JP4139213B2 - ガスタービンノズルとシュラウドとの接合面のためのシール - Google Patents

ガスタービンノズルとシュラウドとの接合面のためのシール Download PDF

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Publication number
JP4139213B2
JP4139213B2 JP2002379701A JP2002379701A JP4139213B2 JP 4139213 B2 JP4139213 B2 JP 4139213B2 JP 2002379701 A JP2002379701 A JP 2002379701A JP 2002379701 A JP2002379701 A JP 2002379701A JP 4139213 B2 JP4139213 B2 JP 4139213B2
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JP
Japan
Prior art keywords
seal
cavity
gas turbine
seal body
turbine
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
JP2002379701A
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English (en)
Japanese (ja)
Other versions
JP2003227355A (ja
JP2003227355A5 (enExample
Inventor
マフマト・ファルク・アクシット
アフマド・サフィ
アブドゥル−アジーズ・モハメッド−ファキーア
スリカント・ベーダーンタム
ニン・ファング
ゲイル・ホッブス・ゲッツェ
ブライアン・ピーター・アーネス
ジョン・エリントン・グリーン
ウェイ−ミン・チー
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 JP2003227355A publication Critical patent/JP2003227355A/ja
Publication of JP2003227355A5 publication Critical patent/JP2003227355A5/ja
Application granted granted Critical
Publication of JP4139213B2 publication Critical patent/JP4139213B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
    • 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
    • F01D11/003—Preventing or minimising internal leakage of working-fluid, e.g. between stages by packing rings; Mechanical seals
    • 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
    • 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

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)
JP2002379701A 2001-12-28 2002-12-27 ガスタービンノズルとシュラウドとの接合面のためのシール Expired - Fee Related JP4139213B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/028,928 US6659472B2 (en) 2001-12-28 2001-12-28 Seal for gas turbine nozzle and shroud interface
US10/028928 2001-12-28

Publications (3)

Publication Number Publication Date
JP2003227355A JP2003227355A (ja) 2003-08-15
JP2003227355A5 JP2003227355A5 (enExample) 2006-02-23
JP4139213B2 true JP4139213B2 (ja) 2008-08-27

Family

ID=21846273

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002379701A Expired - Fee Related JP4139213B2 (ja) 2001-12-28 2002-12-27 ガスタービンノズルとシュラウドとの接合面のためのシール

Country Status (5)

Country Link
US (1) US6659472B2 (enExample)
EP (1) EP1327748B1 (enExample)
JP (1) JP4139213B2 (enExample)
KR (1) KR100681560B1 (enExample)
DE (1) DE60208870T2 (enExample)

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US6752592B2 (en) * 2001-12-28 2004-06-22 General Electric Company Supplemental seal for the chordal hinge seals in a gas turbine
US20040041351A1 (en) * 2002-07-03 2004-03-04 Alexander Beeck Gap seal for sealing a gap between two adjacent components
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
US7207771B2 (en) * 2004-10-15 2007-04-24 Pratt & Whitney Canada Corp. Turbine shroud segment seal
US20070134087A1 (en) * 2005-12-08 2007-06-14 General Electric Company Methods and apparatus for assembling turbine engines
US7600970B2 (en) * 2005-12-08 2009-10-13 General Electric Company Ceramic matrix composite vane seals
US7810816B1 (en) 2005-12-13 2010-10-12 Horace P. Halling Seal
US20070164043A1 (en) * 2005-12-29 2007-07-19 Lang Gary D Sanitary door seal
US7316402B2 (en) * 2006-03-09 2008-01-08 United Technologies Corporation Segmented component seal
US20070237629A1 (en) * 2006-04-05 2007-10-11 General Electric Company Gas turbine compressor casing flowpath rings
EP1988261A1 (de) * 2007-05-04 2008-11-05 ABB Turbo Systems AG Gehäusedichtung
US8122702B2 (en) * 2007-04-30 2012-02-28 General Electric Company Sealing arrangements for gas turbine engine thrust reverser
US7966808B2 (en) * 2007-04-30 2011-06-28 General Electric Company Baffle seal for gas turbine engine thrust reverser
US8104772B2 (en) * 2008-06-27 2012-01-31 Seal Science & Technology, Llc Gas turbine nozzle seals for 2000° F. gas containment
US8118548B2 (en) * 2008-09-15 2012-02-21 General Electric Company Shroud for a turbomachine
US8613171B2 (en) 2008-10-23 2013-12-24 Deerhill Properties, Inc. Window structure with expansion member for inhibiting flood waters
US20090120022A1 (en) * 2008-10-23 2009-05-14 Barbara Dudash Window Structure For Inhibiting Flood Waters
US20100101161A1 (en) * 2008-10-23 2010-04-29 Barbara Dudash Window structure with expansion member for inhibiting flood waters
DE102008057207A1 (de) * 2008-11-13 2010-05-27 Continental Mechanical Components Germany Gmbh Welleneinrichtung mit einer Dichtungsvorrichtung
GB0914187D0 (en) * 2009-08-14 2009-09-16 Rolls Royce Plc A sealing assembly
US8491259B2 (en) * 2009-08-26 2013-07-23 Siemens Energy, Inc. Seal system between transition duct exit section and turbine inlet in a gas turbine engine
US8511972B2 (en) * 2009-12-16 2013-08-20 Siemens Energy, Inc. Seal member for use in a seal system between a transition duct exit section and a turbine inlet in a gas turbine engine
US8231128B2 (en) * 2010-04-01 2012-07-31 General Electric Company Integral seal and sealant packaging
US20130074338A1 (en) * 2010-06-10 2013-03-28 Jeffrey Eugene Swensen Pre-compressed seal including removable pre-compression member
US8366113B2 (en) 2010-06-10 2013-02-05 Eaton Corporation Pre-compressed seal including removable pre-compression member
US8845272B2 (en) 2011-02-25 2014-09-30 General Electric Company Turbine shroud and a method for manufacturing the turbine shroud
US8985944B2 (en) 2011-03-30 2015-03-24 General Electric Company Continuous ring composite turbine shroud
US8789833B2 (en) * 2012-03-28 2014-07-29 General Electric Company Turbine assembly and method for assembling a turbine
US9593585B2 (en) 2013-10-15 2017-03-14 Siemens Aktiengesellschaft Seal assembly for a gap between outlet portions of adjacent transition ducts in a gas turbine engine
CN103711908B (zh) * 2014-01-22 2016-04-13 四川日机密封件股份有限公司 温度触发式非能动停车安全密封装置
US9416675B2 (en) 2014-01-27 2016-08-16 General Electric Company Sealing device for providing a seal in a turbomachine
US9829007B2 (en) 2014-05-23 2017-11-28 General Electric Company Turbine sealing system
US10099290B2 (en) 2014-12-18 2018-10-16 General Electric Company Hybrid additive manufacturing methods using hybrid additively manufactured features for hybrid components
US10280777B2 (en) 2014-12-19 2019-05-07 General Electric Company System and method including a circumferential seal assembly to facilitate sealing in a turbine
US10422239B2 (en) 2015-03-18 2019-09-24 Siemens Energy, Inc. Seal assembly in a gas turbine engine
US9945242B2 (en) * 2015-05-11 2018-04-17 General Electric Company System for thermally isolating a turbine shroud
US9982550B2 (en) * 2016-06-02 2018-05-29 United Technologies Corporation Joined two ply w seal
EP3361127B1 (en) * 2017-02-09 2020-04-15 MANN+HUMMEL GmbH Plug-in-connection between a connecting part and a plug-in-part
US11125098B2 (en) 2019-09-11 2021-09-21 Raytheon Technologies Corporation Blade outer air seal with face seal
US11215063B2 (en) 2019-10-10 2022-01-04 General Electric Company Seal assembly for chute gap leakage reduction in a gas turbine
CN114412583B (zh) * 2022-01-21 2024-12-03 中国联合重型燃气轮机技术有限公司 透平和具有其的燃气轮机

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Also Published As

Publication number Publication date
US6659472B2 (en) 2003-12-09
JP2003227355A (ja) 2003-08-15
EP1327748A1 (en) 2003-07-16
US20030122325A1 (en) 2003-07-03
KR100681560B1 (ko) 2007-02-09
DE60208870D1 (de) 2006-04-13
KR20030057410A (ko) 2003-07-04
EP1327748B1 (en) 2006-01-25
DE60208870T2 (de) 2006-09-07

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