JP2004325069A5 - - Google Patents
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- Publication number
- JP2004325069A5 JP2004325069A5 JP2004130561A JP2004130561A JP2004325069A5 JP 2004325069 A5 JP2004325069 A5 JP 2004325069A5 JP 2004130561 A JP2004130561 A JP 2004130561A JP 2004130561 A JP2004130561 A JP 2004130561A JP 2004325069 A5 JP2004325069 A5 JP 2004325069A5
- 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.)
- Pending
Links
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/424,440 US7052231B2 (en) | 2003-04-28 | 2003-04-28 | Methods and apparatus for injecting fluids in gas turbine engines |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2004325069A JP2004325069A (ja) | 2004-11-18 |
| JP2004325069A5 true JP2004325069A5 (enExample) | 2007-06-14 |
Family
ID=32990347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004130561A Pending JP2004325069A (ja) | 2003-04-28 | 2004-04-27 | ガスタービンエンジンにおいて流体を噴射するための方法及び装置 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7052231B2 (enExample) |
| EP (1) | EP1473518A3 (enExample) |
| JP (1) | JP2004325069A (enExample) |
| CN (1) | CN100507236C (enExample) |
Families Citing this family (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102008015207A1 (de) * | 2008-03-20 | 2009-09-24 | Rolls-Royce Deutschland Ltd & Co Kg | Fluid-Injektor-Düse |
| DE102008017844A1 (de) * | 2008-04-08 | 2009-10-15 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsmaschine mit Fluid-Injektorbaugruppe |
| DE102010027587A1 (de) | 2010-07-19 | 2012-01-19 | Rolls-Royce Deutschland Ltd & Co Kg | Zapfluftauslass im Nebenstromkanal eines Turbofantriebwerks |
| WO2013028163A1 (en) * | 2011-08-22 | 2013-02-28 | Majed Toqan | Tangential and flameless annular combustor for use on gas turbine engines |
| JP6110854B2 (ja) * | 2011-08-22 | 2017-04-05 | トクァン, マジェドTOQAN, Majed | ガス・タービン・エンジンで使用するための予混合燃料空気を用いた接線方向環状燃焼器 |
| WO2013028169A1 (en) * | 2011-08-22 | 2013-02-28 | Majed Toqan | Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines |
| WO2013028167A2 (en) * | 2011-08-22 | 2013-02-28 | Majed Toqan | Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines |
| US9377201B2 (en) | 2013-02-08 | 2016-06-28 | Solar Turbines Incorporated | Forged fuel injector stem |
| EP3076084B1 (en) * | 2015-03-30 | 2021-04-28 | Ansaldo Energia Switzerland AG | Fuel injector device |
| US10329941B2 (en) * | 2016-05-06 | 2019-06-25 | United Technologies Corporation | Impingement manifold |
| DE102017125051A1 (de) * | 2017-10-26 | 2019-05-02 | Man Diesel & Turbo Se | Strömungsmaschine |
| US11085641B2 (en) * | 2018-11-27 | 2021-08-10 | Honeywell International Inc. | Plug resistant effusion holes for gas turbine engine |
| US11021963B2 (en) * | 2019-05-03 | 2021-06-01 | Raytheon Technologies Corporation | Monolithic body including an internal passage with a generally teardrop shaped cross-sectional geometry |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1350471A (en) * | 1971-05-06 | 1974-04-18 | Secr Defence | Gas turbine engine |
| US4966001A (en) * | 1987-10-23 | 1990-10-30 | General Electric Company | Multiple venturi tube gas fuel injector for catalytic combustor |
| US5001895A (en) * | 1987-12-14 | 1991-03-26 | Sundstrand Corporation | Fuel injector for turbine engines |
| US4891936A (en) * | 1987-12-28 | 1990-01-09 | Sundstrand Corporation | Turbine combustor with tangential fuel injection and bender jets |
| CA2014999C (en) * | 1989-04-24 | 1999-09-07 | Kenneth William Bates | Gas injector |
| DE69305326T2 (de) * | 1992-02-10 | 1997-05-07 | United Technologies Corp | Ejektor für kühlfluid |
| US5402636A (en) * | 1993-12-06 | 1995-04-04 | United Technologies Corporation | Anti-contamination thrust balancing system for gas turbine engines |
| US5727378A (en) * | 1995-08-25 | 1998-03-17 | Great Lakes Helicopters Inc. | Gas turbine engine |
| US5759012A (en) * | 1996-12-13 | 1998-06-02 | Caterpillar Inc. | Turbine disc ingress prevention method and apparatus |
| JPH11132002A (ja) * | 1997-10-28 | 1999-05-18 | Mitsubishi Heavy Ind Ltd | 流量調整プラグ |
| US5988531A (en) * | 1997-11-25 | 1999-11-23 | Solar Turbines | Method of making a fuel injector |
| TW513833B (en) * | 1998-09-09 | 2002-12-11 | Honda Motor Co Ltd | Mounting method of sparking plug cap and sparking plug cap |
| US6224329B1 (en) * | 1999-01-07 | 2001-05-01 | Siemens Westinghouse Power Corporation | Method of cooling a combustion turbine |
| US6234746B1 (en) * | 1999-08-04 | 2001-05-22 | General Electric Co. | Apparatus and methods for cooling rotary components in a turbine |
| US6227798B1 (en) * | 1999-11-30 | 2001-05-08 | General Electric Company | Turbine nozzle segment band cooling |
| US6435816B1 (en) * | 2000-11-03 | 2002-08-20 | General Electric Co. | Gas injector system and its fabrication |
| US6431820B1 (en) * | 2001-02-28 | 2002-08-13 | General Electric Company | Methods and apparatus for cooling gas turbine engine blade tips |
-
2003
- 2003-04-28 US US10/424,440 patent/US7052231B2/en not_active Expired - Fee Related
-
2004
- 2004-04-27 JP JP2004130561A patent/JP2004325069A/ja active Pending
- 2004-04-27 EP EP04252426A patent/EP1473518A3/en not_active Withdrawn
- 2004-04-28 CN CNB2004100367002A patent/CN100507236C/zh not_active Expired - Fee Related