BE669775A - - Google Patents

Info

Publication number
BE669775A
BE669775A BE669775DA BE669775A BE 669775 A BE669775 A BE 669775A BE 669775D A BE669775D A BE 669775DA BE 669775 A BE669775 A BE 669775A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE669775A publication Critical patent/BE669775A/xx

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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE669775D 1964-11-17 1965-09-17 BE669775A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US411821A US3300180A (en) 1964-11-17 1964-11-17 Segmented diaphragm assembly

Publications (1)

Publication Number Publication Date
BE669775A true BE669775A (de) 1966-03-17

Family

ID=23630462

Family Applications (1)

Application Number Title Priority Date Filing Date
BE669775D BE669775A (de) 1964-11-17 1965-09-17

Country Status (5)

Country Link
US (1) US3300180A (de)
BE (1) BE669775A (de)
DE (1) DE1426885B2 (de)
GB (1) GB1109457A (de)
NL (1) NL6513461A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0707150A3 (de) * 1994-10-14 1998-01-07 Asea Brown Boveri Ag Verdichtung
DE102009004934A1 (de) * 2009-01-16 2010-08-19 Mtu Aero Engines Gmbh Verfahren zur Montage eines integralen Innenrings eines Turboverdichterstators

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3443791A (en) * 1966-11-23 1969-05-13 United Aircraft Corp Turbine vane assembly
US3408048A (en) * 1967-05-26 1968-10-29 Westinghouse Electric Corp Diaphragm sealing structure
US3536414A (en) * 1968-03-06 1970-10-27 Gen Electric Vanes for turning fluid flow in an annular duct
JPS59120704A (ja) * 1982-12-27 1984-07-12 Toshiba Corp 超高温耐熱壁体
US5772401A (en) * 1995-10-13 1998-06-30 Dresser-Rand Company Diaphragm construction for turbomachinery
DE19547653C2 (de) * 1995-12-20 1999-08-19 Abb Patent Gmbh Leitvorrichtung für eine Turbine mit einem Leitschaufelträger und Verfahren zur Herstellung dieser Leitvorrichtung
US6425738B1 (en) * 2000-05-11 2002-07-30 General Electric Company Accordion nozzle
US6609881B2 (en) * 2001-11-15 2003-08-26 General Electric Company Steam turbine inlet and methods of retrofitting
RU2217598C1 (ru) * 2002-07-22 2003-11-27 Баринберг Григорий Давидович Система подвода пара к цилиндру турбины
US20060088409A1 (en) * 2004-10-21 2006-04-27 General Electric Company Grouped reaction nozzle tip shrouds with integrated seals
RU2296228C2 (ru) * 2005-06-16 2007-03-27 Закрытое акционерное общество "ЭНТЭК" Проточная часть паровой турбины
US20070053773A1 (en) * 2005-09-07 2007-03-08 General Electric Company Integrated nozzle wheel for reaction steam turbine stationary components and related method
RU2307254C1 (ru) * 2006-02-20 2007-09-27 Открытое Акционерное Общество "Теплоэнергосервис-ЭК" (ОАО "Теплоэнергосервис-ЭК") Сопловая коробка для высокотемпературного цилиндра паровой турбины
US7645117B2 (en) 2006-05-05 2010-01-12 General Electric Company Rotary machines and methods of assembling
JP2008169705A (ja) * 2007-01-09 2008-07-24 Toshiba Corp 蒸気タービン
US8887390B2 (en) 2008-08-15 2014-11-18 Dresser-Rand Company Method for correcting downstream deflection in gas turbine nozzles
US8226360B2 (en) * 2008-10-31 2012-07-24 General Electric Company Crenelated turbine nozzle
EP2211023A1 (de) * 2009-01-21 2010-07-28 Siemens Aktiengesellschaft Leitschaufelsystem für eine Strömungsmaschine mit segmentiertem Leitschaufelträger
US8157517B2 (en) * 2009-04-27 2012-04-17 Elliott Company Boltless multi-part diaphragm for use with a centrifugal compressor
US8123474B2 (en) * 2009-05-12 2012-02-28 Dresser-Rand Company Repair of industrial gas turbine nozzle diaphragm packing
JP5342579B2 (ja) * 2011-02-28 2013-11-13 三菱重工業株式会社 回転機械の静翼ユニット、回転機械の静翼ユニットの製造方法及び回転機械の静翼ユニットの結合方法
EP2644833A1 (de) * 2012-03-26 2013-10-02 Alstom Technology Ltd Trägerring
JP6546053B2 (ja) * 2015-09-18 2019-07-17 株式会社東芝 組立式ノズルダイヤフラム及び蒸気タービン
WO2017145190A1 (ja) * 2016-02-23 2017-08-31 三菱重工コンプレッサ株式会社 蒸気タービン
JP6505860B2 (ja) * 2016-03-15 2019-04-24 東芝エネルギーシステムズ株式会社 タービン及びタービン静翼
CN111396140B (zh) * 2020-03-31 2023-01-31 中国航发动力股份有限公司 一种设置有止动结构的静叶环及其加工方法
CN113352134A (zh) * 2021-07-12 2021-09-07 重庆江增船舶重工有限公司 一种过定位式零件的制造方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2197521A (en) * 1938-04-21 1940-04-16 Westinghouse Electric & Mfg Co Turbine apparatus
GB633022A (en) * 1946-09-19 1949-12-05 Svenska Turbinfab Ab Guide blade system for rotary elastic fluid machines
US2609176A (en) * 1950-01-21 1952-09-02 A V Roe Canada Ltd Turbine nozzle guide vane construction
US2654566A (en) * 1950-02-11 1953-10-06 A V Roe Canada Ltd Turbine nozzle guide vane construction

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0707150A3 (de) * 1994-10-14 1998-01-07 Asea Brown Boveri Ag Verdichtung
DE102009004934A1 (de) * 2009-01-16 2010-08-19 Mtu Aero Engines Gmbh Verfahren zur Montage eines integralen Innenrings eines Turboverdichterstators
DE102009004934B4 (de) 2009-01-16 2021-08-26 MTU Aero Engines AG Verfahren zur Montage eines integralen Innenrings eines Turboverdichterstators

Also Published As

Publication number Publication date
DE1426885A1 (de) 1969-10-23
GB1109457A (en) 1968-04-10
NL6513461A (de) 1966-05-18
DE1426885B2 (de) 1971-02-18
US3300180A (en) 1967-01-24

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