JP2004060657A - 蒸気タービンダイアフラムの段間パッキンシールのための端面間隙シール及びそれを組込む方法 - Google Patents

蒸気タービンダイアフラムの段間パッキンシールのための端面間隙シール及びそれを組込む方法 Download PDF

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Publication number
JP2004060657A
JP2004060657A JP2003280540A JP2003280540A JP2004060657A JP 2004060657 A JP2004060657 A JP 2004060657A JP 2003280540 A JP2003280540 A JP 2003280540A JP 2003280540 A JP2003280540 A JP 2003280540A JP 2004060657 A JP2004060657 A JP 2004060657A
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Japan
Prior art keywords
seal
circumferentially
segments
spline
rotor
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Pending
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JP2003280540A
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English (en)
Japanese (ja)
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JP2004060657A5 (enExample
Inventor
Sebastian Burdick Steven
スティーブン・セバスチャン・バーディック
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2004060657A publication Critical patent/JP2004060657A/ja
Publication of JP2004060657A5 publication Critical patent/JP2004060657A5/ja
Pending legal-status Critical Current

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    • 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
    • F01D11/005—Sealing means between non relatively rotating elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Gasket Seals (AREA)
JP2003280540A 2002-07-29 2003-07-28 蒸気タービンダイアフラムの段間パッキンシールのための端面間隙シール及びそれを組込む方法 Pending JP2004060657A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/206,828 US20040017050A1 (en) 2002-07-29 2002-07-29 Endface gap sealing for steam turbine diaphragm interstage packing seals and methods of retrofitting

Publications (2)

Publication Number Publication Date
JP2004060657A true JP2004060657A (ja) 2004-02-26
JP2004060657A5 JP2004060657A5 (enExample) 2006-09-07

Family

ID=30115187

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003280540A Pending JP2004060657A (ja) 2002-07-29 2003-07-28 蒸気タービンダイアフラムの段間パッキンシールのための端面間隙シール及びそれを組込む方法

Country Status (5)

Country Link
US (2) US20040017050A1 (enExample)
EP (1) EP1387043B1 (enExample)
JP (1) JP2004060657A (enExample)
CN (1) CN100396884C (enExample)
AT (1) ATE524637T1 (enExample)

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US7780407B2 (en) * 2006-01-04 2010-08-24 General Electric Company Rotary machines and methods of assembling
FR2902843A1 (fr) * 2006-06-23 2007-12-28 Snecma Sa Secteur de redresseur de compresseur ou secteur de distributeur de turbomachine
US8142142B2 (en) * 2008-09-05 2012-03-27 Siemens Energy, Inc. Turbine transition duct apparatus
US20110164965A1 (en) * 2010-01-06 2011-07-07 General Electric Company Steam turbine stationary component seal
US8201834B1 (en) * 2010-04-26 2012-06-19 Florida Turbine Technologies, Inc. Turbine vane mate face seal assembly
US8348280B2 (en) 2010-10-22 2013-01-08 General Electric Company Seal apparatus
US20120292856A1 (en) * 2011-05-16 2012-11-22 United Technologies Corporation Blade outer seal for a gas turbine engine having non-parallel segment confronting faces
US20130177383A1 (en) * 2012-01-05 2013-07-11 General Electric Company Device and method for sealing a gas path in a turbine
US8845285B2 (en) * 2012-01-10 2014-09-30 General Electric Company Gas turbine stator assembly
US8905708B2 (en) * 2012-01-10 2014-12-09 General Electric Company Turbine assembly and method for controlling a temperature of an assembly
US9382813B2 (en) 2012-12-04 2016-07-05 General Electric Company Turbomachine diaphragm ring with packing retainment apparatus
US9359913B2 (en) 2013-02-27 2016-06-07 General Electric Company Steam turbine inner shell assembly with common grooves
US10156150B2 (en) 2013-03-14 2018-12-18 United Technologies Corporation Gas turbine engine stator vane platform cooling
US10156148B2 (en) * 2015-03-31 2018-12-18 Siemens Aktiengesellschaft Transition duct assembly
FR3036432B1 (fr) * 2015-05-22 2019-04-19 Safran Ceramics Ensemble d'anneau de turbine avec maintien axial
FR3040461B1 (fr) * 2015-09-02 2018-02-23 Safran Aircraft Engines Element de joint d'etancheite a labyrinthe pour turbine
US11248705B2 (en) 2018-06-19 2022-02-15 General Electric Company Curved seal with relief cuts for adjacent gas turbine components
US10982559B2 (en) * 2018-08-24 2021-04-20 General Electric Company Spline seal with cooling features for turbine engines
US11187094B2 (en) 2019-08-26 2021-11-30 General Electric Company Spline for a turbine engine

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US4063845A (en) * 1975-06-04 1977-12-20 General Motors Corporation Turbomachine stator interstage seal
JPS60118306U (ja) * 1984-01-20 1985-08-10 株式会社日立製作所 流体機械における静翼部のシ−ル装置
JPS62248804A (ja) * 1986-04-22 1987-10-29 Toshiba Corp タ−ビンのシ−ル部間隙調整装置
JPS644805U (enExample) * 1987-06-30 1989-01-12
JPH0315605A (ja) * 1989-06-13 1991-01-24 Mitsubishi Heavy Ind Ltd 蒸気タービン
US5524340A (en) * 1994-09-13 1996-06-11 General Electric Co. Method for modifying a turbine diaphragm for use with a reduced rotor lan diameter
JPH11257014A (ja) * 1998-03-06 1999-09-21 Toshiba Corp 軸流タービンの作動流体漏洩防止装置
JP2000034904A (ja) * 1998-04-28 2000-02-02 General Electric Co <Ge> ダイアフラムパッキンリングダブテ―ル上のフック直径を設定する方法
JP2000154877A (ja) * 1998-08-10 2000-06-06 General Electric Co <Ge> シ―ルアセンブリ並びに該シ―ルアセンブリを含む回転機械
US20010007384A1 (en) * 1992-11-19 2001-07-12 General Electric Company Combined brush seal and labyrinth seal segment for rotary machines

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GB1081458A (en) * 1965-12-28 1967-08-31 Rolls Royce Blade assembly for a fluid flow machine such as a gas turbine engine
US3728041A (en) * 1971-10-04 1973-04-17 Gen Electric Fluidic seal for segmented nozzle diaphragm
US4002288A (en) * 1976-04-21 1977-01-11 Klupt Carle D Food container
CH626947A5 (enExample) * 1978-03-02 1981-12-15 Bbc Brown Boveri & Cie
US4537024A (en) * 1979-04-23 1985-08-27 Solar Turbines, Incorporated Turbine engines
US4436311A (en) * 1982-04-20 1984-03-13 Brandon Ronald E Segmented labyrinth-type shaft sealing system for fluid turbines
US4749333A (en) * 1986-05-12 1988-06-07 The United States Of America As Represented By The Secretary Of The Air Force Vane platform sealing and retention means
US4820119A (en) * 1988-05-23 1989-04-11 United Technologies Corporation Inner turbine seal
US5002288A (en) * 1988-10-13 1991-03-26 General Electric Company Positive variable clearance labyrinth seal
US5158430A (en) * 1990-09-12 1992-10-27 United Technologies Corporation Segmented stator vane seal
US5154577A (en) * 1991-01-17 1992-10-13 General Electric Company Flexible three-piece seal assembly
US5224822A (en) * 1991-05-13 1993-07-06 General Electric Company Integral turbine nozzle support and discourager seal
US5271714A (en) * 1992-07-09 1993-12-21 General Electric Company Turbine nozzle support arrangement
US5249920A (en) * 1992-07-09 1993-10-05 General Electric Company Turbine nozzle seal arrangement
US5271712A (en) * 1993-01-06 1993-12-21 Brandon Ronald E Turbine geometry to reduce damage from hard particles
US5429478A (en) * 1994-03-31 1995-07-04 United Technologies Corporation Airfoil having a seal and an integral heat shield
US5657998A (en) * 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine
US5586773A (en) * 1995-06-19 1996-12-24 General Electric Company Gas-path leakage seal for a gas turbine made from metallic mesh
US5624227A (en) * 1995-11-07 1997-04-29 General Electric Co. Seal for gas turbines
US5709530A (en) * 1996-09-04 1998-01-20 United Technologies Corporation Gas turbine vane seal
JP3416447B2 (ja) * 1997-03-11 2003-06-16 三菱重工業株式会社 ガスタービンの翼冷却空気供給システム
US5934687A (en) * 1997-07-07 1999-08-10 General Electric Company Gas-path leakage seal for a turbine
US6193240B1 (en) * 1999-01-11 2001-02-27 General Electric Company Seal assembly
US6394459B1 (en) * 2000-06-16 2002-05-28 General Electric Company Multi-clearance labyrinth seal design and related process
US6722850B2 (en) * 2002-07-22 2004-04-20 General Electric Company Endface gap sealing of steam turbine packing seal segments and retrofitting thereof

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4063845A (en) * 1975-06-04 1977-12-20 General Motors Corporation Turbomachine stator interstage seal
JPS60118306U (ja) * 1984-01-20 1985-08-10 株式会社日立製作所 流体機械における静翼部のシ−ル装置
JPS62248804A (ja) * 1986-04-22 1987-10-29 Toshiba Corp タ−ビンのシ−ル部間隙調整装置
JPS644805U (enExample) * 1987-06-30 1989-01-12
JPH0315605A (ja) * 1989-06-13 1991-01-24 Mitsubishi Heavy Ind Ltd 蒸気タービン
US20010007384A1 (en) * 1992-11-19 2001-07-12 General Electric Company Combined brush seal and labyrinth seal segment for rotary machines
US5524340A (en) * 1994-09-13 1996-06-11 General Electric Co. Method for modifying a turbine diaphragm for use with a reduced rotor lan diameter
JPH11257014A (ja) * 1998-03-06 1999-09-21 Toshiba Corp 軸流タービンの作動流体漏洩防止装置
JP2000034904A (ja) * 1998-04-28 2000-02-02 General Electric Co <Ge> ダイアフラムパッキンリングダブテ―ル上のフック直径を設定する方法
JP2000154877A (ja) * 1998-08-10 2000-06-06 General Electric Co <Ge> シ―ルアセンブリ並びに該シ―ルアセンブリを含む回転機械

Also Published As

Publication number Publication date
CN100396884C (zh) 2008-06-25
US7097423B2 (en) 2006-08-29
CN1475655A (zh) 2004-02-18
US20040239051A1 (en) 2004-12-02
EP1387043A3 (en) 2005-11-02
ATE524637T1 (de) 2011-09-15
EP1387043B1 (en) 2011-09-14
EP1387043A2 (en) 2004-02-04
US20040017050A1 (en) 2004-01-29

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