JP2013213655A5 - - Google Patents
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- Publication number
- JP2013213655A5 JP2013213655A5 JP2013013820A JP2013013820A JP2013213655A5 JP 2013213655 A5 JP2013213655 A5 JP 2013213655A5 JP 2013013820 A JP2013013820 A JP 2013013820A JP 2013013820 A JP2013013820 A JP 2013013820A JP 2013213655 A5 JP2013213655 A5 JP 2013213655A5
- Authority
- JP
- Japan
- Prior art keywords
- combustor
- elliptical
- cross
- head end
- disposed
- 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
Links
- 239000000446 fuel Substances 0.000 claims 10
- 230000007704 transition Effects 0.000 claims 7
- 230000013011 mating Effects 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/437,954 US9145778B2 (en) | 2012-04-03 | 2012-04-03 | Combustor with non-circular head end |
| US13/437,954 | 2012-04-03 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2013213655A JP2013213655A (ja) | 2013-10-17 |
| JP2013213655A5 true JP2013213655A5 (enExample) | 2016-03-10 |
| JP6196449B2 JP6196449B2 (ja) | 2017-09-13 |
Family
ID=47631328
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013013820A Expired - Fee Related JP6196449B2 (ja) | 2012-04-03 | 2013-01-29 | 非円形ヘッドエンドを有する燃焼器 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9145778B2 (enExample) |
| EP (1) | EP2647799B1 (enExample) |
| JP (1) | JP6196449B2 (enExample) |
| CN (1) | CN103363545B (enExample) |
| RU (1) | RU2013104201A (enExample) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9546601B2 (en) * | 2012-11-20 | 2017-01-17 | General Electric Company | Clocked combustor can array |
| CN105373419A (zh) | 2014-08-26 | 2016-03-02 | 阿里巴巴集团控股有限公司 | 一种后台应用的操作方法及装置 |
| GB2533293A (en) * | 2014-12-15 | 2016-06-22 | Edwards Ltd | Inlet assembly |
| US20190315461A1 (en) * | 2018-04-15 | 2019-10-17 | Vaughan Lennox Clift | Rotary-winged vehicle systems and devices |
| CN109099461B (zh) * | 2018-08-03 | 2023-08-15 | 新奥能源动力科技(上海)有限公司 | 燃烧室的头部装置、燃烧室及燃气轮机 |
| CN109185923B (zh) * | 2018-08-03 | 2023-09-12 | 新奥能源动力科技(上海)有限公司 | 一种燃烧室头部装置、燃烧室及燃气轮机 |
| CN109185924B (zh) * | 2018-08-03 | 2023-09-12 | 新奥能源动力科技(上海)有限公司 | 燃烧室的头部装置、燃烧室及燃气轮机 |
Family Cites Families (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE768019C (de) | 1939-05-26 | 1955-05-12 | Messerschmitt Boelkow Blohm | Mit Gleichdruckverbrennung arbeitende Brennkraftturbine, insbesondere fuer Strahltriebwerke |
| US2676460A (en) * | 1950-03-23 | 1954-04-27 | United Aircraft Corp | Burner construction of the can-an-nular type having means for distributing airflow to each can |
| NL95825C (enExample) * | 1950-11-17 | |||
| GB719379A (en) * | 1950-11-17 | 1954-12-01 | Power Jets Res & Dev Ltd | Improvements in combustion apparatus |
| DE1223622B (de) | 1962-05-31 | 1966-08-25 | Bristol Siddeley Engines Ltd | Vorrichtung zur Entnahme von Luft aus der Verbrennungsanlage eines Gasturbinen-triebwerkes |
| JPS5546309A (en) * | 1978-09-27 | 1980-04-01 | Hitachi Ltd | Burner for gas turbine |
| US4719748A (en) * | 1985-05-14 | 1988-01-19 | General Electric Company | Impingement cooled transition duct |
| USH1008H (en) * | 1985-05-28 | 1992-01-07 | The United States Of America As Represented By The Secretary Of The Navy | Dump combustor with noncoherent flow |
| FR2698157B1 (fr) | 1992-11-18 | 1994-12-16 | Snecma | Système d'injection aérodynamique de chambre de combustion. |
| US6442946B1 (en) * | 2000-11-14 | 2002-09-03 | Power Systems Mfg., Llc | Three degrees of freedom aft mounting system for gas turbine transition duct |
| EP1426558A3 (en) * | 2002-11-22 | 2005-02-09 | General Electric Company | Gas turbine transition piece with dimpled surface and cooling method for such a transition piece |
| US7007486B2 (en) * | 2003-03-26 | 2006-03-07 | The Boeing Company | Apparatus and method for selecting a flow mixture |
| JP2004317008A (ja) * | 2003-04-15 | 2004-11-11 | Toshiba Corp | ガスタービン燃焼器 |
| US7111463B2 (en) * | 2004-01-23 | 2006-09-26 | Pratt & Whitney Rocketdyne Inc. | Combustion wave ignition for combustors |
| US7082766B1 (en) * | 2005-03-02 | 2006-08-01 | General Electric Company | One-piece can combustor |
| US7721547B2 (en) * | 2005-06-27 | 2010-05-25 | Siemens Energy, Inc. | Combustion transition duct providing stage 1 tangential turning for turbine engines |
| FR2897143B1 (fr) * | 2006-02-08 | 2012-10-05 | Snecma | Chambre de combustion d'une turbomachine |
| JP4959620B2 (ja) * | 2007-04-26 | 2012-06-27 | 株式会社日立製作所 | 燃焼器及び燃焼器の燃料供給方法 |
| JP5276345B2 (ja) * | 2008-03-28 | 2013-08-28 | 三菱重工業株式会社 | ガスタービン及びガスタービンの燃焼器挿入孔形成方法 |
| JP5010521B2 (ja) * | 2008-03-28 | 2012-08-29 | 三菱重工業株式会社 | 燃焼器尾筒案内治具及びガスタービンの燃焼器の取り外し方法、並びに製造方法 |
| JP5173720B2 (ja) * | 2008-10-01 | 2013-04-03 | 三菱重工業株式会社 | 燃焼器接続構造およびガスタービン |
| US9822649B2 (en) * | 2008-11-12 | 2017-11-21 | General Electric Company | Integrated combustor and stage 1 nozzle in a gas turbine and method |
| US20100170257A1 (en) | 2009-01-08 | 2010-07-08 | General Electric Company | Cooling a one-piece can combustor and related method |
| US20100205972A1 (en) | 2009-02-17 | 2010-08-19 | General Electric Company | One-piece can combustor with heat transfer surface enhacements |
| US8438856B2 (en) | 2009-03-02 | 2013-05-14 | General Electric Company | Effusion cooled one-piece can combustor |
| JP4934696B2 (ja) * | 2009-03-26 | 2012-05-16 | 株式会社日立製作所 | バーナ及び燃焼器 |
| US20100257863A1 (en) | 2009-04-13 | 2010-10-14 | General Electric Company | Combined convection/effusion cooled one-piece can combustor |
| US20110067377A1 (en) * | 2009-09-18 | 2011-03-24 | General Electric Company | Gas turbine combustion dynamics control system |
| US8590314B2 (en) | 2010-04-09 | 2013-11-26 | General Electric Company | Combustor liner helical cooling apparatus |
| US20110259015A1 (en) * | 2010-04-27 | 2011-10-27 | David Richard Johns | Tangential Combustor |
| US8613197B2 (en) * | 2010-08-05 | 2013-12-24 | General Electric Company | Turbine combustor with fuel nozzles having inner and outer fuel circuits |
| US9546601B2 (en) * | 2012-11-20 | 2017-01-17 | General Electric Company | Clocked combustor can array |
-
2012
- 2012-04-03 US US13/437,954 patent/US9145778B2/en not_active Expired - Fee Related
-
2013
- 2013-01-28 EP EP13152858.0A patent/EP2647799B1/en not_active Not-in-force
- 2013-01-29 JP JP2013013820A patent/JP6196449B2/ja not_active Expired - Fee Related
- 2013-02-01 CN CN201310042483.7A patent/CN103363545B/zh not_active Expired - Fee Related
- 2013-02-01 RU RU2013104201/06A patent/RU2013104201A/ru not_active Application Discontinuation
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