JP2013529771A5 - - Google Patents

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Publication number
JP2013529771A5
JP2013529771A5 JP2013517313A JP2013517313A JP2013529771A5 JP 2013529771 A5 JP2013529771 A5 JP 2013529771A5 JP 2013517313 A JP2013517313 A JP 2013517313A JP 2013517313 A JP2013517313 A JP 2013517313A JP 2013529771 A5 JP2013529771 A5 JP 2013529771A5
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JP
Japan
Prior art keywords
full jet
burner device
cap
jet nozzles
central axis
Prior art date
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Application number
JP2013517313A
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English (en)
Japanese (ja)
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JP6005040B2 (ja
JP2013529771A (ja
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Publication date
Priority claimed from EP10168107A external-priority patent/EP2402652A1/de
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Publication of JP2013529771A publication Critical patent/JP2013529771A/ja
Publication of JP2013529771A5 publication Critical patent/JP2013529771A5/ja
Application granted granted Critical
Publication of JP6005040B2 publication Critical patent/JP6005040B2/ja
Active legal-status Critical Current
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JP2013517313A 2010-07-01 2011-07-01 バーナー装置 Active JP6005040B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP10168107.0 2010-07-01
EP10168107A EP2402652A1 (de) 2010-07-01 2010-07-01 Brenner
PCT/EP2011/061101 WO2012001141A1 (de) 2010-07-01 2011-07-01 Brenneranordnung

Publications (3)

Publication Number Publication Date
JP2013529771A JP2013529771A (ja) 2013-07-22
JP2013529771A5 true JP2013529771A5 (enrdf_load_stackoverflow) 2013-09-05
JP6005040B2 JP6005040B2 (ja) 2016-10-12

Family

ID=43531833

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013517313A Active JP6005040B2 (ja) 2010-07-01 2011-07-01 バーナー装置

Country Status (4)

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US (1) US20130104554A1 (enrdf_load_stackoverflow)
EP (2) EP2402652A1 (enrdf_load_stackoverflow)
JP (1) JP6005040B2 (enrdf_load_stackoverflow)
WO (1) WO2012001141A1 (enrdf_load_stackoverflow)

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US9671112B2 (en) 2013-03-12 2017-06-06 General Electric Company Air diffuser for a head end of a combustor
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US9650959B2 (en) 2013-03-12 2017-05-16 General Electric Company Fuel-air mixing system with mixing chambers of various lengths for gas turbine system
US9759425B2 (en) * 2013-03-12 2017-09-12 General Electric Company System and method having multi-tube fuel nozzle with multiple fuel injectors
US9765973B2 (en) 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
US9534787B2 (en) 2013-03-12 2017-01-03 General Electric Company Micromixing cap assembly
JP5984770B2 (ja) * 2013-09-27 2016-09-06 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
CN106715870B (zh) 2014-07-02 2018-11-09 诺沃皮尼奥内股份有限公司 燃料分配装置、燃气涡轮发动机和安装方法
CN104315540B (zh) * 2014-09-26 2018-05-25 北京华清燃气轮机与煤气化联合循环工程技术有限公司 燃气轮机燃烧室预混燃料喷嘴
EP3209940A1 (en) 2014-10-23 2017-08-30 Siemens Aktiengesellschaft Flexible fuel combustion system for turbine engines
US20170328568A1 (en) * 2014-11-26 2017-11-16 Siemens Aktiengesellschaft Fuel lance with means for interacting with a flow of air and improve breakage of an ejected liquid jet of fuel
US10830445B2 (en) 2015-12-30 2020-11-10 General Electric Company Liquid fuel nozzles for dual fuel combustors
US10739003B2 (en) * 2016-10-03 2020-08-11 United Technologies Corporation Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine
US10393030B2 (en) * 2016-10-03 2019-08-27 United Technologies Corporation Pilot injector fuel shifting in an axial staged combustor for a gas turbine engine
US10508811B2 (en) * 2016-10-03 2019-12-17 United Technologies Corporation Circumferential fuel shifting and biasing in an axial staged combustor for a gas turbine engine
US10738704B2 (en) * 2016-10-03 2020-08-11 Raytheon Technologies Corporation Pilot/main fuel shifting in an axial staged combustor for a gas turbine engine
CN107023834B (zh) * 2017-04-19 2019-01-08 中国科学院工程热物理研究所 一种多尺度值班火焰的喷嘴及燃烧器
US10584877B2 (en) 2017-04-28 2020-03-10 DOOSAN Heavy Industries Construction Co., LTD Device to correct flow non-uniformity within a combustion system
DE102020203422B4 (de) * 2020-03-17 2024-02-01 Dometic Sweden Ab Heizvorrichtung, Freizeitfahrzeug mit Heizvorrichtung und Verfahren zum Heizen von Fluiden in einem Freizeitfahrzeug
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
US11421883B2 (en) * 2020-09-11 2022-08-23 Raytheon Technologies Corporation Fuel injector assembly with a helical swirler passage for a turbine engine
US20220205637A1 (en) * 2020-12-30 2022-06-30 General Electric Company Mitigating combustion dynamics using varying liquid fuel cartridges
KR102460672B1 (ko) * 2021-01-06 2022-10-27 두산에너빌리티 주식회사 연료 노즐, 연료 노즐 모듈 및 이를 포함하는 연소기
US12025311B2 (en) * 2021-08-24 2024-07-02 Solar Turbines Incorporated Micromix fuel injection air nozzles
US11617981B1 (en) 2022-01-03 2023-04-04 Saudi Arabian Oil Company Method for capturing CO2 with assisted vapor compression
KR102583223B1 (ko) * 2022-01-28 2023-09-25 두산에너빌리티 주식회사 연소기용 노즐, 연소기 및 이를 포함하는 가스터빈
GB2629434A (en) * 2023-04-28 2024-10-30 Siemens Energy Global Gmbh & Co Kg Fuel lance for burner of gas turbine engine

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