JP6134580B2 - モノリシックノズル部品を含むターボ機械燃焼器ノズル及びその形成方法 - Google Patents
モノリシックノズル部品を含むターボ機械燃焼器ノズル及びその形成方法 Download PDFInfo
- Publication number
- JP6134580B2 JP6134580B2 JP2013109447A JP2013109447A JP6134580B2 JP 6134580 B2 JP6134580 B2 JP 6134580B2 JP 2013109447 A JP2013109447 A JP 2013109447A JP 2013109447 A JP2013109447 A JP 2013109447A JP 6134580 B2 JP6134580 B2 JP 6134580B2
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- plate member
- elements
- plate
- forming
- 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.)
- Active
Links
- 238000000034 method Methods 0.000 title claims description 16
- 239000012530 fluid Substances 0.000 claims description 50
- 230000003750 conditioning effect Effects 0.000 claims description 10
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- 230000001105 regulatory effect Effects 0.000 claims description 3
- 238000005266 casting Methods 0.000 claims description 2
- 238000003466 welding Methods 0.000 claims 1
- 239000007789 gas Substances 0.000 description 12
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 11
- 238000002485 combustion reaction Methods 0.000 description 10
- 239000000446 fuel Substances 0.000 description 9
- 230000008569 process Effects 0.000 description 5
- 239000011324 bead Substances 0.000 description 4
- 230000007704 transition Effects 0.000 description 4
- 239000000567 combustion gas Substances 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000009760 electrical discharge machining Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 238000000149 argon plasma sintering Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00017—Assembling combustion chamber liners or subparts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00018—Manufacturing combustion chamber liners or subparts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
- Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Nozzles (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/482,540 | 2012-05-29 | ||
| US13/482,540 US9267690B2 (en) | 2012-05-29 | 2012-05-29 | Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2013245936A JP2013245936A (ja) | 2013-12-09 |
| JP2013245936A5 JP2013245936A5 (enExample) | 2016-07-07 |
| JP6134580B2 true JP6134580B2 (ja) | 2017-05-24 |
Family
ID=48470864
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2013109447A Active JP6134580B2 (ja) | 2012-05-29 | 2013-05-24 | モノリシックノズル部品を含むターボ機械燃焼器ノズル及びその形成方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9267690B2 (enExample) |
| EP (1) | EP2669579B1 (enExample) |
| JP (1) | JP6134580B2 (enExample) |
| CN (1) | CN103453553B (enExample) |
| RU (1) | RU2013124126A (enExample) |
Families Citing this family (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9140454B2 (en) | 2009-01-23 | 2015-09-22 | General Electric Company | Bundled multi-tube nozzle for a turbomachine |
| US8984888B2 (en) * | 2011-10-26 | 2015-03-24 | General Electric Company | Fuel injection assembly for use in turbine engines and method of assembling same |
| US20130318976A1 (en) * | 2012-05-29 | 2013-12-05 | General Electric Company | Turbomachine combustor nozzle and method of forming the same |
| US9574533B2 (en) * | 2013-06-13 | 2017-02-21 | General Electric Company | Fuel injection nozzle and method of manufacturing the same |
| EP2823952A1 (de) * | 2013-07-09 | 2015-01-14 | Siemens Aktiengesellschaft | Anpassungsverfahren und Herstellverfahren für mittels SLM gefertigte Bauteile |
| US9528703B2 (en) * | 2013-09-20 | 2016-12-27 | General Electric Company | Micro-mixer fuel plenum and methods for fuel tube installation |
| EP3097334B1 (en) | 2014-01-24 | 2018-08-22 | United Technologies Corporation | Fuel fitting |
| US9551490B2 (en) | 2014-04-08 | 2017-01-24 | General Electric Company | System for cooling a fuel injector extending into a combustion gas flow field and method for manufacture |
| US9528705B2 (en) | 2014-04-08 | 2016-12-27 | General Electric Company | Trapped vortex fuel injector and method for manufacture |
| CA2950558C (en) | 2014-05-30 | 2020-10-20 | Kawasaki Jukogyo Kabushiki Kaisha | Combustor for gas turbine engine |
| JP6301774B2 (ja) * | 2014-08-01 | 2018-03-28 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器 |
| US10670272B2 (en) * | 2014-12-11 | 2020-06-02 | Raytheon Technologies Corporation | Fuel injector guide(s) for a turbine engine combustor |
| US20160230993A1 (en) * | 2015-02-10 | 2016-08-11 | United Technologies Corporation | Combustor liner effusion cooling holes |
| US10480787B2 (en) | 2015-03-26 | 2019-11-19 | United Technologies Corporation | Combustor wall cooling channel formed by additive manufacturing |
| JP6423760B2 (ja) * | 2015-06-24 | 2018-11-14 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器の燃料ノズル構造 |
| CN107923618B (zh) * | 2015-06-30 | 2021-02-26 | 安萨尔多能源英国知识产权有限公司 | 燃气轮机燃料构件 |
| US20170350321A1 (en) * | 2016-06-02 | 2017-12-07 | General Electric Company | Bundled Tube Fuel Nozzle Assembly with Tube Extensions |
| JP6633982B2 (ja) * | 2016-07-01 | 2020-01-22 | 三菱日立パワーシステムズ株式会社 | ガスタービン燃焼器、ガスタービン燃焼器の燃料ノズルの製造方法 |
| JP6863718B2 (ja) * | 2016-11-21 | 2021-04-21 | 三菱パワー株式会社 | ガスタービン燃焼器 |
| EP3444441B1 (en) | 2017-08-14 | 2020-04-08 | General Electric Company | Gas turbine engine with inlet frame |
| US11525578B2 (en) * | 2017-08-16 | 2022-12-13 | General Electric Company | Dynamics-mitigating adapter for bundled tube fuel nozzle |
| JP7489759B2 (ja) * | 2018-11-20 | 2024-05-24 | 三菱重工業株式会社 | 燃焼器及びガスタービン |
| US11060460B1 (en) | 2019-04-01 | 2021-07-13 | Marine Turbine Technologies, LLC | Fuel distribution system for gas turbine engine |
| US11486578B2 (en) | 2020-05-26 | 2022-11-01 | Raytheon Technologies Corporation | Multi-walled structure for a gas turbine engine |
| KR102583226B1 (ko) | 2022-02-07 | 2023-09-25 | 두산에너빌리티 주식회사 | 다단 연료 공급부가 구비된 마이크로 믹서 및 이를 포함하는 가스 터빈 |
Family Cites Families (103)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1355887A (en) | 1972-04-14 | 1974-06-05 | Macmanus J | Decorating head |
| US4100733A (en) * | 1976-10-04 | 1978-07-18 | United Technologies Corporation | Premix combustor |
| US4262482A (en) | 1977-11-17 | 1981-04-21 | Roffe Gerald A | Apparatus for the premixed gas phase combustion of liquid fuels |
| US4378744A (en) | 1979-08-01 | 1983-04-05 | Curtiss-Wright Corporation | Fluidized bed combustor and removable windbox and tube assembly therefor |
| DE2950535A1 (de) * | 1979-11-23 | 1981-06-11 | BBC AG Brown, Boveri & Cie., Baden, Aargau | Brennkammer einer gasturbine mit vormisch/vorverdampf-elementen |
| US4429527A (en) | 1981-06-19 | 1984-02-07 | Teets J Michael | Turbine engine with combustor premix system |
| GB2118710B (en) * | 1981-12-31 | 1985-05-22 | Secr Defence | Improvements in or relating to combustion chamber wall cooling |
| US4490171A (en) | 1982-03-31 | 1984-12-25 | Kobe Steel, Limited | Method and apparatus for injecting pulverized fuel into a blast furnace |
| DE3361535D1 (en) | 1982-05-28 | 1986-01-30 | Bbc Brown Boveri & Cie | Gas turbine combustion chamber and method of operating it |
| DE3663847D1 (en) | 1985-06-07 | 1989-07-13 | Ruston Gas Turbines Ltd | Combustor for gas turbine engine |
| US5193346A (en) | 1986-11-25 | 1993-03-16 | General Electric Company | Premixed secondary fuel nozzle with integral swirler |
| GB8720611D0 (en) * | 1987-09-02 | 1987-10-07 | Philips Electronic Associated | Gas chromatography apparatus |
| US5339635A (en) | 1987-09-04 | 1994-08-23 | Hitachi, Ltd. | Gas turbine combustor of the completely premixed combustion type |
| US4845952A (en) | 1987-10-23 | 1989-07-11 | General Electric Company | Multiple venturi tube gas fuel injector for catalytic combustor |
| US5000004A (en) | 1988-08-16 | 1991-03-19 | Kabushiki Kaisha Toshiba | Gas turbine combustor |
| US4986068A (en) | 1988-09-16 | 1991-01-22 | General Electric Company | Hypersonic scramjet engine fuel injector |
| US5277022A (en) | 1990-06-22 | 1994-01-11 | Sundstrand Corporation | Air blast fuel injecton system |
| DE4110507C2 (de) | 1991-03-30 | 1994-04-07 | Mtu Muenchen Gmbh | Brenner für Gasturbinentriebwerke mit mindestens einer für die Zufuhr von Verbrennungsluft lastabhängig regulierbaren Dralleinrichtung |
| US5199265A (en) | 1991-04-03 | 1993-04-06 | General Electric Company | Two stage (premixed/diffusion) gas only secondary fuel nozzle |
| US5235814A (en) | 1991-08-01 | 1993-08-17 | General Electric Company | Flashback resistant fuel staged premixed combustor |
| US5263325A (en) | 1991-12-16 | 1993-11-23 | United Technologies Corporation | Low NOx combustion |
| US5247797A (en) | 1991-12-23 | 1993-09-28 | General Electric Company | Head start partial premixing for reducing oxides of nitrogen emissions in gas turbine combustors |
| US5259184A (en) | 1992-03-30 | 1993-11-09 | General Electric Company | Dry low NOx single stage dual mode combustor construction for a gas turbine |
| US5321951A (en) | 1992-03-30 | 1994-06-21 | General Electric Company | Integral combustor splash plate and sleeve |
| US5487275A (en) | 1992-12-11 | 1996-01-30 | General Electric Co. | Tertiary fuel injection system for use in a dry low NOx combustion system |
| US5400968A (en) | 1993-08-16 | 1995-03-28 | Solar Turbines Incorporated | Injector tip cooling using fuel as the coolant |
| GB9325708D0 (en) | 1993-12-16 | 1994-02-16 | Rolls Royce Plc | A gas turbine engine combustion chamber |
| US5512250A (en) | 1994-03-02 | 1996-04-30 | Catalytica, Inc. | Catalyst structure employing integral heat exchange |
| US5590529A (en) | 1994-09-26 | 1997-01-07 | General Electric Company | Air fuel mixer for gas turbine combustor |
| US5943866A (en) | 1994-10-03 | 1999-08-31 | General Electric Company | Dynamically uncoupled low NOx combustor having multiple premixers with axial staging |
| US5657632A (en) | 1994-11-10 | 1997-08-19 | Westinghouse Electric Corporation | Dual fuel gas turbine combustor |
| JPH08270950A (ja) | 1995-02-01 | 1996-10-18 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器 |
| US5881756A (en) | 1995-12-22 | 1999-03-16 | Institute Of Gas Technology | Process and apparatus for homogeneous mixing of gaseous fluids |
| US5680766A (en) | 1996-01-02 | 1997-10-28 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US5778676A (en) | 1996-01-02 | 1998-07-14 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| US5685139A (en) | 1996-03-29 | 1997-11-11 | General Electric Company | Diffusion-premix nozzle for a gas turbine combustor and related method |
| US5761897A (en) | 1996-12-20 | 1998-06-09 | United Technologies Corporation | Method of combustion with a two stream tangential entry nozzle |
| US5899075A (en) | 1997-03-17 | 1999-05-04 | General Electric Company | Turbine engine combustor with fuel-air mixer |
| US5930999A (en) | 1997-07-23 | 1999-08-03 | General Electric Company | Fuel injector and multi-swirler carburetor assembly |
| EP0918190A1 (de) | 1997-11-21 | 1999-05-26 | Abb Research Ltd. | Brenner für den Betrieb eines Wärmeerzeugers |
| DE69916911T2 (de) | 1998-02-10 | 2005-04-21 | Gen Electric | Brenner mit gleichmässiger Brennstoff/Luft Vormischung zur emissionsarmen Verbrennung |
| US6174160B1 (en) | 1999-03-25 | 2001-01-16 | University Of Washington | Staged prevaporizer-premixer |
| US6363724B1 (en) | 2000-08-31 | 2002-04-02 | General Electric Company | Gas only nozzle fuel tip |
| US6442939B1 (en) | 2000-12-22 | 2002-09-03 | Pratt & Whitney Canada Corp. | Diffusion mixer |
| US6530222B2 (en) | 2001-07-13 | 2003-03-11 | Pratt & Whitney Canada Corp. | Swirled diffusion dump combustor |
| US6813889B2 (en) | 2001-08-29 | 2004-11-09 | Hitachi, Ltd. | Gas turbine combustor and operating method thereof |
| US6895755B2 (en) | 2002-03-01 | 2005-05-24 | Parker-Hannifin Corporation | Nozzle with flow equalizer |
| US6672073B2 (en) | 2002-05-22 | 2004-01-06 | Siemens Westinghouse Power Corporation | System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate |
| US7165405B2 (en) | 2002-07-15 | 2007-01-23 | Power Systems Mfg. Llc | Fully premixed secondary fuel nozzle with dual fuel capability |
| US6962055B2 (en) | 2002-09-27 | 2005-11-08 | United Technologies Corporation | Multi-point staging strategy for low emission and stable combustion |
| US6681578B1 (en) | 2002-11-22 | 2004-01-27 | General Electric Company | Combustor liner with ring turbulators and related method |
| US6623267B1 (en) | 2002-12-31 | 2003-09-23 | Tibbs M. Golladay, Jr. | Industrial burner |
| US7007486B2 (en) | 2003-03-26 | 2006-03-07 | The Boeing Company | Apparatus and method for selecting a flow mixture |
| DE10340826A1 (de) | 2003-09-04 | 2005-03-31 | Rolls-Royce Deutschland Ltd & Co Kg | Homogene Gemischbildung durch verdrallte Einspritzung des Kraftstoffs |
| US7185494B2 (en) | 2004-04-12 | 2007-03-06 | General Electric Company | Reduced center burner in multi-burner combustor and method for operating the combustor |
| US7007477B2 (en) | 2004-06-03 | 2006-03-07 | General Electric Company | Premixing burner with impingement cooled centerbody and method of cooling centerbody |
| US6993916B2 (en) | 2004-06-08 | 2006-02-07 | General Electric Company | Burner tube and method for mixing air and gas in a gas turbine engine |
| US7246494B2 (en) | 2004-09-29 | 2007-07-24 | General Electric Company | Methods and apparatus for fabricating gas turbine engine combustors |
| JP4626251B2 (ja) | 2004-10-06 | 2011-02-02 | 株式会社日立製作所 | 燃焼器及び燃焼器の燃焼方法 |
| US7237384B2 (en) | 2005-01-26 | 2007-07-03 | Peter Stuttaford | Counter swirl shear mixer |
| US7509808B2 (en) | 2005-03-25 | 2009-03-31 | General Electric Company | Apparatus having thermally isolated venturi tube joints |
| CN100570216C (zh) | 2005-06-24 | 2009-12-16 | 株式会社日立制作所 | 喷烧器、燃气轮机燃烧器、喷烧器的冷却方法及喷烧器的改造方法 |
| US7540154B2 (en) | 2005-08-11 | 2009-06-02 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor |
| US7832365B2 (en) | 2005-09-07 | 2010-11-16 | Fives North American Combustion, Inc. | Submerged combustion vaporizer with low NOx |
| US20070074518A1 (en) | 2005-09-30 | 2007-04-05 | Solar Turbines Incorporated | Turbine engine having acoustically tuned fuel nozzle |
| US7556031B2 (en) | 2005-12-12 | 2009-07-07 | Global Sustainability Technologies, LLC | Device for enhancing fuel efficiency of and/or reducing emissions from internal combustion engines |
| US7506510B2 (en) | 2006-01-17 | 2009-03-24 | Delavan Inc | System and method for cooling a staged airblast fuel injector |
| US7413053B2 (en) * | 2006-01-25 | 2008-08-19 | Siemens Power Generation, Inc. | Acoustic resonator with impingement cooling tubes |
| US7827797B2 (en) | 2006-09-05 | 2010-11-09 | General Electric Company | Injection assembly for a combustor |
| US7810333B2 (en) | 2006-10-02 | 2010-10-12 | General Electric Company | Method and apparatus for operating a turbine engine |
| US20080078183A1 (en) | 2006-10-03 | 2008-04-03 | General Electric Company | Liquid fuel enhancement for natural gas swirl stabilized nozzle and method |
| US7832212B2 (en) | 2006-11-10 | 2010-11-16 | General Electric Company | High expansion fuel injection slot jet and method for enhancing mixing in premixing devices |
| US7905094B2 (en) | 2007-09-28 | 2011-03-15 | Honeywell International Inc. | Combustor systems with liners having improved cooling hole patterns |
| US8042339B2 (en) * | 2008-03-12 | 2011-10-25 | General Electric Company | Lean direct injection combustion system |
| US8291688B2 (en) | 2008-03-31 | 2012-10-23 | General Electric Company | Fuel nozzle to withstand a flameholding incident |
| US20090249789A1 (en) | 2008-04-08 | 2009-10-08 | Baifang Zuo | Burner tube premixer and method for mixing air and gas in a gas turbine engine |
| US8147121B2 (en) | 2008-07-09 | 2012-04-03 | General Electric Company | Pre-mixing apparatus for a turbine engine |
| US8112999B2 (en) | 2008-08-05 | 2012-02-14 | General Electric Company | Turbomachine injection nozzle including a coolant delivery system |
| US7886991B2 (en) | 2008-10-03 | 2011-02-15 | General Electric Company | Premixed direct injection nozzle |
| US8007274B2 (en) | 2008-10-10 | 2011-08-30 | General Electric Company | Fuel nozzle assembly |
| US9121609B2 (en) * | 2008-10-14 | 2015-09-01 | General Electric Company | Method and apparatus for introducing diluent flow into a combustor |
| US8312722B2 (en) | 2008-10-23 | 2012-11-20 | General Electric Company | Flame holding tolerant fuel and air premixer for a gas turbine combustor |
| US8209986B2 (en) | 2008-10-29 | 2012-07-03 | General Electric Company | Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event |
| US9140454B2 (en) | 2009-01-23 | 2015-09-22 | General Electric Company | Bundled multi-tube nozzle for a turbomachine |
| US8205452B2 (en) | 2009-02-02 | 2012-06-26 | General Electric Company | Apparatus for fuel injection in a turbine engine |
| US8539773B2 (en) | 2009-02-04 | 2013-09-24 | General Electric Company | Premixed direct injection nozzle for highly reactive fuels |
| US20100192582A1 (en) | 2009-02-04 | 2010-08-05 | Robert Bland | Combustor nozzle |
| US8424311B2 (en) * | 2009-02-27 | 2013-04-23 | General Electric Company | Premixed direct injection disk |
| 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 |
| US8157189B2 (en) | 2009-04-03 | 2012-04-17 | General Electric Company | Premixing direct injector |
| US8333075B2 (en) | 2009-04-16 | 2012-12-18 | General Electric Company | Gas turbine premixer with internal cooling |
| US8359870B2 (en) | 2009-05-12 | 2013-01-29 | General Electric Company | Automatic fuel nozzle flame-holding quench |
| US20110016866A1 (en) * | 2009-07-22 | 2011-01-27 | General Electric Company | Apparatus for fuel injection in a turbine engine |
| US8616002B2 (en) | 2009-07-23 | 2013-12-31 | General Electric Company | Gas turbine premixing systems |
| US8181891B2 (en) * | 2009-09-08 | 2012-05-22 | General Electric Company | Monolithic fuel injector and related manufacturing method |
| US8276385B2 (en) * | 2009-10-08 | 2012-10-02 | General Electric Company | Staged multi-tube premixing injector |
| US8683804B2 (en) | 2009-11-13 | 2014-04-01 | General Electric Company | Premixing apparatus for fuel injection in a turbine engine |
| US8677760B2 (en) * | 2010-01-06 | 2014-03-25 | General Electric Company | Fuel nozzle with integrated passages and method of operation |
| US8959921B2 (en) | 2010-07-13 | 2015-02-24 | General Electric Company | Flame tolerant secondary fuel nozzle |
| US8919137B2 (en) | 2011-08-05 | 2014-12-30 | General Electric Company | Assemblies and apparatus related to integrating late lean injection into combustion turbine engines |
| US8801428B2 (en) | 2011-10-04 | 2014-08-12 | General Electric Company | Combustor and method for supplying fuel to a combustor |
| US8438851B1 (en) * | 2012-01-03 | 2013-05-14 | General Electric Company | Combustor assembly for use in a turbine engine and methods of assembling same |
| US20130318976A1 (en) | 2012-05-29 | 2013-12-05 | General Electric Company | Turbomachine combustor nozzle and method of forming the same |
-
2012
- 2012-05-29 US US13/482,540 patent/US9267690B2/en active Active
-
2013
- 2013-05-24 JP JP2013109447A patent/JP6134580B2/ja active Active
- 2013-05-28 EP EP13169581.9A patent/EP2669579B1/en active Active
- 2013-05-28 RU RU2013124126/06A patent/RU2013124126A/ru not_active Application Discontinuation
- 2013-05-29 CN CN201310205369.1A patent/CN103453553B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US20130318975A1 (en) | 2013-12-05 |
| CN103453553B (zh) | 2017-04-26 |
| US9267690B2 (en) | 2016-02-23 |
| EP2669579A3 (en) | 2017-05-10 |
| EP2669579B1 (en) | 2020-05-06 |
| EP2669579A2 (en) | 2013-12-04 |
| JP2013245936A (ja) | 2013-12-09 |
| RU2013124126A (ru) | 2014-12-10 |
| CN103453553A (zh) | 2013-12-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6134580B2 (ja) | モノリシックノズル部品を含むターボ機械燃焼器ノズル及びその形成方法 | |
| EP2525151B1 (en) | Combustor assembly for a turbomachine | |
| JP7098300B2 (ja) | 燃料供給導管アセンブリにおける燃料流出物を消散させるためのシステム | |
| EP2554910B1 (en) | Methods relating to integrating late lean injection into combustion turbine engines | |
| US6463742B2 (en) | Gas turbine steam-cooled combustor with alternately counter-flowing steam passages | |
| JP5265585B2 (ja) | ターボ機械用の燃料ノズル | |
| US20110107769A1 (en) | Impingement insert for a turbomachine injector | |
| EP2554905A1 (en) | Assemblies and apparatus related to integrating late lean injection into combustion turbine engines | |
| US8297059B2 (en) | Nozzle for a turbomachine | |
| JP2007225273A (ja) | 燃焼器アセンブリ及びガスタービンエンジン | |
| EP3165825B1 (en) | Repairable fuel injector | |
| CN113167474B (zh) | 燃气轮机的燃烧器以及具备该燃烧器的燃气轮机 | |
| JP7202090B2 (ja) | 一体型燃料ノズル接続部 | |
| CN115200040B (zh) | 用于燃气涡轮发动机燃烧器的稀释喇叭对 | |
| EP2554911A2 (en) | Fuel Nozzle | |
| JP2005308389A (ja) | ガスタービンエンジン燃焼器を製作するための方法及び装置 | |
| US20110162377A1 (en) | Turbomachine nozzle | |
| US20190277140A1 (en) | Impeller, centrifugal compressor, gas turbine, and method of manufacturing impeller | |
| US20110265485A1 (en) | Fluid cooled injection nozzle assembly for a gas turbomachine | |
| US11209163B2 (en) | Gas turbine combustor, manufacturing method for gas turbine and gas turbine combustor | |
| US8683805B2 (en) | Injector seal for a gas turbomachine | |
| CN116066854B (zh) | 用于降低排放的波浪形环形稀释槽 | |
| EP3078914A1 (en) | Annular combustor for a gas turbine engine | |
| JP2016040510A (ja) | ガスターボ機械用のオリフィスプラグを有するノズル | |
| US20130318976A1 (en) | Turbomachine combustor nozzle and method of forming the same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20160519 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20160519 |
|
| A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20170329 |
|
| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20170404 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20170424 |
|
| R150 | Certificate of patent or registration of utility model |
Ref document number: 6134580 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| S111 | Request for change of ownership or part of ownership |
Free format text: JAPANESE INTERMEDIATE CODE: R313113 |
|
| R350 | Written notification of registration of transfer |
Free format text: JAPANESE INTERMEDIATE CODE: R350 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |