KR100818821B1 - 가스 터빈 - Google Patents

가스 터빈 Download PDF

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Publication number
KR100818821B1
KR100818821B1 KR1020020084835A KR20020084835A KR100818821B1 KR 100818821 B1 KR100818821 B1 KR 100818821B1 KR 1020020084835 A KR1020020084835 A KR 1020020084835A KR 20020084835 A KR20020084835 A KR 20020084835A KR 100818821 B1 KR100818821 B1 KR 100818821B1
Authority
KR
South Korea
Prior art keywords
turbine
seal
cavity
retaining ring
seal body
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
KR1020020084835A
Other languages
English (en)
Korean (ko)
Other versions
KR20030057409A (ko
Inventor
아크시트마흐무트파루크
사피아마드
모하메드-파키르압둘-아지즈
베단탐스리칸쓰
팡닝
고에쩨게일홉스
아네스브라이언피터
그리네존엘밍톤
치웨이-밍
Original Assignee
제너럴 일렉트릭 캄파니
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 제너럴 일렉트릭 캄파니 filed Critical 제너럴 일렉트릭 캄파니
Publication of KR20030057409A publication Critical patent/KR20030057409A/ko
Application granted granted Critical
Publication of KR100818821B1 publication Critical patent/KR100818821B1/ko
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • 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
    • F02C7/28—Arrangement of seals
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
    • F16J15/0887—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing the sealing effect being obtained by elastic deformation of the packing
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/02—Sealings between relatively-stationary surfaces
    • F16J15/06—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/08—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
    • F16J15/0806—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment
    • F16J15/0812—Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment with a braided or knitted body

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
KR1020020084835A 2001-12-28 2002-12-27 가스 터빈 Expired - Fee Related KR100818821B1 (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/029,216 2001-12-28
US10/029,216 US6609886B2 (en) 2001-12-28 2001-12-28 Composite tubular woven seal for gas turbine nozzle and shroud interface

Publications (2)

Publication Number Publication Date
KR20030057409A KR20030057409A (ko) 2003-07-04
KR100818821B1 true KR100818821B1 (ko) 2008-04-01

Family

ID=21847863

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020020084835A Expired - Fee Related KR100818821B1 (ko) 2001-12-28 2002-12-27 가스 터빈

Country Status (5)

Country Link
US (1) US6609886B2 (enExample)
EP (1) EP1323957B1 (enExample)
JP (1) JP4139212B2 (enExample)
KR (1) KR100818821B1 (enExample)
DE (1) DE60215109T2 (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6742988B2 (en) * 2002-10-30 2004-06-01 General Electric Company Composite tubular woven seal for steam turbine diaphragm horizontal joint interfaces
US7152864B2 (en) 2003-10-02 2006-12-26 Alstom Technology Ltd. Seal assembly
US7562880B2 (en) * 2004-02-09 2009-07-21 Siemens Energy, Inc. Seal usable between thermally movable components
US7188477B2 (en) * 2004-04-21 2007-03-13 United Technologies Corporation High temperature dynamic seal for scramjet variable geometry
US7094026B2 (en) * 2004-04-29 2006-08-22 General Electric Company System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor
US7052234B2 (en) 2004-06-23 2006-05-30 General Electric Company Turbine vane collar seal
GB2434184B (en) * 2006-01-12 2007-12-12 Rolls Royce Plc A sealing arrangement
US20070237629A1 (en) * 2006-04-05 2007-10-11 General Electric Company Gas turbine compressor casing flowpath rings
DE102008057207A1 (de) * 2008-11-13 2010-05-27 Continental Mechanical Components Germany Gmbh Welleneinrichtung mit einer Dichtungsvorrichtung
US20110189008A1 (en) * 2010-01-29 2011-08-04 General Electric Company Retaining ring for a turbine nozzle with improved thermal isolation
US8613451B2 (en) 2010-11-29 2013-12-24 General Electric Company Cloth seal for turbo-machinery
US9534500B2 (en) 2011-04-27 2017-01-03 Pratt & Whitney Canada Corp. Seal arrangement for segmented gas turbine engine components
WO2013163505A1 (en) 2012-04-27 2013-10-31 General Electric Company Shroud assembly and seal for a gas turbine engine
US11125098B2 (en) 2019-09-11 2021-09-21 Raytheon Technologies Corporation Blade outer air seal with face seal

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4384822A (en) * 1980-01-31 1983-05-24 Motoren- Und Turbinen-Union Munchen Gmbh Turbine nozzle vane suspension for gas turbine engines
US4815933A (en) 1987-11-13 1989-03-28 The United States Of America As Represented By The Secretary Of The Air Force Nozzle flange attachment and sealing arrangement
US5657998A (en) * 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3894742A (en) * 1973-07-20 1975-07-15 Hitco Rope sealing means
US5301595A (en) * 1992-06-25 1994-04-12 General Motors Corporation High temperature rope seal type joint packing
US5372476A (en) * 1993-06-18 1994-12-13 General Electric Company Turbine nozzle support assembly
US6039325A (en) * 1996-10-17 2000-03-21 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Resilient braided rope seal
US6076835A (en) * 1997-05-21 2000-06-20 Allison Advanced Development Company Interstage van seal apparatus

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4384822A (en) * 1980-01-31 1983-05-24 Motoren- Und Turbinen-Union Munchen Gmbh Turbine nozzle vane suspension for gas turbine engines
US4815933A (en) 1987-11-13 1989-03-28 The United States Of America As Represented By The Secretary Of The Air Force Nozzle flange attachment and sealing arrangement
US5657998A (en) * 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine

Also Published As

Publication number Publication date
US20030123978A1 (en) 2003-07-03
EP1323957A2 (en) 2003-07-02
DE60215109D1 (de) 2006-11-16
DE60215109T2 (de) 2007-05-16
US6609886B2 (en) 2003-08-26
JP2003227356A (ja) 2003-08-15
EP1323957A3 (en) 2004-01-28
JP4139212B2 (ja) 2008-08-27
EP1323957B1 (en) 2006-10-04
KR20030057409A (ko) 2003-07-04

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