JP2015090229A5 - - Google Patents
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- Publication number
- JP2015090229A5 JP2015090229A5 JP2013229514A JP2013229514A JP2015090229A5 JP 2015090229 A5 JP2015090229 A5 JP 2015090229A5 JP 2013229514 A JP2013229514 A JP 2013229514A JP 2013229514 A JP2013229514 A JP 2013229514A JP 2015090229 A5 JP2015090229 A5 JP 2015090229A5
- Authority
- JP
- Japan
- Prior art keywords
- gas turbine
- turbine combustor
- annular recess
- heat transfer
- transfer medium
- 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
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Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2013229514A JP6246562B2 (ja) | 2013-11-05 | 2013-11-05 | ガスタービン燃焼器 |
| US14/531,253 US10184662B2 (en) | 2013-11-05 | 2014-11-03 | Gas turbine combustion liner with triangular heat transfer element |
| CN201410608240.XA CN104613498B (zh) | 2013-11-05 | 2014-11-03 | 燃气轮机燃烧器 |
| EP14191424.2A EP2868971B1 (en) | 2013-11-05 | 2014-11-03 | Gas turbine combustor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2013229514A JP6246562B2 (ja) | 2013-11-05 | 2013-11-05 | ガスタービン燃焼器 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015090229A JP2015090229A (ja) | 2015-05-11 |
| JP2015090229A5 true JP2015090229A5 (OSRAM) | 2016-12-01 |
| JP6246562B2 JP6246562B2 (ja) | 2017-12-13 |
Family
ID=51842438
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013229514A Active JP6246562B2 (ja) | 2013-11-05 | 2013-11-05 | ガスタービン燃焼器 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US10184662B2 (OSRAM) |
| EP (1) | EP2868971B1 (OSRAM) |
| JP (1) | JP6246562B2 (OSRAM) |
| CN (1) | CN104613498B (OSRAM) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10337736B2 (en) * | 2015-07-24 | 2019-07-02 | Pratt & Whitney Canada Corp. | Gas turbine engine combustor and method of forming same |
| US10378444B2 (en) * | 2015-08-19 | 2019-08-13 | General Electric Company | Engine component for a gas turbine engine |
| US10260751B2 (en) | 2015-09-28 | 2019-04-16 | Pratt & Whitney Canada Corp. | Single skin combustor with heat transfer enhancement |
| US20180180289A1 (en) * | 2016-12-23 | 2018-06-28 | General Electric Company | Turbine engine assembly including a rotating detonation combustor |
| US10823414B2 (en) * | 2018-03-19 | 2020-11-03 | Raytheon Technologies Corporation | Hooded entrance to effusion holes |
| JP7132096B2 (ja) * | 2018-11-14 | 2022-09-06 | 三菱重工業株式会社 | ガスタービン燃焼器 |
| JP7550694B2 (ja) | 2021-03-26 | 2024-09-13 | 本田技研工業株式会社 | ガスタービン用燃焼器 |
Family Cites Families (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4236378A (en) | 1978-03-01 | 1980-12-02 | General Electric Company | Sectoral combustor for burning low-BTU fuel gas |
| US4242871A (en) * | 1979-09-18 | 1981-01-06 | United Technologies Corporation | Louver burner liner |
| US4380906A (en) | 1981-01-22 | 1983-04-26 | United Technologies Corporation | Combustion liner cooling scheme |
| US4622821A (en) * | 1985-01-07 | 1986-11-18 | United Technologies Corporation | Combustion liner for a gas turbine engine |
| US4875339A (en) * | 1987-11-27 | 1989-10-24 | General Electric Company | Combustion chamber liner insert |
| US4916906A (en) * | 1988-03-25 | 1990-04-17 | General Electric Company | Breach-cooled structure |
| US5361828A (en) * | 1993-02-17 | 1994-11-08 | General Electric Company | Scaled heat transfer surface with protruding ramp surface turbulators |
| JPH08254316A (ja) * | 1995-03-16 | 1996-10-01 | Toshiba Corp | ガスタービン燃焼器用ライナおよびその製造方法 |
| WO1999014532A1 (en) | 1997-09-12 | 1999-03-25 | Hitachi, Ltd. | Gas turbine combustor and its liner structure |
| US6145319A (en) * | 1998-07-16 | 2000-11-14 | General Electric Company | Transitional multihole combustion liner |
| JP3967521B2 (ja) | 2000-03-30 | 2007-08-29 | 株式会社日立製作所 | 伝熱装置及びその製造方法並びに伝熱装置を備えたガスタービン燃焼器 |
| US6568079B2 (en) * | 2001-06-11 | 2003-05-27 | General Electric Company | Methods for replacing combustor liner panels |
| US6735949B1 (en) * | 2002-06-11 | 2004-05-18 | General Electric Company | Gas turbine engine combustor can with trapped vortex cavity |
| US7007481B2 (en) * | 2003-09-10 | 2006-03-07 | General Electric Company | Thick coated combustor liner |
| US8397510B2 (en) * | 2003-12-16 | 2013-03-19 | Hitachi, Ltd. | Combustor for gas turbine |
| DE102006026969A1 (de) * | 2006-06-09 | 2007-12-13 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenbrennkammerwand für eine mager-brennende Gasturbinenbrennkammer |
| EP2107314A1 (en) * | 2008-04-01 | 2009-10-07 | Siemens Aktiengesellschaft | Combustor for a gas turbine |
| US20120047895A1 (en) * | 2010-08-26 | 2012-03-01 | General Electric Company | Systems and apparatus relating to combustor cooling and operation in gas turbine engines |
| JP5579011B2 (ja) * | 2010-10-05 | 2014-08-27 | 株式会社日立製作所 | ガスタービン燃焼器 |
| US8365534B2 (en) * | 2011-03-15 | 2013-02-05 | General Electric Company | Gas turbine combustor having a fuel nozzle for flame anchoring |
| US8931280B2 (en) * | 2011-04-26 | 2015-01-13 | General Electric Company | Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities |
| JP5438727B2 (ja) * | 2011-07-27 | 2014-03-12 | 株式会社日立製作所 | 燃焼器、バーナ及びガスタービン |
| GB201114745D0 (en) * | 2011-08-26 | 2011-10-12 | Rolls Royce Plc | Wall elements for gas turbine engines |
| US20130074507A1 (en) * | 2011-09-28 | 2013-03-28 | Karthick Kaleeswaran | Combustion liner for a turbine engine |
| JP6066065B2 (ja) | 2013-02-20 | 2017-01-25 | 三菱日立パワーシステムズ株式会社 | 伝熱装置を備えたガスタービン燃焼器 |
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2013
- 2013-11-05 JP JP2013229514A patent/JP6246562B2/ja active Active
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2014
- 2014-11-03 CN CN201410608240.XA patent/CN104613498B/zh active Active
- 2014-11-03 US US14/531,253 patent/US10184662B2/en active Active
- 2014-11-03 EP EP14191424.2A patent/EP2868971B1/en active Active