ES2389482T3 - Sistema de quemador - Google Patents

Sistema de quemador Download PDF

Info

Publication number
ES2389482T3
ES2389482T3 ES10154116T ES10154116T ES2389482T3 ES 2389482 T3 ES2389482 T3 ES 2389482T3 ES 10154116 T ES10154116 T ES 10154116T ES 10154116 T ES10154116 T ES 10154116T ES 2389482 T3 ES2389482 T3 ES 2389482T3
Authority
ES
Spain
Prior art keywords
support
burner system
fuel
section
fixing element
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.)
Active
Application number
ES10154116T
Other languages
English (en)
Spanish (es)
Inventor
Andreas Böttcher
Timothy A. Fox
Thomas Grieb
Tobias Krieger
Stephen A. Ramier
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.)
Siemens Canada Ltd
Siemens AG
Siemens Corp
Original Assignee
Siemens Canada Ltd
Siemens AG
Siemens Corp
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 Canada Ltd, Siemens AG, Siemens Corp filed Critical Siemens Canada Ltd
Application granted granted Critical
Publication of ES2389482T3 publication Critical patent/ES2389482T3/es
Active 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D23/00—Assemblies of two or more burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
    • F23C2900/07021—Details of lances
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00018—Manufacturing combustion chamber liners or subparts

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Gas Burners (AREA)
ES10154116T 2010-02-19 2010-02-19 Sistema de quemador Active ES2389482T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20100154116 EP2362143B1 (de) 2010-02-19 2010-02-19 Brenneranordnung

Publications (1)

Publication Number Publication Date
ES2389482T3 true ES2389482T3 (es) 2012-10-26

Family

ID=42536358

Family Applications (1)

Application Number Title Priority Date Filing Date
ES10154116T Active ES2389482T3 (es) 2010-02-19 2010-02-19 Sistema de quemador

Country Status (5)

Country Link
US (1) US8955328B2 (https=)
EP (1) EP2362143B1 (https=)
JP (1) JP5791302B2 (https=)
CN (1) CN102162642B (https=)
ES (1) ES2389482T3 (https=)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2327933A1 (de) * 2009-11-30 2011-06-01 Siemens Aktiengesellschaft Brenneranordnung
US9366439B2 (en) * 2013-03-12 2016-06-14 General Electric Company Combustor end cover with fuel plenums
US9322558B2 (en) * 2013-06-27 2016-04-26 Siemens Aktiengesellschaft Combustor apparatus in a gas turbine engine
US10443855B2 (en) 2014-10-23 2019-10-15 Siemens Aktiengesellschaft Flexible fuel combustion system for turbine engines
CN104748132B (zh) * 2015-04-14 2017-01-25 河南宏天实业有限公司 升降式微正压保持聚能火炬燃烧器
US11230976B2 (en) * 2017-07-14 2022-01-25 General Electric Company Integrated fuel nozzle connection

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2036296B (en) * 1978-11-20 1982-12-01 Rolls Royce Gas turbine
JP2544470B2 (ja) * 1989-02-03 1996-10-16 株式会社日立製作所 ガスタ―ビン燃焼器及びその運転方法
DE69515931T2 (de) * 1994-06-10 2000-11-02 General Electric Co., Schenectady Regelung einer Gasturbinenbrennkammer
US5415000A (en) * 1994-06-13 1995-05-16 Westinghouse Electric Corporation Low NOx combustor retro-fit system for gas turbines
JPH08261467A (ja) * 1995-03-28 1996-10-11 Toshiba Corp ガスタービン燃焼器
US6122916A (en) * 1998-01-02 2000-09-26 Siemens Westinghouse Power Corporation Pilot cones for dry low-NOx combustors
US6082111A (en) 1998-06-11 2000-07-04 Siemens Westinghouse Power Corporation Annular premix section for dry low-NOx combustors
JP4323723B2 (ja) * 1998-10-09 2009-09-02 ゼネラル・エレクトリック・カンパニイ ガスタービンエンジン燃焼器の燃料噴射組立体
US6311473B1 (en) * 1999-03-25 2001-11-06 Parker-Hannifin Corporation Stable pre-mixer for lean burn composition
JP3069347B1 (ja) * 1999-06-11 2000-07-24 川崎重工業株式会社 ガスタ―ビンの燃焼器用バ―ナ装置
US6327860B1 (en) * 2000-06-21 2001-12-11 Honeywell International, Inc. Fuel injector for low emissions premixing gas turbine combustor
JP3960166B2 (ja) * 2001-08-29 2007-08-15 株式会社日立製作所 ガスタービン燃焼器およびガスタービン燃焼器の運転方法
US6813889B2 (en) * 2001-08-29 2004-11-09 Hitachi, Ltd. Gas turbine combustor and operating method thereof
US7121481B2 (en) * 2002-10-10 2006-10-17 Volvo Aero Corporation Fuel injector
US7197877B2 (en) * 2004-08-04 2007-04-03 Siemens Power Generation, Inc. Support system for a pilot nozzle of a turbine engine
US20100071377A1 (en) * 2008-09-19 2010-03-25 Fox Timothy A Combustor Apparatus for Use in a Gas Turbine Engine
US8365535B2 (en) * 2009-02-09 2013-02-05 General Electric Company Fuel nozzle with multiple fuel passages within a radial swirler
US8347631B2 (en) * 2009-03-03 2013-01-08 General Electric Company Fuel nozzle liquid cartridge including a fuel insert

Also Published As

Publication number Publication date
CN102162642B (zh) 2015-03-11
CN102162642A (zh) 2011-08-24
EP2362143A1 (de) 2011-08-31
JP2011169577A (ja) 2011-09-01
EP2362143B1 (de) 2012-08-29
US8955328B2 (en) 2015-02-17
US20110203285A1 (en) 2011-08-25
JP5791302B2 (ja) 2015-10-07

Similar Documents

Publication Publication Date Title
ES2389482T3 (es) Sistema de quemador
US10087844B2 (en) Bundled tube fuel nozzle assembly with liquid fuel capability
US6327861B2 (en) Gas turbine combustor
ES2624417T3 (es) Método para reparar un inyector de combustible de haz de tubos
JP6266290B2 (ja) ガス・タービン・エンジンの燃焼器用燃料ノズル
US8261554B2 (en) Fuel nozzle tip assembly
US9664392B2 (en) Bundled tube fuel injector with outer shroud and outer band connection
CN103375262A (zh) 涡轮机系统中具有延迟喷射的过渡管道
CN105765306A (zh) 燃气涡轮发动机中的燃烧器装置
US10139108B2 (en) D5/D5A DF-42 integrated exit cone and splash plate
CN105121963B (zh) 用于燃烧衬套的可移除的旋流器组件
US11162682B2 (en) Fuel injector
US20130234396A1 (en) Transition Piece Aft-Frame Seals
US20110203283A1 (en) Burner arrangement
US10669942B2 (en) Endcover assembly for a combustor
US7926279B2 (en) Extended life fuel nozzle
JP2011047403A (ja) 段間シールリング
JP7012444B2 (ja) 後期噴射特徴部を有するトランジションダクトアセンブリ
US11629857B2 (en) Combustor having a wake energizer
JP4652990B2 (ja) ガスタービン燃焼器
US9109456B2 (en) System for coupling a segment to a rotor of a turbomachine
US10145251B2 (en) Transition duct assembly
US20170350321A1 (en) Bundled Tube Fuel Nozzle Assembly with Tube Extensions
JP2017172585A (ja) 移行ダクト組立体