CN1878986B - 燃气轮机引擎的稳定燃烧装置 - Google Patents

燃气轮机引擎的稳定燃烧装置 Download PDF

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Publication number
CN1878986B
CN1878986B CN2004800328006A CN200480032800A CN1878986B CN 1878986 B CN1878986 B CN 1878986B CN 2004800328006 A CN2004800328006 A CN 2004800328006A CN 200480032800 A CN200480032800 A CN 200480032800A CN 1878986 B CN1878986 B CN 1878986B
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CN
China
Prior art keywords
burner
mixing chamber
fuel
combustion
chamber
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 - Fee Related
Application number
CN2004800328006A
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English (en)
Chinese (zh)
Other versions
CN1878986A (zh
Inventor
M·康韦尔
V·D·米洛萨夫列维奇
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 Industrial Turbomachinery
Siemens AG
Collins Engine Nozzles Inc
Original Assignee
Delavan Inc
Demag Delaval Industrial Turbomachinery Inc
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 Delavan Inc, Demag Delaval Industrial Turbomachinery Inc filed Critical Delavan Inc
Publication of CN1878986A publication Critical patent/CN1878986A/zh
Application granted granted Critical
Publication of CN1878986B publication Critical patent/CN1878986B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F23R3/286Continuous 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
    • 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
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/72Safety devices, e.g. operative in case of failure of gas supply
    • 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
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/72Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/74Preventing flame lift-off
    • 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
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2209/00Safety arrangements
    • F23D2209/20Flame lift-off / stability

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)
CN2004800328006A 2003-09-05 2004-09-03 燃气轮机引擎的稳定燃烧装置 Expired - Fee Related CN1878986B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US50051703P 2003-09-05 2003-09-05
US60/500,517 2003-09-05
PCT/US2004/028768 WO2005040682A2 (en) 2003-09-05 2004-09-03 Device for stabilizing combustion in gas turbine engines

Publications (2)

Publication Number Publication Date
CN1878986A CN1878986A (zh) 2006-12-13
CN1878986B true CN1878986B (zh) 2010-04-28

Family

ID=34519984

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2004800328006A Expired - Fee Related CN1878986B (zh) 2003-09-05 2004-09-03 燃气轮机引擎的稳定燃烧装置

Country Status (9)

Country Link
US (1) US20050106520A1 (ja)
EP (1) EP1668295A2 (ja)
JP (1) JP4767851B2 (ja)
KR (1) KR101178195B1 (ja)
CN (1) CN1878986B (ja)
BR (1) BRPI0413966A (ja)
CA (1) CA2537949C (ja)
RU (1) RU2407950C2 (ja)
WO (1) WO2005040682A2 (ja)

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EP2107312A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Pilot combustor in a burner
JP5462449B2 (ja) * 2008-05-23 2014-04-02 川崎重工業株式会社 燃焼装置のバーナおよびこれを備えた燃焼装置
US8276385B2 (en) * 2009-10-08 2012-10-02 General Electric Company Staged multi-tube premixing injector
EP2434221A1 (en) * 2010-09-22 2012-03-28 Siemens Aktiengesellschaft Method and arrangement for injecting an emulsion into a flame
EP2434218A1 (en) 2010-09-22 2012-03-28 Siemens Aktiengesellschaft Burner with low NOx emissions
US9052112B2 (en) * 2012-02-27 2015-06-09 General Electric Company Combustor and method for purging a combustor
EP2703721B1 (en) 2012-08-31 2019-05-22 Ansaldo Energia IP UK Limited Premix burner
US11460188B2 (en) 2013-02-14 2022-10-04 Clearsign Technologies Corporation Ultra low emissions firetube boiler burner
US10119704B2 (en) 2013-02-14 2018-11-06 Clearsign Combustion Corporation Burner system including a non-planar perforated flame holder
US10386062B2 (en) 2013-02-14 2019-08-20 Clearsign Combustion Corporation Method for operating a combustion system including a perforated flame holder
EP3055616B1 (en) 2013-10-07 2020-12-09 ClearSign Technologies Corporation Pre-mixed fuel burner with perforated flame holder
JP6395363B2 (ja) * 2013-10-11 2018-09-26 川崎重工業株式会社 ガスタービンの燃料噴射装置
CN105960565B (zh) 2014-01-24 2019-11-12 克利尔赛恩燃烧公司 低NOx火管锅炉
JP6177187B2 (ja) * 2014-04-30 2017-08-09 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、ガスタービン、制御装置及び制御方法
EP2942565A1 (de) * 2014-05-05 2015-11-11 Siemens Aktiengesellschaft Verfahren zum Betreiben einer Brenneranordnung
JP5958981B2 (ja) * 2015-02-13 2016-08-02 新潟原動機株式会社 ガスタービン燃焼器における火炎リフト距離変更方法
CN104896510B (zh) * 2015-05-13 2017-02-01 广东电网有限责任公司电力科学研究院 火焰稳定器和带有该火焰稳定器的地面燃机燃烧室
FR3039254B1 (fr) * 2015-07-24 2021-10-08 Snecma Chambre de combustion comportant des dispositifs d'injection additionnels debouchant directement dans les zones de recirculation de coin, turbomachine la comprenant, et procede d'alimentation en carburant de celle-ci
CN105240872B (zh) * 2015-09-17 2018-05-25 中国航空工业集团公司沈阳发动机设计研究所 一种燃烧室头部组件
RU2635958C1 (ru) * 2016-06-09 2017-11-17 федеральное государственное автономное образовательное учреждение высшего образования "Южно-Уральский государственный университет" (национальный исследовательский университет) Вихревая горелка для газовой турбины
US20180010795A1 (en) * 2016-07-06 2018-01-11 General Electric Company Deflector for gas turbine engine combustors and method of using the same
CN110023679A (zh) * 2017-01-19 2019-07-16 克利尔赛恩燃烧公司 包括用于增强稳定性和降低温度的穿孔钝体火焰保持器的炉
US11175045B2 (en) * 2018-01-04 2021-11-16 General Electric Company Fuel nozzle for gas turbine engine combustor
CN109668172B (zh) * 2018-12-10 2020-11-10 中国航天空气动力技术研究院 一种可控脉动涡流的高速燃油掺混器
CN111520750B (zh) * 2020-03-25 2022-05-20 西北工业大学 新型燃烧室头部喷油结构
US11920793B1 (en) * 2023-06-23 2024-03-05 Pratt & Whitney Canada Corp. Adjustable gaseous fuel injector
CN117109029B (zh) * 2023-08-25 2024-02-02 西南科技大学 一种钝体火焰稳定器以及航空发动机燃烧组件

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Also Published As

Publication number Publication date
KR101178195B1 (ko) 2012-08-30
WO2005040682A2 (en) 2005-05-06
EP1668295A2 (en) 2006-06-14
CN1878986A (zh) 2006-12-13
JP2007504429A (ja) 2007-03-01
JP4767851B2 (ja) 2011-09-07
CA2537949C (en) 2011-01-11
RU2407950C2 (ru) 2010-12-27
BRPI0413966A (pt) 2006-10-31
US20050106520A1 (en) 2005-05-19
RU2006110986A (ru) 2006-07-27
WO2005040682A3 (en) 2005-08-11
KR20060086358A (ko) 2006-07-31
CA2537949A1 (en) 2005-05-06

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
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GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: SIEMENS AKTIENGESELLSCHAFT

Free format text: FORMER OWNER: DELAVAN INC.

Effective date: 20140801

Free format text: FORMER OWNER: SIEMENS INDUSTRIAL TURBINE MACHINERY COMPANY

Effective date: 20140801

C41 Transfer of patent application or patent right or utility model
C56 Change in the name or address of the patentee
CP01 Change in the name or title of a patent holder

Address after: Iowa

Patentee after: Delavan Inc.

Patentee after: SIEMENS industrial Turbomachinery

Address before: Iowa

Patentee before: Delavan Inc.

Patentee before: Demag Delaval Ind Turbomachine

TR01 Transfer of patent right

Effective date of registration: 20140801

Address after: Munich, Germany

Patentee after: SIEMENS AG

Address before: Iowa

Patentee before: Delavan Inc.

Patentee before: SIEMENS industrial Turbomachinery

CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100428

Termination date: 20150903

EXPY Termination of patent right or utility model