[go: up one dir, main page]

WO2012016748A3 - Gasturbinenbrennkammer - Google Patents

Gasturbinenbrennkammer Download PDF

Info

Publication number
WO2012016748A3
WO2012016748A3 PCT/EP2011/059901 EP2011059901W WO2012016748A3 WO 2012016748 A3 WO2012016748 A3 WO 2012016748A3 EP 2011059901 W EP2011059901 W EP 2011059901W WO 2012016748 A3 WO2012016748 A3 WO 2012016748A3
Authority
WO
WIPO (PCT)
Prior art keywords
pilot
fuel nozzle
combustion chamber
cone
gas turbine
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/EP2011/059901
Other languages
English (en)
French (fr)
Other versions
WO2012016748A2 (de
Inventor
Bernd Prade
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
Priority to JP2013522155A priority Critical patent/JP5657794B2/ja
Priority to US13/813,494 priority patent/US9194587B2/en
Priority to CN201180037995.3A priority patent/CN103119369B/zh
Priority to EP11725735.2A priority patent/EP2601447A2/de
Priority to RU2013109306/06A priority patent/RU2566866C2/ru
Publication of WO2012016748A2 publication Critical patent/WO2012016748A2/de
Anticipated expiration legal-status Critical
Publication of WO2012016748A3 publication Critical patent/WO2012016748A3/de
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/343Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion

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 eine Gasturbinenbrennkammer mit: - einer Pilotbrennstoffdüse, die im mittleren Abschnitt eines Zylinders (2) angeordnet ist, der sich an einem Ende zu einer Brennkammer hin öffnet, wobei die Pilotbrennstoffdüse eine Brennstoffdüse (1) umfasst, sowie um den Außenumfang der Brennstoffdüse (1) radial beabstandet eine zylindrische Außenverkleidung (9), und wobei zwischen Brennstoffdüse (1) und Außenverkleidung (9) ein Pilotverwirbelungselement (5) angeordnet ist, - mehrere Hauptbrenner, die im Bezug auf die Radialrichtung um die Pilotbrennstoffdüse angeordnet sind, - einen Pilotkonus (4) mit Innenseite (11) und Außenseite (12), wobei der Pilotkonus (4) brennkammerseitig an der Pilotbrennstoffdüse angeordnet ist und eine brennkammerseitige Öffnung (6), so dass durch Mischen von Luft und Pilotbrennstoff eine Pilotflamme im Pilotkonus (4) gebildet wird, um einen von den Hauptbrenner eingespritzten Brennstoff zu zünden, wobei der Pilotkonus (4) an seiner Innenseite (11) und/oder Aussenseite (12) Turbulenzgeneratoren aufweist.
PCT/EP2011/059901 2010-08-02 2011-06-15 Gasturbinenbrennkammer Ceased WO2012016748A2 (de)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2013522155A JP5657794B2 (ja) 2010-08-02 2011-06-15 ガスタービン燃焼室
US13/813,494 US9194587B2 (en) 2010-08-02 2011-06-15 Gas turbine combustion chamber
CN201180037995.3A CN103119369B (zh) 2010-08-02 2011-06-15 燃气涡轮机燃烧室
EP11725735.2A EP2601447A2 (de) 2010-08-02 2011-06-15 Gasturbinenbrennkammer
RU2013109306/06A RU2566866C2 (ru) 2010-08-02 2011-06-15 Камера сгорания газовой турбины

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP10171601.7 2010-08-02
EP10171601A EP2416070A1 (de) 2010-08-02 2010-08-02 Gasturbinenbrennkammer

Publications (2)

Publication Number Publication Date
WO2012016748A2 WO2012016748A2 (de) 2012-02-09
WO2012016748A3 true WO2012016748A3 (de) 2013-03-21

Family

ID=43479914

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2011/059901 Ceased WO2012016748A2 (de) 2010-08-02 2011-06-15 Gasturbinenbrennkammer

Country Status (6)

Country Link
US (1) US9194587B2 (de)
EP (2) EP2416070A1 (de)
JP (1) JP5657794B2 (de)
CN (1) CN103119369B (de)
RU (1) RU2566866C2 (de)
WO (1) WO2012016748A2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6037736B2 (ja) * 2012-09-11 2016-12-07 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およびこれを備えたガスタービン機関
US9528704B2 (en) * 2014-02-21 2016-12-27 General Electric Company Combustor cap having non-round outlets for mixing tubes
US9528702B2 (en) 2014-02-21 2016-12-27 General Electric Company System having a combustor cap
JP6723768B2 (ja) 2016-03-07 2020-07-15 三菱重工業株式会社 バーナアセンブリ、燃焼器、及びガスタービン
JP6692847B2 (ja) * 2018-03-26 2020-05-13 三菱重工業株式会社 ガスタービン燃焼器及びこれを備えたガスタービン機関
JP7096182B2 (ja) * 2019-02-27 2022-07-05 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン
KR102583224B1 (ko) * 2022-01-26 2023-09-25 두산에너빌리티 주식회사 클러스터가 구비된 연소기 및 이를 포함하는 가스 터빈
CN115030837B (zh) * 2022-08-10 2022-11-08 中国空气动力研究与发展中心低速空气动力研究所 一种喷口降噪装置
US12130016B1 (en) * 2023-05-31 2024-10-29 General Electric Company Turbine engine including a combustor
CN117515592A (zh) * 2023-12-04 2024-02-06 浙江燃创透平机械有限公司 一种径向分级低排放燃烧器及燃烧室

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999006767A1 (de) * 1997-07-31 1999-02-11 Siemens Aktiengesellschaft Brenner
US6038861A (en) * 1998-06-10 2000-03-21 Siemens Westinghouse Power Corporation Main stage fuel mixer with premixing transition for dry low Nox (DLN) combustors
US6122916A (en) * 1998-01-02 2000-09-26 Siemens Westinghouse Power Corporation Pilot cones for dry low-NOx combustors
US20010022088A1 (en) * 2000-03-14 2001-09-20 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor
EP2187127A1 (de) * 2007-12-21 2010-05-19 Mitsubishi Heavy Industries, Ltd. Gasturbinenbrennkammer

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3736746A (en) * 1971-08-13 1973-06-05 Gen Electric Recirculating annular slot fuel/air carbureting system for gas turbine combustors
IL93630A0 (en) * 1989-03-27 1990-12-23 Gen Electric Flameholder for gas turbine engine afterburner
US5575153A (en) * 1993-04-07 1996-11-19 Hitachi, Ltd. Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer
JP3435833B2 (ja) * 1993-09-17 2003-08-11 株式会社日立製作所 燃焼器
JP4508474B2 (ja) 2001-06-07 2010-07-21 三菱重工業株式会社 燃焼器
US8113000B2 (en) * 2008-09-15 2012-02-14 Siemens Energy, Inc. Flashback resistant pre-mixer assembly
US8661779B2 (en) * 2008-09-26 2014-03-04 Siemens Energy, Inc. Flex-fuel injector for gas turbines
RU99596U1 (ru) 2010-06-16 2010-11-20 Николай Валентинович Стуценко Горелочное устройство

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999006767A1 (de) * 1997-07-31 1999-02-11 Siemens Aktiengesellschaft Brenner
US6122916A (en) * 1998-01-02 2000-09-26 Siemens Westinghouse Power Corporation Pilot cones for dry low-NOx combustors
US6038861A (en) * 1998-06-10 2000-03-21 Siemens Westinghouse Power Corporation Main stage fuel mixer with premixing transition for dry low Nox (DLN) combustors
US20010022088A1 (en) * 2000-03-14 2001-09-20 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor
EP2187127A1 (de) * 2007-12-21 2010-05-19 Mitsubishi Heavy Industries, Ltd. Gasturbinenbrennkammer

Also Published As

Publication number Publication date
US20130125550A1 (en) 2013-05-23
RU2013109306A (ru) 2014-09-10
EP2416070A1 (de) 2012-02-08
JP5657794B2 (ja) 2015-01-21
JP2013535651A (ja) 2013-09-12
WO2012016748A2 (de) 2012-02-09
CN103119369B (zh) 2016-03-09
EP2601447A2 (de) 2013-06-12
CN103119369A (zh) 2013-05-22
US9194587B2 (en) 2015-11-24
RU2566866C2 (ru) 2015-10-27

Similar Documents

Publication Publication Date Title
WO2012016748A3 (de) Gasturbinenbrennkammer
JP5984770B2 (ja) ガスタービン燃焼器およびこれを備えたガスタービン機関
WO2015076883A3 (en) Dual fuel nozzle with swirling axial gas injection for a gas turbine engine
WO2010127682A3 (en) Swirler, combustion chamber, and gas turbine with improved mixing
EP3341656B1 (de) Brennstoffdüsenanordnung für eine gasturbine
WO2011033242A3 (fr) Chambre de combustion de turbomachine aeronautique avec trous de combustion de configurations differentes
CN105705866B (zh) 喷嘴、燃烧器以及燃气轮机
CN102444911A (zh) 具有贫预喷喷嘴燃料喷射系统的燃烧器
WO2015069354A3 (en) Dual fuel nozzle with liquid filming atomization for a gas turbine engine
EP2551596A3 (de) Brennkammer, Brenner und Gasturbine
MX2014015868A (es) Combustor de alta presion con encendido de superficie caliente.
MY154695A (en) Combustion burner and boiler provided with combustion burner
JP6325930B2 (ja) ガスタービン燃焼器
WO2018026419A3 (en) Combustor assembly for a turbine engine
WO2015108583A3 (en) Circumferentially and axially staged annular combustor for gas turbine engine combustor
EP2439452A3 (de) Gasturbinenbrennkammer
JP2015105766A5 (de)
JP2016061506A5 (de)
EP2884173A3 (de) Montageanordnung eines brennstoff-injektors für eine gasturbinenbrennkammer
WO2018057072A3 (en) Combustor assembly for a gas turbine engine
WO2015147951A3 (en) Axial staged combustor with restricted main fuel injector
EP2778533A3 (de) Verbrenner für Gasturbinentriebwerk
US7827777B2 (en) Combustor with reduced carbon monoxide emissions
WO2011117533A3 (fr) Chambre de combustion a injecteurs decales longitudinalement sur une meme couronne
US20130189632A1 (en) Fuel nozzel

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 201180037995.3

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 11725735

Country of ref document: EP

Kind code of ref document: A2

REEP Request for entry into the european phase

Ref document number: 2011725735

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2011725735

Country of ref document: EP

ENP Entry into the national phase

Ref document number: 2013522155

Country of ref document: JP

Kind code of ref document: A

WWE Wipo information: entry into national phase

Ref document number: 13813494

Country of ref document: US

NENP Non-entry into the national phase

Ref country code: DE

ENP Entry into the national phase

Ref document number: 2013109306

Country of ref document: RU

Kind code of ref document: A