IN2015DN03340A - - Google Patents

Info

Publication number
IN2015DN03340A
IN2015DN03340A IN3340DEN2015A IN2015DN03340A IN 2015DN03340 A IN2015DN03340 A IN 2015DN03340A IN 3340DEN2015 A IN3340DEN2015 A IN 3340DEN2015A IN 2015DN03340 A IN2015DN03340 A IN 2015DN03340A
Authority
IN
India
Prior art keywords
source
cooling fluid
rotor
piping system
cooling
Prior art date
Application number
Other languages
English (en)
Inventor
Kok-Mun Tham
Ching-Pang Lee
Vincent P Laurello
Abdullatif M Chehab
David A Kemp
John A Fussner
Yan Yin
Bijay K Sultanian
Weidong Cai
Original Assignee
Siemens Ag
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Siemens Ag filed Critical Siemens Ag
Publication of IN2015DN03340A publication Critical patent/IN2015DN03340A/en

Links

Classifications

    • 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
    • F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • F01D5/088—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor in a closed cavity
    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/34—Turning or inching gear
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • F05D2270/3032—Temperature excessive temperatures, e.g. caused by overheating
IN3340DEN2015 2012-11-07 2013-11-01 IN2015DN03340A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/670,788 US8820091B2 (en) 2012-11-07 2012-11-07 External cooling fluid injection system in a gas turbine engine
PCT/US2013/067950 WO2014074396A1 (en) 2012-11-07 2013-11-01 External cooling fluid injection system in a gas turbine engine

Publications (1)

Publication Number Publication Date
IN2015DN03340A true IN2015DN03340A (zh) 2015-10-23

Family

ID=49753452

Family Applications (1)

Application Number Title Priority Date Filing Date
IN3340DEN2015 IN2015DN03340A (zh) 2012-11-07 2013-11-01

Country Status (11)

Country Link
US (1) US8820091B2 (zh)
EP (1) EP2917491A1 (zh)
JP (1) JP2015533998A (zh)
KR (1) KR20150091084A (zh)
CN (1) CN104769222A (zh)
BR (1) BR112015010367A2 (zh)
CA (1) CA2888673A1 (zh)
IN (1) IN2015DN03340A (zh)
MX (1) MX2015005683A (zh)
RU (1) RU2015117256A (zh)
WO (1) WO2014074396A1 (zh)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9869190B2 (en) 2014-05-30 2018-01-16 General Electric Company Variable-pitch rotor with remote counterweights
US10072510B2 (en) 2014-11-21 2018-09-11 General Electric Company Variable pitch fan for gas turbine engine and method of assembling the same
CN105089719B (zh) * 2015-06-11 2017-03-01 中国石油天然气股份有限公司 冷却分布器和汽轮机
US10487739B2 (en) 2015-07-20 2019-11-26 General Electric Company Cooling system for a turbine engine
US9995314B2 (en) 2015-07-20 2018-06-12 General Electric Company Cooling system for a turbine engine
US10100653B2 (en) 2015-10-08 2018-10-16 General Electric Company Variable pitch fan blade retention system
US11149642B2 (en) * 2015-12-30 2021-10-19 General Electric Company System and method of reducing post-shutdown engine temperatures
EP3205817A1 (en) 2016-02-09 2017-08-16 Ansaldo Energia Switzerland AG Fluid cooled rotor for a gas turbine
US9988928B2 (en) 2016-05-17 2018-06-05 Siemens Energy, Inc. Systems and methods for determining turbomachine engine safe start clearances following a shutdown of the turbomachine engine
US10677164B2 (en) * 2016-11-15 2020-06-09 General Electric Company Cooling system for a turbine engine
US10739002B2 (en) * 2016-12-19 2020-08-11 General Electric Company Fluidic nozzle assembly for a turbine engine
WO2020046375A1 (en) * 2018-08-31 2020-03-05 Siemens Aktiengesellschaft Method of operation of inlet heating system for clearance control
US11788470B2 (en) 2021-03-01 2023-10-17 General Electric Company Gas turbine engine thermal management
US11674435B2 (en) 2021-06-29 2023-06-13 General Electric Company Levered counterweight feathering system
US11795964B2 (en) 2021-07-16 2023-10-24 General Electric Company Levered counterweight feathering system
US11702958B2 (en) 2021-09-23 2023-07-18 General Electric Company System and method of regulating thermal transport bus pressure

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH06193407A (ja) * 1992-12-24 1994-07-12 Toshiba Corp タ−ビンケ−シング強制冷却装置
CN1219218A (zh) * 1997-03-24 1999-06-09 西屋电气公司 涡轮机的闭路空气冷却系统
WO2000011324A1 (de) 1998-08-18 2000-03-02 Siemens Aktiengesellschaft Turbinengehäuse
US6487863B1 (en) * 2001-03-30 2002-12-03 Siemens Westinghouse Power Corporation Method and apparatus for cooling high temperature components in a gas turbine
DE10233113A1 (de) 2001-10-30 2003-05-15 Alstom Switzerland Ltd Turbomaschine
EP1418319A1 (de) * 2002-11-11 2004-05-12 Siemens Aktiengesellschaft Gasturbine
US6978621B2 (en) * 2002-12-31 2005-12-27 General Electric Company Turbo recuperator device
WO2004090291A1 (de) 2003-04-07 2004-10-21 Alstom Technology Ltd Turbomaschine
JP2006037855A (ja) 2004-07-28 2006-02-09 Mitsubishi Heavy Ind Ltd 車室ケーシング及びガスタービン
DE102004041271A1 (de) 2004-08-23 2006-03-02 Alstom Technology Ltd Einrichtung und Verfahren zum Kühlen eines Gehäuses einer Gasturbine bzw. einer Brennkammer
US7269955B2 (en) * 2004-08-25 2007-09-18 General Electric Company Methods and apparatus for maintaining rotor assembly tip clearances
US7987660B2 (en) 2005-06-10 2011-08-02 Mitsubishi Heavy Industries, Ltd. Gas turbine, method of controlling air supply and computer program product for controlling air supply
US20090051167A1 (en) * 2007-08-22 2009-02-26 General Electric Company Combustion turbine cooling media supply method
US8152446B2 (en) * 2007-08-23 2012-04-10 General Electric Company Apparatus and method for reducing eccentricity and out-of-roundness in turbines
US20090056342A1 (en) 2007-09-04 2009-03-05 General Electric Company Methods and Systems for Gas Turbine Part-Load Operating Conditions
JP4929217B2 (ja) * 2008-03-28 2012-05-09 三菱重工業株式会社 ガスタービンおよびガスタービンの中間軸ならびにガスタービン圧縮機の冷却方法
US8277170B2 (en) * 2008-05-16 2012-10-02 General Electric Company Cooling circuit for use in turbine bucket cooling
US8079802B2 (en) * 2008-06-30 2011-12-20 Mitsubishi Heavy Industries, Ltd. Gas turbine
US8061971B2 (en) * 2008-09-12 2011-11-22 General Electric Company Apparatus and method for cooling a turbine
US8210801B2 (en) 2009-01-29 2012-07-03 General Electric Company Systems and methods of reducing heat loss from a gas turbine during shutdown
JP5566683B2 (ja) * 2009-12-25 2014-08-06 三菱重工業株式会社 ガスタービン

Also Published As

Publication number Publication date
MX2015005683A (es) 2015-08-20
EP2917491A1 (en) 2015-09-16
CN104769222A (zh) 2015-07-08
BR112015010367A2 (pt) 2017-07-11
US20140123657A1 (en) 2014-05-08
RU2015117256A (ru) 2016-12-27
JP2015533998A (ja) 2015-11-26
KR20150091084A (ko) 2015-08-07
CA2888673A1 (en) 2014-05-15
WO2014074396A1 (en) 2014-05-15
US8820091B2 (en) 2014-09-02

Similar Documents

Publication Publication Date Title
IN2015DN03340A (zh)
SA515360105B1 (ar) طريقة لتشغيل محرك توربيني غازي يتضمن نظام إعادة تدوير هواء غلاف وحدة احتراق
CL2012002755A1 (es) Una duela de enfriamiento de placa para su uso en un horno que tiene una pared de blindaje, comprende una porcion superior que aloja al menos una entrada de fluido de enfriamiento y al menos una salida de fluido de enfriamiento para el flujo del fluido de enfriamiento hacia y desde la duela de enfriamiento de placa desde afuera del horno, y un cuerpo principal colocado en un angulo relativo a la porcion superior de tal forma que el cuerpo principal se puede insertar en el horno; metodo para enfriar.
WO2014012896A3 (fr) Procede et dispositif de pompage d'une chambre de procedes
MX356169B (es) Aspirador de múltiples tomas con pasaje de fugas.
IN2015DN00893A (zh)
MX2015010137A (es) Reparacion de valvulas, tuberia y componentes de tuberia.
MX2015010994A (es) Valvula de ajuste con recuperacion de energia.
MX2016013892A (es) Valvula de drenaje por gravedad.
MX2016008942A (es) Equipo de generacion de energia de turbina de gas, y dispositivo y metodo para secar el sistema de aire de enfriamiento de turbina de gas.
GB2570094A (en) Valve module and filter
WO2014191156A3 (de) Verfahren zum prüfen der dichtheit eines einen abgasturbolader aufweisenden verbrennungsmotors sowie abgasturbolader
MX2014001013A (es) Propulsor centrifugo y turbomaquina.
GB2547174A (en) Mechanical downhole pressure maintenance system
UA103413C2 (en) Gas-turbine engine
BR112017014330A2 (pt) dispositivo de extração de poeira
MX2015008033A (es) Metodo para equilibrar empuje, turbina y motor de turbina.
MX2016005390A (es) Aparato de valvula.
NZ714281A (en) Shut-off valve for oscillating water column turbines
NZ724653A (en) Embedded regulator for pneumatic nailer supplemental air tank
CN204420567U (zh) 气化系统氧气管线吹扫用高压氮气系统
GB201115043D0 (en) Steam injected gas turbine engine
WO2015031961A3 (en) Compressor device
GB201305587D0 (en) An air handling system
CN203516251U (zh) 一种双向平衡阀装置