KR100765603B1 - 터빈내에 가요성 시일을 설치하는 방법 및 가요성 시일을 형성하는 방법 - Google Patents

터빈내에 가요성 시일을 설치하는 방법 및 가요성 시일을 형성하는 방법 Download PDF

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Publication number
KR100765603B1
KR100765603B1 KR1020020084923A KR20020084923A KR100765603B1 KR 100765603 B1 KR100765603 B1 KR 100765603B1 KR 1020020084923 A KR1020020084923 A KR 1020020084923A KR 20020084923 A KR20020084923 A KR 20020084923A KR 100765603 B1 KR100765603 B1 KR 100765603B1
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KR
South Korea
Prior art keywords
seal
turbine
installing
flexible
sealing
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
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KR1020020084923A
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English (en)
Korean (ko)
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KR20030057429A (ko
Inventor
아크시트마흐무트파루크
사피아마드
모하메드-파키르압둘-아지즈
Original Assignee
제너럴 일렉트릭 캄파니
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Publication date
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Publication of KR20030057429A publication Critical patent/KR20030057429A/ko
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Publication of KR100765603B1 publication Critical patent/KR100765603B1/ko
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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
    • 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
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00—Seal for a joint or juncture
    • Y10S277/931—Seal including temperature responsive feature

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
KR1020020084923A 2001-12-28 2002-12-27 터빈내에 가요성 시일을 설치하는 방법 및 가요성 시일을 형성하는 방법 Expired - Fee Related KR100765603B1 (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/028,927 US6648333B2 (en) 2001-12-28 2001-12-28 Method of forming and installing a seal
US10/028,927 2001-12-28

Publications (2)

Publication Number Publication Date
KR20030057429A KR20030057429A (ko) 2003-07-04
KR100765603B1 true KR100765603B1 (ko) 2007-10-09

Family

ID=21846269

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020020084923A Expired - Fee Related KR100765603B1 (ko) 2001-12-28 2002-12-27 터빈내에 가요성 시일을 설치하는 방법 및 가요성 시일을 형성하는 방법

Country Status (5)

Country Link
US (1) US6648333B2 (enExample)
EP (1) EP1323893B1 (enExample)
JP (1) JP4234419B2 (enExample)
KR (1) KR100765603B1 (enExample)
DE (1) DE60227039D1 (enExample)

Families Citing this family (34)

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Publication number Priority date Publication date Assignee Title
US7080513B2 (en) * 2001-08-04 2006-07-25 Siemens Aktiengesellschaft Seal element for sealing a gap and combustion turbine having a seal element
US6764081B2 (en) * 2001-12-28 2004-07-20 General Electric Company Supplemental seal for the chordal hinge seals in a gas turbine and methods of installation
GB2391281B (en) * 2002-07-26 2005-11-02 Coflexip Stena Offshore Ltd Seal assembly
EP1391641B1 (en) * 2002-08-21 2011-11-30 Alstom Technology Ltd Bellows seal
ZA200500984B (en) * 2004-02-12 2005-10-26 Weir- Envirotech ( Pty) Ltd Rotary pump
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
US7172388B2 (en) * 2004-08-24 2007-02-06 Pratt & Whitney Canada Corp. Multi-point seal
US7207771B2 (en) 2004-10-15 2007-04-24 Pratt & Whitney Canada Corp. Turbine shroud segment seal
US20060082074A1 (en) * 2004-10-18 2006-04-20 Pratt & Whitney Canada Corp. Circumferential feather seal
US7338253B2 (en) * 2005-09-15 2008-03-04 General Electric Company Resilient seal on trailing edge of turbine inner shroud and method for shroud post impingement cavity sealing
US20070134087A1 (en) * 2005-12-08 2007-06-14 General Electric Company Methods and apparatus for assembling turbine engines
US8016297B2 (en) * 2008-03-27 2011-09-13 United Technologies Corporation Gas turbine engine seals and engines incorporating such seals
FR2933160B1 (fr) * 2008-06-25 2010-09-10 Commissariat Energie Atomique Assemblage comportant un joint d'etancheite intercale entre deux composants de coefficient de dilatation moyen thermique different, joint d'etancheite associe, application a l'etancheite d'electrolyseurs eht et des piles a combustible
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
JP5534214B2 (ja) * 2009-10-05 2014-06-25 ベイバイオサイエンス株式会社 フローサイトメータおよびフローサイトメトリ方法
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
JP5717662B2 (ja) * 2012-01-27 2015-05-13 三菱電線工業株式会社 金属シール
US9611712B2 (en) * 2012-02-09 2017-04-04 Onesubsea Ip Uk Limited Lip seal
US8789833B2 (en) * 2012-03-28 2014-07-29 General Electric Company Turbine assembly and method for assembling a turbine
US9790863B2 (en) 2013-04-05 2017-10-17 Honeywell International Inc. Fluid transfer seal assemblies, fluid transfer systems, and methods for transferring process fluid between stationary and rotating components using the same
WO2015076889A1 (en) * 2013-09-13 2015-05-28 United Technologies Corporation System and apparatus for seal retention and protection
EP3102810B1 (en) * 2014-01-24 2020-02-12 United Technologies Corporation Gas turbine circumferential axial segmented trough seal
US9416675B2 (en) 2014-01-27 2016-08-16 General Electric Company Sealing device for providing a seal in a turbomachine
EP2960439A1 (en) * 2014-06-26 2015-12-30 Siemens Aktiengesellschaft Turbomachine with an outer sealing and use of the turbomachine
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
US10443419B2 (en) 2015-04-30 2019-10-15 Rolls-Royce North American Technologies Inc. Seal for a gas turbine engine assembly
US10385712B2 (en) * 2015-05-22 2019-08-20 United Technologies Corporation Support assembly for a gas turbine engine
EP3361127B1 (en) * 2017-02-09 2020-04-15 MANN+HUMMEL GmbH Plug-in-connection between a connecting part and a plug-in-part
CN115614108B (zh) * 2022-11-02 2025-07-15 中国航发沈阳发动机研究所 一种航空发动机涡轮挡板的封严结构

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4199151A (en) 1978-08-14 1980-04-22 General Electric Company Method and apparatus for retaining seals
US4445694A (en) 1982-12-17 1984-05-01 Westinghouse Electric Corp. All-metal expandable ultra high vacuum seal
US4602795A (en) 1985-12-06 1986-07-29 United Technologies Corporation Thermally expansive slip joint for formed sheet metal seals
US5716052A (en) 1994-09-12 1998-02-10 Eg&G Pressure Science, Inc. Pressure-energized sealing rings
US6164656A (en) 1999-01-29 2000-12-26 General Electric Company Turbine nozzle interface seal and methods
US6237921B1 (en) 1998-09-02 2001-05-29 General Electric Company Nested bridge seal
US6287091B1 (en) 2000-05-10 2001-09-11 General Motors Corporation Turbocharger with nozzle ring coupling

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3893786A (en) * 1973-06-07 1975-07-08 Ford Motor Co Air cooled shroud for a gas turbine engine
US4336943A (en) * 1980-11-14 1982-06-29 United Technologies Corporation Wedge-shaped seal for flanged joints
US4477086A (en) * 1982-11-01 1984-10-16 United Technologies Corporation Seal ring with slidable inner element bridging circumferential gap
US4589666A (en) * 1985-07-25 1986-05-20 Pressure Science Incorporated Slip joint assembly for a split ring seal
US5158305A (en) * 1992-01-31 1992-10-27 Eg&G Pressure Science, Inc. Pressure-energized two-element seal
US5819854A (en) * 1996-02-06 1998-10-13 Baker Hughes Incorporated Activation of downhole tools
US6752592B2 (en) 2001-12-28 2004-06-22 General Electric Company Supplemental seal for the chordal hinge seals in a gas turbine
US6637752B2 (en) 2001-12-28 2003-10-28 General Electric Company Supplemental seal for the chordal hinge seal in a gas turbine

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4199151A (en) 1978-08-14 1980-04-22 General Electric Company Method and apparatus for retaining seals
US4445694A (en) 1982-12-17 1984-05-01 Westinghouse Electric Corp. All-metal expandable ultra high vacuum seal
US4602795A (en) 1985-12-06 1986-07-29 United Technologies Corporation Thermally expansive slip joint for formed sheet metal seals
US5716052A (en) 1994-09-12 1998-02-10 Eg&G Pressure Science, Inc. Pressure-energized sealing rings
US6237921B1 (en) 1998-09-02 2001-05-29 General Electric Company Nested bridge seal
US6164656A (en) 1999-01-29 2000-12-26 General Electric Company Turbine nozzle interface seal and methods
US6287091B1 (en) 2000-05-10 2001-09-11 General Motors Corporation Turbocharger with nozzle ring coupling

Also Published As

Publication number Publication date
KR20030057429A (ko) 2003-07-04
JP2003227306A (ja) 2003-08-15
EP1323893B1 (en) 2008-06-11
EP1323893A3 (en) 2004-04-21
JP4234419B2 (ja) 2009-03-04
EP1323893A2 (en) 2003-07-02
US20030122311A1 (en) 2003-07-03
US6648333B2 (en) 2003-11-18
DE60227039D1 (de) 2008-07-24

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