DE102013201232A1 - Brenner mit einer zentralen Brennstoffzufuhranordnung - Google Patents

Brenner mit einer zentralen Brennstoffzufuhranordnung Download PDF

Info

Publication number
DE102013201232A1
DE102013201232A1 DE201310201232 DE102013201232A DE102013201232A1 DE 102013201232 A1 DE102013201232 A1 DE 102013201232A1 DE 201310201232 DE201310201232 DE 201310201232 DE 102013201232 A DE102013201232 A DE 102013201232A DE 102013201232 A1 DE102013201232 A1 DE 102013201232A1
Authority
DE
Germany
Prior art keywords
fuel
fuel supply
central
burner
nozzles
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.)
Withdrawn
Application number
DE201310201232
Other languages
German (de)
English (en)
Inventor
Jürgen Meisl
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
Original Assignee
Siemens AG
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 filed Critical Siemens AG
Priority to DE201310201232 priority Critical patent/DE102013201232A1/de
Priority to PCT/EP2014/050687 priority patent/WO2014114535A1/fr
Publication of DE102013201232A1 publication Critical patent/DE102013201232A1/de
Withdrawn legal-status Critical Current

Links

Images

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
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • 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
    • F23R3/36—Supply of different fuels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00016—Preventing or reducing deposit build-up on burner parts, e.g. from carbon
    • 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
    • F23R2900/00004—Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE201310201232 2013-01-25 2013-01-25 Brenner mit einer zentralen Brennstoffzufuhranordnung Withdrawn DE102013201232A1 (de)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE201310201232 DE102013201232A1 (de) 2013-01-25 2013-01-25 Brenner mit einer zentralen Brennstoffzufuhranordnung
PCT/EP2014/050687 WO2014114535A1 (fr) 2013-01-25 2014-01-15 Brûleur muni d'un système central d'alimentation en combustible

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE201310201232 DE102013201232A1 (de) 2013-01-25 2013-01-25 Brenner mit einer zentralen Brennstoffzufuhranordnung

Publications (1)

Publication Number Publication Date
DE102013201232A1 true DE102013201232A1 (de) 2014-07-31

Family

ID=49999905

Family Applications (1)

Application Number Title Priority Date Filing Date
DE201310201232 Withdrawn DE102013201232A1 (de) 2013-01-25 2013-01-25 Brenner mit einer zentralen Brennstoffzufuhranordnung

Country Status (2)

Country Link
DE (1) DE102013201232A1 (fr)
WO (1) WO2014114535A1 (fr)

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2641685A1 (de) * 1975-12-24 1977-07-07 Gen Electric Niederdruck-brennstoff-injektionszerstaeubersystem
US4735044A (en) * 1980-11-25 1988-04-05 General Electric Company Dual fuel path stem for a gas turbine engine
CH666340A5 (en) * 1985-05-29 1988-07-15 Bbc Brown Boveri & Cie Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
EP0276696B1 (fr) 1987-01-26 1990-09-12 Siemens Aktiengesellschaft Brûleur hybride pour fonctionnement en prémélange au gaz et/ou au mazout, notamment pour turbines à gaz
EP0495587A1 (fr) * 1991-01-18 1992-07-22 General Electric Company Rampe de distribution de carburant pour turbine à gaz
EP0580683B1 (fr) 1991-04-25 1995-11-08 Siemens Aktiengesellschaft Bruleur, en particulier pour turbines a gaz, pour la combustion peu polluante du gaz de houille et d'autres combustibles
DE102008037480A1 (de) * 2007-10-29 2009-04-30 General Electric Co. Mager vorgemischte Dual-Fuel-Ringrohrbrennkammer mit Radial-Mehrring-Stufendüse
DE102009010604A1 (de) * 2008-02-26 2009-08-27 Delavan Inc. Zuleitungsarm für eine Mehrkreisbrennstoffeinspritzeinrichtung
US7654088B2 (en) * 2004-02-27 2010-02-02 Pratt & Whitney Canada Corp. Dual conduit fuel manifold for gas turbine engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7788927B2 (en) * 2005-11-30 2010-09-07 General Electric Company Turbine engine fuel nozzles and methods of assembling the same
EP2236933A1 (fr) * 2009-03-17 2010-10-06 Siemens Aktiengesellschaft Agencement de brûleur pour combustibles liquides et procédé de fabrication d'un agencement de brûleur
EP2230458A1 (fr) * 2009-03-17 2010-09-22 Siemens Aktiengesellschaft Agencement de brûleur pour combustibles liquides et procédé de fabrication d'un agencement de brûleur
FR2951245B1 (fr) * 2009-10-13 2013-05-17 Snecma Dispositif d'injection multi-point pour une chambre de combustion de turbomachine

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2641685A1 (de) * 1975-12-24 1977-07-07 Gen Electric Niederdruck-brennstoff-injektionszerstaeubersystem
US4735044A (en) * 1980-11-25 1988-04-05 General Electric Company Dual fuel path stem for a gas turbine engine
CH666340A5 (en) * 1985-05-29 1988-07-15 Bbc Brown Boveri & Cie Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
EP0276696B1 (fr) 1987-01-26 1990-09-12 Siemens Aktiengesellschaft Brûleur hybride pour fonctionnement en prémélange au gaz et/ou au mazout, notamment pour turbines à gaz
EP0495587A1 (fr) * 1991-01-18 1992-07-22 General Electric Company Rampe de distribution de carburant pour turbine à gaz
EP0580683B1 (fr) 1991-04-25 1995-11-08 Siemens Aktiengesellschaft Bruleur, en particulier pour turbines a gaz, pour la combustion peu polluante du gaz de houille et d'autres combustibles
US7654088B2 (en) * 2004-02-27 2010-02-02 Pratt & Whitney Canada Corp. Dual conduit fuel manifold for gas turbine engine
DE102008037480A1 (de) * 2007-10-29 2009-04-30 General Electric Co. Mager vorgemischte Dual-Fuel-Ringrohrbrennkammer mit Radial-Mehrring-Stufendüse
DE102009010604A1 (de) * 2008-02-26 2009-08-27 Delavan Inc. Zuleitungsarm für eine Mehrkreisbrennstoffeinspritzeinrichtung

Also Published As

Publication number Publication date
WO2014114535A1 (fr) 2014-07-31

Similar Documents

Publication Publication Date Title
EP2470834B1 (fr) Brûleur notamment destiné à des turbines à gaz
DE102012100368B4 (de) Brennkammerdüse
DE102010061639B4 (de) Verfahren zum Betreiben einer sekundären Brennstoffdüse für eine Brennkammer einer Turbomaschine
DE102014117621A1 (de) Brennstoffinjektor mit Vormisch-Pilotdüse
CH703884B1 (de) Brennstoffdüsenanordnung für Gasturbinensysteme sowie Brenner.
CH710574B1 (de) System und Verfahren zur Nutzung von Kühlluft in einem Brenner.
EP2359065A2 (fr) Lance à combustible pour brûleur
DE10160997A1 (de) Magervormischbrenner für eine Gasturbine sowie Verfahren zum Betrieb eines Magervormischbrenners
DE102009038845A1 (de) Drallschaufel, Brenner und Gasturbine
CH699767B1 (de) Brenner zur Verwendung mit einer Brennkammer eines Gasturbinenmotors sowie Verfahren zur Mischung von Brennstoff in dem Brenner.
DE102009026237A1 (de) Gasturbinenübergangsstück mit Verdünnungslöchern
CH701773A2 (de) Brenner mit radialen Einlassleitschaufeln.
DE102011052159A1 (de) Kraftstoffdüse und Kraftstoffdüsenanordnung und damit ausgestatte Gasturbine
EP2161502A1 (fr) Brûleur à prémélange pour un combustible pauvre et riche
CH697802A2 (de) Leckagen reduzierendes Venturi-Rohr für trockene Stickoxid-(NOx)-Niedrigemissions-Brenner.
EP2264370B1 (fr) Agencement de brûleur pour une installation de combustion destinée à la combustion de combustibles fluidiques et procédé de fonctionnement d'un tel agencement de brûleur
DE102004027702A1 (de) Injektor für Flüssigbrennstoff sowie gestufter Vormischbrenner mit diesem Injektor
EP2558781B1 (fr) Générateur de turbulence pour un brûleur
EP2449310B1 (fr) Brûleur notamment pour turbines à gaz
DE102013201232A1 (de) Brenner mit einer zentralen Brennstoffzufuhranordnung
DE102022201182A1 (de) Düsenbaugruppe mit eine Kraftstoffleitung passierender Verbindungsleitung in einem Düsenhauptkörper für eine Luftströmung
EP3926238B1 (fr) Module d'une turbine à gaz pourvu de dérivation d'air de la chambre de combustion
DE102014115841A1 (de) Brennkammergehäuseverteiler zur Hochdruckluftbelieferung eines Brennstoffdüsenpilotsystems
DE102017218529A1 (de) Düse für eine Brennkammer eines Triebwerks
DE202011101763U1 (de) Gasturbine mit Brennstofflanz und Verteilsystem zum Eindüsen von flüssigen und/oder gasförmigen Brennstoffen

Legal Events

Date Code Title Description
R079 Amendment of ipc main class

Free format text: PREVIOUS MAIN CLASS: F23D0017000000

Ipc: F23R0003280000

R163 Identified publications notified
R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee