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
Application number
Other languages
English (en)
Inventor
Brendan Francis Sexton
Hans Milton Kunijt
Sacheverel Quentin Eldrid
Albert Myers
Kyle Ethan Coneybeer
David Martin Johnson
Iain Roberton Kellock
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IN186474B publication Critical patent/IN186474B/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
    • 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)
IN211CA1996 1995-03-31 1996-02-06 IN186474B (ja)

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 (ja) 2001-09-08

Family

ID=23642564

Family Applications (1)

Application Number Title Priority Date Filing Date
IN211CA1996 IN186474B (ja) 1995-03-31 1996-02-06

Country Status (6)

Country Link
US (6) US5685693A (ja)
EP (1) EP0735243B1 (ja)
JP (1) JP3863938B2 (ja)
KR (1) KR100416014B1 (ja)
DE (1) DE69611737T2 (ja)
IN (1) IN186474B (ja)

Families Citing this family (116)

* Cited by examiner, † Cited by third party
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
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
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
DE102006004785A1 (de) * 2006-02-02 2007-08-30 Alstom Technology Ltd. Strömungsmaschine
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
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
PL1905948T3 (pl) * 2006-09-12 2013-03-29 Cryostar Sas Urządzenie do odzyskiwania energii
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
KR101148813B1 (ko) * 2007-10-23 2012-05-24 미츠비시 쥬고교 가부시키가이샤 날개 고리를 떼어내는 방법, 날개 고리를 떼어내는 부재
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
US20110100020A1 (en) * 2009-10-30 2011-05-05 General Electric Company Apparatus and method for turbine engine cooling
US20110103939A1 (en) * 2009-10-30 2011-05-05 General Electric Company Turbine rotor blade tip and shroud clearance control
EP2513431A1 (en) * 2009-12-17 2012-10-24 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
EP2706199B1 (en) * 2012-09-10 2018-12-12 Ansaldo Energia Switzerland AG Method and guide for removing an inner casing from a turbomachine
EP2706198A1 (en) * 2012-09-10 2014-03-12 Alstom Technology Ltd Method for removing an inner casing from a machine
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
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
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
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)

* Cited by examiner, † Cited by third party
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
CH397360A (de) * 1961-11-28 1965-08-15 Licentia Gmbh Rotordichtung mit radial beweglichen Dichtringsegmenten, insbesondere bei Turbomaschinen
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
DE3071161D1 (en) * 1980-05-19 1985-11-14 Bbc Brown Boveri & Cie Cooled turbine stator
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
US5018942A (en) * 1989-09-08 1991-05-28 General Electric Company Mechanical blade tip clearance control apparatus for a gas turbine engine
US5104287A (en) * 1989-09-08 1992-04-14 General Electric Company 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

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

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