IN186474B - - Google Patents
Info
- Publication number
- IN186474B IN186474B IN211CA1996A IN186474B IN 186474 B IN186474 B IN 186474B IN 211CA1996 A IN211CA1996 A IN 211CA1996A IN 186474 B IN186474 B IN 186474B
- Authority
- IN
- India
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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
- F01D11/20—Actively adjusting tip-clearance
- F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
-
- 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
- F01D25/14—Casings modified therefor
-
- 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
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/26—Double casings; Measures against temperature strain in casings
-
- 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
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
- F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such 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
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
-
- 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/644—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins for adjusting the position or the alignment, e.g. wedges or eccenters
-
- 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
- F05D2230/00—Manufacture
- F05D2230/70—Disassembly methods
-
- 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
- F05D2240/00—Components
- F05D2240/90—Mounting on supporting structures or systems
-
- 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
- F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
-
- 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
- F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
-
- 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
- F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
- F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/414,698 US5685693A (en) | 1995-03-31 | 1995-03-31 | Removable inner turbine shell with bucket tip clearance control |
Publications (1)
Publication Number | Publication Date |
---|---|
IN186474B true IN186474B (zh) | 2001-09-08 |
Family
ID=23642564
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN211CA1996 IN186474B (zh) | 1995-03-31 | 1996-02-06 |
Country Status (6)
Country | Link |
---|---|
US (6) | US5685693A (zh) |
EP (1) | EP0735243B1 (zh) |
JP (1) | JP3863938B2 (zh) |
KR (1) | KR100416014B1 (zh) |
DE (1) | DE69611737T2 (zh) |
IN (1) | IN186474B (zh) |
Families Citing this family (116)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5685693A (en) * | 1995-03-31 | 1997-11-11 | General Electric Co. | Removable inner turbine shell with bucket tip clearance control |
US5667358A (en) * | 1995-11-30 | 1997-09-16 | Westinghouse Electric Corporation | Method for reducing steady state rotor blade tip clearance in a land-based gas turbine to improve efficiency |
GB2313414B (en) * | 1996-05-24 | 2000-05-17 | Rolls Royce Plc | Gas turbine engine blade tip clearance control |
JPH1061457A (ja) | 1996-08-27 | 1998-03-03 | Mitsubishi Heavy Ind Ltd | 複合サイクル発電プラント用ガスタービン |
US5819525A (en) * | 1997-03-14 | 1998-10-13 | Westinghouse Electric Corporation | Cooling supply manifold assembly for cooling combustion turbine components |
US5846048A (en) * | 1997-05-22 | 1998-12-08 | Mitsubishi Heavy Industries, Ltd. | Gas turbine stationary blade unit |
US6065282A (en) * | 1997-10-29 | 2000-05-23 | Mitsubishi Heavy Industries, Ltd. | System for cooling blades in a gas turbine |
JP3564290B2 (ja) * | 1997-12-24 | 2004-09-08 | 三菱重工業株式会社 | 蒸気冷却型ガスタービン |
US6019573A (en) * | 1998-01-29 | 2000-02-01 | Mitsubishi Heavy Industries, Ltd. | Heat recovery type gas turbine |
CA2285286C (en) * | 1998-02-03 | 2005-01-11 | Mitsubishi Heavy Industries, Ltd. | Gas turbine for combined cycle power plant |
US6105363A (en) * | 1998-04-27 | 2000-08-22 | Siemens Westinghouse Power Corporation | Cooling scheme for turbine hot parts |
US6626635B1 (en) * | 1998-09-30 | 2003-09-30 | General Electric Company | System for controlling clearance between blade tips and a surrounding casing in rotating machinery |
US6139182A (en) * | 1999-03-01 | 2000-10-31 | Thermoscan, Inc | Enhanced protective cover for use in an IR thermometer |
EP1046787B1 (en) | 1999-04-23 | 2006-06-07 | General Electric Company | Turbine inner shell heating and cooling flow circuit |
US6224332B1 (en) | 1999-05-14 | 2001-05-01 | General Electric Co. | Apparatus and methods for installing, removing and adjusting an inner turbine shell section relative to an outer turbine shell section |
KR20010007065A (ko) * | 1999-05-18 | 2001-01-26 | 제이 엘. 차스킨 | 터빈 |
JP4274666B2 (ja) | 2000-03-07 | 2009-06-10 | 三菱重工業株式会社 | ガスタービン |
JP4301692B2 (ja) | 2000-03-31 | 2009-07-22 | 三菱重工業株式会社 | ガスタービン |
JP4698860B2 (ja) | 2000-04-18 | 2011-06-08 | 三菱重工業株式会社 | タービンの蒸気制御装置 |
US6506013B1 (en) | 2000-04-28 | 2003-01-14 | General Electric Company | Film cooling for a closed loop cooled airfoil |
US6435814B1 (en) | 2000-05-16 | 2002-08-20 | General Electric Company | Film cooling air pocket in a closed loop cooled airfoil |
US6468031B1 (en) | 2000-05-16 | 2002-10-22 | General Electric Company | Nozzle cavity impingement/area reduction insert |
US6398486B1 (en) | 2000-06-01 | 2002-06-04 | General Electric Company | Steam exit flow design for aft cavities of an airfoil |
US6454526B1 (en) | 2000-09-28 | 2002-09-24 | Siemens Westinghouse Power Corporation | Cooled turbine vane with endcaps |
US6593547B1 (en) | 2000-11-30 | 2003-07-15 | Pacific Scientific Electro Kinetics Division | Air gap deicing device |
US6435823B1 (en) | 2000-12-08 | 2002-08-20 | General Electric Company | Bucket tip clearance control system |
US6454529B1 (en) | 2001-03-23 | 2002-09-24 | General Electric Company | Methods and apparatus for maintaining rotor assembly tip clearances |
JP3825279B2 (ja) * | 2001-06-04 | 2006-09-27 | 三菱重工業株式会社 | ガスタービン |
US6402468B1 (en) | 2001-06-18 | 2002-06-11 | General Electric Company | Method and apparatus for axially aligning inner and outer turbine shell components |
US6589010B2 (en) | 2001-08-27 | 2003-07-08 | General Electric Company | Method for controlling coolant flow in airfoil, flow control structure and airfoil incorporating the same |
EP1375822B1 (en) * | 2002-06-25 | 2016-02-03 | Mitsubishi Hitachi Power Systems, Ltd. | Gas turbine production process |
US6776583B1 (en) | 2003-02-27 | 2004-08-17 | General Electric Company | Turbine bucket damper pin |
US7001144B2 (en) * | 2003-02-27 | 2006-02-21 | General Electric Company | Gas turbine and method for reducing bucket tip shroud creep rate |
US7093419B2 (en) * | 2003-07-02 | 2006-08-22 | General Electric Company | Methods and apparatus for operating gas turbine engine combustors |
US6913441B2 (en) | 2003-09-04 | 2005-07-05 | Siemens Westinghouse Power Corporation | Turbine blade ring assembly and clocking method |
US6997679B2 (en) * | 2003-12-12 | 2006-02-14 | General Electric Company | Airfoil cooling holes |
US7269955B2 (en) * | 2004-08-25 | 2007-09-18 | General Electric Company | Methods and apparatus for maintaining rotor assembly tip clearances |
US7165937B2 (en) * | 2004-12-06 | 2007-01-23 | General Electric Company | Methods and apparatus for maintaining rotor assembly tip clearances |
WO2006103152A1 (de) * | 2005-03-29 | 2006-10-05 | Alstom Technology Ltd | Verfahren und vorrichtung zum austausch von bauteilen einer strömungsrotationsmaschine |
US7434402B2 (en) * | 2005-03-29 | 2008-10-14 | Siemens Power Generation, Inc. | System for actively controlling compressor clearances |
US7708518B2 (en) * | 2005-06-23 | 2010-05-04 | Siemens Energy, Inc. | Turbine blade tip clearance control |
US8065022B2 (en) * | 2005-09-06 | 2011-11-22 | General Electric Company | Methods and systems for neural network modeling of turbine components |
US7273348B2 (en) * | 2005-09-23 | 2007-09-25 | General Electric Company | Method and assembly for aligning a turbine |
US7293953B2 (en) * | 2005-11-15 | 2007-11-13 | General Electric Company | Integrated turbine sealing air and active clearance control system and method |
DE102006004785A1 (de) * | 2006-02-02 | 2007-08-30 | Alstom Technology Ltd. | Strömungsmaschine |
WO2007104973A2 (en) * | 2006-03-14 | 2007-09-20 | Goodman, Simon, John, Nye | Rotor and nozzle assembly for a radial turbine and method of operation |
US20070237629A1 (en) * | 2006-04-05 | 2007-10-11 | General Electric Company | Gas turbine compressor casing flowpath rings |
WO2008012195A1 (de) * | 2006-07-24 | 2008-01-31 | Siemens Aktiengesellschaft | Verfahren zum herausdrehen einer ringhälfte eines insgesamt ringförmigen leitapparats aus einer unteren gehäusehälfte einer axial durchströmbaren, stationären strömungsmaschine, montagevorrichtung, montagevorrichtungsverbund und hilfshalbring hierfür |
EP1905948B1 (en) * | 2006-09-12 | 2012-10-24 | Cryostar SAS | Power recovery machine |
US8801370B2 (en) * | 2006-10-12 | 2014-08-12 | General Electric Company | Turbine case impingement cooling for heavy duty gas turbines |
US7686569B2 (en) * | 2006-12-04 | 2010-03-30 | Siemens Energy, Inc. | Blade clearance system for a turbine engine |
US8276273B2 (en) * | 2007-10-23 | 2012-10-02 | Mitsubishi Heavy Industries, Ltd. | Method for removing blade ring and member for removing blade ring |
FR2925109B1 (fr) * | 2007-12-14 | 2015-05-15 | Snecma | Module de turbomachine muni d'un dispositif d'amelioration des jeux radiaux |
US20090162139A1 (en) * | 2007-12-19 | 2009-06-25 | General Electric Company | Thermally Insulated Flange Bolts |
US8182207B2 (en) | 2008-03-17 | 2012-05-22 | General Electric Company | Inner turbine shell support configuration and methods |
US8197197B2 (en) * | 2009-01-08 | 2012-06-12 | General Electric Company | Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith |
US8443607B2 (en) * | 2009-02-20 | 2013-05-21 | General Electric Company | Coaxial fuel and air premixer for a gas turbine combustor |
US8231338B2 (en) | 2009-05-05 | 2012-07-31 | General Electric Company | Turbine shell with pin support |
JP5804668B2 (ja) * | 2009-06-10 | 2015-11-04 | 三菱重工業株式会社 | 面内圧縮強度評価装置及び方法 |
US8342798B2 (en) * | 2009-07-28 | 2013-01-01 | General Electric Company | System and method for clearance control in a rotary machine |
US20110103939A1 (en) * | 2009-10-30 | 2011-05-05 | General Electric Company | Turbine rotor blade tip and shroud clearance control |
US20110100020A1 (en) * | 2009-10-30 | 2011-05-05 | General Electric Company | Apparatus and method for turbine engine cooling |
WO2011075013A1 (en) * | 2009-12-17 | 2011-06-23 | Volvo Aero Corporation | Arrangement and method for closed flow cooling of a gas turbine engine component |
US9062565B2 (en) * | 2009-12-31 | 2015-06-23 | Rolls-Royce Corporation | Gas turbine engine containment device |
US8662824B2 (en) * | 2010-01-28 | 2014-03-04 | Pratt & Whitney Canada Corp. | Rotor containment structure for gas turbine engine |
US10337404B2 (en) * | 2010-03-08 | 2019-07-02 | General Electric Company | Preferential cooling of gas turbine nozzles |
GB201004381D0 (en) * | 2010-03-17 | 2010-04-28 | Rolls Royce Plc | Rotor blade tip clearance control |
US8939715B2 (en) * | 2010-03-22 | 2015-01-27 | General Electric Company | Active tip clearance control for shrouded gas turbine blades and related method |
US8453454B2 (en) | 2010-04-14 | 2013-06-04 | General Electric Company | Coannular oil injection nozzle |
US20110255959A1 (en) * | 2010-04-15 | 2011-10-20 | General Electric Company | Turbine alignment control system and method |
GB2479865B (en) * | 2010-04-26 | 2013-07-10 | Rolls Royce Plc | An installation having a thermal transfer arrangement |
US8572979B2 (en) | 2010-06-24 | 2013-11-05 | United Technologies Corporation | Gas turbine combustor liner cap assembly |
US8651809B2 (en) * | 2010-10-13 | 2014-02-18 | General Electric Company | Apparatus and method for aligning a turbine casing |
CN102140940B (zh) * | 2011-03-22 | 2013-09-18 | 东方电气集团东方汽轮机有限公司 | 大功率半转速汽轮机组低压模块落地结构 |
US8888436B2 (en) | 2011-06-23 | 2014-11-18 | General Electric Company | Systems and methods for cooling high pressure and intermediate pressure sections of a steam turbine |
US8899909B2 (en) | 2011-06-27 | 2014-12-02 | General Electric Company | Systems and methods for steam turbine wheel space cooling |
US8876460B2 (en) * | 2011-08-11 | 2014-11-04 | General Electric Company | Method and apparatus for measuring turbine shell clearance |
US9297277B2 (en) | 2011-09-30 | 2016-03-29 | General Electric Company | Power plant |
US9017015B2 (en) * | 2011-10-27 | 2015-04-28 | General Electric Company | Turbomachine including an inner-to-outer turbine casing seal assembly and method |
US8973373B2 (en) | 2011-10-31 | 2015-03-10 | General Electric Company | Active clearance control system and method for gas turbine |
US9151173B2 (en) | 2011-12-15 | 2015-10-06 | General Electric Company | Use of multi-faceted impingement openings for increasing heat transfer characteristics on gas turbine components |
US9032599B2 (en) | 2012-02-06 | 2015-05-19 | General Electric Company | Component removal apparatus for use in turbine engines and methods of removing components from turbine engines |
US20130326875A1 (en) * | 2012-06-08 | 2013-12-12 | General Electric Company | Method and apparatus for roll-in and alignment of a casing shell of a gas turbine |
US9097123B2 (en) * | 2012-07-26 | 2015-08-04 | General Electric Company | Method and system for assembling and disassembling turbomachines |
US9382810B2 (en) * | 2012-07-27 | 2016-07-05 | General Electric Company | Closed loop cooling system for a gas turbine |
US9188062B2 (en) | 2012-08-30 | 2015-11-17 | Mitsubishi Hitachi Power Systems, Ltd. | Gas turbine |
EP2706198A1 (en) * | 2012-09-10 | 2014-03-12 | Alstom Technology Ltd | Method for removing an inner casing from a machine |
EP2706199B1 (en) | 2012-09-10 | 2018-12-12 | Ansaldo Energia Switzerland AG | Method and guide for removing an inner casing from a turbomachine |
WO2014126961A1 (en) | 2013-02-18 | 2014-08-21 | United Technologies Corporation | Cooling manifold for turbine section |
WO2014137471A1 (en) | 2013-03-07 | 2014-09-12 | Rivers Jonathan M | Gas turbine engine access panel |
US9453429B2 (en) | 2013-03-11 | 2016-09-27 | General Electric Company | Flow sleeve for thermal control of a double-wall turbine shell and related method |
US20140301834A1 (en) * | 2013-04-03 | 2014-10-09 | Barton M. Pepperman | Turbine cylinder cavity heated recirculation system |
JP6049565B2 (ja) * | 2013-07-31 | 2016-12-21 | 三菱日立パワーシステムズ株式会社 | 地熱タービン |
EP2851522A1 (de) * | 2013-09-19 | 2015-03-25 | Siemens Aktiengesellschaft | Drehvorrichtung für eine Gasturbine und Verfahren zum Drehen eines Bauteils |
US9759081B2 (en) | 2013-10-08 | 2017-09-12 | General Electric Company | Method and system to facilitate sealing in gas turbines |
JP6223774B2 (ja) * | 2013-10-15 | 2017-11-01 | 三菱日立パワーシステムズ株式会社 | ガスタービン |
JP6238056B2 (ja) | 2013-11-26 | 2017-11-29 | 三菱日立パワーシステムズ株式会社 | 静翼セグメントの取外用ダミーリングアッセンブリ、及びこれを用いた静翼セグメントの取外方法 |
US9708980B2 (en) | 2014-06-05 | 2017-07-18 | General Electric Company | Apparatus and system for compressor clearance control |
US9897318B2 (en) | 2014-10-29 | 2018-02-20 | General Electric Company | Method for diverting flow around an obstruction in an internal cooling circuit |
US20160326915A1 (en) * | 2015-05-08 | 2016-11-10 | General Electric Company | System and method for waste heat powered active clearance control |
US10113556B2 (en) | 2016-01-08 | 2018-10-30 | General Electric Company | Centrifugal compressor assembly for use in a turbine engine and method of assembly |
JP6499777B2 (ja) * | 2016-01-13 | 2019-04-10 | 三菱日立パワーシステムズ株式会社 | 翼引き抜き装置及び方法 |
US10138752B2 (en) * | 2016-02-25 | 2018-11-27 | General Electric Company | Active HPC clearance control |
US10415420B2 (en) * | 2016-04-08 | 2019-09-17 | United Technologies Corporation | Thermal lifting member for blade outer air seal support |
US10280802B2 (en) * | 2016-09-07 | 2019-05-07 | General Electric Company | Turbine casing jack |
US10641174B2 (en) | 2017-01-18 | 2020-05-05 | General Electric Company | Rotor shaft cooling |
JP6925862B2 (ja) * | 2017-05-16 | 2021-08-25 | 三菱パワー株式会社 | ガスタービン、及び翼環部の製造方法 |
US10883377B2 (en) * | 2017-10-27 | 2021-01-05 | Rolls-Royce North American Technolgies Inc. | System and method of controlling tip clearance in a shroud assembly for a bladed disc |
US10947993B2 (en) * | 2017-11-27 | 2021-03-16 | General Electric Company | Thermal gradient attenuation structure to mitigate rotor bow in turbine engine |
WO2019171495A1 (ja) * | 2018-03-07 | 2019-09-12 | 川崎重工業株式会社 | ガスタービンのシュラウド取付構造、シュラウド集合体及びシュラウド要素 |
JP6971924B2 (ja) * | 2018-07-06 | 2021-11-24 | 三菱重工コンプレッサ株式会社 | 持ち上げ治具、蒸気タービンの分解方法、蒸気タービンの部品交換方法、及び蒸気タービンの製造方法 |
CN109737578B (zh) * | 2018-12-28 | 2020-09-01 | 广东美的暖通设备有限公司 | 安装底座以及风管机风轮安装方法 |
CN111927579B (zh) * | 2020-07-31 | 2022-09-06 | 中国航发贵阳发动机设计研究所 | 一种涡轮机匣热变形调节结构及调节方法 |
US11879411B2 (en) | 2022-04-07 | 2024-01-23 | General Electric Company | System and method for mitigating bowed rotor in a gas turbine engine |
US11746678B1 (en) * | 2022-10-31 | 2023-09-05 | General Electric Company | Apparatus and method for protecting a replacement part of a turbine assembly |
WO2024199735A1 (en) * | 2023-03-31 | 2024-10-03 | Nuovo Pignone Tecnologie - S.R.L. | An expander with a pre-heating system and method |
Family Cites Families (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2453547A (en) * | 1944-01-28 | 1948-11-09 | United Aircraft Corp | Turbine construction |
GB826087A (en) * | 1956-11-14 | 1959-12-23 | John Cameron Mcgregor | Rigid assembly, particularly for gas turbine engines, capable of accommodating inaccuracies of alignment in one direction |
US2994472A (en) * | 1958-12-29 | 1961-08-01 | Gen Electric | Tip clearance control system for turbomachines |
FR1339482A (fr) * | 1961-11-28 | 1963-10-04 | Licentia Gmbh | Joint de rotor à segments annulaires d'étanchéité radialement mobiles, notammentpour turbo-moteurs |
GB969579A (en) * | 1962-11-09 | 1964-09-09 | Rolls Royce | Gas turbine engine |
CH425341A (de) * | 1965-07-23 | 1966-11-30 | Bbc Brown Boveri & Cie | Gasturbine mit Kühlung der Schaufelträger |
US3493212A (en) * | 1968-06-24 | 1970-02-03 | Westinghouse Electric Corp | Rotary machine apparatus |
US3628884A (en) * | 1970-06-26 | 1971-12-21 | Westinghouse Electric Corp | Method and apparatus for supporting an inner casing structure |
FR2275651A1 (fr) * | 1974-06-21 | 1976-01-16 | Snecma | Perfectionnements aux stators de turbomachines axiales |
FR2282550A1 (fr) * | 1974-08-21 | 1976-03-19 | Shur Lok International Sa | Stator de compresseur a carter monobloc |
US4023731A (en) * | 1974-12-19 | 1977-05-17 | General Electric Company | Thermal actuated valve for clearance control |
DE2607776C2 (de) * | 1976-02-26 | 1982-05-27 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | In der Meridianebene geteilte Deckscheibe für Radiallaufräder von Strömungsmaschinen, insbesondere Gasturbinentriebwerken |
US4230436A (en) * | 1978-07-17 | 1980-10-28 | General Electric Company | Rotor/shroud clearance control system |
US4329114A (en) * | 1979-07-25 | 1982-05-11 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Active clearance control system for a turbomachine |
US4304093A (en) * | 1979-08-31 | 1981-12-08 | General Electric Company | Variable clearance control for a gas turbine engine |
FR2467292A1 (fr) * | 1979-10-09 | 1981-04-17 | Snecma | Dispositif de reglage du jeu entre les aubes mobiles et l'anneau de turbine |
US4363599A (en) * | 1979-10-31 | 1982-12-14 | General Electric Company | Clearance control |
ATE16035T1 (de) * | 1980-05-19 | 1985-10-15 | Bbc Brown Boveri & Cie | Gekuehlter leitschaufeltraeger. |
GB2169962B (en) * | 1985-01-22 | 1988-07-13 | Rolls Royce | Blade tip clearance control |
DE3509359A1 (de) * | 1985-02-12 | 1986-08-14 | BBC Aktiengesellschaft Brown, Boveri & Cie., Baden, Aargau | Waermebewegliche durchfuehrung |
US4842477A (en) * | 1986-12-24 | 1989-06-27 | General Electric Company | Active clearance control |
US4928240A (en) * | 1988-02-24 | 1990-05-22 | General Electric Company | Active clearance control |
US5012420A (en) * | 1988-03-31 | 1991-04-30 | General Electric Company | Active clearance control for gas turbine engine |
US4893983A (en) * | 1988-04-07 | 1990-01-16 | General Electric Company | Clearance control system |
US4893984A (en) * | 1988-04-07 | 1990-01-16 | General Electric Company | Clearance control system |
US5104287A (en) * | 1989-09-08 | 1992-04-14 | General Electric Company | Blade tip clearance control apparatus for a gas turbine engine |
US5018942A (en) * | 1989-09-08 | 1991-05-28 | General Electric Company | Mechanical blade tip clearance control apparatus for a gas turbine engine |
FR2653171B1 (fr) * | 1989-10-18 | 1991-12-27 | Snecma | Carter de compresseur de turbomachine muni d'un dispositif de pilotage de son diametre interne. |
US5054997A (en) * | 1989-11-22 | 1991-10-08 | General Electric Company | Blade tip clearance control apparatus using bellcrank mechanism |
US5056988A (en) * | 1990-02-12 | 1991-10-15 | General Electric Company | Blade tip clearance control apparatus using shroud segment position modulation |
US5049033A (en) * | 1990-02-20 | 1991-09-17 | General Electric Company | Blade tip clearance control apparatus using cam-actuated shroud segment positioning mechanism |
US5100291A (en) * | 1990-03-28 | 1992-03-31 | General Electric Company | Impingement manifold |
US5281090A (en) * | 1990-04-03 | 1994-01-25 | General Electric Co. | Thermally-tuned rotary labyrinth seal with active seal clearance control |
US5127793A (en) * | 1990-05-31 | 1992-07-07 | General Electric Company | Turbine shroud clearance control assembly |
US5131811A (en) * | 1990-09-12 | 1992-07-21 | United Technologies Corporation | Fastener mounting for multi-stage compressor |
US5116199A (en) * | 1990-12-20 | 1992-05-26 | General Electric Company | Blade tip clearance control apparatus using shroud segment annular support ring thermal expansion |
US5281085A (en) * | 1990-12-21 | 1994-01-25 | General Electric Company | Clearance control system for separately expanding or contracting individual portions of an annular shroud |
US5228828A (en) * | 1991-02-15 | 1993-07-20 | General Electric Company | Gas turbine engine clearance control apparatus |
GB9103809D0 (en) * | 1991-02-23 | 1991-04-10 | Rolls Royce Plc | Blade tip clearance control apparatus |
US5212940A (en) * | 1991-04-16 | 1993-05-25 | General Electric Company | Tip clearance control apparatus and method |
US5167488A (en) * | 1991-07-03 | 1992-12-01 | General Electric Company | Clearance control assembly having a thermally-controlled one-piece cylindrical housing for radially positioning shroud segments |
US5205115A (en) * | 1991-11-04 | 1993-04-27 | General Electric Company | Gas turbine engine case counterflow thermal control |
US5219268A (en) * | 1992-03-06 | 1993-06-15 | General Electric Company | Gas turbine engine case thermal control flange |
US5333993A (en) * | 1993-03-01 | 1994-08-02 | General Electric Company | Stator seal assembly providing improved clearance control |
US5685693A (en) * | 1995-03-31 | 1997-11-11 | General Electric Co. | Removable inner turbine shell with bucket tip clearance control |
US8212940B2 (en) * | 2006-12-06 | 2012-07-03 | Dave Xiao Dong Yang | Hybrid architecture of TV receiving devices |
-
1995
- 1995-03-31 US US08/414,698 patent/US5685693A/en not_active Expired - Fee Related
- 1995-08-02 US US08/510,402 patent/US5779442A/en not_active Expired - Fee Related
-
1996
- 1996-02-06 IN IN211CA1996 patent/IN186474B/en unknown
- 1996-03-20 DE DE69611737T patent/DE69611737T2/de not_active Expired - Lifetime
- 1996-03-20 EP EP96301896A patent/EP0735243B1/en not_active Expired - Lifetime
- 1996-03-30 KR KR1019960009657A patent/KR100416014B1/ko not_active IP Right Cessation
- 1996-04-01 JP JP07861196A patent/JP3863938B2/ja not_active Expired - Lifetime
-
1997
- 1997-05-16 US US08/857,749 patent/US5913658A/en not_active Expired - Lifetime
- 1997-11-20 US US08/975,358 patent/US5906473A/en not_active Expired - Lifetime
-
1999
- 1999-02-12 US US09/249,047 patent/US6082963A/en not_active Expired - Lifetime
- 1999-04-19 US US09/293,920 patent/US6079943A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0735243A2 (en) | 1996-10-02 |
DE69611737D1 (de) | 2001-03-15 |
JP3863938B2 (ja) | 2006-12-27 |
JPH094411A (ja) | 1997-01-07 |
US5779442A (en) | 1998-07-14 |
EP0735243B1 (en) | 2001-02-07 |
KR960034694A (ko) | 1996-10-24 |
DE69611737T2 (de) | 2002-03-07 |
US5906473A (en) | 1999-05-25 |
US6082963A (en) | 2000-07-04 |
US5913658A (en) | 1999-06-22 |
US5685693A (en) | 1997-11-11 |
KR100416014B1 (ko) | 2004-04-28 |
EP0735243A3 (en) | 1996-12-04 |
US6079943A (en) | 2000-06-27 |