GB0524097D0 - A combustion apparatus - Google Patents

A combustion apparatus

Info

Publication number
GB0524097D0
GB0524097D0 GBGB0524097.3A GB0524097A GB0524097D0 GB 0524097 D0 GB0524097 D0 GB 0524097D0 GB 0524097 A GB0524097 A GB 0524097A GB 0524097 D0 GB0524097 D0 GB 0524097D0
Authority
GB
United Kingdom
Prior art keywords
combustion apparatus
combustion
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Withdrawn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
GBGB0524097.3A
Other versions
GB2432655A (en
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 GB0524097A priority Critical patent/GB2432655A/en
Publication of GB0524097D0 publication Critical patent/GB0524097D0/en
Priority to JP2008541752A priority patent/JP4785932B2/en
Priority to US12/084,601 priority patent/US20090142716A1/en
Priority to EP06819738.3A priority patent/EP1952066B1/en
Priority to RU2008125896/06A priority patent/RU2419031C2/en
Priority to PCT/EP2006/068870 priority patent/WO2007060216A1/en
Priority to CN2006800436353A priority patent/CN101313178B/en
Publication of GB2432655A publication Critical patent/GB2432655A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F23D14/04—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
    • F23D14/06—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner with radial outlets at the burner head
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/76—Protecting flame and burner parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/82—Preventing flashback or blowback
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cyclones (AREA)
  • Gas Burners (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
GB0524097A 2005-11-26 2005-11-26 Combustion apparatus Withdrawn GB2432655A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
GB0524097A GB2432655A (en) 2005-11-26 2005-11-26 Combustion apparatus
JP2008541752A JP4785932B2 (en) 2005-11-26 2006-11-24 Combustion device
US12/084,601 US20090142716A1 (en) 2005-11-26 2006-11-24 Combustion Apparatus
EP06819738.3A EP1952066B1 (en) 2005-11-26 2006-11-24 A combustion apparatus
RU2008125896/06A RU2419031C2 (en) 2005-11-26 2006-11-24 Combustion unit
PCT/EP2006/068870 WO2007060216A1 (en) 2005-11-26 2006-11-24 A combustion apparatus
CN2006800436353A CN101313178B (en) 2005-11-26 2006-11-24 A combustion apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0524097A GB2432655A (en) 2005-11-26 2005-11-26 Combustion apparatus

Publications (2)

Publication Number Publication Date
GB0524097D0 true GB0524097D0 (en) 2006-01-04
GB2432655A GB2432655A (en) 2007-05-30

Family

ID=35601270

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0524097A Withdrawn GB2432655A (en) 2005-11-26 2005-11-26 Combustion apparatus

Country Status (7)

Country Link
US (1) US20090142716A1 (en)
EP (1) EP1952066B1 (en)
JP (1) JP4785932B2 (en)
CN (1) CN101313178B (en)
GB (1) GB2432655A (en)
RU (1) RU2419031C2 (en)
WO (1) WO2007060216A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104329689B (en) * 2014-03-26 2016-08-17 中国科学院工程热物理研究所 A kind of combustor using swirl vane trailing edge pre-film atomizing type
CN114294676A (en) * 2021-12-16 2022-04-08 北京动力机械研究所 Precombustion chamber structure with wide ignition boundary

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1867925A1 (en) * 2006-06-12 2007-12-19 Siemens Aktiengesellschaft Burner
JP5172468B2 (en) * 2008-05-23 2013-03-27 川崎重工業株式会社 Combustion device and control method of combustion device
EP2169312A1 (en) 2008-09-25 2010-03-31 Siemens Aktiengesellschaft Stepped swirler for dynamic control
EP2192347B1 (en) 2008-11-26 2014-01-01 Siemens Aktiengesellschaft Tubular swirling chamber
FR2945854B1 (en) * 2009-05-19 2015-08-07 Snecma MIXTURE SPINDLE FOR A FUEL INJECTOR IN A COMBUSTION CHAMBER OF A GAS TURBINE AND CORRESPONDING COMBUSTION DEVICE
EP2327933A1 (en) * 2009-11-30 2011-06-01 Siemens Aktiengesellschaft Burner assembly
JP5156066B2 (en) * 2010-08-27 2013-03-06 株式会社日立製作所 Gas turbine combustor
CN102310199B (en) * 2011-10-10 2013-08-07 西南大学 Method for preparing WC-Co nano composite powder by in situ reduction and carbonization
US9322549B2 (en) * 2011-12-20 2016-04-26 Exxonmobil Chemical Patents Inc. Mixer/flow distributors
JP5584260B2 (en) * 2012-08-08 2014-09-03 日野自動車株式会社 Exhaust purification device burner
US9447974B2 (en) 2012-09-13 2016-09-20 United Technologies Corporation Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine
US9534790B2 (en) * 2013-01-07 2017-01-03 General Electric Company Fuel injector for supplying fuel to a combustor
CN103486618B (en) * 2013-09-29 2015-07-01 北京动力机械研究所 Cyclone for aviation gas turbine engine
CN104534514B (en) * 2014-11-27 2017-09-15 北京华清燃气轮机与煤气化联合循环工程技术有限公司 A kind of gas-turbine combustion chamber blade bleed swirl nozzle
CA2994119A1 (en) * 2015-07-31 2017-02-09 Nuvera Fuel Cells, LLC Burner assembly with low nox emissions
EP3159609A1 (en) * 2015-10-21 2017-04-26 Siemens Aktiengesellschaft Combustor for a gas turbine
EP3403028B1 (en) 2016-01-15 2021-02-24 Siemens Energy Global GmbH & Co. KG Combustor for a gas turbine
CN107014618B (en) * 2017-03-29 2019-03-29 浙江大学 A kind of combustion chamber and turbine coupling mechanism experiment research device
GB2561190A (en) * 2017-04-04 2018-10-10 Edwards Ltd Purge gas feeding means, abatement systems and methods of modifying abatement systems
US11280495B2 (en) * 2020-03-04 2022-03-22 General Electric Company Gas turbine combustor fuel injector flow device including vanes
CN112684099B (en) * 2020-12-18 2022-09-09 郑州大学 Assembled turbulent flame extinguishing device
US11761632B2 (en) * 2021-08-05 2023-09-19 General Electric Company Combustor swirler with vanes incorporating open area

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3618317A (en) * 1969-04-17 1971-11-09 Gen Electric Fuel delivery apparatus
DE4228816C2 (en) * 1992-08-29 1998-08-06 Mtu Muenchen Gmbh Burners for gas turbine engines
JP2666117B2 (en) * 1994-06-10 1997-10-22 財団法人石油産業活性化センター Pre-evaporation premix combustor
ATE206513T1 (en) * 1994-07-13 2001-10-15 Volvo Aero Corp GAS TURBINE CHAMBER WITH LOW POLLUTANT EMISSIONS
EP0728989B1 (en) * 1995-01-13 2001-11-28 European Gas Turbines Limited Gas turbine engine combustor
GB2299399A (en) * 1995-03-25 1996-10-02 Rolls Royce Plc Variable geometry air-fuel injector
FR2752917B1 (en) * 1996-09-05 1998-10-02 Snecma ADVANCED HOMOGENIZATION INJECTION SYSTEM
FR2753779B1 (en) * 1996-09-26 1998-10-16 AERODYNAMIC INJECTION SYSTEM FOR A FUEL AIR MIXTURE
EP0849530A3 (en) * 1996-12-20 1999-06-09 United Technologies Corporation Fuel nozzles and centerbodies therefor
US6550251B1 (en) * 1997-12-18 2003-04-22 General Electric Company Venturiless swirl cup
GB2333832A (en) * 1998-01-31 1999-08-04 Europ Gas Turbines Ltd Multi-fuel gas turbine engine combustor
GB2337102A (en) * 1998-05-09 1999-11-10 Europ Gas Turbines Ltd Gas-turbine engine combustor
GB9818160D0 (en) * 1998-08-21 1998-10-14 Rolls Royce Plc A combustion chamber
US6865889B2 (en) * 2002-02-01 2005-03-15 General Electric Company Method and apparatus to decrease combustor emissions
FR2836986B1 (en) * 2002-03-07 2004-11-19 Snecma Moteurs MULTI-MODEL INJECTION SYSTEM FOR AN AIR / FUEL MIXTURE IN A COMBUSTION CHAMBER
US7104066B2 (en) * 2003-08-19 2006-09-12 General Electric Company Combuster swirler assembly
US7065972B2 (en) * 2004-05-21 2006-06-27 Honeywell International, Inc. Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104329689B (en) * 2014-03-26 2016-08-17 中国科学院工程热物理研究所 A kind of combustor using swirl vane trailing edge pre-film atomizing type
CN114294676A (en) * 2021-12-16 2022-04-08 北京动力机械研究所 Precombustion chamber structure with wide ignition boundary
CN114294676B (en) * 2021-12-16 2023-05-12 北京动力机械研究所 Pre-combustion chamber structure with wide ignition boundary

Also Published As

Publication number Publication date
EP1952066B1 (en) 2016-08-31
RU2419031C2 (en) 2011-05-20
GB2432655A (en) 2007-05-30
CN101313178A (en) 2008-11-26
EP1952066A1 (en) 2008-08-06
US20090142716A1 (en) 2009-06-04
JP2009517621A (en) 2009-04-30
CN101313178B (en) 2011-08-31
RU2008125896A (en) 2010-01-10
WO2007060216A1 (en) 2007-05-31
JP4785932B2 (en) 2011-10-05

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)