DE60215109T2 - Verbundgewebeschlauchdichtung für eine Kontaktfläche zwischen Mantel und Gasturbinendüse - Google Patents

Verbundgewebeschlauchdichtung für eine Kontaktfläche zwischen Mantel und Gasturbinendüse Download PDF

Info

Publication number
DE60215109T2
DE60215109T2 DE60215109T DE60215109T DE60215109T2 DE 60215109 T2 DE60215109 T2 DE 60215109T2 DE 60215109 T DE60215109 T DE 60215109T DE 60215109 T DE60215109 T DE 60215109T DE 60215109 T2 DE60215109 T2 DE 60215109T2
Authority
DE
Germany
Prior art keywords
cavity
gas turbine
seal
shell
retaining ring
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 - Lifetime
Application number
DE60215109T
Other languages
German (de)
English (en)
Other versions
DE60215109D1 (de
Inventor
Abdul-Azeez Schenectady Mohammed-Fakir
Mahmut Faruk Erenkoy Aksit
Ahmad Gulshan-e Iqbal Safi
Srikanth Niskayuna Vedantam
Ning West Chester Fang
Gayle Hobbs Greenville Goetze
Brian Peter Simpsonville Arness
Wei-Ming Fremont Chi
John Ellington Simpsonville Greene
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE60215109D1 publication Critical patent/DE60215109D1/de
Application granted granted Critical
Publication of DE60215109T2 publication Critical patent/DE60215109T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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)
DE60215109T 2001-12-28 2002-12-23 Verbundgewebeschlauchdichtung für eine Kontaktfläche zwischen Mantel und Gasturbinendüse Expired - Lifetime DE60215109T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/029,216 US6609886B2 (en) 2001-12-28 2001-12-28 Composite tubular woven seal for gas turbine nozzle and shroud interface
US29216 2001-12-28

Publications (2)

Publication Number Publication Date
DE60215109D1 DE60215109D1 (de) 2006-11-16
DE60215109T2 true DE60215109T2 (de) 2007-05-16

Family

ID=21847863

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60215109T Expired - Lifetime DE60215109T2 (de) 2001-12-28 2002-12-23 Verbundgewebeschlauchdichtung für eine Kontaktfläche zwischen Mantel und Gasturbinendüse

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
CN104508251B (zh) 2012-04-27 2016-08-24 通用电气公司 用于燃气涡轮发动机的护罩组件和密封件
US11125098B2 (en) 2019-09-11 2021-09-21 Raytheon Technologies Corporation Blade outer air seal with face seal

Family Cites Families (8)

* 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
DE3003470C2 (de) * 1980-01-31 1982-02-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Turbinenleitschaufelaufhängung für Gasturbinenstrahltriebwerke
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
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
US5657998A (en) * 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine
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

Also Published As

Publication number Publication date
US20030123978A1 (en) 2003-07-03
KR20030057409A (ko) 2003-07-04
JP2003227356A (ja) 2003-08-15
EP1323957A3 (en) 2004-01-28
EP1323957B1 (en) 2006-10-04
DE60215109D1 (de) 2006-11-16
US6609886B2 (en) 2003-08-26
EP1323957A2 (en) 2003-07-02
KR100818821B1 (ko) 2008-04-01
JP4139212B2 (ja) 2008-08-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition