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 (ko) | 2001-09-08 |
Family
ID=23642564
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IN211CA1996 IN186474B (ko) | 1995-03-31 | 1996-02-06 |
Country Status (6)
Country | Link |
---|---|
US (6) | US5685693A (ko) |
EP (1) | EP0735243B1 (ko) |
JP (1) | JP3863938B2 (ko) |
KR (1) | KR100416014B1 (ko) |
DE (1) | DE69611737T2 (ko) |
IN (1) | IN186474B (ko) |
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 |
CA2228350C (en) * | 1998-01-29 | 2001-05-01 | Kiyoshi Suenaga | Heat recovery type gas turbine |
DE69828274T2 (de) * | 1998-02-03 | 2005-12-15 | Mitsubishi Heavy Industries, Ltd. | Gasturbine für eine gas-dampfkraftzentrale |
US6105363A (en) * | 1998-04-27 | 2000-08-22 | Siemens Westinghouse Power Corporation | Cooling scheme for turbine hot parts |
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US6139182A (en) * | 1999-03-01 | 2000-10-31 | Thermoscan, Inc | Enhanced protective cover for use in an IR thermometer |
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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 |
US6468031B1 (en) | 2000-05-16 | 2002-10-22 | General Electric Company | Nozzle cavity impingement/area reduction insert |
US6435814B1 (en) | 2000-05-16 | 2002-08-20 | General Electric Company | Film cooling air pocket in a closed loop cooled airfoil |
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 |
EP1918547B1 (en) * | 2002-06-25 | 2017-05-03 | 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 |
US7434402B2 (en) * | 2005-03-29 | 2008-10-14 | Siemens Power Generation, Inc. | System for actively controlling compressor clearances |
WO2006103152A1 (de) * | 2005-03-29 | 2006-10-05 | Alstom Technology Ltd | Verfahren und vorrichtung zum austausch von bauteilen einer strömungsrotationsmaschine |
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 |
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GB2450061B (en) | 2006-03-14 | 2011-12-21 | Cambridge Res And Dev Ltd | Rotor for a Radial-Flow Turbine and Method of Driving a Rotor |
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PL1905948T3 (pl) * | 2006-09-12 | 2013-03-29 | Cryostar Sas | Urządzenie do odzyskiwania energii |
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FR2925109B1 (fr) * | 2007-12-14 | 2015-05-15 | Snecma | Module de turbomachine muni d'un dispositif d'amelioration des jeux radiaux |
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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 |
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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 |
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US8453454B2 (en) | 2010-04-14 | 2013-06-04 | General Electric Company | Coannular oil injection nozzle |
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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 |
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EP2706199B1 (en) * | 2012-09-10 | 2018-12-12 | Ansaldo Energia Switzerland AG | Method and guide for removing an inner casing from a turbomachine |
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EP2956645B1 (en) * | 2013-02-18 | 2017-12-13 | United Technologies Corporation | Cooling manifold for turbine section |
US9759095B2 (en) | 2013-03-07 | 2017-09-12 | Rolls-Royce Corporation | 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 |
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CN108474264B (zh) * | 2016-01-13 | 2020-10-09 | 三菱日立电力系统株式会社 | 叶片取出装置及方法 |
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 |
JP7065941B2 (ja) * | 2018-03-07 | 2022-05-12 | 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 |
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-
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 EP EP96301896A patent/EP0735243B1/en not_active Expired - Lifetime
- 1996-03-20 DE DE69611737T patent/DE69611737T2/de 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 |
---|---|
EP0735243A3 (en) | 1996-12-04 |
US5685693A (en) | 1997-11-11 |
KR100416014B1 (ko) | 2004-04-28 |
EP0735243B1 (en) | 2001-02-07 |
US5779442A (en) | 1998-07-14 |
US6079943A (en) | 2000-06-27 |
KR960034694A (ko) | 1996-10-24 |
JPH094411A (ja) | 1997-01-07 |
JP3863938B2 (ja) | 2006-12-27 |
EP0735243A2 (en) | 1996-10-02 |
US5913658A (en) | 1999-06-22 |
DE69611737T2 (de) | 2002-03-07 |
DE69611737D1 (de) | 2001-03-15 |
US5906473A (en) | 1999-05-25 |
US6082963A (en) | 2000-07-04 |