AR072358A1 - Sistema de refrigeracion mediante un venturi - Google Patents
Sistema de refrigeracion mediante un venturiInfo
- Publication number
- AR072358A1 AR072358A1 ARP090101612A ARP090101612A AR072358A1 AR 072358 A1 AR072358 A1 AR 072358A1 AR P090101612 A ARP090101612 A AR P090101612A AR P090101612 A ARP090101612 A AR P090101612A AR 072358 A1 AR072358 A1 AR 072358A1
- Authority
- AR
- Argentina
- Prior art keywords
- venturi
- combustor
- combustion chamber
- nozzle
- passage
- Prior art date
Links
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
- F23R3/002—Wall structures
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
-
- 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
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
-
- 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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/26—Controlling the air flow
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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)
- Gas Burners (AREA)
- Spray-Type Burners (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
Se provee un combustor para una turbina de gas que posee un montaje de boquilla ubicado en un extremo y una cámara de combustion que define a un segundo extremo del combustor. Un venturi está posicionado dentro del combustor entre la boquilla y la cámara de combustion. El venturi define un pasadizo donde un primer lado enfrenta a la boquilla y un segundo lado enfrenta a la cámara de combustion. El aire comprimido es dirigido adentro de una entrada en comunicacion fluida con los lados primero y segundo del pasadizo de un venturi. El pasadizo de un venturi dirige el aire comprimido desde la entrada y en direcciones opuestas dentro de los lados primero y segundo del pasadizo para refrigerar el venturi.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/357,029 US7712314B1 (en) | 2009-01-21 | 2009-01-21 | Venturi cooling system |
Publications (1)
Publication Number | Publication Date |
---|---|
AR072358A1 true AR072358A1 (es) | 2010-08-25 |
Family
ID=40566393
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ARP090101612A AR072358A1 (es) | 2009-01-21 | 2009-05-05 | Sistema de refrigeracion mediante un venturi |
ARP130103609A AR092910A2 (es) | 2009-01-21 | 2013-10-04 | Combustor para turbina de gas y venturi dispuesto en el interior de dicho combustor |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ARP130103609A AR092910A2 (es) | 2009-01-21 | 2013-10-04 | Combustor para turbina de gas y venturi dispuesto en el interior de dicho combustor |
Country Status (16)
Country | Link |
---|---|
US (2) | US7712314B1 (es) |
EP (1) | EP2211104B1 (es) |
JP (1) | JP4933578B2 (es) |
KR (1) | KR101131646B1 (es) |
CN (1) | CN101782232B (es) |
AR (2) | AR072358A1 (es) |
AU (1) | AU2009201420B8 (es) |
BR (1) | BRPI0901605A2 (es) |
CA (1) | CA2661248C (es) |
CL (1) | CL2009001101A1 (es) |
HK (1) | HK1146108A1 (es) |
IL (1) | IL198653A (es) |
MX (1) | MX2009004301A (es) |
MY (1) | MY149412A (es) |
SG (2) | SG163466A1 (es) |
TW (2) | TWI376484B (es) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8707704B2 (en) * | 2007-05-31 | 2014-04-29 | General Electric Company | Method and apparatus for assembling turbine engines |
US8096133B2 (en) * | 2008-05-13 | 2012-01-17 | General Electric Company | Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface |
US8646277B2 (en) * | 2010-02-19 | 2014-02-11 | General Electric Company | Combustor liner for a turbine engine with venturi and air deflector |
RU2519014C2 (ru) * | 2010-03-02 | 2014-06-10 | Дженерал Электрик Компани | Диффузор для камеры сгорания турбины (варианты) и камера сгорания турбины |
US8959886B2 (en) * | 2010-07-08 | 2015-02-24 | Siemens Energy, Inc. | Mesh cooled conduit for conveying combustion gases |
US8894363B2 (en) | 2011-02-09 | 2014-11-25 | Siemens Energy, Inc. | Cooling module design and method for cooling components of a gas turbine system |
US20120047895A1 (en) * | 2010-08-26 | 2012-03-01 | General Electric Company | Systems and apparatus relating to combustor cooling and operation in gas turbine engines |
US9518739B2 (en) | 2013-03-08 | 2016-12-13 | Pratt & Whitney Canada Corp. | Combustor heat shield with carbon avoidance feature |
US9453424B2 (en) * | 2013-10-21 | 2016-09-27 | Siemens Energy, Inc. | Reverse bulk flow effusion cooling |
CN104566463B (zh) * | 2014-11-29 | 2016-12-07 | 哈尔滨广瀚燃气轮机有限公司 | 燃气轮机低排放燃烧室空气调节装置 |
US10100730B2 (en) | 2015-03-11 | 2018-10-16 | Pratt & Whitney Canada Corp. | Secondary air system with venturi |
CN104807042A (zh) * | 2015-05-15 | 2015-07-29 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种燃烧室 |
CN105157063B (zh) * | 2015-09-18 | 2018-04-13 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种流量分配可调的火焰筒 |
CN105465455B (zh) * | 2015-12-25 | 2021-09-07 | 深圳荣钜源科技有限公司 | 出水单元、喷头以及花洒 |
CN107013941B (zh) * | 2016-01-27 | 2019-09-17 | 中国航发商用航空发动机有限责任公司 | 燃烧室燃油喷嘴装置 |
US10316803B2 (en) * | 2017-09-25 | 2019-06-11 | Woodward, Inc. | Passive pumping for recirculating exhaust gas |
CN109084329A (zh) * | 2018-07-05 | 2018-12-25 | 西北工业大学 | 一种多点直接喷射燃烧室头部结构 |
US10995705B2 (en) | 2019-02-07 | 2021-05-04 | Woodward, Inc. | Modular exhaust gas recirculation system |
CN213175878U (zh) | 2020-01-08 | 2021-05-11 | 伍德沃德有限公司 | 排气气体再循环混合器和发动机*** |
US11215132B1 (en) | 2020-12-15 | 2022-01-04 | Woodward, Inc. | Controlling an internal combustion engine system |
US11174809B1 (en) | 2020-12-15 | 2021-11-16 | Woodward, Inc. | Controlling an internal combustion engine system |
CN116265810A (zh) | 2021-12-16 | 2023-06-20 | 通用电气公司 | 利用成形冷却栅栏的旋流器反稀释 |
US11835236B1 (en) | 2022-07-05 | 2023-12-05 | General Electric Company | Combustor with reverse dilution air introduction |
US11747019B1 (en) * | 2022-09-02 | 2023-09-05 | General Electric Company | Aerodynamic combustor liner design for emissions reductions |
Family Cites Families (109)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2935841A (en) * | 1956-06-18 | 1960-05-10 | Bell Aircraft Corp | Thrust chamber with integrated cooling and structural members |
US3656303A (en) | 1970-04-13 | 1972-04-18 | Robert C La Force | Combustion engine pollution control |
US4010607A (en) | 1973-01-02 | 1977-03-08 | Hopping Alvin S | Internal combustion engine with afterburner, venturi cooler and exhaust turbine |
US3904307A (en) | 1974-04-10 | 1975-09-09 | United Technologies Corp | Gas generator turbine cooling scheme |
US3938324A (en) * | 1974-12-12 | 1976-02-17 | General Motors Corporation | Premix combustor with flow constricting baffle between combustion and dilution zones |
UST962010I4 (en) | 1976-03-25 | 1977-09-06 | Variable venturi carburetor idle speed fuel control | |
US4250856A (en) | 1980-01-25 | 1981-02-17 | Abbey Harold | Fuel-air ratio automatic control system using variable venturi structure |
US4200124A (en) | 1978-02-21 | 1980-04-29 | Eaton Corporation | Valve assembly |
DE7810865U1 (de) | 1978-04-12 | 1978-09-21 | Dolmar Maschinen-Fabrik Gmbh & Co, 2000 Hamburg | Abgasschalldaempfer fuer auspuffvorrichtungen von brennkraftmaschinen, insbesondere von brennkraftmaschinenangetriebenen handarbeitsgeraeten |
US4303374A (en) | 1978-12-15 | 1981-12-01 | General Electric Company | Film cooled airfoil body |
US4420929A (en) | 1979-01-12 | 1983-12-20 | General Electric Company | Dual stage-dual mode low emission gas turbine combustion system |
US4292801A (en) | 1979-07-11 | 1981-10-06 | General Electric Company | Dual stage-dual mode low nox combustor |
US4361010A (en) * | 1980-04-02 | 1982-11-30 | United Technologies Corporation | Combustor liner construction |
US4413477A (en) * | 1980-12-29 | 1983-11-08 | General Electric Company | Liner assembly for gas turbine combustor |
US4690245A (en) | 1983-03-17 | 1987-09-01 | Stemco, Inc. | Flattened venturi, method and apparatus for making |
US4719748A (en) | 1985-05-14 | 1988-01-19 | General Electric Company | Impingement cooled transition duct |
US4982570A (en) | 1986-11-25 | 1991-01-08 | General Electric Company | Premixed pilot nozzle for dry low Nox combustor |
US4984429A (en) * | 1986-11-25 | 1991-01-15 | General Electric Company | Impingement cooled liner for dry low NOx venturi combustor |
US5329773A (en) | 1989-08-31 | 1994-07-19 | Alliedsignal Inc. | Turbine combustor cooling system |
US5101624A (en) | 1989-09-07 | 1992-04-07 | General Electric Company | Exhaust nozzle hinge |
US5285631A (en) | 1990-02-05 | 1994-02-15 | General Electric Company | Low NOx emission in gas turbine system |
US5117636A (en) * | 1990-02-05 | 1992-06-02 | General Electric Company | Low nox emission in gas turbine system |
US5123248A (en) | 1990-03-28 | 1992-06-23 | General Electric Company | Low emissions combustor |
US5127221A (en) | 1990-05-03 | 1992-07-07 | General Electric Company | Transpiration cooled throat section for low nox combustor and related process |
US5125227A (en) | 1990-07-10 | 1992-06-30 | General Electric Company | Movable combustion system for a gas turbine |
US5257499A (en) | 1991-09-23 | 1993-11-02 | General Electric Company | Air staged premixed dry low NOx combustor with venturi modulated flow split |
US5253478A (en) * | 1991-12-30 | 1993-10-19 | General Electric Company | Flame holding diverging centerbody cup construction for a dry low NOx combustor |
US5487275A (en) | 1992-12-11 | 1996-01-30 | General Electric Co. | Tertiary fuel injection system for use in a dry low NOx combustion system |
US5377483A (en) | 1993-07-07 | 1995-01-03 | Mowill; R. Jan | Process for single stage premixed constant fuel/air ratio combustion |
US5454221A (en) | 1994-03-14 | 1995-10-03 | General Electric Company | Dilution flow sleeve for reducing emissions in a gas turbine combustor |
SE504431C2 (sv) | 1994-06-29 | 1997-02-10 | Iggesund Tools Ab | Knivanordning |
US5584651A (en) | 1994-10-31 | 1996-12-17 | General Electric Company | Cooled shroud |
US5612006A (en) | 1995-07-05 | 1997-03-18 | Fisk; James C. | Catalytic converter and phase-spreading spiral muffler assembly |
JP3619599B2 (ja) | 1995-11-30 | 2005-02-09 | 株式会社東芝 | ガスタービンプラント |
GB2311596B (en) | 1996-03-29 | 2000-07-12 | Europ Gas Turbines Ltd | Combustor for gas - or liquid - fuelled turbine |
US5787703A (en) | 1996-05-10 | 1998-08-04 | Fougerousse; Russell | Combined ramjet and rocket engine having rectilinear duct |
US5950417A (en) | 1996-07-19 | 1999-09-14 | Foster Wheeler Energy International Inc. | Topping combustor for low oxygen vitiated air streams |
US6250066B1 (en) | 1996-11-26 | 2001-06-26 | Honeywell International Inc. | Combustor with dilution bypass system and venturi jet deflector |
US5829245A (en) | 1996-12-31 | 1998-11-03 | Westinghouse Electric Corporation | Cooling system for gas turbine vane |
US5738493A (en) | 1997-01-03 | 1998-04-14 | General Electric Company | Turbulator configuration for cooling passages of an airfoil in a gas turbine engine |
US5896742A (en) | 1997-03-20 | 1999-04-27 | General Electric Co. | Tapered cross-fire tube for gas turbine combustors |
US6139257A (en) | 1998-03-23 | 2000-10-31 | General Electric Company | Shroud cooling assembly for gas turbine engine |
CA2288557C (en) | 1998-11-12 | 2007-02-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor cooling structure |
GB2345942B (en) | 1998-12-24 | 2002-08-07 | Rolls Royce Plc | Gas turbine engine internal air system |
RU2158841C2 (ru) * | 1999-01-21 | 2000-11-10 | Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" | Камера жидкостного ракетного двигателя и ее корпус |
US6925809B2 (en) | 1999-02-26 | 2005-08-09 | R. Jan Mowill | Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities |
DE19912365A1 (de) | 1999-03-19 | 2000-09-21 | Roche Diagnostics Gmbh | Mehrschichtiges analytisches Hilfsmittel |
US6037684A (en) | 1999-04-28 | 2000-03-14 | Campbell Haufeld/Scott Fetzer Company | HVLP motor assembly |
GB9926257D0 (en) | 1999-11-06 | 2000-01-12 | Rolls Royce Plc | Wall elements for gas turbine engine combustors |
US6267106B1 (en) | 1999-11-09 | 2001-07-31 | Caterpillar Inc. | Induction venturi for an exhaust gas recirculation system in an internal combustion engine |
DE10019437A1 (de) | 2000-04-19 | 2001-12-20 | Rolls Royce Deutschland | Verfahren und Vorrichtung zum Kühlen der Gehäuse von Turbinen von Strahltriebwerken |
US6446438B1 (en) | 2000-06-28 | 2002-09-10 | Power Systems Mfg., Llc | Combustion chamber/venturi cooling for a low NOx emission combustor |
WO2003093664A1 (en) * | 2000-06-28 | 2003-11-13 | Power Systems Mfg. Llc | Combustion chamber/venturi cooling for a low nox emission combustor |
US6374594B1 (en) | 2000-07-12 | 2002-04-23 | Power Systems Mfg., Llc | Silo/can-annular low emissions combustor |
US6427446B1 (en) | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
US6672570B2 (en) | 2000-11-17 | 2004-01-06 | Walbro Japan, Inc. | Variable venturi carburetor |
US6536201B2 (en) | 2000-12-11 | 2003-03-25 | Pratt & Whitney Canada Corp. | Combustor turbine successive dual cooling |
US6698924B2 (en) | 2000-12-21 | 2004-03-02 | Tank, Inc. | Cooling system comprising a circular venturi |
US6623160B2 (en) | 2000-12-21 | 2003-09-23 | Mccarthy, Jr. Joseph H. | Method and system for cooling heat-generating component in a closed-loop system |
US6430932B1 (en) | 2001-07-19 | 2002-08-13 | Power Systems Mfg., Llc | Low NOx combustion liner with cooling air plenum recesses |
FR2836986B1 (fr) | 2002-03-07 | 2004-11-19 | Snecma Moteurs | Systeme d'injection multi-modes d'un melange air/carburant dans une chambre de combustion |
US6705088B2 (en) | 2002-04-05 | 2004-03-16 | Power Systems Mfg, Llc | Advanced crossfire tube cooling scheme for gas turbine combustors |
US6832482B2 (en) | 2002-06-25 | 2004-12-21 | Power Systems Mfg, Llc | Pressure ram device on a gas turbine combustor |
US6772595B2 (en) | 2002-06-25 | 2004-08-10 | Power Systems Mfg., Llc | Advanced cooling configuration for a low emissions combustor venturi |
US6898937B2 (en) | 2002-07-15 | 2005-05-31 | Power Systems Mfg., Llc | Gas only fin mixer secondary fuel nozzle |
US6675581B1 (en) | 2002-07-15 | 2004-01-13 | Power Systems Mfg, Llc | Fully premixed secondary fuel nozzle |
US6691516B2 (en) | 2002-07-15 | 2004-02-17 | Power Systems Mfg, Llc | Fully premixed secondary fuel nozzle with improved stability |
US7290394B2 (en) | 2002-11-21 | 2007-11-06 | Parker-Hannifin Corporation | Fuel injector flexible feed with moveable nozzle tip |
US6969230B2 (en) | 2002-12-17 | 2005-11-29 | General Electric Company | Venturi outlet turbine airfoil |
US6865892B2 (en) * | 2002-12-17 | 2005-03-15 | Power Systems Mfg, Llc | Combustion chamber/venturi configuration and assembly method |
EP1601864B1 (en) | 2003-02-24 | 2010-07-07 | Pratt & Whitney Canada Corp. | Integral cooling system for rotary engine |
US6912838B2 (en) | 2003-03-06 | 2005-07-05 | Power Systems Mfg, Llc | Coated crossfire tube assembly |
US6981846B2 (en) | 2003-03-12 | 2006-01-03 | Florida Turbine Technologies, Inc. | Vortex cooling of turbine blades |
US6935116B2 (en) | 2003-04-28 | 2005-08-30 | Power Systems Mfg., Llc | Flamesheet combustor |
US6986254B2 (en) | 2003-05-14 | 2006-01-17 | Power Systems Mfg, Llc | Method of operating a flamesheet combustor |
US7051524B1 (en) | 2003-06-30 | 2006-05-30 | Bernard A Kraft | Venturi device |
JP4040556B2 (ja) | 2003-09-04 | 2008-01-30 | 株式会社日立製作所 | ガスタービン設備及び冷却空気供給方法 |
US7021892B2 (en) | 2003-11-19 | 2006-04-04 | Massachusetts Institute Of Technology | Method for assembling gas turbine engine components |
US7096668B2 (en) | 2003-12-22 | 2006-08-29 | Martling Vincent C | Cooling and sealing design for a gas turbine combustion system |
US7082770B2 (en) | 2003-12-24 | 2006-08-01 | Martling Vincent C | Flow sleeve for a low NOx combustor |
US6951109B2 (en) | 2004-01-06 | 2005-10-04 | General Electric Company | Apparatus and methods for minimizing and/or eliminating dilution air leakage in a combustion liner assembly |
JP4495603B2 (ja) | 2004-01-15 | 2010-07-07 | 株式会社日立製作所 | ガスタービン発電装置およびそれに用いる消音装置 |
US7127899B2 (en) | 2004-02-26 | 2006-10-31 | United Technologies Corporation | Non-swirl dry low NOx (DLN) combustor |
US7013649B2 (en) | 2004-05-25 | 2006-03-21 | General Electric Company | Gas turbine engine combustor mixer |
US7007482B2 (en) | 2004-05-28 | 2006-03-07 | Power Systems Mfg., Llc | Combustion liner seal with heat transfer augmentation |
US7152410B2 (en) | 2004-06-10 | 2006-12-26 | Honeywell International, Inc. | System and method for dumping surge flow into eductor primary nozzle for free turbine |
US6983600B1 (en) | 2004-06-30 | 2006-01-10 | General Electric Company | Multi-venturi tube fuel injector for gas turbine combustors |
US7003958B2 (en) | 2004-06-30 | 2006-02-28 | General Electric Company | Multi-sided diffuser for a venturi in a fuel injector for a gas turbine |
WO2006008221A1 (de) | 2004-07-19 | 2006-01-26 | Alstom Technology Ltd | Verfahren zum betrieb einer gasturbogruppe |
US7153488B2 (en) | 2004-08-03 | 2006-12-26 | Millennium Inorganic Chemicals, Inc. | Suppression of the formation of noxious substances during chloride processes |
US20060042257A1 (en) | 2004-08-27 | 2006-03-02 | Pratt & Whitney Canada Corp. | Combustor heat shield and method of cooling |
US7237384B2 (en) | 2005-01-26 | 2007-07-03 | Peter Stuttaford | Counter swirl shear mixer |
US7389643B2 (en) * | 2005-01-31 | 2008-06-24 | General Electric Company | Inboard radial dump venturi for combustion chamber of a gas turbine |
US7677025B2 (en) | 2005-02-01 | 2010-03-16 | Power Systems Mfg., Llc | Self-purging pilot fuel injection system |
US7386980B2 (en) | 2005-02-02 | 2008-06-17 | Power Systems Mfg., Llc | Combustion liner with enhanced heat transfer |
US7513115B2 (en) | 2005-05-23 | 2009-04-07 | Power Systems Mfg., Llc | Flashback suppression system for a gas turbine combustor |
US7451600B2 (en) | 2005-07-06 | 2008-11-18 | Pratt & Whitney Canada Corp. | Gas turbine engine combustor with improved cooling |
CN1932316B (zh) | 2005-09-16 | 2010-09-29 | 深圳富泰宏精密工业有限公司 | 多段式转轴结构 |
US7559203B2 (en) | 2005-09-16 | 2009-07-14 | Pratt & Whitney Canada Corp. | Cooled support boss for a combustor in a gas turbine engine |
US7546737B2 (en) | 2006-01-24 | 2009-06-16 | Honeywell International Inc. | Segmented effusion cooled gas turbine engine combustor |
FR2897107B1 (fr) | 2006-02-09 | 2013-01-18 | Snecma | Paroi transversale de chambre de combustion munie de trous de multiperforation |
US7770395B2 (en) | 2006-02-27 | 2010-08-10 | Mitsubishi Heavy Industries, Ltd. | Combustor |
US7624577B2 (en) | 2006-03-31 | 2009-12-01 | Pratt & Whitney Canada Corp. | Gas turbine engine combustor with improved cooling |
US8109098B2 (en) | 2006-05-04 | 2012-02-07 | Siemens Energy, Inc. | Combustor liner for gas turbine engine |
US7669411B2 (en) | 2006-05-10 | 2010-03-02 | Caterpillar Inc. | Cooling device |
FR2904048B1 (fr) | 2006-07-19 | 2012-12-14 | Snecma | Systeme de ventilation de paroi de chambre de combustion dans une turbomachine |
US7631503B2 (en) | 2006-09-12 | 2009-12-15 | Pratt & Whitney Canada Corp. | Combustor with enhanced cooling access |
US8182199B2 (en) | 2007-02-01 | 2012-05-22 | Pratt & Whitney Canada Corp. | Turbine shroud cooling system |
US20090019854A1 (en) | 2007-07-16 | 2009-01-22 | General Electric Company | APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTOR |
-
2009
- 2009-01-21 US US12/357,029 patent/US7712314B1/en active Active
- 2009-04-01 EP EP09004835.6A patent/EP2211104B1/en active Active
- 2009-04-02 CA CA2661248A patent/CA2661248C/en active Active
- 2009-04-02 SG SG200902292-2A patent/SG163466A1/en unknown
- 2009-04-02 SG SG2011091501A patent/SG177888A1/en unknown
- 2009-04-08 AU AU2009201420A patent/AU2009201420B8/en active Active
- 2009-04-22 MX MX2009004301A patent/MX2009004301A/es active IP Right Grant
- 2009-04-28 JP JP2009110007A patent/JP4933578B2/ja active Active
- 2009-05-05 CN CN2009101359487A patent/CN101782232B/zh active Active
- 2009-05-05 AR ARP090101612A patent/AR072358A1/es active IP Right Grant
- 2009-05-07 IL IL198653A patent/IL198653A/en active IP Right Grant
- 2009-05-07 BR BRPI0901605-8A patent/BRPI0901605A2/pt not_active Application Discontinuation
- 2009-05-07 CL CL2009001101A patent/CL2009001101A1/es unknown
- 2009-05-07 MY MYPI20091855A patent/MY149412A/en unknown
- 2009-05-08 KR KR1020090040209A patent/KR101131646B1/ko active IP Right Grant
- 2009-05-11 TW TW098115593A patent/TWI376484B/zh active
- 2009-05-11 TW TW101113646A patent/TWI452242B/zh active
- 2009-08-06 US US12/536,861 patent/US7707836B1/en active Active
-
2010
- 2010-12-23 HK HK10112048.5A patent/HK1146108A1/xx unknown
-
2013
- 2013-10-04 AR ARP130103609A patent/AR092910A2/es active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP2211104B1 (en) | 2017-06-14 |
US7707836B1 (en) | 2010-05-04 |
JP4933578B2 (ja) | 2012-05-16 |
EP2211104A2 (en) | 2010-07-28 |
TWI376484B (en) | 2012-11-11 |
TW201028622A (en) | 2010-08-01 |
SG163466A1 (en) | 2010-08-30 |
MY149412A (en) | 2013-08-30 |
CN101782232A (zh) | 2010-07-21 |
JP2010169076A (ja) | 2010-08-05 |
TW201241369A (en) | 2012-10-16 |
HK1146108A1 (en) | 2011-05-13 |
US7712314B1 (en) | 2010-05-11 |
SG177888A1 (en) | 2012-02-28 |
KR20100085810A (ko) | 2010-07-29 |
MX2009004301A (es) | 2010-07-20 |
AU2009201420B8 (en) | 2011-02-17 |
EP2211104A3 (en) | 2014-08-06 |
AU2009201420A1 (en) | 2010-08-05 |
CN101782232B (zh) | 2012-11-28 |
KR101131646B1 (ko) | 2012-03-28 |
IL198653A (en) | 2013-01-31 |
CL2009001101A1 (es) | 2011-08-19 |
IL198653A0 (en) | 2010-02-17 |
CA2661248C (en) | 2011-02-08 |
AU2009201420B2 (en) | 2011-01-27 |
CA2661248A1 (en) | 2010-07-21 |
TWI452242B (zh) | 2014-09-11 |
BRPI0901605A2 (pt) | 2010-12-21 |
AR092910A2 (es) | 2015-05-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AR072358A1 (es) | Sistema de refrigeracion mediante un venturi | |
AR090511A1 (es) | Conjunto de combustor de turbomaquina | |
CL2010000876A1 (es) | Sistema y metodo que mejora la eficacia y eficiencia del lavado del interior de un compresor de turbina que tiene una admision y una pluralidad de alabes, que comprende: una bomba de suministro de fuido, una pluralidad de lineas de fluido, una pluralidad de juegos de boquillas, y una pluralidad de valvulas de control dispuestas entre la bomba y el correspondiente juego de boquillas. | |
BR112014022049B8 (pt) | Turbina a gás aeroderivativa e método para destravar um rotor em uma turbina a gás | |
CO6180472A2 (es) | Conjunto de motores de gas-viento y vehiculo de motor que comprende el mismo | |
JP2014206162A5 (es) | ||
WO2009041435A1 (ja) | ガスタービン燃焼器の冷却構造 | |
RU2014133525A (ru) | Горелочное устройство и способ работы горелочного устройства | |
AR094836A1 (es) | Quemador-reactor de vacío y mezcla de combustibles | |
WO2014189589A3 (en) | Gas turbine engine with soft mounted pre-swirl nozzle | |
CL2013001147A1 (es) | Dispositivo para la inyeccion de amoniaco instalado en un gasoducto de escape a traves del cual fluye un gas de escape generado en una camara de combustion y configurado para inyectar amoniaco al gas de escape, donde dicho dispositivo comprende una pluralidad de tuberias para la inyeccion de amoniaco, en donde una pluralidad de tubos de tobera se instalan en una tuberia para la inyeccion de amoniaco en una direccion longitudinal, y donde ademas en los tubos de tobera se forman paneles difusores. | |
WO2015130380A3 (en) | Blade outer air seal cooling passage | |
RU2013108923A (ru) | Узел задней рамы переходного элемента и система сжигания топлива | |
WO2014114652A3 (en) | Gas turbine outer case active ambient cooling including air exhaust into a sub-ambient region of exhaust flow | |
CO6680661A2 (es) | Aparato y método para curar por calor revestimientos de tuberias | |
BR102016013592A8 (pt) | motor de turbina a gás | |
RU2009107639A (ru) | Турбореактивный двигатель | |
MY184256A (en) | Centrifugal compressor and water chilling unit having the same | |
RU2016126693A (ru) | Способ и устройство охлаждения вала авиационного газотурбинного двигателя | |
AR093323A1 (es) | Sistema y metodo para la combustion por difusion en un sistema de turbina de gas con recirculacion de gases de escape estequiometrico | |
CN201779383U (zh) | 防回火软管接头 | |
ECSP11010769A (es) | Quemador de gas para hornos | |
AR093322A1 (es) | Sistema y metodo para la combustion por difusion con una mezcla de combustible-diluyente en un sistema de turbina de gas con recirculacion de gases de escape estequiometrico | |
AR093325A1 (es) | Sistema y metodo para la combustion por difusion con una mezcla de oxidante-diluyente en un sistema de turbina de gas con recirculacion de gases de escape estequiometrico | |
CL2013003295A1 (es) | Quemador de gas con al menos dos difusores de llamas, con una camara de difusion para una mezcla primaria aire/gas, un conducto de encendido cruzado definiendo una primera y segunda region con paredes laterales y una pared superior con un agujero, donde el conducto comprende una abertura inferior enfrentando la pared superior. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant, registration |