CN106461228A - 用于燃气涡轮发动机的燃烧器的旋流器、燃气涡轮发动机的燃烧器以及燃气涡轮发动机 - Google Patents

用于燃气涡轮发动机的燃烧器的旋流器、燃气涡轮发动机的燃烧器以及燃气涡轮发动机 Download PDF

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Publication number
CN106461228A
CN106461228A CN201580024161.7A CN201580024161A CN106461228A CN 106461228 A CN106461228 A CN 106461228A CN 201580024161 A CN201580024161 A CN 201580024161A CN 106461228 A CN106461228 A CN 106461228A
Authority
CN
China
Prior art keywords
cyclone
fuel
injection device
pilot
hybrid channel
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.)
Pending
Application number
CN201580024161.7A
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English (en)
Chinese (zh)
Inventor
T·多尔曼斯利
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
Publication of CN106461228A publication Critical patent/CN106461228A/zh
Pending 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
    • F23R3/38Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00Combustion apparatus characterised by arrangements for air supply
    • F23C7/002Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
    • 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
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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)
CN201580024161.7A 2014-05-09 2015-05-07 用于燃气涡轮发动机的燃烧器的旋流器、燃气涡轮发动机的燃烧器以及燃气涡轮发动机 Pending CN106461228A (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP14167655.1 2014-05-09
EP14167655.1A EP2942563A1 (fr) 2014-05-09 2014-05-09 Élément de tourbillonnement d'un brûleur de moteur de turbine à gaz, brûleur de moteur de turbine à gaz et moteur de turbine à gaz
PCT/EP2015/060127 WO2015169930A1 (fr) 2014-05-09 2015-05-07 Coupelle rotative pour brûleur de turbine à gaz, brûleur de turbine à gaz et turbine à gaz

Publications (1)

Publication Number Publication Date
CN106461228A true CN106461228A (zh) 2017-02-22

Family

ID=50678080

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201580024161.7A Pending CN106461228A (zh) 2014-05-09 2015-05-07 用于燃气涡轮发动机的燃烧器的旋流器、燃气涡轮发动机的燃烧器以及燃气涡轮发动机

Country Status (4)

Country Link
US (1) US20170051919A1 (fr)
EP (2) EP2942563A1 (fr)
CN (1) CN106461228A (fr)
WO (1) WO2015169930A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111520711A (zh) * 2020-03-17 2020-08-11 西北工业大学 一种改善离心式喷嘴积碳的结构

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD787041S1 (en) * 2015-09-17 2017-05-16 Whirlpool Corporation Gas burner
US10837643B2 (en) 2018-08-06 2020-11-17 General Electric Company Mixer assembly for a combustor
US11280495B2 (en) * 2020-03-04 2022-03-22 General Electric Company Gas turbine combustor fuel injector flow device including vanes

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030084667A1 (en) * 2001-11-05 2003-05-08 Miklos Gerendas Device for the injection of fuel into the flow wake of swirler vanes
CN101514819A (zh) * 2008-02-20 2009-08-26 英格索尔-兰德能源系统公司 气冷旋流式喷嘴头
CN101688669A (zh) * 2007-05-18 2010-03-31 西门子公司 燃料分配器
CN101876436A (zh) * 2009-04-29 2010-11-03 西门子公司 用于燃气涡轮发动机的燃烧器
CN101881448A (zh) * 2009-04-23 2010-11-10 通用电气公司 径向贫直接注射燃烧器
EP2314923A2 (fr) * 2009-10-23 2011-04-27 MAN Diesel & Turbo SE Tourbillonneur
CN102062412A (zh) * 2009-11-18 2011-05-18 西门子公司 旋流器叶片、旋流器和燃烧器组件
CN102378878A (zh) * 2009-04-06 2012-03-14 西门子公司 旋流器、燃烧腔以及具有改善的涡流的燃气涡轮机
CN104114944A (zh) * 2012-02-15 2014-10-22 西门子公司 将燃料以倾斜的燃料喷射方式喷入旋流器槽缝

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2333832A (en) 1998-01-31 1999-08-04 Europ Gas Turbines Ltd Multi-fuel gas turbine engine combustor
DE60122414T2 (de) * 2000-04-01 2006-12-21 Alstom Technology Ltd. Verbrennungssystem für eine Gasturbine
US7506511B2 (en) * 2003-12-23 2009-03-24 Honeywell International Inc. Reduced exhaust emissions gas turbine engine combustor
EP1835231A1 (fr) 2006-03-13 2007-09-19 Siemens Aktiengesellschaft Brûleur pour une chambre de combustion de turbine à gaz et procédé d'opération du brûleur
GB2444737B (en) 2006-12-13 2009-03-04 Siemens Ag Improvements in or relating to burners for a gas turbine engine

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030084667A1 (en) * 2001-11-05 2003-05-08 Miklos Gerendas Device for the injection of fuel into the flow wake of swirler vanes
CN101688669A (zh) * 2007-05-18 2010-03-31 西门子公司 燃料分配器
CN101514819A (zh) * 2008-02-20 2009-08-26 英格索尔-兰德能源系统公司 气冷旋流式喷嘴头
CN102378878A (zh) * 2009-04-06 2012-03-14 西门子公司 旋流器、燃烧腔以及具有改善的涡流的燃气涡轮机
CN101881448A (zh) * 2009-04-23 2010-11-10 通用电气公司 径向贫直接注射燃烧器
CN101876436A (zh) * 2009-04-29 2010-11-03 西门子公司 用于燃气涡轮发动机的燃烧器
EP2314923A2 (fr) * 2009-10-23 2011-04-27 MAN Diesel & Turbo SE Tourbillonneur
CN102062412A (zh) * 2009-11-18 2011-05-18 西门子公司 旋流器叶片、旋流器和燃烧器组件
CN104114944A (zh) * 2012-02-15 2014-10-22 西门子公司 将燃料以倾斜的燃料喷射方式喷入旋流器槽缝

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111520711A (zh) * 2020-03-17 2020-08-11 西北工业大学 一种改善离心式喷嘴积碳的结构

Also Published As

Publication number Publication date
US20170051919A1 (en) 2017-02-23
EP3140594A1 (fr) 2017-03-15
EP2942563A1 (fr) 2015-11-11
WO2015169930A1 (fr) 2015-11-12

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Application publication date: 20170222