JP2000009319A5 - - Google Patents

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Publication number
JP2000009319A5
JP2000009319A5 JP1999161306A JP16130699A JP2000009319A5 JP 2000009319 A5 JP2000009319 A5 JP 2000009319A5 JP 1999161306 A JP1999161306 A JP 1999161306A JP 16130699 A JP16130699 A JP 16130699A JP 2000009319 A5 JP2000009319 A5 JP 2000009319A5
Authority
JP
Japan
Prior art keywords
combustion
combustion chamber
air
injection means
region
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.)
Granted
Application number
JP1999161306A
Other languages
English (en)
Japanese (ja)
Other versions
JP4435331B2 (ja
JP2000009319A (ja
Filing date
Publication date
Priority claimed from FR9807409A external-priority patent/FR2779807B1/fr
Application filed filed Critical
Publication of JP2000009319A publication Critical patent/JP2000009319A/ja
Publication of JP2000009319A5 publication Critical patent/JP2000009319A5/ja
Application granted granted Critical
Publication of JP4435331B2 publication Critical patent/JP4435331B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

JP16130699A 1998-06-11 1999-06-08 可変スロートガスタービン燃焼チャンバー Expired - Lifetime JP4435331B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9807409A FR2779807B1 (fr) 1998-06-11 1998-06-11 Chambre de combustion de turbine a gaz a geometrie variable
FR9807409 1998-06-11

Publications (3)

Publication Number Publication Date
JP2000009319A JP2000009319A (ja) 2000-01-14
JP2000009319A5 true JP2000009319A5 (enExample) 2006-07-27
JP4435331B2 JP4435331B2 (ja) 2010-03-17

Family

ID=9527308

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16130699A Expired - Lifetime JP4435331B2 (ja) 1998-06-11 1999-06-08 可変スロートガスタービン燃焼チャンバー

Country Status (5)

Country Link
US (1) US6263663B1 (enExample)
EP (1) EP0964206B1 (enExample)
JP (1) JP4435331B2 (enExample)
DE (1) DE69922437T2 (enExample)
FR (1) FR2779807B1 (enExample)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1819964A2 (en) * 2004-06-11 2007-08-22 Vast Power Systems, Inc. Low emissions combustion apparatus and method
JP4670035B2 (ja) * 2004-06-25 2011-04-13 独立行政法人 宇宙航空研究開発機構 ガスタービン燃焼器
JP2007113888A (ja) * 2005-10-24 2007-05-10 Kawasaki Heavy Ind Ltd ガスタービンエンジンの燃焼器構造
US8915086B2 (en) 2006-08-07 2014-12-23 General Electric Company System for controlling combustion dynamics and method for operating the same
GB0815761D0 (en) * 2008-09-01 2008-10-08 Rolls Royce Plc Swirler for a fuel injector
US8099941B2 (en) * 2008-12-31 2012-01-24 General Electric Company Methods and systems for controlling a combustor in turbine engines
US8276386B2 (en) * 2010-09-24 2012-10-02 General Electric Company Apparatus and method for a combustor
US9316155B2 (en) * 2013-03-18 2016-04-19 General Electric Company System for providing fuel to a combustor
US9803555B2 (en) * 2014-04-23 2017-10-31 General Electric Company Fuel delivery system with moveably attached fuel tube
FR3065059B1 (fr) 2017-04-11 2020-11-06 Office National Detudes Rech Aerospatiales Foyer de turbine a gaz a geometrie variable auto-adaptative
WO2022079523A1 (en) * 2020-10-14 2022-04-21 King Abdullah University Of Science And Technology Adjustable fuel injector for flame dynamics control
RU2757705C1 (ru) * 2021-01-13 2021-10-20 Роман Лазирович Илиев Горелка с двухслойным вихревым противоточным течением
GB202112642D0 (en) 2021-09-06 2021-10-20 Rolls Royce Plc Controlling soot
GB202112641D0 (en) * 2021-09-06 2021-10-20 Rolls Royce Plc Controlling soot
CN116592391A (zh) * 2022-02-07 2023-08-15 通用电气公司 具有可变初级区燃烧室的燃烧器
CN115031260B (zh) * 2022-05-30 2023-08-22 中国人民解放军空军工程大学 一种旋转爆震燃烧室出口喉道位置固定的可调喷管
JP2025535131A (ja) * 2022-10-11 2025-10-22 イノロム アイヴイ ホールディングス イノベーション アンド ベンチャーズ リミテッド ２層渦対向流を有する２段バーナ

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3691761A (en) * 1967-11-10 1972-09-19 Squire Ronald Jackson Apparatus for regulation of airflow to flame tubes for gas turbine engines
DE2020416A1 (de) * 1970-04-27 1971-11-11 Motoren Turbinen Union Brennkammer fuer Gasturbinentriebwerke
US3869246A (en) * 1973-12-26 1975-03-04 Gen Motors Corp Variable configuration combustion apparatus
FR2270448A1 (en) * 1974-05-10 1975-12-05 Bennes Marrel Gas turbine combustion chamber - has spring loaded bellows controlling annular air flow control membrane
US4296599A (en) * 1979-03-30 1981-10-27 General Electric Company Turbine cooling air modulation apparatus
JP2644745B2 (ja) * 1987-03-06 1997-08-25 株式会社日立製作所 ガスタービン用燃焼器
FR2661714B1 (fr) * 1990-05-03 1994-06-17 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz.

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