DE69621867D1 - System um den Rotor eines Gasturbinenkompressors zu kühlen - Google Patents

System um den Rotor eines Gasturbinenkompressors zu kühlen

Info

Publication number
DE69621867D1
DE69621867D1 DE69621867T DE69621867T DE69621867D1 DE 69621867 D1 DE69621867 D1 DE 69621867D1 DE 69621867 T DE69621867 T DE 69621867T DE 69621867 T DE69621867 T DE 69621867T DE 69621867 D1 DE69621867 D1 DE 69621867D1
Authority
DE
Germany
Prior art keywords
rotor
cool
gas turbine
turbine compressor
compressor
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
DE69621867T
Other languages
English (en)
Other versions
DE69621867T2 (de
Inventor
Dean Thomas Lenahan
Christopher Charles Glynn
Poul Dyhr Pedersen
Frederick Martin Miller
Larry Wayne Plemmons
Curtis Walton Stover
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE69621867D1 publication Critical patent/DE69621867D1/de
Publication of DE69621867T2 publication Critical patent/DE69621867T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185Cooling means for reducing the temperature of the cooling air or gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/081Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/582Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/584Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling or heating the machine

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69621867T 1995-03-31 1996-03-20 System um den Rotor eines Gasturbinenkompressors zu kühlen Expired - Fee Related DE69621867T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/414,699 US5685158A (en) 1995-03-31 1995-03-31 Compressor rotor cooling system for a gas turbine

Publications (2)

Publication Number Publication Date
DE69621867D1 true DE69621867D1 (de) 2002-07-25
DE69621867T2 DE69621867T2 (de) 2003-01-23

Family

ID=23642568

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69621867T Expired - Fee Related DE69621867T2 (de) 1995-03-31 1996-03-20 System um den Rotor eines Gasturbinenkompressors zu kühlen

Country Status (6)

Country Link
US (1) US5685158A (de)
EP (1) EP0735255B1 (de)
JP (1) JP3894980B2 (de)
KR (1) KR100413754B1 (de)
DE (1) DE69621867T2 (de)
IN (1) IN186064B (de)

Families Citing this family (116)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5906093A (en) * 1997-02-21 1999-05-25 Siemens Westinghouse Power Corporation Gas turbine combustor transition
US6065282A (en) * 1997-10-29 2000-05-23 Mitsubishi Heavy Industries, Ltd. System for cooling blades in a gas turbine
US6267553B1 (en) 1999-06-01 2001-07-31 Joseph C. Burge Gas turbine compressor spool with structural and thermal upgrades
DE10041413B4 (de) * 1999-08-25 2011-05-05 Alstom (Switzerland) Ltd. Verfahren zum Betrieb einer Kraftwerksanlage
US6572337B1 (en) 1999-11-30 2003-06-03 General Electric Co. Turbine rotor torque transmission
US6875801B2 (en) * 1999-12-10 2005-04-05 Construction Research & Technology Gmbh Solubilized defoamers for cementitious compositions
US6375429B1 (en) 2001-02-05 2002-04-23 General Electric Company Turbomachine blade-to-rotor sealing arrangement
US6575703B2 (en) 2001-07-20 2003-06-10 General Electric Company Turbine disk side plate
US6853945B2 (en) * 2003-03-27 2005-02-08 General Electric Company Method of on-line monitoring of radial clearances in steam turbines
US20040211342A1 (en) * 2003-04-25 2004-10-28 Mbt Holding Ag Rheology stabilizer for cementitious compositions
US6968696B2 (en) 2003-09-04 2005-11-29 Siemens Westinghouse Power Corporation Part load blade tip clearance control
US7096673B2 (en) 2003-10-08 2006-08-29 Siemens Westinghouse Power Corporation Blade tip clearance control
US20050120719A1 (en) * 2003-12-08 2005-06-09 Olsen Andrew J. Internally insulated turbine assembly
US20100236244A1 (en) * 2006-06-28 2010-09-23 Longardner Robert L Heat absorbing and reflecting shield for air breathing heat engine
US7914254B2 (en) * 2007-02-13 2011-03-29 General Electric Company Integrated support/thermocouple housing for impingement cooling manifolds and cooling method
CN101981272B (zh) 2008-03-28 2014-06-11 埃克森美孚上游研究公司 低排放发电和烃采收系统及方法
CN101981162B (zh) 2008-03-28 2014-07-02 埃克森美孚上游研究公司 低排放发电和烃采收系统及方法
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
JP5580320B2 (ja) 2008-10-14 2014-08-27 エクソンモービル アップストリーム リサーチ カンパニー 燃焼生成物を制御するための方法およびシステム
US8123406B2 (en) * 2008-11-10 2012-02-28 General Electric Company Externally adjustable impingement cooling manifold mount and thermocouple housing
US7993102B2 (en) * 2009-01-09 2011-08-09 General Electric Company Rotor cooling circuit
DE102009021384A1 (de) * 2009-05-14 2010-11-18 Mtu Aero Engines Gmbh Strömungsvorrichtung mit Kavitätenkühlung
CN102597418A (zh) 2009-11-12 2012-07-18 埃克森美孚上游研究公司 低排放发电和烃采收系统及方法
US8616832B2 (en) * 2009-11-30 2013-12-31 Honeywell International Inc. Turbine assemblies with impingement cooling
US8540482B2 (en) 2010-06-07 2013-09-24 United Technologies Corporation Rotor assembly for gas turbine engine
US9732675B2 (en) 2010-07-02 2017-08-15 Exxonmobil Upstream Research Company Low emission power generation systems and methods
JP5906555B2 (ja) 2010-07-02 2016-04-20 エクソンモービル アップストリーム リサーチ カンパニー 排ガス再循環方式によるリッチエアの化学量論的燃焼
BR112012031153A2 (pt) 2010-07-02 2016-11-08 Exxonmobil Upstream Res Co sistemas e métodos de geração de energia de triplo-ciclo de baixa emissão
JP5759543B2 (ja) 2010-07-02 2015-08-05 エクソンモービル アップストリーム リサーチ カンパニー 排ガス再循環方式及び直接接触型冷却器による化学量論的燃焼
EP2418352B1 (de) * 2010-08-10 2019-09-11 Ansaldo Energia Switzerland AG Gasturbinenmotor umfassend einen Verdichter mit longitudinalen Kühlkanälen
GB201015029D0 (en) * 2010-09-10 2010-10-20 Rolls Royce Plc Gas turbine engine
EP2450531B1 (de) 2010-11-04 2013-05-15 Siemens Aktiengesellschaft Axialverdichterkühlung
DE102010063071A1 (de) * 2010-12-14 2012-06-14 Rolls-Royce Deutschland Ltd & Co Kg Kühlvorrichtung für ein Strahltriebwerk
TWI564474B (zh) 2011-03-22 2017-01-01 艾克頌美孚上游研究公司 於渦輪系統中控制化學計量燃燒的整合系統和使用彼之產生動力的方法
TWI563165B (en) 2011-03-22 2016-12-21 Exxonmobil Upstream Res Co Power generation system and method for generating power
TWI563166B (en) 2011-03-22 2016-12-21 Exxonmobil Upstream Res Co Integrated generation systems and methods for generating power
TWI593872B (zh) 2011-03-22 2017-08-01 艾克頌美孚上游研究公司 整合系統及產生動力之方法
US9080449B2 (en) * 2011-08-16 2015-07-14 United Technologies Corporation Gas turbine engine seal assembly having flow-through tube
US9194246B2 (en) 2011-09-23 2015-11-24 General Electric Company Steam turbine LP casing cylindrical struts between stages
CH705840A1 (de) 2011-12-06 2013-06-14 Alstom Technology Ltd Hochdruck-Verdichter, insbesondere in einer Gasturbine.
CN104428490B (zh) 2011-12-20 2018-06-05 埃克森美孚上游研究公司 提高的煤层甲烷生产
US10502135B2 (en) 2012-01-31 2019-12-10 United Technologies Corporation Buffer system for communicating one or more buffer supply airs throughout a gas turbine engine
US10415468B2 (en) 2012-01-31 2019-09-17 United Technologies Corporation Gas turbine engine buffer system
US10018116B2 (en) 2012-01-31 2018-07-10 United Technologies Corporation Gas turbine engine buffer system providing zoned ventilation
US9353682B2 (en) 2012-04-12 2016-05-31 General Electric Company Methods, systems and apparatus relating to combustion turbine power plants with exhaust gas recirculation
US9032738B2 (en) * 2012-04-25 2015-05-19 Siemens Aktiengeselischaft Gas turbine compressor with bleed path
US9784185B2 (en) 2012-04-26 2017-10-10 General Electric Company System and method for cooling a gas turbine with an exhaust gas provided by the gas turbine
US10273880B2 (en) 2012-04-26 2019-04-30 General Electric Company System and method of recirculating exhaust gas for use in a plurality of flow paths in a gas turbine engine
US20140050558A1 (en) * 2012-08-15 2014-02-20 General Electric Company Temperature gradient management arrangement for a turbine system and method of managing a temperature gradient of a turbine system
US9188009B2 (en) * 2012-10-30 2015-11-17 United Technologies Corporation Bore cavity thermal conditioning system
US10215412B2 (en) 2012-11-02 2019-02-26 General Electric Company System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system
US9631815B2 (en) 2012-12-28 2017-04-25 General Electric Company System and method for a turbine combustor
US9611756B2 (en) 2012-11-02 2017-04-04 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
US10161312B2 (en) 2012-11-02 2018-12-25 General Electric Company System and method for diffusion combustion with fuel-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system
US9803865B2 (en) 2012-12-28 2017-10-31 General Electric Company System and method for a turbine combustor
US9599070B2 (en) 2012-11-02 2017-03-21 General Electric Company System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
US9869279B2 (en) 2012-11-02 2018-01-16 General Electric Company System and method for a multi-wall turbine combustor
US10107495B2 (en) 2012-11-02 2018-10-23 General Electric Company Gas turbine combustor control system for stoichiometric combustion in the presence of a diluent
US9574496B2 (en) 2012-12-28 2017-02-21 General Electric Company System and method for a turbine combustor
US9708977B2 (en) 2012-12-28 2017-07-18 General Electric Company System and method for reheat in gas turbine with exhaust gas recirculation
US9476313B2 (en) 2012-12-21 2016-10-25 United Technologies Corporation Gas turbine engine including a pre-diffuser heat exchanger
US10208677B2 (en) 2012-12-31 2019-02-19 General Electric Company Gas turbine load control system
US9581081B2 (en) 2013-01-13 2017-02-28 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
US9512759B2 (en) 2013-02-06 2016-12-06 General Electric Company System and method for catalyst heat utilization for gas turbine with exhaust gas recirculation
EP2959109B1 (de) * 2013-02-19 2019-01-30 United Technologies Corporation Gasturbinenmotor mit rotorscheibenbohrungsbeheizung
US9938861B2 (en) 2013-02-21 2018-04-10 Exxonmobil Upstream Research Company Fuel combusting method
TW201502356A (zh) 2013-02-21 2015-01-16 Exxonmobil Upstream Res Co 氣渦輪機排氣中氧之減少
RU2637609C2 (ru) 2013-02-28 2017-12-05 Эксонмобил Апстрим Рисерч Компани Система и способ для камеры сгорания турбины
US9618261B2 (en) 2013-03-08 2017-04-11 Exxonmobil Upstream Research Company Power generation and LNG production
US20140250945A1 (en) 2013-03-08 2014-09-11 Richard A. Huntington Carbon Dioxide Recovery
TW201500635A (zh) 2013-03-08 2015-01-01 Exxonmobil Upstream Res Co 處理廢氣以供用於提高油回收
US9784182B2 (en) 2013-03-08 2017-10-10 Exxonmobil Upstream Research Company Power generation and methane recovery from methane hydrates
EP2971518B1 (de) 2013-03-11 2019-11-20 United Technologies Corporation Zugwellen-strömungsauslöser
US9631542B2 (en) 2013-06-28 2017-04-25 General Electric Company System and method for exhausting combustion gases from gas turbine engines
US9617914B2 (en) 2013-06-28 2017-04-11 General Electric Company Systems and methods for monitoring gas turbine systems having exhaust gas recirculation
TWI654368B (zh) 2013-06-28 2019-03-21 美商艾克頌美孚上游研究公司 用於控制在廢氣再循環氣渦輪機系統中的廢氣流之系統、方法與媒體
US9835089B2 (en) 2013-06-28 2017-12-05 General Electric Company System and method for a fuel nozzle
WO2015009537A1 (en) * 2013-07-15 2015-01-22 United Technologies Corporation Cooled compressor
US9587510B2 (en) 2013-07-30 2017-03-07 General Electric Company System and method for a gas turbine engine sensor
US9903588B2 (en) 2013-07-30 2018-02-27 General Electric Company System and method for barrier in passage of combustor of gas turbine engine with exhaust gas recirculation
US9951658B2 (en) 2013-07-31 2018-04-24 General Electric Company System and method for an oxidant heating system
WO2015038451A1 (en) 2013-09-10 2015-03-19 United Technologies Corporation Fluid injector for cooling a gas turbine engine component
EP3058176B1 (de) 2013-10-02 2020-08-26 United Technologies Corporation Gasturbinentriebwerk mit verdichterplattendeflektoren
EP2868865A1 (de) * 2013-10-31 2015-05-06 Siemens Aktiengesellschaft Gasturbine sowie Verfahren zu deren Kühlung
US10030588B2 (en) 2013-12-04 2018-07-24 General Electric Company Gas turbine combustor diagnostic system and method
US9752458B2 (en) 2013-12-04 2017-09-05 General Electric Company System and method for a gas turbine engine
US10227920B2 (en) 2014-01-15 2019-03-12 General Electric Company Gas turbine oxidant separation system
US9915200B2 (en) 2014-01-21 2018-03-13 General Electric Company System and method for controlling the combustion process in a gas turbine operating with exhaust gas recirculation
US9863267B2 (en) 2014-01-21 2018-01-09 General Electric Company System and method of control for a gas turbine engine
US10079564B2 (en) 2014-01-27 2018-09-18 General Electric Company System and method for a stoichiometric exhaust gas recirculation gas turbine system
US10047633B2 (en) 2014-05-16 2018-08-14 General Electric Company Bearing housing
US10655542B2 (en) 2014-06-30 2020-05-19 General Electric Company Method and system for startup of gas turbine system drive trains with exhaust gas recirculation
US10060359B2 (en) 2014-06-30 2018-08-28 General Electric Company Method and system for combustion control for gas turbine system with exhaust gas recirculation
US9885290B2 (en) 2014-06-30 2018-02-06 General Electric Company Erosion suppression system and method in an exhaust gas recirculation gas turbine system
EP2995769B1 (de) * 2014-09-12 2019-11-13 United Technologies Corporation Wärmeregelungssysteme eines turbomaschinenrotors
US9869247B2 (en) 2014-12-31 2018-01-16 General Electric Company Systems and methods of estimating a combustion equivalence ratio in a gas turbine with exhaust gas recirculation
US9819292B2 (en) 2014-12-31 2017-11-14 General Electric Company Systems and methods to respond to grid overfrequency events for a stoichiometric exhaust recirculation gas turbine
US10788212B2 (en) 2015-01-12 2020-09-29 General Electric Company System and method for an oxidant passageway in a gas turbine system with exhaust gas recirculation
US10316746B2 (en) 2015-02-04 2019-06-11 General Electric Company Turbine system with exhaust gas recirculation, separation and extraction
US10094566B2 (en) 2015-02-04 2018-10-09 General Electric Company Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation
US10253690B2 (en) 2015-02-04 2019-04-09 General Electric Company Turbine system with exhaust gas recirculation, separation and extraction
US10267270B2 (en) 2015-02-06 2019-04-23 General Electric Company Systems and methods for carbon black production with a gas turbine engine having exhaust gas recirculation
US10145269B2 (en) 2015-03-04 2018-12-04 General Electric Company System and method for cooling discharge flow
US10480792B2 (en) 2015-03-06 2019-11-19 General Electric Company Fuel staging in a gas turbine engine
US10612383B2 (en) * 2016-01-27 2020-04-07 General Electric Company Compressor aft rotor rim cooling for high OPR (T3) engine
US10138752B2 (en) 2016-02-25 2018-11-27 General Electric Company Active HPC clearance control
US10436115B2 (en) * 2016-08-22 2019-10-08 United Technologies Corporation Heat exchanger for gas turbine engine with support damper mounting
US10641174B2 (en) 2017-01-18 2020-05-05 General Electric Company Rotor shaft cooling
US11377957B2 (en) 2017-05-09 2022-07-05 General Electric Company Gas turbine engine with a diffuser cavity cooled compressor
US10907545B2 (en) * 2017-06-27 2021-02-02 General Electric Company Cooling system for a turbine engine
US10746098B2 (en) 2018-03-09 2020-08-18 General Electric Company Compressor rotor cooling apparatus
US10927706B2 (en) 2018-11-01 2021-02-23 Raytheon Technologies Corporation Intercooled tangential air injector for gas turbine engines
US10989411B2 (en) 2019-01-03 2021-04-27 General Electric Company Heat exchanger for turbo machine
CN109624618A (zh) * 2019-01-09 2019-04-16 湖北军缔悍隆科技发展有限公司 一种有线胎压传输装置
US11306604B2 (en) 2020-04-14 2022-04-19 Raytheon Technologies Corporation HPC case clearance control thermal control ring spoke system
US11674396B2 (en) 2021-07-30 2023-06-13 General Electric Company Cooling air delivery assembly

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3546882A (en) * 1968-04-24 1970-12-15 Gen Electric Gas turbine engines
US4291531A (en) * 1978-04-06 1981-09-29 Rolls-Royce Limited Gas turbine engine
DE3428892A1 (de) * 1984-08-04 1986-02-13 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Schaufel- und dichtspaltoptimierungseinrichtung fuer verdichter von gasturbinentriebwerken, insbesondere gasturbinenstrahltriebwerken
DE8605507U1 (de) * 1986-02-28 1987-04-16 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur Belüftung von Rotorbauteilen für Verdichter von Gasturbinentriebwerken
DE3638961A1 (de) * 1986-11-14 1988-05-26 Mtu Muenchen Gmbh Gasturbinentriebwerk mit einem hochdruckverdichter
JPH0658168A (ja) * 1992-08-06 1994-03-01 Hitachi Ltd ガスタービン用圧縮機及びガスタービン
FR2695161B1 (fr) * 1992-08-26 1994-11-04 Snecma Système de refroidissement d'un compresseur de turbomachine et de contrôle des jeux.
US5310319A (en) * 1993-01-12 1994-05-10 United Technologies Corporation Free standing turbine disk sideplate assembly

Also Published As

Publication number Publication date
JP3894980B2 (ja) 2007-03-22
KR960034693A (ko) 1996-10-24
EP0735255B1 (de) 2002-06-19
US5685158A (en) 1997-11-11
KR100413754B1 (ko) 2004-04-03
IN186064B (de) 2001-06-16
EP0735255A1 (de) 1996-10-02
DE69621867T2 (de) 2003-01-23
JPH094467A (ja) 1997-01-07

Similar Documents

Publication Publication Date Title
DE69621867D1 (de) System um den Rotor eines Gasturbinenkompressors zu kühlen
DE69623370D1 (de) Dampfgekühlte Gasturbine
DE69720476D1 (de) Konfiguration eines durch verdampfung gekühlten gasturbinenrotors
DE69511802D1 (de) Zusatzliche Gasturbinentriebwerke
DE69809532D1 (de) Dampfgekühlte Gasturbinenanlage
DE69406993D1 (de) Gasturbinenrotorlagerungssystem
DE69626382D1 (de) Hitzerückgewinnungs-gasturbinenrotor
DE69302813D1 (de) Rotor für gasturbinen
DE69612319D1 (de) Gasturbinenschaufel
DE69822720D1 (de) Dichtung zwischen den Stufen einer Gasturbine
DE69503122D1 (de) Synchronisierung von gasturbinenschaufeln
IL112275A0 (en) Gas turbine engine generator set
DE69631991D1 (de) Gasturbinenbrennkammer
DE69622252D1 (de) Gasturbinenrotor
DE69924953D1 (de) Schaufel eines Gasturbinentriebwerks
DE69531806D1 (de) Gasturbinenbrennkammer
DE59701158D1 (de) Abgasturbine eines Abgasturboladers
DE59508574D1 (de) Gas- und Dampfturbinenanlage
GB9608196D0 (en) Gas turbine engine
EP0728989A3 (de) Verbrennungsgerät für Gasturbinenmotor
DE69328425D1 (de) Rotor für gasturbinen
DE69811764D1 (de) Kühlung eines Gasturbinengehäuses
DE69406071D1 (de) Kühlungssystem für den Turbinenstator und die Turbinenrotorscheiben einer Turbomaschine
DE69729026D1 (de) Gasturbinenleitschaufel
DE69821586D1 (de) Dampfgekühlte Gasturbine

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN

8339 Ceased/non-payment of the annual fee