JPH11201454A5 - - Google Patents

Info

Publication number
JPH11201454A5
JPH11201454A5 JP1998205225A JP20522598A JPH11201454A5 JP H11201454 A5 JPH11201454 A5 JP H11201454A5 JP 1998205225 A JP1998205225 A JP 1998205225A JP 20522598 A JP20522598 A JP 20522598A JP H11201454 A5 JPH11201454 A5 JP H11201454A5
Authority
JP
Japan
Prior art keywords
fuel
air
axis
nozzle
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.)
Pending
Application number
JP1998205225A
Other languages
English (en)
Japanese (ja)
Other versions
JPH11201454A (ja
Filing date
Publication date
Priority claimed from US09/033,615 external-priority patent/US6220034B1/en
Application filed filed Critical
Publication of JPH11201454A publication Critical patent/JPH11201454A/ja
Publication of JPH11201454A5 publication Critical patent/JPH11201454A5/ja
Pending legal-status Critical Current

Links

JP20522598A 1997-12-31 1998-07-21 空燃比が制御可能な改良された対流冷却・ 単段階・ 完全予備混合式燃焼器 Pending JPH11201454A (ja)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US162897A 1997-12-31 1997-12-31
US09/001628 1997-12-31
US09/033615 1997-12-31
US09/033,615 US6220034B1 (en) 1993-07-07 1998-03-03 Convectively cooled, single stage, fully premixed controllable fuel/air combustor

Publications (2)

Publication Number Publication Date
JPH11201454A JPH11201454A (ja) 1999-07-30
JPH11201454A5 true JPH11201454A5 (fr) 2005-10-27

Family

ID=26669291

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20522598A Pending JPH11201454A (ja) 1997-12-31 1998-07-21 空燃比が制御可能な改良された対流冷却・ 単段階・ 完全予備混合式燃焼器

Country Status (1)

Country Link
JP (1) JPH11201454A (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9929601D0 (en) * 1999-12-16 2000-02-09 Rolls Royce Plc A combustion chamber
WO2001071251A1 (fr) 2000-03-24 2001-09-27 Webasto Thermosysteme International Gmbh Bruleur binaire avec atomisation de combustible par tube de venturi, et tube de venturi pour atomisation de combustible liquide
US8281601B2 (en) * 2009-03-20 2012-10-09 General Electric Company Systems and methods for reintroducing gas turbine combustion bypass flow
DK177462B1 (en) * 2012-02-03 2013-06-17 Man Diesel & Turbo Deutschland Large turbocharged two-stroke diesel engine with exhaust gas purification
US9765973B2 (en) * 2013-03-12 2017-09-19 General Electric Company System and method for tube level air flow conditioning
NL2024101B1 (en) 2019-10-25 2021-07-19 Bekaert Combustion Tech Bv Surface stabilized fully premixed gas premix burner for burning hydrogen gas, and method for starting such burner

Similar Documents

Publication Publication Date Title
US5657632A (en) Dual fuel gas turbine combustor
US4891936A (en) Turbine combustor with tangential fuel injection and bender jets
US10502426B2 (en) Dual fuel injectors and methods of use in gas turbine combustor
US6109038A (en) Combustor with two stage primary fuel assembly
US5408825A (en) Dual fuel gas turbine combustor
CN111065860B (zh) 辅助火炬点火
US5479782A (en) Gas turbine combustor
CN1106533C (zh) 单级双模式燃烧器
US5862668A (en) Gas turbine engine combustion equipment
US7533531B2 (en) Internal fuel manifold with airblast nozzles
JP2009192214A (ja) ガスタービンエンジン用の燃料ノズル及びその製造方法
CN109424980A (zh) 预混燃料喷射器和在燃气涡轮燃烧器中的使用方法
KR20010024477A (ko) 독립적으로 제어 가능한 서로 다른 스테이지로의 연료유동을 가진 연소기
EP0863369A3 (fr) Chambre de combustion à étage unique avec prémélange
US20250251134A1 (en) Rotating detonation combustor with discrete detonation annuli
JP2009270816A (ja) ガスタービンエンジン用の燃料ノズル及びそれを製作する方法
JPH07305848A (ja) 燃料ノズル・アセンブリ、ガスタービン装置及び低NOxガスタービン装置における燃焼不安定性を低減する方法
JPH08509058A (ja) 低い先端温度を有するインジェクター
JPH02146228A (ja) 燃料噴射器
CN109899832A (zh) 用于燃气涡轮机燃烧器的轴向燃料分级系统
US7716933B2 (en) Multi-channel fuel manifold
CN106051823A (zh) 用于涡轮系统的微混合器系统及相关的方法
CN111911959B (zh) 包括入口唇缘的燃烧器预混合器组件
US2907171A (en) Combustion chamber inlet for thermal power plants
CN111520765A (zh) 具有非圆形横截面的旋转爆震燃烧器