JP2002048342A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2002048342A5 JP2002048342A5 JP2001193831A JP2001193831A JP2002048342A5 JP 2002048342 A5 JP2002048342 A5 JP 2002048342A5 JP 2001193831 A JP2001193831 A JP 2001193831A JP 2001193831 A JP2001193831 A JP 2001193831A JP 2002048342 A5 JP2002048342 A5 JP 2002048342A5
- Authority
- JP
- Japan
- 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
Links
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/604,985 US6540162B1 (en) | 2000-06-28 | 2000-06-28 | Methods and apparatus for decreasing combustor emissions with spray bar assembly |
US09/604985 | 2000-06-28 |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2002048342A JP2002048342A (ja) | 2002-02-15 |
JP2002048342A5 true JP2002048342A5 (ja) | 2008-07-31 |
JP4648580B2 JP4648580B2 (ja) | 2011-03-09 |
Family
ID=24421810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2001193831A Expired - Fee Related JP4648580B2 (ja) | 2000-06-28 | 2001-06-27 | 噴霧バー組立体を用いて燃焼器のエミッションを減少させる方法及び装置 |
Country Status (6)
Country | Link |
---|---|
US (2) | US6540162B1 (ja) |
EP (1) | EP1167882B1 (ja) |
JP (1) | JP4648580B2 (ja) |
DE (1) | DE60119436T2 (ja) |
ES (1) | ES2262609T3 (ja) |
IL (1) | IL143789A0 (ja) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6540162B1 (en) * | 2000-06-28 | 2003-04-01 | General Electric Company | Methods and apparatus for decreasing combustor emissions with spray bar assembly |
US7104464B2 (en) * | 2003-12-25 | 2006-09-12 | Kawasaki Jukogyo Kabushiki Kaisha | Fuel supply method and fuel supply system |
JP3840560B2 (ja) * | 2004-01-21 | 2006-11-01 | 川崎重工業株式会社 | 燃料供給方法および燃料供給装置 |
US7481059B2 (en) * | 2004-08-12 | 2009-01-27 | Volvo Aero Corporation | Method and apparatus for providing an afterburner fuel-feed arrangement |
FR2880391A1 (fr) * | 2005-01-06 | 2006-07-07 | Snecma Moteurs Sa | Diffuseur pour chambre annulaire de combustion, en particulier pour un turbomoteur d'avion |
FR2892181B1 (fr) † | 2005-10-18 | 2008-02-01 | Snecma Sa | Fixation d'une chambre de combustion a l'interieur de son carter |
JP4894295B2 (ja) * | 2006-02-28 | 2012-03-14 | 株式会社日立製作所 | 燃焼装置と燃焼装置の燃焼方法、及び燃焼装置の改造方法 |
US8596071B2 (en) * | 2006-05-05 | 2013-12-03 | General Electric Company | Method and apparatus for assembling a gas turbine engine |
EP1936276A1 (de) * | 2006-12-22 | 2008-06-25 | Siemens Aktiengesellschaft | Brenner für eine Gasturbine |
US8459034B2 (en) | 2007-05-22 | 2013-06-11 | General Electric Company | Methods and apparatus for operating gas turbine engines |
US8122725B2 (en) * | 2007-11-01 | 2012-02-28 | General Electric Company | Methods and systems for operating gas turbine engines |
US8640464B2 (en) * | 2009-02-23 | 2014-02-04 | Williams International Co., L.L.C. | Combustion system |
US8919127B2 (en) * | 2011-05-24 | 2014-12-30 | General Electric Company | System and method for flow control in gas turbine engine |
US9074773B2 (en) * | 2012-02-07 | 2015-07-07 | General Electric Company | Combustor assembly with trapped vortex cavity |
GB2524914B (en) * | 2013-01-02 | 2017-08-23 | Parker Hannifin Corp | Direct injection multipoint nozzle |
WO2014123850A1 (en) | 2013-02-06 | 2014-08-14 | United Technologies Corporation | Gas turbine engine component with upstream-directed cooling film holes |
US10174949B2 (en) | 2013-02-08 | 2019-01-08 | United Technologies Corporation | Gas turbine engine combustor liner assembly with convergent hyperbolic profile |
EP2971973B1 (en) | 2013-03-14 | 2018-02-21 | United Technologies Corporation | Combustor panel and combustor with heat shield with increased durability |
US9371998B2 (en) | 2013-05-13 | 2016-06-21 | Solar Turbines Incorporated | Shrouded pilot liquid tube |
WO2015009449A1 (en) * | 2013-07-17 | 2015-01-22 | United Technologies Corporation | Supply duct for cooling air |
RU2612449C1 (ru) * | 2016-02-09 | 2017-03-09 | Владимир Леонидович Письменный | Камера сгорания авиационного газотурбинного двигателя |
US11262073B2 (en) | 2017-05-02 | 2022-03-01 | General Electric Company | Trapped vortex combustor for a gas turbine engine with a driver airflow channel |
CN107387150A (zh) * | 2017-08-24 | 2017-11-24 | 武汉工程大学 | 多功能隧道降尘车 |
US10823422B2 (en) * | 2017-10-17 | 2020-11-03 | General Electric Company | Tangential bulk swirl air in a trapped vortex combustor for a gas turbine engine |
US11255270B2 (en) | 2018-12-18 | 2022-02-22 | Delavan Inc. | Heat shielding for internal fuel manifolds |
US11226100B2 (en) | 2019-07-22 | 2022-01-18 | Delavan Inc. | Fuel manifolds |
US11187155B2 (en) | 2019-07-22 | 2021-11-30 | Delavan Inc. | Sectional fuel manifolds |
US11117155B2 (en) * | 2019-10-04 | 2021-09-14 | Delavan Inc. | Fluid nozzles with heat shielding |
CN115127126A (zh) * | 2021-03-26 | 2022-09-30 | 中国航发商用航空发动机有限责任公司 | 环形燃烧室及分级燃油喷嘴和抑制振荡燃烧的方法 |
CN115076721B (zh) * | 2022-06-01 | 2023-04-07 | 南京航空航天大学 | 一种预蒸发驻涡值班火焰稳定器及其工作方法 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4019320A (en) * | 1975-12-05 | 1977-04-26 | United Technologies Corporation | External gas turbine engine cooling for clearance control |
US4132204A (en) * | 1976-08-30 | 1979-01-02 | Chrysler Corporation | Fuel spray bar and pressure regulator system |
US4553901A (en) * | 1983-12-21 | 1985-11-19 | United Technologies Corporation | Stator structure for a gas turbine engine |
US4798048A (en) * | 1987-12-21 | 1989-01-17 | United Technologies Corporation | Augmentor pilot |
US4901527A (en) * | 1988-02-18 | 1990-02-20 | General Electric Company | Low turbulence flame holder mount |
US4887425A (en) * | 1988-03-18 | 1989-12-19 | General Electric Company | Fuel spraybar |
EP0550126A1 (en) * | 1992-01-02 | 1993-07-07 | General Electric Company | Thrust augmentor heat shield |
FR2689567B1 (fr) * | 1992-04-01 | 1994-05-27 | Snecma | Injecteur de carburant pour chambre de post-combustion d'une turbomachine. |
US5423178A (en) * | 1992-09-28 | 1995-06-13 | Parker-Hannifin Corporation | Multiple passage cooling circuit method and device for gas turbine engine fuel nozzle |
US5385015A (en) * | 1993-07-02 | 1995-01-31 | United Technologies Corporation | Augmentor burner |
US5619855A (en) * | 1995-06-07 | 1997-04-15 | General Electric Company | High inlet mach combustor for gas turbine engine |
US6286298B1 (en) | 1998-12-18 | 2001-09-11 | General Electric Company | Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavity |
US6286317B1 (en) | 1998-12-18 | 2001-09-11 | General Electric Company | Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity |
US6540162B1 (en) * | 2000-06-28 | 2003-04-01 | General Electric Company | Methods and apparatus for decreasing combustor emissions with spray bar assembly |
-
2000
- 2000-06-28 US US09/604,985 patent/US6540162B1/en not_active Expired - Fee Related
-
2001
- 2001-06-15 IL IL14378901A patent/IL143789A0/xx not_active IP Right Cessation
- 2001-06-22 ES ES01305440T patent/ES2262609T3/es not_active Expired - Lifetime
- 2001-06-22 DE DE60119436T patent/DE60119436T2/de not_active Expired - Lifetime
- 2001-06-22 EP EP01305440A patent/EP1167882B1/en not_active Expired - Lifetime
- 2001-06-27 JP JP2001193831A patent/JP4648580B2/ja not_active Expired - Fee Related
-
2003
- 2003-02-07 US US10/361,049 patent/US6736338B2/en not_active Expired - Fee Related