hollow sections
ceramic hollow
support structure
metallic
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.)
Granted
Application number
EP08021918.1A
Other languages
English (en)
French (fr)
Other versions
EP2075506A2 (de
EP2075506B1 (de
Inventor
Miklos Dr. Gerendas
Sermed Sadig
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
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 Rolls Royce Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Publication of EP2075506A2 publication Critical patent/EP2075506A2/de
Publication of EP2075506A3 publication Critical patent/EP2075506A3/de
Application granted granted Critical
Publication of EP2075506B1 publication Critical patent/EP2075506B1/de
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03041Effusion cooled combustion chamber walls or domes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03042Film cooled combustion chamber walls or domes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044Impingement cooled combustion chamber walls or subassemblies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Die Erfindung bezieht sich auf eine Brennkammer für eine Gasturbine mit einer metallischen Tragstruktur 6 sowie mit mehreren am Umfang verteilt angeordneten keramischen Hohlprofilen 2, welche an der Tragstruktur 6 befestigt sind, dadurch gekennzeichnet, dass die keramischen Hohlprofile 2 jeweils geradlinig ausgebildet und als einzelne Segmente angeordnet sind und dass in den keramischen Hohlprofilen 2 jeweils zumindest ein metallischer Hohlkörper 1 angeordnet ist, welcher an zumindest einer Wandung mit Luftdurchtrittsöffnungen 5 versehen ist und durch welche Kühlluft durchleitbar ist.
EP08021918.1A 2007-12-27 2008-12-17 Brennkammerauskleidung Expired - Fee Related EP2075506B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102007062699A DE102007062699A1 (de) 2007-12-27 2007-12-27 Brennkammerauskleidung

Publications (3)

Publication Number Publication Date
EP2075506A2 EP2075506A2 (de) 2009-07-01
EP2075506A3 true EP2075506A3 (de) 2014-11-12
EP2075506B1 EP2075506B1 (de) 2016-04-27

Family

ID=40482017

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08021918.1A Expired - Fee Related EP2075506B1 (de) 2007-12-27 2008-12-17 Brennkammerauskleidung

Country Status (3)

Country Link
US (1) US8074453B2 (de)
EP (1) EP2075506B1 (de)
DE (1) DE102007062699A1 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012213637A1 (de) * 2012-08-02 2014-02-06 Siemens Aktiengesellschaft Brennkammerkühlung
US9651258B2 (en) 2013-03-15 2017-05-16 Rolls-Royce Corporation Shell and tiled liner arrangement for a combustor
EP3022424B1 (de) * 2013-07-16 2019-10-09 United Technologies Corporation Keramikplattenanordnung eines gasturbinenmotors und verfahren zur herstellung einer keramikplattenanordnung eines gasturbinenmotors
CA2927502C (en) * 2013-10-17 2022-01-04 Harnischfeger Technologies, Inc. Liner system for a dipper

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6047552A (en) * 1996-09-26 2000-04-11 Siemens Aktiengesellschaft Heat-shield component with cooling-fluid return and heat-shield configuration for a component directing hot gas
EP1271056A1 (de) * 2001-06-20 2003-01-02 Siemens Aktiengesellschaft Gasturbinen-Brennkammer und für diese vorgesehenes Verfahren zur Luftführung
EP1431661A1 (de) * 2002-12-19 2004-06-23 Siemens Aktiengesellschaft Ströhmungsführungskörper

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3956886A (en) * 1973-12-07 1976-05-18 Joseph Lucas (Industries) Limited Flame tubes for gas turbine engines
US4269032A (en) * 1979-06-13 1981-05-26 General Motors Corporation Waffle pattern porous material
US4512699A (en) 1983-05-17 1985-04-23 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Daze fasteners
US4838031A (en) * 1987-08-06 1989-06-13 Avco Corporation Internally cooled combustion chamber liner
DE58908665D1 (de) * 1988-06-13 1995-01-05 Siemens Ag Hitzeschildanordnung mit geringem kühlfluidbedarf.
DE19502730A1 (de) 1995-01-28 1996-08-01 Abb Management Ag Keramische Auskleidung
DE19730751A1 (de) * 1996-07-24 1998-01-29 Siemens Ag Keramisches Bauteil für eine Wärmeschutzschicht sowie Wärmeschutzschicht
DE19727407A1 (de) * 1997-06-27 1999-01-07 Siemens Ag Hitzeschild
DE29714742U1 (de) * 1997-08-18 1998-12-17 Siemens AG, 80333 München Hitzeschildkomponente mit Kühlfluidrückführung und Hitzeschildanordnung für eine heißgasführende Komponente
EP0943867B1 (de) 1998-03-17 2002-12-18 ALSTOM (Switzerland) Ltd Keramische Auskleidung einer Brennkammer
FR2777634B1 (fr) * 1998-04-16 2000-05-19 Snecma Separateur pour chambre de combustion a deux tetes
DE10003728A1 (de) * 2000-01-28 2001-08-09 Siemens Ag Hitzeschildanordnung für eine Heißgas führende Komponente, insbesondere für Strukturteile von Gasturbinen
US6514046B1 (en) * 2000-09-29 2003-02-04 Siemens Westinghouse Power Corporation Ceramic composite vane with metallic substructure
EP1284390A1 (de) * 2001-06-27 2003-02-19 Siemens Aktiengesellschaft Hitzeschildanordnung für eine Heissgas führende Komponente, insbesondere für Strukturteile von Gasturbinen
US7908867B2 (en) * 2007-09-14 2011-03-22 Siemens Energy, Inc. Wavy CMC wall hybrid ceramic apparatus

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6047552A (en) * 1996-09-26 2000-04-11 Siemens Aktiengesellschaft Heat-shield component with cooling-fluid return and heat-shield configuration for a component directing hot gas
EP1271056A1 (de) * 2001-06-20 2003-01-02 Siemens Aktiengesellschaft Gasturbinen-Brennkammer und für diese vorgesehenes Verfahren zur Luftführung
EP1431661A1 (de) * 2002-12-19 2004-06-23 Siemens Aktiengesellschaft Ströhmungsführungskörper

Also Published As

Publication number Publication date
EP2075506A2 (de) 2009-07-01
US8074453B2 (en) 2011-12-13
DE102007062699A1 (de) 2009-07-02
EP2075506B1 (de) 2016-04-27
US20090193810A1 (en) 2009-08-06

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