DE69409332T2 - Dichtung in einer Gasturbine - Google Patents

Dichtung in einer Gasturbine

Info

Publication number
DE69409332T2
DE69409332T2 DE69409332T DE69409332T DE69409332T2 DE 69409332 T2 DE69409332 T2 DE 69409332T2 DE 69409332 T DE69409332 T DE 69409332T DE 69409332 T DE69409332 T DE 69409332T DE 69409332 T2 DE69409332 T2 DE 69409332T2
Authority
DE
Germany
Prior art keywords
seal
gas turbine
turbine
gas
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
DE69409332T
Other languages
English (en)
Other versions
DE69409332D1 (de
Inventor
George W Kelch
Thomas A Auxier
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69409332D1 publication Critical patent/DE69409332D1/de
Application granted granted Critical
Publication of DE69409332T2 publication Critical patent/DE69409332T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • 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
    • F01D25/12—Cooling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69409332T 1993-12-13 1994-12-12 Dichtung in einer Gasturbine Expired - Lifetime DE69409332T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/166,426 US5374161A (en) 1993-12-13 1993-12-13 Blade outer air seal cooling enhanced with inter-segment film slot

Publications (2)

Publication Number Publication Date
DE69409332D1 DE69409332D1 (de) 1998-05-07
DE69409332T2 true DE69409332T2 (de) 1998-10-29

Family

ID=22603259

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69409332T Expired - Lifetime DE69409332T2 (de) 1993-12-13 1994-12-12 Dichtung in einer Gasturbine

Country Status (4)

Country Link
US (1) US5374161A (de)
EP (1) EP0657625B1 (de)
JP (1) JP3607331B2 (de)
DE (1) DE69409332T2 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004037356B4 (de) * 2004-07-30 2017-11-23 Ansaldo Energia Ip Uk Limited Wandstruktur zur Begrenzung eines Heißgaspfads

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US5486090A (en) * 1994-03-30 1996-01-23 United Technologies Corporation Turbine shroud segment with serpentine cooling channels
US5531457A (en) * 1994-12-07 1996-07-02 Pratt & Whitney Canada, Inc. Gas turbine engine feather seal arrangement
US5538393A (en) * 1995-01-31 1996-07-23 United Technologies Corporation Turbine shroud segment with serpentine cooling channels having a bend passage
EP0852659B1 (de) * 1995-09-29 2002-04-03 Siemens Aktiengesellschaft Dichtelement zur dichtung eines spaltes sowie gasturbinenanlage
US5823741A (en) * 1996-09-25 1998-10-20 General Electric Co. Cooling joint connection for abutting segments in a gas turbine engine
EP0902167B1 (de) * 1997-09-15 2003-10-29 ALSTOM (Switzerland) Ltd Kühlvorrichtung für Gasturbinenkomponenten
GB9725623D0 (en) 1997-12-03 2006-09-20 Rolls Royce Plc Improvements in or relating to a blade tip clearance system
GB9815611D0 (en) 1998-07-18 1998-09-16 Rolls Royce Plc Improvements in or relating to turbine cooling
US6393331B1 (en) 1998-12-16 2002-05-21 United Technologies Corporation Method of designing a turbine blade outer air seal
JP3999395B2 (ja) * 1999-03-03 2007-10-31 三菱重工業株式会社 ガスタービン分割環
GB2356022B (en) * 1999-11-02 2003-12-10 Rolls Royce Plc Gas turbine engines
DE19963371A1 (de) * 1999-12-28 2001-07-12 Alstom Power Schweiz Ag Baden Gekühltes Hitzeschild
GB0029337D0 (en) * 2000-12-01 2001-01-17 Rolls Royce Plc A seal segment for a turbine
JP2002213207A (ja) * 2001-01-15 2002-07-31 Mitsubishi Heavy Ind Ltd ガスタービン分割環
EP1245792A1 (de) * 2001-03-30 2002-10-02 Siemens Aktiengesellschaft Gekühlter Mantelring für eine Turbine und Verfahren zur Herstellung eines Mantelrings
US6910854B2 (en) * 2002-10-08 2005-06-28 United Technologies Corporation Leak resistant vane cluster
US7094029B2 (en) * 2003-05-06 2006-08-22 General Electric Company Methods and apparatus for controlling gas turbine engine rotor tip clearances
US20050067788A1 (en) * 2003-09-25 2005-03-31 Siemens Westinghouse Power Corporation Outer air seal assembly
US7217081B2 (en) * 2004-10-15 2007-05-15 Siemens Power Generation, Inc. Cooling system for a seal for turbine vane shrouds
FR2877036B1 (fr) * 2004-10-27 2006-12-22 Snecma Moteurs Sa Dispositif de lubrification d'un composant dans une turbomachine
US7520715B2 (en) * 2005-07-19 2009-04-21 Pratt & Whitney Canada Corp. Turbine shroud segment transpiration cooling with individual cast inlet and outlet cavities
GB0523106D0 (en) * 2005-11-12 2005-12-21 Rolls Royce Plc A cooliing arrangement
US7665955B2 (en) * 2006-08-17 2010-02-23 Siemens Energy, Inc. Vortex cooled turbine blade outer air seal for a turbine engine
US7922444B2 (en) * 2007-01-19 2011-04-12 United Technologies Corporation Chamfer rail pockets for turbine vane shrouds
US20090096174A1 (en) * 2007-02-28 2009-04-16 United Technologies Corporation Blade outer air seal for a gas turbine engine
US20100021716A1 (en) * 2007-06-19 2010-01-28 Strock Christopher W Thermal barrier system and bonding method
US7887929B2 (en) * 2007-08-28 2011-02-15 United Technologies Corporation Oriented fiber ceramic matrix composite abradable thermal barrier coating
US20090110546A1 (en) * 2007-10-29 2009-04-30 United Technologies Corp. Feather Seals and Gas Turbine Engine Systems Involving Such Seals
US8240981B2 (en) * 2007-11-02 2012-08-14 United Technologies Corporation Turbine airfoil with platform cooling
US8177492B2 (en) * 2008-03-04 2012-05-15 United Technologies Corporation Passage obstruction for improved inlet coolant filling
US7942188B2 (en) * 2008-03-12 2011-05-17 Vent-Tek Designs, Llc Refractory metal core
US8317461B2 (en) * 2008-08-27 2012-11-27 United Technologies Corporation Gas turbine engine component having dual flow passage cooling chamber formed by single core
GB2468848B (en) * 2009-03-23 2011-10-26 Rolls Royce Plc An assembly for a turbomachine
US20110044803A1 (en) * 2009-08-18 2011-02-24 Pratt & Whitney Canada Corp. Blade outer air seal anti-rotation
US8287234B1 (en) * 2009-08-20 2012-10-16 Florida Turbine Technologies, Inc. Turbine inter-segment mate-face cooling design
US8727695B2 (en) * 2009-12-09 2014-05-20 Rolls-Royce Corporation Chamfer-fillet gap for thermal management
US8585354B1 (en) * 2010-01-19 2013-11-19 Florida Turbine Technologies, Inc. Turbine ring segment with riffle seal
US8727704B2 (en) 2010-09-07 2014-05-20 Siemens Energy, Inc. Ring segment with serpentine cooling passages
RU2543101C2 (ru) * 2010-11-29 2015-02-27 Альстом Текнолоджи Лтд Осевая газовая турбина
JP2012211527A (ja) 2011-03-30 2012-11-01 Mitsubishi Heavy Ind Ltd ガスタービン
US9017012B2 (en) 2011-10-26 2015-04-28 Siemens Energy, Inc. Ring segment with cooling fluid supply trench
US8992168B2 (en) * 2011-10-28 2015-03-31 United Technologies Corporation Rotating vane seal with cooling air passages
CN104066934B (zh) * 2012-01-26 2016-12-28 通用电器技术有限公司 用于涡轮机的具有分段式内部环的定子构件
JP5461636B2 (ja) * 2012-08-24 2014-04-02 三菱重工業株式会社 タービン分割環
WO2014133706A1 (en) 2013-02-26 2014-09-04 United Technologies Corporation Edge treatment for gas turbine engine component
EP3042045A4 (de) * 2013-09-06 2017-06-14 United Technologies Corporation Geneigte boas-intersegment-geometrie
US10221767B2 (en) 2014-09-02 2019-03-05 United Technologies Corporation Actively cooled blade outer air seal
US10443423B2 (en) 2014-09-22 2019-10-15 United Technologies Corporation Gas turbine engine blade outer air seal assembly
US10233844B2 (en) 2015-05-11 2019-03-19 General Electric Company System for thermally shielding a portion of a gas turbine shroud assembly
US10641120B2 (en) 2015-07-24 2020-05-05 Rolls-Royce Corporation Seal segment for a gas turbine engine
RU2706211C2 (ru) * 2016-01-25 2019-11-14 Ансалдо Энерджиа Свитзерлэнд Аг Охлаждаемая стенка компонента турбины и способ охлаждения этой стенки
US11156117B2 (en) * 2016-04-25 2021-10-26 Raytheon Technologies Corporation Seal arc segment with sloped circumferential sides
US10697464B2 (en) * 2016-07-29 2020-06-30 Raytheon Technologies Corporation Abradable material
US20180230839A1 (en) * 2017-02-14 2018-08-16 General Electric Company Turbine engine shroud assembly
GB2559804A (en) * 2017-02-21 2018-08-22 Siemens Ag Heatshield for a gas turbine
US10794206B2 (en) 2018-09-05 2020-10-06 Raytheon Technologies Corporation CMC BOAS intersegment seal
US20200072070A1 (en) * 2018-09-05 2020-03-05 United Technologies Corporation Unified boas support and vane platform
US11359505B2 (en) * 2019-05-04 2022-06-14 Raytheon Technologies Corporation Nesting CMC components
US11255208B2 (en) * 2019-05-15 2022-02-22 Raytheon Technologies Corporation Feather seal for CMC BOAS
US11384654B2 (en) 2019-11-18 2022-07-12 Raytheon Technologies Corporation Mateface for blade outer air seals in a gas turbine engine

Family Cites Families (8)

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US3365172A (en) * 1966-11-02 1968-01-23 Gen Electric Air cooled shroud seal
CH525419A (de) * 1970-12-18 1972-07-15 Bbc Sulzer Turbomaschinen Dichtungsvorrichtung für Turbomaschinen
US3990807A (en) * 1974-12-23 1976-11-09 United Technologies Corporation Thermal response shroud for rotating body
GB2125111B (en) * 1982-03-23 1985-06-05 Rolls Royce Shroud assembly for a gas turbine engine
US4650394A (en) * 1984-11-13 1987-03-17 United Technologies Corporation Coolable seal assembly for a gas turbine engine
US4642024A (en) * 1984-12-05 1987-02-10 United Technologies Corporation Coolable stator assembly for a rotary machine
JPH03213602A (ja) * 1990-01-08 1991-09-19 General Electric Co <Ge> ガスタービンエンジンの当接セグメントを連結する自己冷却式ジョイント連結構造
US5169287A (en) * 1991-05-20 1992-12-08 General Electric Company Shroud cooling assembly for gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004037356B4 (de) * 2004-07-30 2017-11-23 Ansaldo Energia Ip Uk Limited Wandstruktur zur Begrenzung eines Heißgaspfads

Also Published As

Publication number Publication date
EP0657625A1 (de) 1995-06-14
US5374161A (en) 1994-12-20
DE69409332D1 (de) 1998-05-07
EP0657625B1 (de) 1998-04-01
JPH07233735A (ja) 1995-09-05
JP3607331B2 (ja) 2005-01-05

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Legal Events

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