WO2014027005A3 - Brenner mit in einer basis ausgebildetem brennstoffplenum - Google Patents

Brenner mit in einer basis ausgebildetem brennstoffplenum Download PDF

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Publication number
WO2014027005A3
WO2014027005A3 PCT/EP2013/066943 EP2013066943W WO2014027005A3 WO 2014027005 A3 WO2014027005 A3 WO 2014027005A3 EP 2013066943 W EP2013066943 W EP 2013066943W WO 2014027005 A3 WO2014027005 A3 WO 2014027005A3
Authority
WO
WIPO (PCT)
Prior art keywords
fuel
base
burner
air
fuel plenum
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.)
Ceased
Application number
PCT/EP2013/066943
Other languages
English (en)
French (fr)
Other versions
WO2014027005A2 (de
Inventor
Axel Widenhorn
Roland STOLL
Dominik LEBKÜCHNER
Thilo KISSEL
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.)
Duerr Systems AG
Original Assignee
Duerr Systems 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 Duerr Systems AG filed Critical Duerr Systems AG
Priority to EP13750036.9A priority Critical patent/EP2885582B1/de
Publication of WO2014027005A2 publication Critical patent/WO2014027005A2/de
Publication of WO2014027005A3 publication Critical patent/WO2014027005A3/de
Priority to US14/563,532 priority patent/US9982891B2/en
Anticipated expiration legal-status Critical
Priority to US15/961,428 priority patent/US20180238549A1/en
Ceased 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
    • F23R3/286—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
    • 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
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • 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
    • F23R2900/03282—High speed injection of air and/or fuel inducing internal recirculation

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)

Abstract

Die Erfindung betrifft einen Brenner(10)zum Erzeugen von Heißgas und hat ein an eine Turbine anschließbares Flammrohr(12). Der Brenner (10) enthält eine das Flammrohr (12) umgebende Luftführungseinrichtung(14), die einen Strömungsweg (21) für Luft aufweist.Der Brenner (10) hat einen an einer Basis (34) festgelegten Brennerkopf(16), der für das Zuführen von mit Luft vermischtem Brennstoff in den Brennraum (12) mehrere dem Strömungsweg (25) für Luft in der Luftführungseinrichtung (14) kommunizierende Düsenkanäle (20) aufweist. In die Düsenkanäle(20) ragtjeweils eine an der Basis (34) festgelegte Brennstoffdüse (17). Die Brennstoffdüsen (17) sind für das Versorgen mit Brennstoff an einen in der Basis (34) ausgebildeten Ringkanal (52) angeschlossen, der mit einer Brennstoff-Zuführleitung verbunden werdenkann. Erfindungsgemäß sind die Brennstoffdüsen (17) für das Versorgen mit Brennstoff an einem in der Basis (34) ausgebildeten Ringkanal (52) angeschlossen, der mit einer Brennstoff-Zuführleitung verbunden werden kann.
PCT/EP2013/066943 2012-08-17 2013-08-13 Brenner Ceased WO2014027005A2 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP13750036.9A EP2885582B1 (de) 2012-08-17 2013-08-13 Brenner
US14/563,532 US9982891B2 (en) 2012-08-17 2014-12-08 Burners having fuel plenums
US15/961,428 US20180238549A1 (en) 2012-08-17 2018-04-24 Burners having fuel plenums

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE102012214707.1 2012-08-17
DE102012214707 2012-08-17
DE102012216080.9 2012-09-11
DE102012216080.9A DE102012216080A1 (de) 2012-08-17 2012-09-11 Brenner

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US14/563,532 Continuation-In-Part US9982891B2 (en) 2012-08-17 2014-12-08 Burners having fuel plenums

Publications (2)

Publication Number Publication Date
WO2014027005A2 WO2014027005A2 (de) 2014-02-20
WO2014027005A3 true WO2014027005A3 (de) 2014-06-12

Family

ID=50029638

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2013/066943 Ceased WO2014027005A2 (de) 2012-08-17 2013-08-13 Brenner

Country Status (4)

Country Link
US (2) US9982891B2 (de)
EP (1) EP2885582B1 (de)
DE (1) DE102012216080A1 (de)
WO (1) WO2014027005A2 (de)

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DE102012216080A1 (de) 2012-08-17 2014-02-20 Dürr Systems GmbH Brenner
US20160252254A1 (en) * 2013-10-31 2016-09-01 Siemens Aktiengesellschaft Gas turbine burner hub with pilot burner
US9423134B2 (en) * 2013-12-13 2016-08-23 General Electric Company Bundled tube fuel injector with a multi-configuration tube tip
US20150167983A1 (en) * 2013-12-13 2015-06-18 General Electric Company Bundled tube fuel injector tube tip
US9664392B2 (en) * 2013-12-13 2017-05-30 General Electric Company Bundled tube fuel injector with outer shroud and outer band connection
EP2980482A1 (de) * 2014-07-30 2016-02-03 Siemens Aktiengesellschaft Brenner für eine Verbrennungsmaschine und Verbrennungsmaschine
JP6301774B2 (ja) * 2014-08-01 2018-03-28 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
DE102015003920A1 (de) * 2014-09-25 2016-03-31 Dürr Systems GmbH Brennerkopf eines Brenners und Gasturbine mit einem solchen Brenner
KR101853464B1 (ko) 2015-06-22 2018-06-04 두산중공업 주식회사 실링구조를 포함하는 연료공급노즐.
JP6423760B2 (ja) 2015-06-24 2018-11-14 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器の燃料ノズル構造
KR101845702B1 (ko) * 2015-06-29 2018-04-05 두산중공업 주식회사 나사 고정식 결합구조가 마련된 노즐 후단부를 포함하는 연료공급노즐.
JP6535525B2 (ja) * 2015-07-01 2019-06-26 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
DE102016118633B4 (de) 2016-09-30 2021-03-25 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennerkopf, Brennersystem und Verwendung des Brennersystems
DE102016118632A1 (de) * 2016-09-30 2018-04-05 Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR) Brennkammersystem, Verwendung eines Brennkammersystems mit einer angeschlossenen Turbine und Verfahren zur Durchführung eines Verbrennungsprozesses
WO2018132185A1 (en) * 2017-01-11 2018-07-19 Siemens Energy, Inc. Mechanical attachment of a fuel rocket on a support housing base
DE102018104543A1 (de) * 2018-02-28 2019-08-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennkammersystem und Mikrogasturbinenanordnung
DE102018114870B3 (de) 2018-06-20 2019-11-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennersystem und Verfahren zur Erzeugung von Heißgas in einer Gasturbinenanlage
DE102018128128B4 (de) 2018-11-09 2026-03-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennerkopf, Brennersystem und Verfahren zum Betreiben eines Brennersystems
DE102019111827B4 (de) * 2019-05-07 2021-01-14 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum Betreiben einer Pyrolyseanlage und Pyrolyseanlage
CN115046197B (zh) * 2022-05-25 2025-03-14 北京瑞晨航宇能源科技有限公司 一种火焰分割式高速低氮燃烧器及其燃烧方法

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EP2213944A2 (de) * 2009-02-02 2010-08-04 General Electric Company Brennstoff-Einspritzeinrichtung für eine Gasturbine

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US20100139238A1 (en) * 2008-12-04 2010-06-10 General Electric Company Combustor Housing for Combustion of Low-BTU Fuel Gases and Methods of Making and Using the Same
EP2213944A2 (de) * 2009-02-02 2010-08-04 General Electric Company Brennstoff-Einspritzeinrichtung für eine Gasturbine

Also Published As

Publication number Publication date
EP2885582B1 (de) 2018-12-05
US9982891B2 (en) 2018-05-29
EP2885582A2 (de) 2015-06-24
DE102012216080A1 (de) 2014-02-20
WO2014027005A2 (de) 2014-02-20
US20150089954A1 (en) 2015-04-02
US20180238549A1 (en) 2018-08-23

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