JP2013250046A5 - - Google Patents
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- Publication number
- JP2013250046A5 JP2013250046A5 JP2013109446A JP2013109446A JP2013250046A5 JP 2013250046 A5 JP2013250046 A5 JP 2013250046A5 JP 2013109446 A JP2013109446 A JP 2013109446A JP 2013109446 A JP2013109446 A JP 2013109446A JP 2013250046 A5 JP2013250046 A5 JP 2013250046A5
- Authority
- JP
- Japan
- Prior art keywords
- plenum
- rear plate
- assembly
- fuel
- outer diameter
- 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 26
- 239000012809 cooling fluid Substances 0.000 claims 14
- 238000002347 injection Methods 0.000 claims 13
- 239000007924 injection Substances 0.000 claims 13
- 239000012530 fluid Substances 0.000 claims 11
- 238000002485 combustion reaction Methods 0.000 claims 8
- 230000000712 assembly Effects 0.000 claims 7
- 238000000429 assembly Methods 0.000 claims 7
- 238000001816 cooling Methods 0.000 claims 2
- 238000011144 upstream manufacturing Methods 0.000 claims 2
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/483,153 | 2012-05-30 | ||
| US13/483,153 US9212822B2 (en) | 2012-05-30 | 2012-05-30 | Fuel injection assembly for use in turbine engines and method of assembling same |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2013250046A JP2013250046A (ja) | 2013-12-12 |
| JP2013250046A5 true JP2013250046A5 (enExample) | 2016-07-07 |
| JP6138584B2 JP6138584B2 (ja) | 2017-05-31 |
Family
ID=48537822
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013109446A Active JP6138584B2 (ja) | 2012-05-30 | 2013-05-24 | タービンエンジンに使用するための燃料注入組立体及びそれを組み立てる方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9212822B2 (enExample) |
| EP (1) | EP2669580B1 (enExample) |
| JP (1) | JP6138584B2 (enExample) |
| CN (1) | CN103453554B (enExample) |
| RU (1) | RU2632073C2 (enExample) |
Families Citing this family (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9476592B2 (en) * | 2013-09-19 | 2016-10-25 | General Electric Company | System for injecting fuel in a gas turbine combustor |
| WO2015176887A1 (de) * | 2014-05-19 | 2015-11-26 | Siemens Aktiengesellschaft | Brenneranordnung mit resonator |
| CN106461211B (zh) * | 2014-05-30 | 2019-03-22 | 川崎重工业株式会社 | 燃气涡轮发动机的燃烧装置 |
| EP3150918B1 (en) * | 2014-05-30 | 2019-12-18 | Kawasaki Jukogyo Kabushiki Kaisha | Combustion device for gas turbine engine |
| US10101032B2 (en) * | 2015-04-01 | 2018-10-16 | General Electric Company | Micromixer system for a turbine system and an associated method thereof |
| US10670271B2 (en) * | 2016-09-30 | 2020-06-02 | DOOSAN Heavy Industries Construction Co., LTD | Acoustic dampening liner cap and gas turbine combustor including the same |
| US10344982B2 (en) | 2016-12-30 | 2019-07-09 | General Electric Company | Compact multi-residence time bundled tube fuel nozzle having transition portions of different lengths |
| JP6822894B2 (ja) * | 2017-04-28 | 2021-01-27 | 三菱パワー株式会社 | 燃料噴射器及びガスタービン |
| JP6979343B2 (ja) * | 2017-11-30 | 2021-12-15 | 三菱パワー株式会社 | 燃料噴射器、燃焼器、及びガスタービン |
| US10890329B2 (en) | 2018-03-01 | 2021-01-12 | General Electric Company | Fuel injector assembly for gas turbine engine |
| US10935245B2 (en) | 2018-11-20 | 2021-03-02 | General Electric Company | Annular concentric fuel nozzle assembly with annular depression and radial inlet ports |
| US10948188B2 (en) * | 2018-12-12 | 2021-03-16 | Solar Turbines Incorporated | Fuel injector with perforated plate |
| US11073114B2 (en) | 2018-12-12 | 2021-07-27 | General Electric Company | Fuel injector assembly for a heat engine |
| US11286884B2 (en) | 2018-12-12 | 2022-03-29 | General Electric Company | Combustion section and fuel injector assembly for a heat engine |
| US11156360B2 (en) | 2019-02-18 | 2021-10-26 | General Electric Company | Fuel nozzle assembly |
| KR102460001B1 (ko) * | 2021-02-17 | 2022-10-26 | 두산에너빌리티 주식회사 | 마이크로 믹서모듈 및 이를 포함하는 연소기 |
| KR20240145968A (ko) * | 2021-11-03 | 2024-10-07 | 파워 시스템즈 엠에프지., 엘엘씨 | 가스 터빈 엔진용의 분할 공기류를 갖는 멀티튜브 파일럿 분사기 |
| CN114234232B (zh) * | 2021-12-24 | 2023-05-02 | 中国科学院工程热物理研究所 | 微预混直喷燃烧室 |
| US12215866B2 (en) | 2022-02-18 | 2025-02-04 | General Electric Company | Combustor for a turbine engine having a fuel-air mixer including a set of mixing passages |
| US12379108B2 (en) | 2023-01-06 | 2025-08-05 | Ge Vernova Infrastructure Technology Llc | Method of operating gas turbine combustor with multiple fuel stages |
| US20240230094A1 (en) * | 2023-01-06 | 2024-07-11 | Ge Infrastructure Technology Llc | Combustor head end section with integrated cooling system |
| KR102863421B1 (ko) * | 2023-12-15 | 2025-09-22 | 두산에너빌리티 주식회사 | 연소기용 노즐, 연소기, 및 이를 포함하는 가스 터빈 |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4100733A (en) * | 1976-10-04 | 1978-07-18 | United Technologies Corporation | Premix combustor |
| US5274991A (en) * | 1992-03-30 | 1994-01-04 | General Electric Company | Dry low NOx multi-nozzle combustion liner cap assembly |
| US5372008A (en) * | 1992-11-10 | 1994-12-13 | Solar Turbines Incorporated | Lean premix combustor system |
| FR2756593B1 (fr) * | 1996-12-03 | 1999-01-22 | Aerospatiale | Mat d'injection de combustible pour un statoreacteur fonctionnant sur une large plage de nombre de mach |
| US6358040B1 (en) | 2000-03-17 | 2002-03-19 | Precision Combustion, Inc. | Method and apparatus for a fuel-rich catalytic reactor |
| US6915636B2 (en) * | 2002-07-15 | 2005-07-12 | Power Systems Mfg., Llc | Dual fuel fin mixer secondary fuel nozzle |
| US7617682B2 (en) | 2002-12-13 | 2009-11-17 | Siemens Energy, Inc. | Catalytic oxidation element for a gas turbine engine |
| FR2911667B1 (fr) * | 2007-01-23 | 2009-10-02 | Snecma Sa | Systeme d'injection de carburant a double injecteur. |
| US8438853B2 (en) * | 2008-01-29 | 2013-05-14 | Alstom Technology Ltd. | Combustor end cap assembly |
| US20090223227A1 (en) | 2008-03-05 | 2009-09-10 | General Electric Company | Combustion cap with crown mixing holes |
| US8806871B2 (en) * | 2008-04-11 | 2014-08-19 | General Electric Company | Fuel nozzle |
| US8147121B2 (en) | 2008-07-09 | 2012-04-03 | General Electric Company | Pre-mixing apparatus for a turbine engine |
| US8327642B2 (en) | 2008-10-21 | 2012-12-11 | General Electric Company | Multiple tube premixing device |
| US20100180564A1 (en) | 2009-01-21 | 2010-07-22 | General Electric Company | Systems and Methods for Mitigating a Flashback Condition in a Premixed Combustor |
| US9140454B2 (en) | 2009-01-23 | 2015-09-22 | General Electric Company | Bundled multi-tube nozzle for a turbomachine |
| US8539773B2 (en) | 2009-02-04 | 2013-09-24 | General Electric Company | Premixed direct injection nozzle for highly reactive fuels |
| US8424311B2 (en) | 2009-02-27 | 2013-04-23 | General Electric Company | Premixed direct injection disk |
| US8522555B2 (en) | 2009-05-20 | 2013-09-03 | General Electric Company | Multi-premixer fuel nozzle support system |
| US8789372B2 (en) * | 2009-07-08 | 2014-07-29 | General Electric Company | Injector with integrated resonator |
| US20110005189A1 (en) | 2009-07-08 | 2011-01-13 | General Electric Company | Active Control of Flame Holding and Flashback in Turbine Combustor Fuel Nozzle |
| US8276385B2 (en) * | 2009-10-08 | 2012-10-02 | General Electric Company | Staged multi-tube premixing injector |
| US20110225947A1 (en) * | 2010-03-17 | 2011-09-22 | Benjamin Paul Lacy | System and methods for altering air flow in a combustor |
| US20120058437A1 (en) * | 2010-09-08 | 2012-03-08 | General Electric Company | Apparatus and method for mixing fuel in a gas turbine nozzle |
| US20120055163A1 (en) * | 2010-09-08 | 2012-03-08 | Jong Ho Uhm | Fuel injection assembly for use in turbine engines and method of assembling same |
| US8943832B2 (en) * | 2011-10-26 | 2015-02-03 | General Electric Company | Fuel nozzle assembly for use in turbine engines and methods of assembling same |
| US8438851B1 (en) * | 2012-01-03 | 2013-05-14 | General Electric Company | Combustor assembly for use in a turbine engine and methods of assembling same |
-
2012
- 2012-05-30 US US13/483,153 patent/US9212822B2/en active Active
-
2013
- 2013-05-24 JP JP2013109446A patent/JP6138584B2/ja active Active
- 2013-05-29 EP EP13169670.0A patent/EP2669580B1/en active Active
- 2013-05-29 RU RU2013124953A patent/RU2632073C2/ru active
- 2013-05-30 CN CN201310208723.6A patent/CN103453554B/zh active Active
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