JP5802059B2 - 燃料噴射ノズル本体上の火炎安定化用のディンプル付き／グルーブ付き面及び関連する方法 - Google Patents

燃料噴射ノズル本体上の火炎安定化用のディンプル付き／グルーブ付き面及び関連する方法 Download PDF

Info

Publication number
JP5802059B2
JP5802059B2 JP2011128763A JP2011128763A JP5802059B2 JP 5802059 B2 JP5802059 B2 JP 5802059B2 JP 2011128763 A JP2011128763 A JP 2011128763A JP 2011128763 A JP2011128763 A JP 2011128763A JP 5802059 B2 JP5802059 B2 JP 5802059B2
Authority
JP
Japan
Prior art keywords
face
fuel
fuel injection
downstream end
injection head
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
JP2011128763A
Other languages
English (en)
Japanese (ja)
Other versions
JP2012042194A (ja
JP2012042194A5 (enExample
Inventor
ジョン・ホー・オム
トーマス・エドワード・ジョンソン
カンウー・キム
バイファン・ツオ
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JP2012042194A publication Critical patent/JP2012042194A/ja
Publication of JP2012042194A5 publication Critical patent/JP2012042194A5/ja
Application granted granted Critical
Publication of JP5802059B2 publication Critical patent/JP5802059B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F23R3/16—Continuous 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
    • 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
    • F23D14/48—Nozzles
    • F23D14/58—Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00004—Preventing formation of deposits on surfaces of gas turbine components, e.g. coke deposits
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
JP2011128763A 2010-08-13 2011-06-09 燃料噴射ノズル本体上の火炎安定化用のディンプル付き／グルーブ付き面及び関連する方法 Expired - Fee Related JP5802059B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/855,801 2010-08-13
US12/855,801 US8511092B2 (en) 2010-08-13 2010-08-13 Dimpled/grooved face on a fuel injection nozzle body for flame stabilization and related method

Publications (3)

Publication Number Publication Date
JP2012042194A JP2012042194A (ja) 2012-03-01
JP2012042194A5 JP2012042194A5 (enExample) 2014-07-24
JP5802059B2 true JP5802059B2 (ja) 2015-10-28

Family

ID=45528539

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011128763A Expired - Fee Related JP5802059B2 (ja) 2010-08-13 2011-06-09 燃料噴射ノズル本体上の火炎安定化用のディンプル付き／グルーブ付き面及び関連する方法

Country Status (5)

Country Link
US (1) US8511092B2 (enExample)
JP (1) JP5802059B2 (enExample)
CN (1) CN102374535B (enExample)
CH (1) CH703548B1 (enExample)
DE (1) DE102011050781A1 (enExample)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9163839B2 (en) * 2012-03-19 2015-10-20 General Electric Company Micromixer combustion head end assembly
US9534781B2 (en) 2012-05-10 2017-01-03 General Electric Company System and method having multi-tube fuel nozzle with differential flow
US8701419B2 (en) 2012-05-10 2014-04-22 General Electric Company Multi-tube fuel nozzle with mixing features
US9709277B2 (en) 2012-05-15 2017-07-18 General Electric Company Fuel plenum premixing tube with surface treatment
US9175855B2 (en) 2012-10-29 2015-11-03 General Electric Company Combustion nozzle with floating aft plate
US9151503B2 (en) * 2013-01-04 2015-10-06 General Electric Company Coaxial fuel supply for a micromixer
WO2014141397A1 (ja) 2013-03-13 2014-09-18 株式会社日立製作所 ガスタービン燃焼器
EP3224544A1 (en) * 2014-11-26 2017-10-04 Siemens Aktiengesellschaft Fuel lance with means for interacting with a flow of air and improve breakage of an ejected liquid jet of fuel
CN107750322A (zh) * 2015-06-24 2018-03-02 通用电气公司 具有预混合火焰稳定器的燃料喷嘴组件
CN106287816B (zh) * 2016-08-12 2019-01-18 中国航空工业集团公司沈阳发动机设计研究所 一种干式低排放燃烧器
WO2018144006A1 (en) * 2017-02-03 2018-08-09 Siemens Aktiengesellschaft Method for normalizing fuel-air mixture within a combustor
US11719440B2 (en) 2018-12-19 2023-08-08 Doosan Enerbility Co., Ltd. Pre-swirler having dimples
WO2023145218A1 (ja) 2022-01-31 2023-08-03 株式会社Ihi 燃焼装置およびガスタービンシステム
CN116658935B (zh) * 2022-02-17 2025-07-25 中国航发商用航空发动机有限责任公司 燃烧室头部、燃烧室、燃气轮机
US20240230095A1 (en) * 2023-01-06 2024-07-11 Ge Infrastructure Technology Llc Gas turbine combustor with multiple fuel stages and method of operation

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4100733A (en) * 1976-10-04 1978-07-18 United Technologies Corporation Premix combustor
DE3361535D1 (en) * 1982-05-28 1986-01-30 Bbc Brown Boveri & Cie Gas turbine combustion chamber and method of operating it
GB2333832A (en) * 1998-01-31 1999-08-04 Europ Gas Turbines Ltd Multi-fuel gas turbine engine combustor
JP2005106305A (ja) * 2003-09-29 2005-04-21 Hitachi Ltd 燃料燃焼用ノズルおよびガスタービン燃焼器の燃料供給方法
US7007478B2 (en) 2004-06-30 2006-03-07 General Electric Company Multi-venturi tube fuel injector for a gas turbine combustor
US7827797B2 (en) * 2006-09-05 2010-11-09 General Electric Company Injection assembly for a combustor
US7861528B2 (en) * 2007-08-21 2011-01-04 General Electric Company Fuel nozzle and diffusion tip therefor
US8209986B2 (en) * 2008-10-29 2012-07-03 General Electric Company Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event
US9140454B2 (en) * 2009-01-23 2015-09-22 General Electric Company Bundled multi-tube nozzle for a turbomachine
US8205452B2 (en) * 2009-02-02 2012-06-26 General Electric Company Apparatus for fuel injection in a turbine engine
US8539773B2 (en) * 2009-02-04 2013-09-24 General Electric Company Premixed direct injection nozzle for highly reactive fuels
US8261555B2 (en) * 2010-07-08 2012-09-11 General Electric Company Injection nozzle for a turbomachine

Also Published As

Publication number Publication date
JP2012042194A (ja) 2012-03-01
CH703548B1 (de) 2016-02-29
CN102374535B (zh) 2015-11-25
US8511092B2 (en) 2013-08-20
US20120036856A1 (en) 2012-02-16
CN102374535A (zh) 2012-03-14
DE102011050781A1 (de) 2012-02-16
CH703548A2 (de) 2012-02-15

Similar Documents

Publication Publication Date Title
JP5802059B2 (ja) 燃料噴射ノズル本体上の火炎安定化用のディンプル付き／グルーブ付き面及び関連する方法
JP6285081B2 (ja) ガスタービンエンジンの燃焼装置
JP5528756B2 (ja) 二次燃料ノズル用の管状燃料噴射器
JP6285022B2 (ja) ガスタービンエンジンの燃焼装置
JP4744953B2 (ja) ガスタービン燃焼器用多ベンチュリ管燃料インジェクタ
JP4906689B2 (ja) バーナ，燃焼装置及び燃焼装置の改造方法
US8113000B2 (en) Flashback resistant pre-mixer assembly
CN206973615U (zh) 先导预混合喷嘴和燃料喷嘴组件
US10480414B2 (en) Combustor and gas turbine with phase adjusting units in the fuel nozzles
US20120180487A1 (en) System for flow control in multi-tube fuel nozzle
JP2018115849A (ja) ガスタービン燃焼器の燃料噴射器および使用方法
JP2009074792A (ja) Ｄｌｎガスタービンの二次燃料ノズル用トロイダルリングマニホルド
US20230408097A1 (en) Multitube pilot injector having a flame anchor for a gas tubine engine
WO2014141397A1 (ja) ガスタービン燃焼器
JP2005326144A (ja) 燃料噴射装置および燃料噴射装置の設計方法
US8661825B2 (en) Pegless secondary fuel nozzle including a unitary fuel injection manifold
US20200284431A1 (en) Combustor and combustor array
KR102462494B1 (ko) 버너 장치 및 다관식 관류 보일러 장치
JP2014105886A (ja) 燃焼器
CN111868441B (zh) 燃烧器装置
JP6092007B2 (ja) ガスタービン燃焼器
JP5893879B2 (ja) ガスタービン燃焼器
JP5241906B2 (ja) バーナ及びバーナの運転方法
JP2015072077A (ja) ガスタービン燃焼器
WO2019093382A1 (ja) バーナ装置

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20140605

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20140605

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20150413

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20150421

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20150707

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20150804

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20150828

R150 Certificate of patent or registration of utility model

Ref document number: 5802059

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees