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EP1635118A3 - Hot gas chamber and shingle for a hot gas chamber - Google Patents

Hot gas chamber and shingle for a hot gas chamber Download PDF

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Publication number
EP1635118A3
EP1635118A3 EP05017348A EP05017348A EP1635118A3 EP 1635118 A3 EP1635118 A3 EP 1635118A3 EP 05017348 A EP05017348 A EP 05017348A EP 05017348 A EP05017348 A EP 05017348A EP 1635118 A3 EP1635118 A3 EP 1635118A3
Authority
EP
European Patent Office
Prior art keywords
hot gas
gas chamber
shingle
chamber
chamber liner
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
EP05017348A
Other languages
German (de)
French (fr)
Other versions
EP1635118B1 (en
EP1635118A2 (en
Inventor
Bernhard Heidenreich
Michael Kriescher
Stefan Dr. Hackemann
Bernhard Kanka
Walter Luxem
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
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 Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of EP1635118A2 publication Critical patent/EP1635118A2/en
Publication of EP1635118A3 publication Critical patent/EP1635118A3/en
Application granted granted Critical
Publication of EP1635118B1 publication Critical patent/EP1635118B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Gas Burners (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Furnace Details (AREA)
  • Fuel Cell (AREA)

Abstract

Es wird eine Heißgaskammer, insbesondere Brennkammer, umfassend eine Kammerauskleidung und eine Tragstruktur für die Kammerauskleidung, vorgeschlagen, wobei zwischen der Tragstruktur und der Kammerauskleidung ein oder mehrere Zwischenräume gebildet sind, wobei die Kammerauskleidung eine Mehrzahl von Schindeln umfaßt und die Schindeln aus einem keramischen Material hergestellt sind.

Figure imgaf001
There is provided a hot gas chamber, particularly a combustion chamber, comprising a chamber liner and a support structure for the chamber liner, wherein one or more gaps are formed between the support structure and the chamber liner, the chamber liner comprising a plurality of shingles and the shingles made of a ceramic material are.
Figure imgaf001
EP20050017348 2004-09-10 2005-08-10 Hot gas chamber and shingle for a hot gas chamber Expired - Lifetime EP1635118B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE200410044852 DE102004044852A1 (en) 2004-09-10 2004-09-10 Hot gas chamber and shingle for a hot gas chamber

Publications (3)

Publication Number Publication Date
EP1635118A2 EP1635118A2 (en) 2006-03-15
EP1635118A3 true EP1635118A3 (en) 2006-04-19
EP1635118B1 EP1635118B1 (en) 2008-09-03

Family

ID=35431256

Family Applications (1)

Application Number Title Priority Date Filing Date
EP20050017348 Expired - Lifetime EP1635118B1 (en) 2004-09-10 2005-08-10 Hot gas chamber and shingle for a hot gas chamber

Country Status (2)

Country Link
EP (1) EP1635118B1 (en)
DE (2) DE102004044852A1 (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8256223B2 (en) * 2007-10-16 2012-09-04 United Technologies Corporation Ceramic combustor liner panel for a gas turbine engine
FR2929689B1 (en) * 2008-04-03 2013-04-12 Snecma Propulsion Solide GAS TURBINE COMBUSTION CHAMBER WITH SECTORIZED INTERNAL AND EXTERNAL WALLS
FR2929690B1 (en) 2008-04-03 2012-08-17 Snecma Propulsion Solide COMBUSTION CHAMBER SECTORIZED IN CMC FOR GAS TURBINE
DE102013220482B3 (en) * 2013-10-10 2015-04-09 Deutsches Zentrum für Luft- und Raumfahrt e.V. Retaining device for thermal expansion-compensating, clamping fixation of a heat-resistant wall element of a combustion chamber
US9664389B2 (en) 2013-12-12 2017-05-30 United Technologies Corporation Attachment assembly for protective panel
GB201322838D0 (en) 2013-12-23 2014-02-12 Rolls Royce Plc A combustion chamber
DE102014204481A1 (en) 2014-03-11 2015-09-17 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine
DE102014204476A1 (en) * 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine
GB201413194D0 (en) 2014-07-25 2014-09-10 Rolls Royce Plc A liner element for a combustor, and a related method
GB201501817D0 (en) 2015-02-04 2015-03-18 Rolls Royce Plc A combustion chamber and a combustion chamber segment
DE102015225107A1 (en) 2015-12-14 2017-06-14 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber with shingle fastening by means of locking elements
US10663167B2 (en) 2017-06-16 2020-05-26 General Electric Company Combustor assembly with CMC combustor dome
DE102018200926A1 (en) * 2018-01-22 2019-07-25 Siemens Aktiengesellschaft Component for positioning a heat shield element
CN111707473B (en) * 2020-06-19 2022-05-13 中航工程集成设备有限公司 Engine test run injection cylinder with tile type lining plate protection structure and design method thereof
CN116928695A (en) * 2022-03-31 2023-10-24 通用电气公司 Annular dome assembly for a combustor
US12313261B1 (en) 2024-04-05 2025-05-27 Rtx Corporation Combustor liner panels

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1052750B (en) * 1954-02-26 1959-03-12 Rolls Royce Wall of a combustion chamber for liquid fuel, especially in gas turbines
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly
EP0895027A1 (en) * 1997-07-28 1999-02-03 Abb Research Ltd. Ceramic lining
EP1310735A1 (en) * 2001-11-12 2003-05-14 Rolls-Royce Deutschland Ltd & Co KG Heat shield arrangement with sealing elements

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1052750B (en) * 1954-02-26 1959-03-12 Rolls Royce Wall of a combustion chamber for liquid fuel, especially in gas turbines
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly
EP0895027A1 (en) * 1997-07-28 1999-02-03 Abb Research Ltd. Ceramic lining
EP1310735A1 (en) * 2001-11-12 2003-05-14 Rolls-Royce Deutschland Ltd & Co KG Heat shield arrangement with sealing elements

Also Published As

Publication number Publication date
EP1635118B1 (en) 2008-09-03
DE102004044852A1 (en) 2006-03-16
DE502005005244D1 (en) 2008-10-16
EP1635118A2 (en) 2006-03-15

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