CH707852A2 - System zur Zuführung von Brennstoff zu einer Brennkammer. - Google Patents
System zur Zuführung von Brennstoff zu einer Brennkammer. Download PDFInfo
- Publication number
- CH707852A2 CH707852A2 CH00399/14A CH3992014A CH707852A2 CH 707852 A2 CH707852 A2 CH 707852A2 CH 00399/14 A CH00399/14 A CH 00399/14A CH 3992014 A CH3992014 A CH 3992014A CH 707852 A2 CH707852 A2 CH 707852A2
- Authority
- CH
- Switzerland
- Prior art keywords
- fuel
- passage
- lli
- flange
- flow
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title claims abstract description 153
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 36
- 239000012530 fluid Substances 0.000 claims abstract description 77
- 238000004891 communication Methods 0.000 claims abstract description 23
- 238000002347 injection Methods 0.000 claims description 64
- 239000007924 injection Substances 0.000 claims description 64
- 230000007704 transition Effects 0.000 claims description 26
- WYTGDNHDOZPMIW-RCBQFDQVSA-N alstonine Natural products C1=CC2=C3C=CC=CC3=NC2=C2N1C[C@H]1[C@H](C)OC=C(C(=O)OC)[C@H]1C2 WYTGDNHDOZPMIW-RCBQFDQVSA-N 0.000 claims description 5
- 239000003570 air Substances 0.000 description 44
- 239000007789 gas Substances 0.000 description 39
- 238000001816 cooling Methods 0.000 description 26
- 238000011144 upstream manufacturing Methods 0.000 description 24
- 230000001105 regulatory effect Effects 0.000 description 15
- 230000007423 decrease Effects 0.000 description 13
- 239000000567 combustion gas Substances 0.000 description 12
- 238000009434 installation Methods 0.000 description 8
- 230000033228 biological regulation Effects 0.000 description 7
- MWUXSHHQAYIFBG-UHFFFAOYSA-N nitrogen oxide Inorganic materials O=[N] MWUXSHHQAYIFBG-UHFFFAOYSA-N 0.000 description 7
- 230000008878 coupling Effects 0.000 description 5
- 238000010168 coupling process Methods 0.000 description 5
- 238000005859 coupling reaction Methods 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008646 thermal stress Effects 0.000 description 3
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000002737 fuel gas Substances 0.000 description 2
- 238000010297 mechanical methods and process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000036316 preload Effects 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 238000005219 brazing Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000007865 diluting Methods 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000037361 pathway Effects 0.000 description 1
- 235000020004 porter Nutrition 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 102000012498 secondary active transmembrane transporter activity proteins Human genes 0.000 description 1
- 108040003878 secondary active transmembrane transporter activity proteins Proteins 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/222—Fuel flow conduits, e.g. manifolds
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- 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
- F23R3/34—Feeding into different combustion zones
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)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/845,365 US9316155B2 (en) | 2013-03-18 | 2013-03-18 | System for providing fuel to a combustor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CH707852A2 true CH707852A2 (de) | 2014-09-30 |
Family
ID=51419085
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CH00399/14A CH707852A2 (de) | 2013-03-18 | 2014-03-17 | System zur Zuführung von Brennstoff zu einer Brennkammer. |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9316155B2 (enExample) |
| JP (1) | JP6506503B2 (enExample) |
| CN (1) | CN104061599B (enExample) |
| CH (1) | CH707852A2 (enExample) |
| DE (1) | DE102014103087A1 (enExample) |
Families Citing this family (54)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9316155B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | System for providing fuel to a combustor |
| US9400114B2 (en) | 2013-03-18 | 2016-07-26 | General Electric Company | Combustor support assembly for mounting a combustion module of a gas turbine |
| US9383104B2 (en) | 2013-03-18 | 2016-07-05 | General Electric Company | Continuous combustion liner for a combustor of a gas turbine |
| US20140260318A1 (en) * | 2013-03-18 | 2014-09-18 | General Electric Company | Side seal slot for a combustion liner |
| US9322556B2 (en) | 2013-03-18 | 2016-04-26 | General Electric Company | Flow sleeve assembly for a combustion module of a gas turbine combustor |
| US9631812B2 (en) | 2013-03-18 | 2017-04-25 | General Electric Company | Support frame and method for assembly of a combustion module of a gas turbine |
| US9360217B2 (en) * | 2013-03-18 | 2016-06-07 | General Electric Company | Flow sleeve for a combustion module of a gas turbine |
| US10436445B2 (en) | 2013-03-18 | 2019-10-08 | General Electric Company | Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine |
| US9316396B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | Hot gas path duct for a combustor of a gas turbine |
| US20150159877A1 (en) * | 2013-12-06 | 2015-06-11 | General Electric Company | Late lean injection manifold mixing system |
| US9803555B2 (en) * | 2014-04-23 | 2017-10-31 | General Electric Company | Fuel delivery system with moveably attached fuel tube |
| US10066837B2 (en) | 2015-02-20 | 2018-09-04 | General Electric Company | Combustor aft mount assembly |
| US9951693B2 (en) * | 2015-02-24 | 2018-04-24 | General Electric Company | Fuel supply system for a gas turbine combustor |
| US20160265781A1 (en) * | 2015-03-10 | 2016-09-15 | General Electric Company | Air shield for a fuel injector of a combustor |
| US20160265782A1 (en) * | 2015-03-10 | 2016-09-15 | General Electric Company | Air shield for a fuel injector of a combustor |
| WO2017018982A1 (en) * | 2015-07-24 | 2017-02-02 | Siemens Aktiengesellschaft | Gas turbine transition duct with late lean injection having reduced combustion residence time |
| CN107923254A (zh) * | 2015-08-28 | 2018-04-17 | 西门子公司 | 用于燃烧室的非轴向对称过渡管道 |
| US20170226929A1 (en) * | 2016-02-09 | 2017-08-10 | General Electric Company | Fuel injector covers and methods of fabricating same |
| US10203114B2 (en) | 2016-03-04 | 2019-02-12 | General Electric Company | Sleeve assemblies and methods of fabricating same |
| US10228141B2 (en) | 2016-03-04 | 2019-03-12 | General Electric Company | Fuel supply conduit assemblies |
| US10260424B2 (en) | 2016-03-24 | 2019-04-16 | General Electric Company | Transition duct assembly with late injection features |
| US10605459B2 (en) * | 2016-03-25 | 2020-03-31 | General Electric Company | Integrated combustor nozzle for a segmented annular combustion system |
| US10329941B2 (en) * | 2016-05-06 | 2019-06-25 | United Technologies Corporation | Impingement manifold |
| US10689995B2 (en) * | 2016-05-27 | 2020-06-23 | General Electric Company | Side seal with reduced corner leakage |
| US10513987B2 (en) * | 2016-12-30 | 2019-12-24 | General Electric Company | System for dissipating fuel egress in fuel supply conduit assemblies |
| US10851999B2 (en) | 2016-12-30 | 2020-12-01 | General Electric Company | Fuel injectors and methods of use in gas turbine combustor |
| US10865992B2 (en) | 2016-12-30 | 2020-12-15 | General Electric Company | Fuel injectors and methods of use in gas turbine combustor |
| US10816208B2 (en) | 2017-01-20 | 2020-10-27 | General Electric Company | Fuel injectors and methods of fabricating same |
| US20180245792A1 (en) * | 2017-02-24 | 2018-08-30 | General Electric Company | Combustion System with Axially Staged Fuel Injection |
| US10718523B2 (en) | 2017-05-12 | 2020-07-21 | General Electric Company | Fuel injectors with multiple outlet slots for use in gas turbine combustor |
| US10502426B2 (en) | 2017-05-12 | 2019-12-10 | General Electric Company | Dual fuel injectors and methods of use in gas turbine combustor |
| US11230976B2 (en) * | 2017-07-14 | 2022-01-25 | General Electric Company | Integrated fuel nozzle connection |
| US10690349B2 (en) | 2017-09-01 | 2020-06-23 | General Electric Company | Premixing fuel injectors and methods of use in gas turbine combustor |
| JP6345331B1 (ja) * | 2017-11-20 | 2018-06-20 | 三菱日立パワーシステムズ株式会社 | ガスタービンの燃焼筒及び燃焼器並びにガスタービン |
| US11137144B2 (en) * | 2017-12-11 | 2021-10-05 | General Electric Company | Axial fuel staging system for gas turbine combustors |
| US11187153B2 (en) | 2018-09-25 | 2021-11-30 | Woodward, Inc. | Composite spray bars |
| US11156112B2 (en) * | 2018-11-02 | 2021-10-26 | Chromalloy Gas Turbine Llc | Method and apparatus for mounting a transition duct in a gas turbine engine |
| US10890328B2 (en) * | 2018-11-29 | 2021-01-12 | DOOSAN Heavy Industries Construction Co., LTD | Fin-pin flow guide for efficient transition piece cooling |
| RU2769616C2 (ru) * | 2018-12-25 | 2022-04-04 | Ансальдо Энергия Свитзерленд Аг | Инжекционная головка для камеры сгорания газовой турбины |
| US11421601B2 (en) | 2019-03-28 | 2022-08-23 | Woodward, Inc. | Second stage combustion for igniter |
| KR102149359B1 (ko) * | 2019-11-11 | 2020-08-28 | 성균관대학교 산학협력단 | 연소기 |
| EP3848113A1 (en) * | 2020-01-07 | 2021-07-14 | SABIC Global Technologies B.V. | Systems, devices, and methods of a reactor feed distribution system |
| CN116209823A (zh) | 2020-06-23 | 2023-06-02 | 伍德沃德有限公司 | 针对功率生成发动机的点火系统 |
| US11371709B2 (en) | 2020-06-30 | 2022-06-28 | General Electric Company | Combustor air flow path |
| US12044411B2 (en) | 2021-06-17 | 2024-07-23 | Ge Infrastructure Technology Llc | Combustor having fuel sweeping structures |
| US11435080B1 (en) * | 2021-06-17 | 2022-09-06 | General Electric Company | Combustor having fuel sweeping structures |
| US12270543B2 (en) | 2021-08-20 | 2025-04-08 | Rtx Corporation | Multi-function monolithic combustion liner |
| US11898753B2 (en) | 2021-10-11 | 2024-02-13 | Ge Infrastructure Technology Llc | System and method for sweeping leaked fuel in gas turbine system |
| US11933216B2 (en) * | 2022-01-04 | 2024-03-19 | General Electric Company | Systems and methods for providing output products to a combustion chamber of a gas turbine engine |
| US12188658B1 (en) | 2023-07-07 | 2025-01-07 | Ge Infrastructure Technology Llc | Fuel injection assembly for a combustor |
| US12467630B2 (en) | 2023-07-07 | 2025-11-11 | Ge Vernova Infrastructure Technology Llc | Fuel injection assembly having a boss with a serpentine cooling passage |
| US12281793B1 (en) | 2024-01-29 | 2025-04-22 | Ge Infrastructure Technology Llc | Fuel injection assembly for a combustor |
| WO2025205231A1 (ja) * | 2024-03-25 | 2025-10-02 | 三菱重工業株式会社 | 燃料供給管アセンブリ、ガスタービン燃焼器、及びガスタービン |
| US12449128B1 (en) | 2024-11-27 | 2025-10-21 | Ge Vernova Infrastructure Technology Llc | Boss for a fuel injection assembly having cooling circuit and combustor provided therewith |
Family Cites Families (61)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3872664A (en) | 1973-10-15 | 1975-03-25 | United Aircraft Corp | Swirl combustor with vortex burning and mixing |
| US4265615A (en) | 1978-12-11 | 1981-05-05 | United Technologies Corporation | Fuel injection system for low emission burners |
| US4420929A (en) | 1979-01-12 | 1983-12-20 | General Electric Company | Dual stage-dual mode low emission gas turbine combustion system |
| JPS6057131A (ja) * | 1983-09-08 | 1985-04-02 | Hitachi Ltd | ガスタ−ビン燃焼器の燃料供給方法 |
| JPS6139275U (ja) * | 1984-08-14 | 1986-03-12 | 三菱重工業株式会社 | 燃焼器 |
| JPH0663648B2 (ja) * | 1986-12-05 | 1994-08-22 | 株式会社日立製作所 | ガスタ−ビン燃焼器 |
| JP2644745B2 (ja) | 1987-03-06 | 1997-08-25 | 株式会社日立製作所 | ガスタービン用燃焼器 |
| CA2070511C (en) | 1991-07-22 | 2001-08-21 | Steven Milo Toborg | Turbine nozzle support |
| JP2512256B2 (ja) * | 1992-01-20 | 1996-07-03 | 株式会社日立製作所 | ガスタ―ビン燃焼器 |
| US5271714A (en) | 1992-07-09 | 1993-12-21 | General Electric Company | Turbine nozzle support arrangement |
| JP3335713B2 (ja) * | 1993-06-28 | 2002-10-21 | 株式会社東芝 | ガスタービン燃焼器 |
| GB9325708D0 (en) | 1993-12-16 | 1994-02-16 | Rolls Royce Plc | A gas turbine engine combustion chamber |
| JP2950720B2 (ja) | 1994-02-24 | 1999-09-20 | 株式会社東芝 | ガスタービン燃焼装置およびその燃焼制御方法 |
| US5380154A (en) | 1994-03-18 | 1995-01-10 | Solar Turbines Incorporated | Turbine nozzle positioning system |
| US6047550A (en) * | 1996-05-02 | 2000-04-11 | General Electric Co. | Premixing dry low NOx emissions combustor with lean direct injection of gas fuel |
| EP0962874A1 (en) | 1998-06-04 | 1999-12-08 | Asea Brown Boveri AG | Method for designing a flow device |
| FR2779807B1 (fr) * | 1998-06-11 | 2000-07-13 | Inst Francais Du Petrole | Chambre de combustion de turbine a gaz a geometrie variable |
| GB9813972D0 (en) | 1998-06-30 | 1998-08-26 | Rolls Royce Plc | A combustion chamber |
| US6212870B1 (en) | 1998-09-22 | 2001-04-10 | General Electric Company | Self fixturing combustor dome assembly |
| DE69940948D1 (de) | 1999-01-25 | 2009-07-16 | Gen Electric | Interner Kühlkreislauf für eine Gasturbinenschaufel |
| JP2001289062A (ja) * | 2000-04-07 | 2001-10-19 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器の壁面冷却構造 |
| US6374594B1 (en) | 2000-07-12 | 2002-04-23 | Power Systems Mfg., Llc | Silo/can-annular low emissions combustor |
| US6442946B1 (en) | 2000-11-14 | 2002-09-03 | Power Systems Mfg., Llc | Three degrees of freedom aft mounting system for gas turbine transition duct |
| US6543993B2 (en) | 2000-12-28 | 2003-04-08 | General Electric Company | Apparatus and methods for localized cooling of gas turbine nozzle walls |
| US6450762B1 (en) | 2001-01-31 | 2002-09-17 | General Electric Company | Integral aft seal for turbine applications |
| US6553767B2 (en) * | 2001-06-11 | 2003-04-29 | General Electric Company | Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form |
| US20030039542A1 (en) | 2001-08-21 | 2003-02-27 | Cromer Robert Harold | Transition piece side sealing element and turbine assembly containing such seal |
| JP2004125379A (ja) | 2002-07-29 | 2004-04-22 | Miura Co Ltd | 低ＮＯｘ燃焼方法とその装置 |
| EP1439349A1 (de) | 2003-01-14 | 2004-07-21 | Alstom Technology Ltd | Verbrennungsverfahren sowie Brenner zur Durchführung des Verfahrens |
| US6923002B2 (en) | 2003-08-28 | 2005-08-02 | General Electric Company | Combustion liner cap assembly for combustion dynamics reduction |
| US7284378B2 (en) | 2004-06-04 | 2007-10-23 | General Electric Company | Methods and apparatus for low emission gas turbine energy generation |
| US7047723B2 (en) * | 2004-04-30 | 2006-05-23 | Martling Vincent C | Apparatus and method for reducing the heat rate of a gas turbine powerplant |
| US7082766B1 (en) | 2005-03-02 | 2006-08-01 | General Electric Company | One-piece can combustor |
| JP4652990B2 (ja) * | 2006-02-16 | 2011-03-16 | 株式会社日立製作所 | ガスタービン燃焼器 |
| JP4824499B2 (ja) | 2006-08-03 | 2011-11-30 | 株式会社神戸製鋼所 | ダイスの設計方法、ダイス、中空パネルの製造方法及び中空パネル |
| US7743612B2 (en) | 2006-09-22 | 2010-06-29 | Pratt & Whitney Canada Corp. | Internal fuel manifold and fuel inlet connection |
| US8171738B2 (en) | 2006-10-24 | 2012-05-08 | Pratt & Whitney Canada Corp. | Gas turbine internal manifold mounting arrangement |
| US7757492B2 (en) | 2007-05-18 | 2010-07-20 | General Electric Company | Method and apparatus to facilitate cooling turbine engines |
| US7886539B2 (en) | 2007-09-14 | 2011-02-15 | Siemens Energy, Inc. | Multi-stage axial combustion system |
| US8096131B2 (en) | 2007-11-14 | 2012-01-17 | Pratt & Whitney Canada Corp. | Fuel inlet with crescent shaped passage for gas turbine engines |
| US7908863B2 (en) | 2008-02-12 | 2011-03-22 | General Electric Company | Fuel nozzle for a gas turbine engine and method for fabricating the same |
| US8118549B2 (en) | 2008-08-26 | 2012-02-21 | Siemens Energy, Inc. | Gas turbine transition duct apparatus |
| US20100071377A1 (en) * | 2008-09-19 | 2010-03-25 | Fox Timothy A | Combustor Apparatus for Use in a Gas Turbine Engine |
| JP2010085052A (ja) * | 2008-10-01 | 2010-04-15 | Mitsubishi Heavy Ind Ltd | 燃焼器尾筒およびその設計方法ならびにガスタービン |
| US8327648B2 (en) | 2008-12-09 | 2012-12-11 | Pratt & Whitney Canada Corp. | Combustor liner with integrated anti-rotation and removal feature |
| US20100170258A1 (en) * | 2009-01-06 | 2010-07-08 | General Electric Company | Cooling apparatus for combustor transition piece |
| EP2206964A3 (en) * | 2009-01-07 | 2012-05-02 | General Electric Company | Late lean injection fuel injector configurations |
| US8701383B2 (en) | 2009-01-07 | 2014-04-22 | General Electric Company | Late lean injection system configuration |
| US8112216B2 (en) | 2009-01-07 | 2012-02-07 | General Electric Company | Late lean injection with adjustable air splits |
| US20100263386A1 (en) | 2009-04-16 | 2010-10-21 | General Electric Company | Turbine engine having a liner |
| JP5260402B2 (ja) | 2009-04-30 | 2013-08-14 | 三菱重工業株式会社 | 板状体の製造方法、板状体、ガスタービン燃焼器およびガスタービン |
| US8991192B2 (en) | 2009-09-24 | 2015-03-31 | Siemens Energy, Inc. | Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engine |
| US8082739B2 (en) | 2010-04-12 | 2011-12-27 | General Electric Company | Combustor exit temperature profile control via fuel staging and related method |
| US8398090B2 (en) | 2010-06-09 | 2013-03-19 | General Electric Company | Spring loaded seal assembly for turbines |
| US8158428B1 (en) | 2010-12-30 | 2012-04-17 | General Electric Company | Methods, systems and apparatus for detecting material defects in combustors of combustion turbine engines |
| US20120186260A1 (en) | 2011-01-25 | 2012-07-26 | General Electric Company | Transition piece impingement sleeve for a gas turbine |
| US8448444B2 (en) | 2011-02-18 | 2013-05-28 | General Electric Company | Method and apparatus for mounting transition piece in combustor |
| CH704829A2 (de) | 2011-04-08 | 2012-11-15 | Alstom Technology Ltd | Gasturbogruppe und zugehöriges Betriebsverfahren. |
| US8601820B2 (en) * | 2011-06-06 | 2013-12-10 | General Electric Company | Integrated late lean injection on a combustion liner and late lean injection sleeve assembly |
| US9010120B2 (en) * | 2011-08-05 | 2015-04-21 | General Electric Company | Assemblies and apparatus related to integrating late lean injection into combustion turbine engines |
| US9316155B2 (en) | 2013-03-18 | 2016-04-19 | General Electric Company | System for providing fuel to a combustor |
-
2013
- 2013-03-18 US US13/845,365 patent/US9316155B2/en active Active
-
2014
- 2014-03-07 DE DE102014103087.7A patent/DE102014103087A1/de active Pending
- 2014-03-14 JP JP2014050934A patent/JP6506503B2/ja active Active
- 2014-03-17 CH CH00399/14A patent/CH707852A2/de not_active Application Discontinuation
- 2014-03-18 CN CN201410100637.8A patent/CN104061599B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US9316155B2 (en) | 2016-04-19 |
| CN104061599B (zh) | 2018-01-09 |
| CN104061599A (zh) | 2014-09-24 |
| JP6506503B2 (ja) | 2019-04-24 |
| JP2014181902A (ja) | 2014-09-29 |
| US20140260272A1 (en) | 2014-09-18 |
| DE102014103087A1 (de) | 2014-09-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CH707852A2 (de) | System zur Zuführung von Brennstoff zu einer Brennkammer. | |
| DE102011000225B4 (de) | Über einen Anzapfdiffusor gespeistes sekundäres Verbrennungssystem für Gasturbinen | |
| CH707849A2 (de) | System zur Steuerung der Luftflussrate eines komprimierten Arbeitsfluids zu einem Brennstoffinjektor eines Brenners. | |
| DE102011000587B4 (de) | Systeme und Verfahren zur Zufuhr von Hochdruckluft zum Kopfende einer Brennkammer | |
| CH707456A2 (de) | Brennstoffinjektor zur Zuführung von Brennstoff zu einer Brennkammer. | |
| DE102014103008A1 (de) | Verfahren zur stromabwärtigen Brennstoff- und Luftinjektion in Gasturbinen | |
| CH707828A2 (de) | Durchgehende Brennkammerauskleidung für eine Brennkammer einer Gasturbine. | |
| DE102018131660A1 (de) | Brennstoffinjektionsanordnungen zur axialen Brennstoffstufung in Gasturbinenbrennkammern | |
| CH707851A2 (de) | Brennkammermodul für einen Brenner einer Gasturbine. | |
| CH710574B1 (de) | System und Verfahren zur Nutzung von Kühlluft in einem Brenner. | |
| CH708388A2 (de) | Brennstoffzufuhrsystem für eine Brennkammer einer Gasturbine. | |
| DE102018110969A1 (de) | Dual-Brennstoff-Injektoren und Verfahren zur Verwendung in einer Gasturbinenbrennkammer | |
| CH708992A2 (de) | Brennstoffinjektor mit Vormisch-Pilotdüse. | |
| CH709993A2 (de) | Stromabwärtige Düse in einer Brennkammer einer Verbrennungsturbine. | |
| CH707853A2 (de) | Strömungshülsenanordnung für ein Verbrennungsmodul eines Gasturbinenbrenners. | |
| EP2808611B1 (de) | Injektor zum Einbringen eines Brennstoff-Luft-Gemisches in eine Brennkammer | |
| DE102015120448A1 (de) | Vormischbrennstoffdüsenanordnung | |
| DE102014103020A1 (de) | Systeme und Vorrichtungen zur stromabwärtigen Brennstoff- und Luftinjektion bei Gasturbinen | |
| DE102015122924A1 (de) | Pilotdüse in einer Gasturbinenbrennkammer | |
| DE102014113326A1 (de) | Innengekühlter Übergangskanalhinterrahmen | |
| DE102016106491A1 (de) | Brennstoffdüsenanordnung mit einer Pilotdüse | |
| CH710052A2 (de) | Brennkammerkappenanordnung, Brennkammer und Gasturbine. | |
| CH707454A2 (de) | Brennstoffinjektor mit einem Zünder für eine Brennkammer einer Gasturbine. | |
| DE102015119749A1 (de) | Vormischbrennstoffdüsenanordnung | |
| CH710049A2 (de) | Brennkammerkappenanordnung, Brennkammer und Gasturbine. |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| NV | New agent |
Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH |
|
| AZW | Rejection (application) |