[go: up one dir, main page]

ES2550096T3 - Quemador de turbina de gas - Google Patents

Quemador de turbina de gas Download PDF

Info

Publication number
ES2550096T3
ES2550096T3 ES03794901.3T ES03794901T ES2550096T3 ES 2550096 T3 ES2550096 T3 ES 2550096T3 ES 03794901 T ES03794901 T ES 03794901T ES 2550096 T3 ES2550096 T3 ES 2550096T3
Authority
ES
Spain
Prior art keywords
burner
flow
swirl vane
angle
vane
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.)
Expired - Lifetime
Application number
ES03794901.3T
Other languages
English (en)
Inventor
Peter Berenbrink
Malte Blomeyer
Werner Krebs
Bernd Prade
Holger Streb
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 AG
Siemens Corp
Original Assignee
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 AG, Siemens Corp filed Critical Siemens AG
Application granted granted Critical
Publication of ES2550096T3 publication Critical patent/ES2550096T3/es
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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Spray-Type Burners (AREA)
  • Air Supply (AREA)

Abstract

Quemador (1), en el que se alimenta aire y/u oxígeno (4), que fluye en un sentido (88) de flujo, presentando el quemador (1) un canal (13), en el que fluye un medio, estando dispuesta en el canal (13) al menos una paleta (16) de remolino, presentando la paleta (16) de remolino una hoja (61) de paleta, que presenta una torsión alrededor de un eje (76) de torsión, de modo que el gas que fluye en el sentido (88) de flujo pasando por la paleta (16) de remolino a lo largo de un canto de la hoja (61) de paleta, que presenta con el sentido (88) de flujo un ángulo de corte distinto de cero, presenta diferentes ángulos de salida de flujo (α), de modo que el aire y/o el oxígeno (4) en un plano perpendicular al sentido (88) de flujo presenta una distribución de un ángulo de salida de flujo, y la distribución del ángulo de salida de flujo no es constante, para evitar inestabilidades en la combustión durante el funcionamiento del quemador (1), presentando el quemador (1) un eje (46) longitudinal de quemador, que representa el área interna del quemador (1), presentando el quemador (1) una dirección (55) radial dispuesta en perpendicular al eje (46) longitudinal de quemador, presentando el ángulo de salida de flujo (α) entre su sentido (88) de flujo y un plano perpendicular al eje (46) longitudinal de quemador de un gas que fluye pasando por una paleta (16) de remolino en la dirección (55) radial en la paleta (16) de remolino diferentes ángulos de salida de flujo (α), caracterizado porque el ángulo de salida de flujo (α) disminuye en la dirección (55) radial de dentro hacia fuera.

Description

imagen1
imagen2
imagen3

Claims (1)

  1. imagen1
ES03794901.3T 2002-09-02 2003-08-20 Quemador de turbina de gas Expired - Lifetime ES2550096T3 (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP02019530A EP1394471A1 (de) 2002-09-02 2002-09-02 Brenner
EP02019530 2002-09-02
PCT/EP2003/009222 WO2004025183A2 (de) 2002-09-02 2003-08-20 Brenner

Publications (1)

Publication Number Publication Date
ES2550096T3 true ES2550096T3 (es) 2015-11-04

Family

ID=31197882

Family Applications (1)

Application Number Title Priority Date Filing Date
ES03794901.3T Expired - Lifetime ES2550096T3 (es) 2002-09-02 2003-08-20 Quemador de turbina de gas

Country Status (6)

Country Link
US (1) US7753677B2 (es)
EP (2) EP1394471A1 (es)
JP (2) JP4369370B2 (es)
CN (1) CN100432531C (es)
ES (1) ES2550096T3 (es)
WO (1) WO2004025183A2 (es)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004059882A1 (de) * 2004-12-10 2006-06-22 Rolls-Royce Deutschland Ltd & Co Kg Magervormischbrenner mit integriertem Stützbrenner
JP4476176B2 (ja) * 2005-06-06 2010-06-09 三菱重工業株式会社 ガスタービンの予混合燃焼バーナー
US20070269755A2 (en) * 2006-01-05 2007-11-22 Petro-Chem Development Co., Inc. Systems, apparatus and method for flameless combustion absent catalyst or high temperature oxidants
US20080078182A1 (en) * 2006-09-29 2008-04-03 Andrei Tristan Evulet Premixing device, gas turbines comprising the premixing device, and methods of use
KR100820233B1 (ko) * 2006-10-31 2008-04-08 한국전력공사 연소기 및 이를 포함하는 멀티 연소기, 그리고 연소방법
EP1992878A1 (en) * 2007-05-18 2008-11-19 Siemens Aktiengesellschaft Fuel distributor
US9016601B2 (en) 2007-05-18 2015-04-28 Siemens Aktiengesellschaft Fuel distributor
EP2042807A1 (de) * 2007-09-25 2009-04-01 Siemens Aktiengesellschaft Vormischstufe für einen Gasturbinenbrenner
JP5172468B2 (ja) * 2008-05-23 2013-03-27 川崎重工業株式会社 燃焼装置および燃焼装置の制御方法
EP2312215A1 (de) * 2008-10-01 2011-04-20 Siemens Aktiengesellschaft Brenner und Verfahren zum Betrieb eines Brenners
KR101049359B1 (ko) * 2008-10-31 2011-07-13 한국전력공사 삼중 스월형 가스터빈 연소기
US20100180599A1 (en) * 2009-01-21 2010-07-22 Thomas Stephen R Insertable Pre-Drilled Swirl Vane for Premixing Fuel Nozzle
IT1393555B1 (it) * 2009-04-07 2012-04-27 Ansaldo Energia Spa Impianto a turbina a gas e metodo per operare detto impianto a turbina a gas
EP2270398A1 (de) * 2009-06-30 2011-01-05 Siemens Aktiengesellschaft Brenner, insbesondere für Gasturbinen
DE102009038848A1 (de) * 2009-08-26 2011-03-03 Siemens Aktiengesellschaft Brenner, insbesondere für Gasturbinen
DE102009038845A1 (de) * 2009-08-26 2011-03-03 Siemens Aktiengesellschaft Drallschaufel, Brenner und Gasturbine
UA106387C2 (ru) 2009-09-13 2014-08-26 Лин Флейм, Инк. Камера сгорания для поэтапного изменения подачи топлива и узел, который содержит камеру сгорания
DE102009045950A1 (de) * 2009-10-23 2011-04-28 Man Diesel & Turbo Se Drallerzeuger
US9163841B2 (en) * 2011-09-23 2015-10-20 Siemens Aktiengesellschaft Cast manifold for dry low NOx gas turbine engine
US10012386B2 (en) 2012-08-06 2018-07-03 Siemens Aktiengesellschaft Local improvement of the mixture of air and fuel in burners comprising swirl generators having blade ends that are crossed in the outer region
EP2728260A1 (en) * 2012-11-06 2014-05-07 Alstom Technology Ltd Axial swirler
US20150316266A1 (en) 2014-04-30 2015-11-05 Siemens Aktiengesellschaft Burner with adjustable radial fuel profile
EP2966350B1 (en) 2014-07-10 2018-06-13 Ansaldo Energia Switzerland AG Axial swirler
CN107514636B (zh) * 2017-10-10 2023-09-08 安徽科达洁能股份有限公司 一种悬浮焙烧炉用烧嘴及其应用
DE102018205874A1 (de) * 2018-04-18 2019-10-24 Siemens Aktiengesellschaft Brenner mit selektiver Anpassung des Bohrungsmusters für die Gaseindüsung
KR102429643B1 (ko) 2018-05-15 2022-08-04 에어 프로덕츠 앤드 케미칼스, 인코오포레이티드 가스 터빈의 연소 안정성 개선 시스템 및 방법
CN113272594B (zh) 2019-01-22 2022-11-22 三菱电机株式会社 空气调和装置
EA039073B1 (ru) * 2020-09-07 2021-11-30 Некоммерческое Акционерное Общество "Алматинский Университет Энергетики И Связи Имени Гумарбека Даукеева" Двухъярусная горелка
US12454909B2 (en) 2021-12-03 2025-10-28 General Electric Company Combustor size rating for a gas turbine engine using hydrogen fuel
US12331932B2 (en) * 2022-01-31 2025-06-17 General Electric Company Turbine engine fuel mixer

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1126654A (en) * 1915-01-26 Babcock & Wilcox Co Apparatus for burning finely-divided fuel.
US746525A (en) * 1902-11-21 1903-12-08 Peter M Kling Hydrocarbon-burner.
US1086715A (en) * 1911-07-03 1914-02-10 Babcock & Wilcox Co Apparatus for burning finely-divided fuel.
US1102510A (en) * 1911-07-15 1914-07-07 Babcock & Wilcox Co Apparatus for burning finely-divided fuel.
JPS6099933A (ja) * 1983-11-04 1985-06-03 Mitsubishi Heavy Ind Ltd スワラの製作方法
DE3446211A1 (de) * 1984-12-19 1986-07-03 MAN Gutehoffnungshütte GmbH, 4200 Oberhausen Zahnradgetriebe
JPH0780216B2 (ja) * 1987-08-13 1995-08-30 東芝機械株式会社 樹脂材料の焼け，分解防止方法
JPH0647954B2 (ja) * 1988-09-07 1994-06-22 株式会社日立製作所 ガスタービンの予混合器
CH687347A5 (de) * 1993-04-08 1996-11-15 Abb Management Ag Wärmeerzeuger.
US5435126A (en) 1994-03-14 1995-07-25 General Electric Company Fuel nozzle for a turbine having dual capability for diffusion and premix combustion and methods of operation
JPH07332621A (ja) 1994-06-13 1995-12-22 Hitachi Ltd ガスタービン燃焼器用旋回バーナ
US5511375A (en) 1994-09-12 1996-04-30 General Electric Company Dual fuel mixer for gas turbine combustor
JPH08158892A (ja) * 1994-12-02 1996-06-18 Ishikawajima Harima Heavy Ind Co Ltd ガスタービン用燃料噴射弁
RU2190804C2 (ru) * 1996-09-09 2002-10-10 Сименсакциенгезелльшафт Устройство и способ для сжигания топлива в воздухе
DE19640818B4 (de) * 1996-10-02 2006-04-27 Siemens Ag Vorrichtung und Verfahren zur Verbrennung eines Brennstoffs in Luft
GB2324147B (en) * 1997-04-10 2001-09-05 Europ Gas Turbines Ltd Fuel-injection arrangement for a gas turbine combuster
JPH1183016A (ja) * 1997-09-10 1999-03-26 Mitsubishi Heavy Ind Ltd ３次元スワーラ
DE69916911T2 (de) * 1998-02-10 2005-04-21 Gen Electric Brenner mit gleichmässiger Brennstoff/Luft Vormischung zur emissionsarmen Verbrennung
US6092363A (en) 1998-06-19 2000-07-25 Siemens Westinghouse Power Corporation Low Nox combustor having dual fuel injection system
DE19948673B4 (de) 1999-10-08 2009-02-26 Alstom Verfahren zum Erzeugen von heissen Gasen in einer Verbrennungseinrichtung sowie Verbrennungseinrichtung zur Durchführung des Verfahrens
EP1096201A1 (de) * 1999-10-29 2001-05-02 Siemens Aktiengesellschaft Brenner
JP4629945B2 (ja) * 1999-12-15 2011-02-09 大阪瓦斯株式会社 流体分配器及びバーナ装置及びガスタービンエンジン及びコジェネレーションシステム
DE10056243A1 (de) 2000-11-14 2002-05-23 Alstom Switzerland Ltd Brennkammer und Verfahren zum Betrieb dieser Brennkammer
DE10064893A1 (de) * 2000-12-23 2002-11-14 Alstom Switzerland Ltd Brenner mit gestufter Brennstoffeindüsung
DE10108560A1 (de) 2001-02-22 2002-09-05 Alstom Switzerland Ltd Verfahren zum Betrieb einer Ringbrennkammer sowie eine diesbezügliche Ringbrennkammer

Also Published As

Publication number Publication date
JP4369370B2 (ja) 2009-11-18
EP1534997B1 (de) 2015-07-29
US20060035188A1 (en) 2006-02-16
JP2008256357A (ja) 2008-10-23
WO2004025183A3 (de) 2005-01-20
CN100432531C (zh) 2008-11-12
US7753677B2 (en) 2010-07-13
EP1534997A2 (de) 2005-06-01
JP4841587B2 (ja) 2011-12-21
JP2006507466A (ja) 2006-03-02
WO2004025183A2 (de) 2004-03-25
EP1394471A1 (de) 2004-03-03
CN1678871A (zh) 2005-10-05

Similar Documents

Publication Publication Date Title
ES2550096T3 (es) Quemador de turbina de gas
EP1443215A3 (en) Integral tip seal in a fan-shroud structure
ES2880801T3 (es) Dispositivo de ventilación de túnel energéticamente eficiente
US20040219013A1 (en) Radial fan
ATE325939T1 (de) Rezirkulationsstruktur für turboverdichter
DE10390754D2 (de) Rezirkulationsstruktur für Turboverdichter
US7549838B2 (en) Taking air away from the tips of the rotor wheels of a high pressure compressor in a turbojet
RU2013134238A (ru) Безлопастной полочный вентилятор
RU2011136078A (ru) Вентилятор
EP1892399A3 (en) Aero engine bleed valve
JP2006207586A (ja) タービン翼形部の高効率ファン冷却孔
CO5640154A2 (es) Dispositivo para regular selectivamente la proporcion de flu jo de un fluido
BRPI0512828A (pt) ventilador axial de alta eficiência
EP1764608A3 (en) Optical flow cell capable of use in high temperature and high pressure environment
RU2004121800A (ru) Устройство для снижения шума реактивной струи газотурбинного двигателя и сопло газотурбинного двигателя
US12490688B2 (en) Concentrator attachment for blower air tube
ES2370402T3 (es) Pala de compresor.
ATE482326T1 (de) Strömungsmaschine mit einem im gehäusemittelteil vorgesehenen spiralkanal
AR007236A1 (es) Aparato eductor
EP1627991A3 (en) A component having a cooling arrangement
KR20060085944A (ko) 사류 압축기의 임펠러
US2261463A (en) Impeller
JP2005106415A (ja) 給排気管
CN104024738A (zh) 流速分布均匀化装置
Ishak et al. The effect of swirl number on discharge coefficient for various orifice sizes in a burner system