EP2093487A3 - Gas turbine combustion chamber with ceramic flame tube - Google Patents

Gas turbine combustion chamber with ceramic flame tube Download PDF

Info

Publication number
EP2093487A3
EP2093487A3 EP09002226.0A EP09002226A EP2093487A3 EP 2093487 A3 EP2093487 A3 EP 2093487A3 EP 09002226 A EP09002226 A EP 09002226A EP 2093487 A3 EP2093487 A3 EP 2093487A3
Authority
EP
European Patent Office
Prior art keywords
combustion chamber
gas turbine
flame tube
turbine combustion
ceramic flame
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
EP09002226.0A
Other languages
German (de)
French (fr)
Other versions
EP2093487B1 (en
EP2093487A2 (en
Inventor
Miklos Dr. Gerendás
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 EP2093487A2 publication Critical patent/EP2093487A2/en
Publication of EP2093487A3 publication Critical patent/EP2093487A3/en
Application granted granted Critical
Publication of EP2093487B1 publication Critical patent/EP2093487B1/en
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/04—Supports for linings
    • 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
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2212/00—Burner material specifications
    • F23D2212/10—Burner material specifications ceramic

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 vorliegende Erfindung betrifft eine Gasturbinenbrennkammer mit einem im Wesentlichen zylindrischen Flammenrohr (2), welches aus einem keramischen Werkstoff gefertigt ist und in Umfangsrichtung in mehrere Umfangselemente (10,11,12) unterteilt ist.

Figure imgaf001
The present invention relates to a gas turbine combustion chamber with a substantially cylindrical flame tube (2), which is made of a ceramic material and in the circumferential direction into a plurality of peripheral elements (10,11,12) is divided.
Figure imgaf001
EP09002226.0A 2008-02-21 2009-02-17 Arrangement with an annular gas turbine combustion chamber with a ceramic flame tube for an engine Not-in-force EP2093487B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102008010294A DE102008010294A1 (en) 2008-02-21 2008-02-21 Gas turbine combustor with ceramic flame tube

Publications (3)

Publication Number Publication Date
EP2093487A2 EP2093487A2 (en) 2009-08-26
EP2093487A3 true EP2093487A3 (en) 2013-11-27
EP2093487B1 EP2093487B1 (en) 2016-08-17

Family

ID=40512449

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09002226.0A Not-in-force EP2093487B1 (en) 2008-02-21 2009-02-17 Arrangement with an annular gas turbine combustion chamber with a ceramic flame tube for an engine

Country Status (3)

Country Link
US (1) US8281598B2 (en)
EP (1) EP2093487B1 (en)
DE (1) DE102008010294A1 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014149108A1 (en) 2013-03-15 2014-09-25 Graves Charles B Shell and tiled liner arrangement for a combustor
US10100737B2 (en) 2013-05-16 2018-10-16 Siemens Energy, Inc. Impingement cooling arrangement having a snap-in plate
RU2598964C2 (en) * 2014-12-12 2016-10-10 Федеральное агентство научных организаций Федеральное Государственное Бюджетное Научное Учреждение Всероссийский научно-исследовательский институт электрификации сельского хозяйства (ФГБНУ ВИЭСХ) Combustion chamber with adjustable opening to supply cooling air for micro gas turbine engine
US10533740B2 (en) 2015-07-09 2020-01-14 Carrier Corporation Inward fired ultra low NOX insulating burner flange
CN205016725U (en) * 2015-09-10 2016-02-03 欧品电子(昆山)有限公司 Supply socket terminal
DE102015226079A1 (en) * 2015-12-18 2017-06-22 Dürr Systems Ag Combustion chamber device and gas turbine device
US11015812B2 (en) * 2018-05-07 2021-05-25 Rolls-Royce North American Technologies Inc. Combustor bolted segmented architecture
CN110107402B (en) * 2019-04-29 2021-06-08 中国航空工业集团公司金城南京机电液压工程研究中心 Ceramic turbine engine
CN114484505B (en) * 2022-01-27 2023-05-16 西安鑫垚陶瓷复合材料有限公司 Ceramic matrix composite full-ring flame tube, shaping mold and preparation method thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB543918A (en) * 1939-09-29 1942-03-19 Bbc Brown Boveri & Cie Improvements and relating to combustion chambers
US3854503A (en) * 1971-08-05 1974-12-17 Lucas Industries Ltd Flame tubes
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1346600A (en) * 1913-10-10 1920-07-13 Stock Motorpflug Gmbh Moldboard for plows
US2686655A (en) * 1949-09-02 1954-08-17 Maschf Augsburg Nuernberg Ag Joint between ceramic and metallic parts
GB1450894A (en) 1972-11-01 1976-09-29 Lucas Industries Ltd Flame tubes
US3956886A (en) * 1973-12-07 1976-05-18 Joseph Lucas (Industries) Limited Flame tubes for gas turbine engines
DE4114768A1 (en) * 1990-05-17 1991-11-21 Siemens Ag Ceramic heat shield for gas turbine flame tube - comprises number of blocks arranged next to one another clamped on cold side of holder
US5636508A (en) * 1994-10-07 1997-06-10 Solar Turbines Incorporated Wedge edge ceramic combustor tile
DE59806717D1 (en) * 1998-03-17 2003-01-30 Alstom Switzerland Ltd Ceramic lining of a combustion chamber
US6397603B1 (en) 2000-05-05 2002-06-04 The United States Of America As Represented By The Secretary Of The Air Force Conbustor having a ceramic matrix composite liner
US7665307B2 (en) * 2005-12-22 2010-02-23 United Technologies Corporation Dual wall combustor liner
DE102006060857B4 (en) * 2006-12-22 2014-02-13 Deutsches Zentrum für Luft- und Raumfahrt e.V. CMC combustion chamber lining in double-layer construction
US7861535B2 (en) * 2007-09-24 2011-01-04 United Technologies Corporation Self-aligning liner support hanger

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB543918A (en) * 1939-09-29 1942-03-19 Bbc Brown Boveri & Cie Improvements and relating to combustion chambers
US3854503A (en) * 1971-08-05 1974-12-17 Lucas Industries Ltd Flame tubes
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly

Also Published As

Publication number Publication date
DE102008010294A1 (en) 2009-08-27
US8281598B2 (en) 2012-10-09
EP2093487B1 (en) 2016-08-17
US20090235667A1 (en) 2009-09-24
EP2093487A2 (en) 2009-08-26

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