CL2009001406A1 - Corredera para entrega de fluido para un sistema de aumento de potencia de una turbina a gas, para humedecer la toma de aire, que comprende; una o mas etapas que tiene una valvula de pre llenado y una valvula principal, donde el fluido es presurizado y descargado; sistema de aumento de potencia; y metodo para inyectar fluido desde la corredera. - Google Patents
Corredera para entrega de fluido para un sistema de aumento de potencia de una turbina a gas, para humedecer la toma de aire, que comprende; una o mas etapas que tiene una valvula de pre llenado y una valvula principal, donde el fluido es presurizado y descargado; sistema de aumento de potencia; y metodo para inyectar fluido desde la corredera.Info
- Publication number
- CL2009001406A1 CL2009001406A1 CL2009001406A CL2009001406A CL2009001406A1 CL 2009001406 A1 CL2009001406 A1 CL 2009001406A1 CL 2009001406 A CL2009001406 A CL 2009001406A CL 2009001406 A CL2009001406 A CL 2009001406A CL 2009001406 A1 CL2009001406 A1 CL 2009001406A1
- Authority
- CL
- Chile
- Prior art keywords
- fluid
- slide
- valve
- stages
- power increase
- Prior art date
Links
Classifications
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- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
-
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/057—Control or regulation
-
- 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
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
- F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
-
- 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
-
- 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
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
- F02C7/1435—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages by water injection
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/16—Control of working fluid flow
Landscapes
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Jet Pumps And Other Pumps (AREA)
- Control Of Non-Positive-Displacement Pumps (AREA)
- Regulating Braking Force (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
- Flow Control (AREA)
- Details Of Reciprocating Pumps (AREA)
- Reciprocating Pumps (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
CORREDERA O PATÍN PARA ENTREGA DE FLUIDO 10 ADAPTADA PARA AUMENTAR LA POTENCIA CON UN SISTEMA DE PRE-LLENADO 100 DESTINADO A SUMINISTRAR FLUIDO DE ALTA PRESIÓN, QUE TIENE UNA O MÁS ETAPAS 160 E INCLUYE UNA VÁLVULA DE PRE LLENADO 140 Y UNA VÁLVULA PRINCIPAL 120, CADA UNA DE LAS CUALES TIENE UNA POSICIÓN ABIERTA Y CERRADA. LAS ETAPAS 160 TIENEN UN ESTADO O CONDICIÓN ACTIVA E INACTIVA A FIN DE SUMINISTRAR UNA VELOCIDAD DESEADA DEL FLUJO DE FLUIDO A UN APARATO 225 DISEÑADO PARA LA DISTRIBUCIÓN DE FLUIDOS. EN UNA CONDICIÓN ACTIVA, EL FLUIDO ES RECIBIDO EN LA ETAPA 160 Y PRESURIZADO CON LA VÁLVULA DE PRE LLENADO 140 ABIERTA Y LA VÁLVULA PRINCIPAL 120 CERRADA. ADEMÁS, EN LA CONDICIÓN ACTIVA, EL FLUIDO ES LIBERADO AL ESTAR LA VÁLVULA DE PRE LLENADO 140 CERRADA Y LA VÁLVULA PRINCIPAL 120 ABIERTA. EN LA CONDICIÓN INACTIVA, AL MENOS LA VÁLVULA PRINCIPAL 120 ESTÁ CERRADA. UNA UNIDAD DE CONTROL 210 SE CONECTA CON UNA UNIDAD DE BOMBA 110 Y CONTROLA LA OPERACIÓN DE LA BOMBA 110 PARA REGULAR LAS ETAPAS 160 DE SUMINISTRO DE PRESIÓN A UN NIVEL DETERMINADO, A FIN DE ALCANZAR LA VELOCIDAD DE FLUJO DESEADA. ADEMÁS, UN SISTEMA DE AUMENTO DE POTENCIA 200 PARA PROVEER FLUIDO DE ALTA PRESIÓN QUE COMPRENDE LA CORREDERA DE ENTREGA DE FLUIDO 10 ES PROVISTO ADEMÁS DE UN MÉTODO PARA INYECTAR FLUIDO DE ALTA PRESIÓN DESDE LA CORREDERA DE ENTREGA DE FLUIDO 10 A UN APARATO DE INYECCIÓN 225.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/143,254 US7647777B2 (en) | 2008-06-20 | 2008-06-20 | Skid architecture for a power augmentation system |
Publications (1)
Publication Number | Publication Date |
---|---|
CL2009001406A1 true CL2009001406A1 (es) | 2010-11-12 |
Family
ID=40779530
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CL2009001406A CL2009001406A1 (es) | 2008-06-20 | 2009-06-12 | Corredera para entrega de fluido para un sistema de aumento de potencia de una turbina a gas, para humedecer la toma de aire, que comprende; una o mas etapas que tiene una valvula de pre llenado y una valvula principal, donde el fluido es presurizado y descargado; sistema de aumento de potencia; y metodo para inyectar fluido desde la corredera. |
Country Status (16)
Country | Link |
---|---|
US (1) | US7647777B2 (es) |
EP (1) | EP2136051B1 (es) |
JP (2) | JP4922348B2 (es) |
KR (1) | KR101141824B1 (es) |
CN (1) | CN101608576B (es) |
AR (1) | AR072255A1 (es) |
AU (1) | AU2009201880B2 (es) |
BR (1) | BRPI0902078A2 (es) |
CA (1) | CA2665329C (es) |
CL (1) | CL2009001406A1 (es) |
IL (1) | IL199109A (es) |
MX (1) | MX2009006412A (es) |
MY (1) | MY147076A (es) |
RU (1) | RU2425994C2 (es) |
SG (1) | SG158009A1 (es) |
TW (1) | TWI367281B (es) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
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JP5554104B2 (ja) * | 2010-03-24 | 2014-07-23 | 三菱重工業株式会社 | 吸気システム、これを備えたガスタービンおよびこれを備えた発電プラント |
JP5422456B2 (ja) * | 2010-03-24 | 2014-02-19 | 三菱重工業株式会社 | 吸気システム、これを備えたガスタービンおよびこれを備えた発電プラント |
JP5818510B2 (ja) * | 2011-05-24 | 2015-11-18 | 株式会社東芝 | ガスタービン吸気冷却装置及び方法 |
US9086019B2 (en) | 2012-07-02 | 2015-07-21 | United Technologies Corporation | Turbomachine thermal energy exchange |
EP3336332A1 (en) * | 2012-11-06 | 2018-06-20 | Al Mahmood, Fuad | Process of reducing the load consumed by a gas turbine compressor and maximizing turbine mass flow |
JP5831486B2 (ja) * | 2013-03-29 | 2015-12-09 | トヨタ自動車株式会社 | ブレーキシステム |
DE102013208320A1 (de) * | 2013-05-07 | 2014-11-13 | Deere & Company | Verfahren zur Bestimmung eines Kontrollparameters eines Leistungs- oder Drehmomentverteilungsreglers für einen Hybridantrieb einer Arbeitsmaschine |
DE102013216083A1 (de) * | 2013-08-14 | 2015-02-19 | ES Vertrieb und Service GmbH | Luftbefeuchtungsanordnung und Verfahren zum Befeuchten eines Luftstroms |
US9850816B2 (en) * | 2013-11-04 | 2017-12-26 | General Electric Company | Gas turbine inlet system and related method for cooling gas turbine inlet air |
FR3013073B1 (fr) * | 2013-11-08 | 2016-01-15 | Continental Automotive France | Procede permettant de determiner si un injecteur est dans un etat bloque |
DE102015206918A1 (de) | 2014-06-13 | 2015-12-17 | Ford Global Technologies, Llc | Verfahren zum Betrieb eines elektromechanischen Fahrzeugbremssystems |
DE102014211380B4 (de) | 2014-06-13 | 2021-08-05 | Ford Global Technologies, Llc | Verfahren zum Betrieb eines elektromechanischen Fahrzeugbremssystems |
DE102015207636B4 (de) * | 2014-06-13 | 2021-11-18 | Ford Global Technologies, Llc | Verfahren zum Betrieb eines elektromechanischen Fahrzeugbremssystems |
US10557413B1 (en) * | 2014-11-26 | 2020-02-11 | Caldwell Tanks, Inc. | Systems and methods for controlling liquid flow to a turbine fogging array |
US9527585B2 (en) * | 2014-12-11 | 2016-12-27 | Bell Helicopter Textron Inc. | Aircraft ground steering system |
US20170370286A1 (en) * | 2016-06-22 | 2017-12-28 | General Electric Company | Systems and Methods for Variable Water Injection Flow Control |
CN110091588B (zh) * | 2018-12-13 | 2024-06-04 | 株洲三新包装技术有限公司 | 一种两端向内喷水清理的刮墨腔 |
Family Cites Families (19)
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FR1217588A (fr) * | 1959-02-27 | 1960-05-04 | Nord Aviat | Dispositif de préremplissage adapté au circuit d'alimentation en combustible d'un statoréacteur |
US3976661A (en) | 1971-11-23 | 1976-08-24 | Eastman Kodak Company | Pyrrolo hemioxonol |
GB9025778D0 (en) * | 1990-11-27 | 1991-01-09 | Rolls Royce Plc | Improvements in or relating to gas generators |
US5170622A (en) * | 1991-04-02 | 1992-12-15 | Cheng Dah Y | Advanced regenerative parallel compound dual fluid heat engine Advanced Cheng Cycle (ACC) |
US5784875A (en) * | 1995-11-27 | 1998-07-28 | Innovative Control Systems, Inc. | Water injection into a gas turbine using purge air |
US5867977A (en) * | 1996-05-14 | 1999-02-09 | The Dow Chemical Company | Method and apparatus for achieving power augmentation in gas turbines via wet compression |
DE59710054D1 (de) * | 1997-11-10 | 2003-06-12 | Alstom Switzerland Ltd | Verfahren zur Überwachung des Versorgungssystems einer Gasturbine mit Mehrbrennersystem sowie Vorrichtung zur Durchführung des Verfahrens |
GB2333805B (en) * | 1998-01-30 | 2001-09-19 | Speciality Chemical Holdings L | Cleaning method and apparatus |
US6718771B1 (en) | 1999-09-03 | 2004-04-13 | Enhanced Turbine Output Holding Llc | Gas turbine operative at high ambient temperatures |
US6398518B1 (en) | 2000-03-29 | 2002-06-04 | Watson Cogeneration Company | Method and apparatus for increasing the efficiency of a multi-stage compressor |
US6553768B1 (en) * | 2000-11-01 | 2003-04-29 | General Electric Company | Combined water-wash and wet-compression system for a gas turbine compressor and related method |
US6478289B1 (en) * | 2000-11-06 | 2002-11-12 | General Electric Company | Apparatus and methods for controlling the supply of water mist to a gas-turbine compressor |
WO2003089770A1 (en) * | 2002-04-15 | 2003-10-30 | Mee Industries, Inc. | Water injection for gas turbine inlet air |
ITMI20031245A1 (it) * | 2003-06-19 | 2004-12-20 | Edoardo Lossa S P A | Sistema di trattamento e messa in pressione d'acqua per il raffreddamento adiabatico d'aria comburente |
US6938425B2 (en) * | 2003-08-11 | 2005-09-06 | Siemens Westinghouse Power Corporation | System and method for controlling water injection in a turbine engine |
DE102004004135A1 (de) * | 2004-01-28 | 2005-09-29 | Alstom Technology Ltd | Fördervorrichtung |
US7428818B2 (en) * | 2005-09-13 | 2008-09-30 | Gas Turbine Efficiency Ab | System and method for augmenting power output from a gas turbine engine |
US7487642B2 (en) * | 2005-11-01 | 2009-02-10 | General Electric Comapny | Methods and apparatus for operating gas turbine engines |
US7703272B2 (en) * | 2006-09-11 | 2010-04-27 | Gas Turbine Efficiency Sweden Ab | System and method for augmenting turbine power output |
-
2008
- 2008-06-20 US US12/143,254 patent/US7647777B2/en active Active
-
2009
- 2009-05-06 CA CA2665329A patent/CA2665329C/en not_active Expired - Fee Related
- 2009-05-12 SG SG200903245-9A patent/SG158009A1/en unknown
- 2009-05-12 AU AU2009201880A patent/AU2009201880B2/en not_active Ceased
- 2009-05-22 EP EP09006909.7A patent/EP2136051B1/en not_active Not-in-force
- 2009-05-27 CN CN2009101452170A patent/CN101608576B/zh not_active Expired - Fee Related
- 2009-05-28 AR ARP090101907A patent/AR072255A1/es active IP Right Grant
- 2009-06-02 IL IL199109A patent/IL199109A/en not_active IP Right Cessation
- 2009-06-12 CL CL2009001406A patent/CL2009001406A1/es unknown
- 2009-06-15 TW TW098119974A patent/TWI367281B/zh not_active IP Right Cessation
- 2009-06-15 MX MX2009006412A patent/MX2009006412A/es active IP Right Grant
- 2009-06-18 MY MYPI20092528A patent/MY147076A/en unknown
- 2009-06-19 KR KR1020090054913A patent/KR101141824B1/ko active IP Right Grant
- 2009-06-19 RU RU2009123447/06A patent/RU2425994C2/ru not_active IP Right Cessation
- 2009-06-19 BR BRPI0902078-0A patent/BRPI0902078A2/pt not_active Application Discontinuation
- 2009-06-19 JP JP2009146845A patent/JP4922348B2/ja not_active Expired - Fee Related
-
2011
- 2011-09-26 JP JP2011209073A patent/JP5400117B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US20090314256A1 (en) | 2009-12-24 |
EP2136051A3 (en) | 2010-12-22 |
BRPI0902078A2 (pt) | 2010-05-18 |
KR20090132549A (ko) | 2009-12-30 |
KR101141824B1 (ko) | 2012-05-07 |
AR072255A1 (es) | 2010-08-18 |
AU2009201880B2 (en) | 2012-06-14 |
EP2136051A2 (en) | 2009-12-23 |
JP2011256880A (ja) | 2011-12-22 |
JP5400117B2 (ja) | 2014-01-29 |
US7647777B2 (en) | 2010-01-19 |
CA2665329C (en) | 2013-10-22 |
MX2009006412A (es) | 2010-01-15 |
CA2665329A1 (en) | 2009-12-20 |
RU2425994C2 (ru) | 2011-08-10 |
JP4922348B2 (ja) | 2012-04-25 |
TW201016952A (en) | 2010-05-01 |
SG158009A1 (en) | 2010-01-29 |
MY147076A (en) | 2012-10-31 |
CN101608576A (zh) | 2009-12-23 |
JP2010001893A (ja) | 2010-01-07 |
TWI367281B (en) | 2012-07-01 |
IL199109A (en) | 2012-06-28 |
IL199109A0 (en) | 2010-03-28 |
AU2009201880A1 (en) | 2010-01-14 |
EP2136051B1 (en) | 2015-11-25 |
CN101608576B (zh) | 2013-06-05 |
RU2009123447A (ru) | 2010-12-27 |
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