CH707828A2 - Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine. - Google Patents

Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine. Download PDF

Info

Publication number
CH707828A2
CH707828A2 CH00398/14A CH3982014A CH707828A2 CH 707828 A2 CH707828 A2 CH 707828A2 CH 00398/14 A CH00398/14 A CH 00398/14A CH 3982014 A CH3982014 A CH 3982014A CH 707828 A2 CH707828 A2 CH 707828A2
Authority
CH
Switzerland
Prior art keywords
main body
transition
section
combustor liner
combustion
Prior art date
Application number
CH00398/14A
Other languages
German (de)
English (en)
Inventor
Patrick Benedict Melton
Lucas John Stoia
Richard Martin Dicinto
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH707828A2 publication Critical patent/CH707828A2/de

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
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones

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)
CH00398/14A 2013-03-18 2014-03-17 Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine. CH707828A2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/845,384 US9383104B2 (en) 2013-03-18 2013-03-18 Continuous combustion liner for a combustor of a gas turbine

Publications (1)

Publication Number Publication Date
CH707828A2 true CH707828A2 (de) 2014-09-30

Family

ID=51419073

Family Applications (1)

Application Number Title Priority Date Filing Date
CH00398/14A CH707828A2 (de) 2013-03-18 2014-03-17 Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine.

Country Status (5)

Country Link
US (1) US9383104B2 (enExample)
JP (1) JP6306908B2 (enExample)
CN (1) CN104061595B (enExample)
CH (1) CH707828A2 (enExample)
DE (1) DE102014103022B4 (enExample)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9453424B2 (en) * 2013-10-21 2016-09-27 Siemens Energy, Inc. Reverse bulk flow effusion cooling
US20150159877A1 (en) * 2013-12-06 2015-06-11 General Electric Company Late lean injection manifold mixing system
US9803555B2 (en) * 2014-04-23 2017-10-31 General Electric Company Fuel delivery system with moveably attached fuel tube
US10066837B2 (en) 2015-02-20 2018-09-04 General Electric Company Combustor aft mount assembly
US20160265781A1 (en) * 2015-03-10 2016-09-15 General Electric Company Air shield for a fuel injector of a combustor
US20160281992A1 (en) * 2015-03-24 2016-09-29 General Electric Company Injection boss for a unibody combustor
EP3325887A1 (en) * 2015-07-24 2018-05-30 Siemens Aktiengesellschaft Gas turbine transition duct with late lean injection having reduced combustion residence time
US9989260B2 (en) * 2015-12-22 2018-06-05 General Electric Company Staged fuel and air injection in combustion systems of gas turbines
US10228141B2 (en) * 2016-03-04 2019-03-12 General Electric Company Fuel supply conduit assemblies
US10203114B2 (en) 2016-03-04 2019-02-12 General Electric Company Sleeve assemblies and methods of fabricating same
US20170260866A1 (en) * 2016-03-10 2017-09-14 Siemens Energy, Inc. Ducting arrangement in a combustion system of a gas turbine engine
US10851999B2 (en) 2016-12-30 2020-12-01 General Electric Company Fuel injectors and methods of use in gas turbine combustor
US10513987B2 (en) 2016-12-30 2019-12-24 General Electric Company System for dissipating fuel egress in fuel supply conduit assemblies
US10865992B2 (en) 2016-12-30 2020-12-15 General Electric Company Fuel injectors and methods of use in gas turbine combustor
US10816208B2 (en) 2017-01-20 2020-10-27 General Electric Company Fuel injectors and methods of fabricating same
US10718523B2 (en) 2017-05-12 2020-07-21 General Electric Company Fuel injectors with multiple outlet slots for use in gas turbine combustor
US10502426B2 (en) 2017-05-12 2019-12-10 General Electric Company Dual fuel injectors and methods of use in gas turbine combustor
US10690349B2 (en) 2017-09-01 2020-06-23 General Electric Company Premixing fuel injectors and methods of use in gas turbine combustor
JP6345331B1 (ja) 2017-11-20 2018-06-20 三菱日立パワーシステムズ株式会社 ガスタービンの燃焼筒及び燃焼器並びにガスタービン
US11156112B2 (en) * 2018-11-02 2021-10-26 Chromalloy Gas Turbine Llc Method and apparatus for mounting a transition duct in a gas turbine engine
US10890328B2 (en) * 2018-11-29 2021-01-12 DOOSAN Heavy Industries Construction Co., LTD Fin-pin flow guide for efficient transition piece cooling
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
US11371709B2 (en) * 2020-06-30 2022-06-28 General Electric Company Combustor air flow path
US11435080B1 (en) 2021-06-17 2022-09-06 General Electric Company Combustor having fuel sweeping structures
US12044411B2 (en) 2021-06-17 2024-07-23 Ge Infrastructure Technology Llc Combustor having fuel sweeping structures
US11898753B2 (en) 2021-10-11 2024-02-13 Ge Infrastructure Technology Llc System and method for sweeping leaked fuel in gas turbine system
JP2023166152A (ja) * 2022-05-09 2023-11-21 三菱重工業株式会社 燃焼器用筒、燃焼器、及びガスタービン
US12188658B1 (en) 2023-07-07 2025-01-07 Ge Infrastructure Technology Llc Fuel injection assembly for a combustor
US12467630B2 (en) 2023-07-07 2025-11-11 Ge Vernova Infrastructure Technology Llc Fuel injection assembly having a boss with a serpentine cooling passage
US20250216077A1 (en) * 2023-12-29 2025-07-03 Ge Infrastructure Technology Llc Additively manufactured tapered transition portion and aft frame for replacement of existing combustor parts
US12281793B1 (en) 2024-01-29 2025-04-22 Ge Infrastructure Technology Llc Fuel injection assembly for a combustor
US12449128B1 (en) 2024-11-27 2025-10-21 Ge Vernova Infrastructure Technology Llc Boss for a fuel injection assembly having cooling circuit and combustor provided therewith

Family Cites Families (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3872664A (en) 1973-10-15 1975-03-25 United Aircraft Corp Swirl combustor with vortex burning and mixing
US4265615A (en) 1978-12-11 1981-05-05 United Technologies Corporation Fuel injection system for low emission burners
US4420929A (en) 1979-01-12 1983-12-20 General Electric Company Dual stage-dual mode low emission gas turbine combustion system
JP2644745B2 (ja) 1987-03-06 1997-08-25 株式会社日立製作所 ガスタービン用燃焼器
CA2070511C (en) 1991-07-22 2001-08-21 Steven Milo Toborg Turbine nozzle support
US5271714A (en) 1992-07-09 1993-12-21 General Electric Company Turbine nozzle support arrangement
JP3335713B2 (ja) 1993-06-28 2002-10-21 株式会社東芝 ガスタービン燃焼器
GB9325708D0 (en) 1993-12-16 1994-02-16 Rolls Royce Plc A gas turbine engine combustion chamber
JP2950720B2 (ja) 1994-02-24 1999-09-20 株式会社東芝 ガスタービン燃焼装置およびその燃焼制御方法
US5380154A (en) 1994-03-18 1995-01-10 Solar Turbines Incorporated Turbine nozzle positioning system
US6047550A (en) * 1996-05-02 2000-04-11 General Electric Co. Premixing dry low NOx emissions combustor with lean direct injection of gas fuel
EP0962874A1 (en) 1998-06-04 1999-12-08 Asea Brown Boveri AG Method for designing a flow device
GB9813972D0 (en) 1998-06-30 1998-08-26 Rolls Royce Plc A combustion chamber
US6212870B1 (en) 1998-09-22 2001-04-10 General Electric Company Self fixturing combustor dome assembly
DE69940948D1 (de) 1999-01-25 2009-07-16 Gen Electric Interner Kühlkreislauf für eine Gasturbinenschaufel
US6374594B1 (en) 2000-07-12 2002-04-23 Power Systems Mfg., Llc Silo/can-annular low emissions combustor
US6442946B1 (en) 2000-11-14 2002-09-03 Power Systems Mfg., Llc Three degrees of freedom aft mounting system for gas turbine transition duct
US6543993B2 (en) 2000-12-28 2003-04-08 General Electric Company Apparatus and methods for localized cooling of gas turbine nozzle walls
US6450762B1 (en) 2001-01-31 2002-09-17 General Electric Company Integral aft seal for turbine applications
US6553767B2 (en) * 2001-06-11 2003-04-29 General Electric Company Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form
US20030039542A1 (en) 2001-08-21 2003-02-27 Cromer Robert Harold Transition piece side sealing element and turbine assembly containing such seal
US6813889B2 (en) * 2001-08-29 2004-11-09 Hitachi, Ltd. Gas turbine combustor and operating method thereof
JP2004125379A (ja) 2002-07-29 2004-04-22 Miura Co Ltd 低ＮＯｘ燃焼方法とその装置
EP1439349A1 (de) 2003-01-14 2004-07-21 Alstom Technology Ltd Verbrennungsverfahren sowie Brenner zur Durchführung des Verfahrens
JP2005002899A (ja) * 2003-06-12 2005-01-06 Hitachi Ltd ガスタービン燃焼器
US6923002B2 (en) 2003-08-28 2005-08-02 General Electric Company Combustion liner cap assembly for combustion dynamics reduction
US7284378B2 (en) 2004-06-04 2007-10-23 General Electric Company Methods and apparatus for low emission gas turbine energy generation
US7047723B2 (en) * 2004-04-30 2006-05-23 Martling Vincent C Apparatus and method for reducing the heat rate of a gas turbine powerplant
US7082766B1 (en) 2005-03-02 2006-08-01 General Electric Company One-piece can combustor
JP4824499B2 (ja) 2006-08-03 2011-11-30 株式会社神戸製鋼所 ダイスの設計方法、ダイス、中空パネルの製造方法及び中空パネル
US7743612B2 (en) 2006-09-22 2010-06-29 Pratt & Whitney Canada Corp. Internal fuel manifold and fuel inlet connection
US8171738B2 (en) 2006-10-24 2012-05-08 Pratt & Whitney Canada Corp. Gas turbine internal manifold mounting arrangement
US7757492B2 (en) * 2007-05-18 2010-07-20 General Electric Company Method and apparatus to facilitate cooling turbine engines
US7665309B2 (en) * 2007-09-14 2010-02-23 Siemens Energy, Inc. Secondary fuel delivery system
US7886539B2 (en) 2007-09-14 2011-02-15 Siemens Energy, Inc. Multi-stage axial combustion system
US8096131B2 (en) 2007-11-14 2012-01-17 Pratt & Whitney Canada Corp. Fuel inlet with crescent shaped passage for gas turbine engines
US7908863B2 (en) 2008-02-12 2011-03-22 General Electric Company Fuel nozzle for a gas turbine engine and method for fabricating the same
US8118549B2 (en) 2008-08-26 2012-02-21 Siemens Energy, Inc. Gas turbine transition duct apparatus
US20100071377A1 (en) * 2008-09-19 2010-03-25 Fox Timothy A Combustor Apparatus for Use in a Gas Turbine Engine
US8327648B2 (en) 2008-12-09 2012-12-11 Pratt & Whitney Canada Corp. Combustor liner with integrated anti-rotation and removal feature
US8701383B2 (en) 2009-01-07 2014-04-22 General Electric Company Late lean injection system configuration
US8112216B2 (en) 2009-01-07 2012-02-07 General Electric Company Late lean injection with adjustable air splits
US20100263386A1 (en) 2009-04-16 2010-10-21 General Electric Company Turbine engine having a liner
JP5260402B2 (ja) 2009-04-30 2013-08-14 三菱重工業株式会社 板状体の製造方法、板状体、ガスタービン燃焼器およびガスタービン
US8991192B2 (en) 2009-09-24 2015-03-31 Siemens Energy, Inc. Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine
US20110162375A1 (en) * 2010-01-05 2011-07-07 General Electric Company Secondary Combustion Fuel Supply Systems
US8082739B2 (en) 2010-04-12 2011-12-27 General Electric Company Combustor exit temperature profile control via fuel staging and related method
US8398090B2 (en) 2010-06-09 2013-03-19 General Electric Company Spring loaded seal assembly for turbines
JP2012145098A (ja) * 2010-12-21 2012-08-02 Toshiba Corp トランジションピースおよびガスタービン
US8158428B1 (en) 2010-12-30 2012-04-17 General Electric Company Methods, systems and apparatus for detecting material defects in combustors of combustion turbine engines
US20120186260A1 (en) 2011-01-25 2012-07-26 General Electric Company Transition piece impingement sleeve for a gas turbine
US8448444B2 (en) 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
CH704829A2 (de) * 2011-04-08 2012-11-15 Alstom Technology Ltd Gasturbogruppe und zugehöriges Betriebsverfahren.
US8601820B2 (en) 2011-06-06 2013-12-10 General Electric Company Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
US20120304656A1 (en) * 2011-06-06 2012-12-06 General Electric Company Combustion liner and transition piece
US8919137B2 (en) * 2011-08-05 2014-12-30 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US9316155B2 (en) 2013-03-18 2016-04-19 General Electric Company System for providing fuel to a combustor

Also Published As

Publication number Publication date
JP2014181906A (ja) 2014-09-29
DE102014103022B4 (de) 2025-12-18
JP6306908B2 (ja) 2018-04-04
CN104061595A (zh) 2014-09-24
US9383104B2 (en) 2016-07-05
US20140260273A1 (en) 2014-09-18
CN104061595B (zh) 2018-02-27
DE102014103022A1 (de) 2014-09-18

Similar Documents

Publication Publication Date Title
CH707828A2 (de) Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine.
CH707851A2 (de) Brennkammermodul für einen Brenner einer Gasturbine.
DE102011000225B4 (de) Über einen Anzapfdiffusor gespeistes sekundäres Verbrennungssystem für Gasturbinen
CH710574B1 (de) System und Verfahren zur Nutzung von Kühlluft in einem Brenner.
DE102012100368B4 (de) Brennkammerdüse
CH708388A2 (de) Brennstoffzufuhrsystem für eine Brennkammer einer Gasturbine.
DE102011000587B4 (de) Systeme und Verfahren zur Zufuhr von Hochdruckluft zum Kopfende einer Brennkammer
CH707852A2 (de) System zur Zuführung von Brennstoff zu einer Brennkammer.
CH707456A2 (de) Brennstoffinjektor zur Zuführung von Brennstoff zu einer Brennkammer.
CH708325A2 (de) Mantelringblocksegment für eine Gasturbine.
DE102014103081A1 (de) Strömungshülsenanordnung für ein Verbrennungsmodul eines Gasturbinenbrenners
DE102016106491A1 (de) Brennstoffdüsenanordnung mit einer Pilotdüse
DE102015120448A1 (de) Vormischbrennstoffdüsenanordnung
DE102014116971B4 (de) Vormischeranordnung zur Vermischung von Luft und Brennstoff zur Verbrennung
CH708646A2 (de) Innengekühlter Übergangskanalhinterrahmen.
CH710052A2 (de) Brennkammerkappenanordnung, Brennkammer und Gasturbine.
CH707849A2 (de) System zur Steuerung der Luftflussrate eines komprimierten Arbeitsfluids zu einem Brennstoffinjektor eines Brenners.
DE102014115402A1 (de) Übergangskanalanordnung mit modifizierter Hinterkante in einem Turbinensystem
CH702556A2 (de) Düse und Verfahren zur Brennstoffzufuhr durch eine mit gegenläufigem Drall arbeitende Düse.
DE102018113824A1 (de) System und Verfahren zur Verbrennung eines flüssigen Brennstoffs in einer Gasturbinenbrennkammer
DE102011051665A1 (de) Brennkammer und Verfahren zur Verringerung des Brennkammerkreischens
CH702550A2 (de) Halterung für Brennkammerübergangsstück mit integriertem Brennstoffkanal.
CH710425A2 (de) Vormischbrennstoffdüsenanordnung.
CH707726A2 (de) Verbrennungsanordnung und Verfahren zur Reduktion von Druckschwankungen einer Verbrennungsanordnung.
DE102015113009A1 (de) Brennkammerkappenanordnung

Legal Events

Date Code Title Description
NV New agent

Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH

AZW Rejection (application)