IT1395820B1 - Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamento - Google Patents
Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamentoInfo
- Publication number
- IT1395820B1 IT1395820B1 ITCO2009A000034A ITCO20090034A IT1395820B1 IT 1395820 B1 IT1395820 B1 IT 1395820B1 IT CO2009A000034 A ITCO2009A000034 A IT CO2009A000034A IT CO20090034 A ITCO20090034 A IT CO20090034A IT 1395820 B1 IT1395820 B1 IT 1395820B1
- Authority
- IT
- Italy
- Prior art keywords
- gas turbine
- cooling system
- functioning method
- functioning
- cooling
- Prior art date
Links
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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
-
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
- F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
-
- 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
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing 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
- F02C7/12—Cooling of 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
- F02C7/16—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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
- F05D2260/601—Fluid transfer using an ejector or a jet pump
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITCO2009A000034A IT1395820B1 (it) | 2009-09-25 | 2009-09-25 | Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamento |
CA2715169A CA2715169C (en) | 2009-09-25 | 2010-09-16 | Cooling system for a gas turbine and corresponding operation method |
CN201010298593.6A CN102032046B (zh) | 2009-09-25 | 2010-09-20 | 用于燃气涡轮机的冷却系统和对应的操作方法 |
KR1020100092267A KR101747431B1 (ko) | 2009-09-25 | 2010-09-20 | 가스 터빈의 냉각 시스템 및 대응하는 작동 방법 |
JP2010212453A JP5841321B2 (ja) | 2009-09-25 | 2010-09-22 | ガスタービン用の冷却システム及び対応する作動方法 |
EP10178721A EP2305982A1 (en) | 2009-09-25 | 2010-09-23 | Cooling and tapping system for a gas turbine engine and corresponding operation method |
US12/888,484 US8726672B2 (en) | 2009-09-25 | 2010-09-23 | Cooling system for a gas turbine and corresponding operation method |
RU2010139249/06A RU2550371C2 (ru) | 2009-09-25 | 2010-09-24 | Способ эксплуатации газовой турбины, система охлаждения газовой турбины и газовая турбина, содержащая такую систему |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITCO2009A000034A IT1395820B1 (it) | 2009-09-25 | 2009-09-25 | Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamento |
Publications (2)
Publication Number | Publication Date |
---|---|
ITCO20090034A1 ITCO20090034A1 (it) | 2011-03-26 |
IT1395820B1 true IT1395820B1 (it) | 2012-10-26 |
Family
ID=42115652
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ITCO2009A000034A IT1395820B1 (it) | 2009-09-25 | 2009-09-25 | Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamento |
Country Status (8)
Country | Link |
---|---|
US (1) | US8726672B2 (it) |
EP (1) | EP2305982A1 (it) |
JP (1) | JP5841321B2 (it) |
KR (1) | KR101747431B1 (it) |
CN (1) | CN102032046B (it) |
CA (1) | CA2715169C (it) |
IT (1) | IT1395820B1 (it) |
RU (1) | RU2550371C2 (it) |
Families Citing this family (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8267122B2 (en) * | 2009-06-30 | 2012-09-18 | Ge Aviation Systems Llc | Method and systems for bleed air supply |
JP4958967B2 (ja) * | 2009-12-15 | 2012-06-20 | 川崎重工業株式会社 | 換気構造を改良したガスタービンエンジン |
US9376933B2 (en) * | 2011-04-29 | 2016-06-28 | Leonard M. Andersen | Apparatus for distributing fluid into a gas turbine |
US9334753B2 (en) * | 2011-10-12 | 2016-05-10 | General Electric Company | Control system and methods for controlling the operation of power generation systems |
US8997498B2 (en) * | 2011-10-12 | 2015-04-07 | General Electric Company | System for use in controlling the operation of power generation systems |
US9316111B2 (en) * | 2011-12-15 | 2016-04-19 | Pratt & Whitney Canada Corp. | Active turbine tip clearance control system |
RU2623336C2 (ru) * | 2012-03-30 | 2017-06-23 | АНСАЛДО ЭНЕРДЖИА АйПи ЮКей ЛИМИТЕД | Газовая турбина с регулируемой системой воздушного охлаждения |
US9091171B2 (en) * | 2012-10-30 | 2015-07-28 | Siemens Aktiengesellschaft | Temperature control within a cavity of a turbine engine |
US8893510B2 (en) * | 2012-11-07 | 2014-11-25 | Siemens Aktiengesellschaft | Air injection system in a gas turbine engine |
US9714611B2 (en) * | 2013-02-15 | 2017-07-25 | Siemens Energy, Inc. | Heat shield manifold system for a midframe case of a gas turbine engine |
FR3007459B1 (fr) * | 2013-06-19 | 2016-10-14 | Airbus Operations Sas | Systeme et procede de mise en rotation d'un element rotatif d'un dispositif mecanique, en particulier d'une turbomachine. |
US9617921B2 (en) * | 2013-07-31 | 2017-04-11 | General Electric Company | Thermal actuator including fluid with high temperature stability |
EP3068996B1 (en) * | 2013-12-12 | 2019-01-02 | United Technologies Corporation | Multiple injector holes for gas turbine engine vane |
US9938904B2 (en) * | 2013-12-20 | 2018-04-10 | United Technologies Corporation | Method of controlling a gas turbine engine using real-time component temperature data |
JP6320063B2 (ja) * | 2014-02-03 | 2018-05-09 | 三菱日立パワーシステムズ株式会社 | ガスタービン、ガスタービンの制御装置、ガスタービンの冷却方法 |
EP3023582A1 (de) * | 2014-11-18 | 2016-05-25 | Siemens Aktiengesellschaft | Gasturbinenanlage |
KR101790146B1 (ko) * | 2015-07-14 | 2017-10-25 | 두산중공업 주식회사 | 외부 케이싱으로 우회하는 냉각공기 공급유로가 마련된 냉각시스템을 포함하는 가스터빈. |
US10731469B2 (en) * | 2016-05-16 | 2020-08-04 | Raytheon Technologies Corporation | Method and apparatus to enhance laminar flow for gas turbine engine components |
JP6639338B2 (ja) * | 2016-07-11 | 2020-02-05 | 三菱日立パワーシステムズ株式会社 | ガスタービン及びガスタービンの運転方法 |
US10961911B2 (en) * | 2017-01-17 | 2021-03-30 | Raytheon Technologies Corporation | Injection cooled cooling air system for a gas turbine engine |
FR3062677B1 (fr) * | 2017-02-07 | 2019-12-13 | Safran Aircraft Engines | Turboreacteur a double flux comprenant un distributeur precedant deux etages de turbines basse pression qui sont ventiles par de l'air de refroidissement du distributeur |
US11739697B2 (en) * | 2017-05-22 | 2023-08-29 | Raytheon Technologies Corporation | Bleed flow safety system |
GB201714293D0 (en) * | 2017-09-06 | 2017-10-18 | Rolls Royce Plc | Heat exchange systems for turbomachines |
FR3072414B1 (fr) * | 2017-10-16 | 2019-11-01 | Safran Aircraft Engines | Dispositif et procede de refroidissement d'une turbine basse pression dans une turbomachine |
US20190186269A1 (en) * | 2017-12-14 | 2019-06-20 | Rolls-Royce Corporation | Modulated Cooling Air Control System and Method for a Turbine Engine |
DE102018211907A1 (de) * | 2018-07-17 | 2020-01-23 | Rolls-Royce Deutschland Ltd & Co Kg | Luftversorgungssystem für ein Luftfahrzeug |
US10753208B2 (en) | 2018-11-30 | 2020-08-25 | General Electric Company | Airfoils including plurality of nozzles and venturi |
US10815828B2 (en) | 2018-11-30 | 2020-10-27 | General Electric Company | Hot gas path components including plurality of nozzles and venturi |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1348127A (en) * | 1971-04-19 | 1974-03-13 | Secr Defence | Gas turbine engine |
EP0062932B1 (de) | 1981-04-03 | 1984-12-05 | BBC Aktiengesellschaft Brown, Boveri & Cie. | Kombiniertes Gas-Dampfturbinen-Kraftwerk |
JPS6445926A (en) | 1987-08-13 | 1989-02-20 | Toshiba Corp | Cooling method for gas turbine |
US5579631A (en) | 1994-04-28 | 1996-12-03 | Westinghouse Electric Corporation | Steam cooling of gas turbine with backup air cooling |
DE59912179D1 (de) | 1998-10-20 | 2005-07-21 | Alstom Technology Ltd Baden | Turbomaschine und Verfahren zum Betrieb derselben |
EP1028230B2 (de) | 1999-02-09 | 2008-09-03 | ALSTOM (Switzerland) Ltd | Gekühlte Gasturbinenkomponente mit verstellbarer Kühlung |
DE19907907A1 (de) | 1999-02-24 | 2000-08-31 | Abb Alstom Power Ch Ag | Mehrstufiger Turboverdichter |
US6615574B1 (en) * | 2000-01-14 | 2003-09-09 | General Electric Co. | System for combining flow from compressor bleeds of an industrial gas turbine for gas turbine performance optimization |
RU2186233C1 (ru) * | 2000-11-23 | 2002-07-27 | Гойхенберг Михаил Михайлович | Газотурбинный двигатель |
US6550253B2 (en) * | 2001-09-12 | 2003-04-22 | General Electric Company | Apparatus and methods for controlling flow in turbomachinery |
US6640550B2 (en) | 2001-11-02 | 2003-11-04 | Alstom (Switzerland) Ltd | Gas turbo-group with cooling air system |
US6644012B2 (en) * | 2001-11-02 | 2003-11-11 | Alston (Switzerland) Ltd | Gas turbine set |
RU2217597C1 (ru) * | 2002-11-28 | 2003-11-27 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Газотурбинный двигатель |
RU2236609C1 (ru) * | 2003-02-20 | 2004-09-20 | Открытое акционерное общество "Научно-производственное объединение "Сатурн" | Газотурбинный двигатель |
US6983602B2 (en) | 2004-04-21 | 2006-01-10 | General Electric Company | Ejector cooled nozzle |
US7980054B2 (en) | 2004-12-01 | 2011-07-19 | United Technologies Corporation | Ejector cooling of outer case for tip turbine engine |
US7536864B2 (en) * | 2005-12-07 | 2009-05-26 | General Electric Company | Variable motive nozzle ejector for use with turbine engines |
US7861536B2 (en) * | 2006-03-27 | 2011-01-04 | Pratt & Whitney Canada Corp. | Ejector controlled twin air source gas turbine pressurizing air system |
US8057157B2 (en) * | 2007-10-22 | 2011-11-15 | General Electric Company | System for delivering air from a multi-stage compressor to a turbine portion of a gas turbine engine |
US20090205310A1 (en) * | 2008-02-20 | 2009-08-20 | General Electric Company | Power generation system having an exhaust gas attemperating device and system for controlling a temperature of exhaust gases |
US8240153B2 (en) * | 2008-05-14 | 2012-08-14 | General Electric Company | Method and system for controlling a set point for extracting air from a compressor to provide turbine cooling air in a gas turbine |
JP5297114B2 (ja) | 2008-08-06 | 2013-09-25 | 三菱重工業株式会社 | ガスタービン |
US8355854B2 (en) * | 2009-05-08 | 2013-01-15 | General Electric Company | Methods relating to gas turbine control and operation |
-
2009
- 2009-09-25 IT ITCO2009A000034A patent/IT1395820B1/it active
-
2010
- 2010-09-16 CA CA2715169A patent/CA2715169C/en not_active Expired - Fee Related
- 2010-09-20 KR KR1020100092267A patent/KR101747431B1/ko active IP Right Grant
- 2010-09-20 CN CN201010298593.6A patent/CN102032046B/zh active Active
- 2010-09-22 JP JP2010212453A patent/JP5841321B2/ja active Active
- 2010-09-23 US US12/888,484 patent/US8726672B2/en active Active
- 2010-09-23 EP EP10178721A patent/EP2305982A1/en not_active Ceased
- 2010-09-24 RU RU2010139249/06A patent/RU2550371C2/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CN102032046B (zh) | 2015-11-25 |
RU2010139249A (ru) | 2012-03-27 |
ITCO20090034A1 (it) | 2011-03-26 |
JP2011069368A (ja) | 2011-04-07 |
KR101747431B1 (ko) | 2017-06-14 |
US8726672B2 (en) | 2014-05-20 |
JP5841321B2 (ja) | 2016-01-13 |
CN102032046A (zh) | 2011-04-27 |
EP2305982A1 (en) | 2011-04-06 |
KR20110033793A (ko) | 2011-03-31 |
CA2715169A1 (en) | 2011-03-25 |
RU2550371C2 (ru) | 2015-05-10 |
US20110072827A1 (en) | 2011-03-31 |
CA2715169C (en) | 2018-06-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT1395820B1 (it) | Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamento | |
BR112012000888A2 (pt) | sistema e método para iniciar um sistema operacional multiambiente | |
BRPI1007723A2 (pt) | sistema de armazenamento e conversão de turbina a gás | |
BRPI1009314A2 (pt) | sistema e método para armazenar e liberar energia | |
BR112012015293A2 (pt) | sistema vedante para um compressor centrífugo, método para reduzir o fluxo de vazamento e compressor centrífugo | |
BRPI1016218A2 (pt) | sistema, e, método | |
BRPI1013630A2 (pt) | sistema, e método | |
BRPI1014894A2 (pt) | método, e sistema | |
BRPI1012144A2 (pt) | sistema e método para controlar uma turbina eólica | |
DK2292928T3 (da) | Fremgangsmåder og systemer til vindmøllestyring | |
BR112012001960A2 (pt) | turbina de recuperação de energia de gás de exaustão para um sistema turbocomposto. | |
BRPI1015978A2 (pt) | método, sistema, e, fluxímetro | |
BRPI0823414A2 (pt) | método para embalar e sistemas de embalagem para três pás de aerogeradores | |
BR112012015294A2 (pt) | sistema de termopar, compressor e método | |
BRPI0924433A2 (pt) | método de operação para um sistema de pós-tratamento de exaustão e sistema de pós-tratamento de exaustão | |
BRPI0918769A2 (pt) | sistema para melhoria de performance de turbina a gás em uma usina a gás natural | |
IT1395110B1 (it) | Aerostato autostabile perfezionato e relativo sistema di involo e di recupero | |
BRPI0924215A2 (pt) | método e sistema para execução de medição | |
BR112012001083A2 (pt) | sistema de refrigeração de gás de exaustão de turbina a gás | |
DK2495437T3 (da) | Fremgangsmåde og system til at drive en vindmølle | |
BR112012015092A2 (pt) | método e sistema para diagnóstico de um compressor | |
IT1404179B1 (it) | Sistema per la gestione di energia in almeno un edificio e relativo metodo | |
BRPI1007113A2 (pt) | método para iniciar um sistema em um chip e equipamento para iniciar um sistema em um chip | |
IT1394477B1 (it) | Sistema di sicurezza per turbine eoliche e turbina eolica dotata di tale sistema | |
IT1393309B1 (it) | Perfezionamenti ad una turbina per espansione di gas/vapore |