DE602007008001D1 - Dichtung für segmentierte Gasturbinenkomponenten - Google Patents

Dichtung für segmentierte Gasturbinenkomponenten

Info

Publication number
DE602007008001D1
DE602007008001D1 DE602007008001T DE602007008001T DE602007008001D1 DE 602007008001 D1 DE602007008001 D1 DE 602007008001D1 DE 602007008001 T DE602007008001 T DE 602007008001T DE 602007008001 T DE602007008001 T DE 602007008001T DE 602007008001 D1 DE602007008001 D1 DE 602007008001D1
Authority
DE
Germany
Prior art keywords
seal
gas turbine
turbine components
segmented gas
segmented
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.)
Active
Application number
DE602007008001T
Other languages
English (en)
Inventor
Corneil Paauwe
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 DE602007008001D1 publication Critical patent/DE602007008001D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • 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
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/55—Seals
DE602007008001T 2006-03-09 2007-03-09 Dichtung für segmentierte Gasturbinenkomponenten Active DE602007008001D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/372,404 US20070212214A1 (en) 2006-03-09 2006-03-09 Segmented component seal

Publications (1)

Publication Number Publication Date
DE602007008001D1 true DE602007008001D1 (de) 2010-09-09

Family

ID=37930384

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007008001T Active DE602007008001D1 (de) 2006-03-09 2007-03-09 Dichtung für segmentierte Gasturbinenkomponenten

Country Status (3)

Country Link
US (1) US20070212214A1 (de)
EP (1) EP1832715B1 (de)
DE (1) DE602007008001D1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1991762B1 (de) * 2006-03-06 2015-03-11 Alstom Technology Ltd Gasturbine mit ringförmigem hitzeschild und abgewinkelten dichtungsstreifen
FR2957969B1 (fr) * 2010-03-26 2013-03-29 Snecma Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine
US8834109B2 (en) * 2011-08-03 2014-09-16 United Technologies Corporation Vane assembly for a gas turbine engine
US9810086B2 (en) * 2011-11-06 2017-11-07 General Electric Company Asymmetric radial spline seal for a gas turbine engine
US9115808B2 (en) * 2012-02-13 2015-08-25 General Electric Company Transition piece seal assembly for a turbomachine
US9316109B2 (en) * 2012-04-10 2016-04-19 General Electric Company Turbine shroud assembly and method of forming
EP2657455A1 (de) * 2012-04-27 2013-10-30 Siemens Aktiengesellschaft Hitzeschild und Herstellungsverfahren dafür
JP6021675B2 (ja) * 2013-02-13 2016-11-09 三菱重工業株式会社 燃焼器のシール構造及び燃焼器用シール
WO2014138320A1 (en) * 2013-03-08 2014-09-12 United Technologies Corporation Gas turbine engine component having variable width feather seal slot
DE102013205028A1 (de) * 2013-03-21 2014-09-25 Siemens Aktiengesellschaft Dichtelement zur Dichtung eines Spaltes
EP3025030B1 (de) * 2013-07-24 2021-04-21 Raytheon Technologies Corporation Rinnendichtung für gasturbinenmotor
US9759081B2 (en) * 2013-10-08 2017-09-12 General Electric Company Method and system to facilitate sealing in gas turbines
US10358932B2 (en) * 2015-06-29 2019-07-23 United Technologies Corporation Segmented non-contact seal assembly for rotational equipment
FR3065986B1 (fr) * 2017-05-02 2021-07-09 Safran Aircraft Engines Ensemble pour turbine a gaz, turbine a gaz associee
FR3081188B1 (fr) * 2018-05-15 2021-03-19 Safran Aircraft Engines Aubage de stator pour une turbomachine
US10890079B2 (en) * 2018-12-04 2021-01-12 Raytheon Technologies Corporation Gas turbine engine arc segments with arced walls
US11649732B2 (en) * 2021-03-11 2023-05-16 Raytheon Technologies Corporation Vane assembly with spring device for biasing mate face seal

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4537024A (en) * 1979-04-23 1985-08-27 Solar Turbines, Incorporated Turbine engines
US4311432A (en) * 1979-11-20 1982-01-19 United Technologies Corporation Radial seal
US5154577A (en) * 1991-01-17 1992-10-13 General Electric Company Flexible three-piece seal assembly
US5125796A (en) * 1991-05-14 1992-06-30 General Electric Company Transition piece seal spring for a gas turbine
US5435576A (en) * 1992-12-28 1995-07-25 Rode; John E. Spring gasket
US5709530A (en) * 1996-09-04 1998-01-20 United Technologies Corporation Gas turbine vane seal
GB2335470B (en) * 1998-03-18 2002-02-13 Rolls Royce Plc A seal
US6431825B1 (en) * 2000-07-28 2002-08-13 Alstom (Switzerland) Ltd Seal between static turbine parts
EP1448874B1 (de) * 2001-09-25 2007-12-26 ALSTOM Technology Ltd Dichtungsanordnung zur dichtspaltreduzierung innerhalb einer strömungsrotationsmaschine
GB2401658B (en) * 2003-05-16 2006-07-26 Rolls Royce Plc Sealing arrangement
JP4577813B2 (ja) * 2003-08-20 2010-11-10 イーグル・エンジニアリング・エアロスペース株式会社 シール装置
US7152864B2 (en) * 2003-10-02 2006-12-26 Alstom Technology Ltd. Seal assembly
US20060082074A1 (en) * 2004-10-18 2006-04-20 Pratt & Whitney Canada Corp. Circumferential feather seal
US7316402B2 (en) * 2006-03-09 2008-01-08 United Technologies Corporation Segmented component seal

Also Published As

Publication number Publication date
EP1832715A2 (de) 2007-09-12
EP1832715A3 (de) 2008-07-09
US20070212214A1 (en) 2007-09-13
EP1832715B1 (de) 2010-07-28

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