DE602005004447D1 - Manschettendichtung für Turbinenleitschaufeln - Google Patents

Manschettendichtung für Turbinenleitschaufeln

Info

Publication number
DE602005004447D1
DE602005004447D1 DE602005004447T DE602005004447T DE602005004447D1 DE 602005004447 D1 DE602005004447 D1 DE 602005004447D1 DE 602005004447 T DE602005004447 T DE 602005004447T DE 602005004447 T DE602005004447 T DE 602005004447T DE 602005004447 D1 DE602005004447 D1 DE 602005004447D1
Authority
DE
Germany
Prior art keywords
turbine vanes
collar gasket
gasket
collar
vanes
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
DE602005004447T
Other languages
English (en)
Other versions
DE602005004447T2 (de
Inventor
Thomas Allen Wells
David Edward Bulman
Mark Eugene Noe
Nitin Bhate
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 DE602005004447D1 publication Critical patent/DE602005004447D1/de
Application granted granted Critical
Publication of DE602005004447T2 publication Critical patent/DE602005004447T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/06Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/08Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
    • F16J15/0806Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing characterised by material or surface treatment
    • F16J15/0812Sealings 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/06Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces
    • F16J15/08Sealings between relatively-stationary surfaces with solid packing compressed between sealing surfaces with exclusively metal packing
    • F16J15/0887Sealings 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/55Seals
    • F05D2240/57Leaf seals
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
DE602005004447T 2004-06-23 2005-06-22 Manschettendichtung für Turbinenleitschaufeln Active DE602005004447T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/874,518 US7052234B2 (en) 2004-06-23 2004-06-23 Turbine vane collar seal
US874518 2004-06-23

Publications (2)

Publication Number Publication Date
DE602005004447D1 true DE602005004447D1 (de) 2008-03-13
DE602005004447T2 DE602005004447T2 (de) 2009-01-15

Family

ID=34982319

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005004447T Active DE602005004447T2 (de) 2004-06-23 2005-06-22 Manschettendichtung für Turbinenleitschaufeln

Country Status (10)

Country Link
US (1) US7052234B2 (de)
EP (1) EP1609952B1 (de)
JP (1) JP4781017B2 (de)
CN (1) CN1712674B (de)
BR (1) BRPI0502751A (de)
CA (1) CA2509743C (de)
DE (1) DE602005004447T2 (de)
MX (1) MXPA05006608A (de)
MY (1) MY138366A (de)
SG (1) SG118372A1 (de)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7329087B2 (en) * 2005-09-19 2008-02-12 General Electric Company Seal-less CMC vane to platform interfaces
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
EP1845193A1 (de) 2006-04-14 2007-10-17 Georgia-Pacific France Mehrlagiger saugfähiger Papierbogen, Rolle und Verfahren zu seiner Herstellung
US7625170B2 (en) * 2006-09-25 2009-12-01 General Electric Company CMC vane insulator and method of use
US7798769B2 (en) * 2007-02-15 2010-09-21 Siemens Energy, Inc. Flexible, high-temperature ceramic seal element
US7766609B1 (en) * 2007-05-24 2010-08-03 Florida Turbine Technologies, Inc. Turbine vane endwall with float wall heat shield
US8465062B2 (en) * 2007-08-20 2013-06-18 The Eastern Company Armored vehicle door hardware providing access, egress, rescue and security
EP2247830B1 (de) 2008-02-27 2019-04-10 General Electric Company Flexible dichtung für eine turbine und zugehörige turbine
US7736131B1 (en) * 2008-07-21 2010-06-15 Florida Turbine Technologies, Inc. Turbine blade with carbon nanotube shell
ES2370307B1 (es) * 2008-11-04 2012-11-27 Industria De Turbo Propulsores, S.A. Estructura soporte de rodamiento para turbina.
US8690159B2 (en) * 2009-07-14 2014-04-08 Dresser-Rand Company Spiral wound bound seal
KR101023783B1 (ko) * 2009-08-05 2011-03-21 한국전력공사 가스터빈 압축기의 고정익 고정구조
US8668442B2 (en) * 2010-06-30 2014-03-11 Honeywell International Inc. Turbine nozzles and methods of manufacturing the same
US8668448B2 (en) * 2010-10-29 2014-03-11 United Technologies Corporation Airfoil attachment arrangement
CH704252A1 (de) 2010-12-21 2012-06-29 Alstom Technology Ltd Gebaute schaufelanordnung für eine gasturbine sowie verfahren zum betrieb einer solchen schaufelanordnung.
GB2491562A (en) 2011-05-23 2012-12-12 Alstom Technology Ltd Fossil fuel power plant with gas turbine and MCFC arrangements
US9726028B2 (en) 2011-06-29 2017-08-08 Siemens Energy, Inc. Ductile alloys for sealing modular component interfaces
US8888445B2 (en) 2011-08-19 2014-11-18 General Electric Company Turbomachine seal assembly
US9951639B2 (en) * 2012-02-10 2018-04-24 Pratt & Whitney Canada Corp. Vane assemblies for gas turbine engines
US9909503B2 (en) 2012-09-26 2018-03-06 United Technologies Corporation Gas turbine engine including vane structure and seal to control fluid leakage
US20140169979A1 (en) * 2012-12-14 2014-06-19 United Technologies Corporation Gas turbine engine fan blade platform seal
EP2959113B1 (de) 2013-02-23 2018-10-31 Rolls-Royce Corporation Profildichtung für einen gasturbinen-keramikmatrixverbundwerkstoff
US10267168B2 (en) 2013-12-23 2019-04-23 Rolls-Royce Corporation Vane ring for a turbine engine having retention devices
US10294802B2 (en) 2014-12-05 2019-05-21 Rolls-Royce American Technologies, Inc. Turbine engine components with chemical vapor infiltrated isolation layers
US10233764B2 (en) * 2015-10-12 2019-03-19 Rolls-Royce North American Technologies Inc. Fabric seal and assembly for gas turbine engine
US10724390B2 (en) * 2018-03-16 2020-07-28 General Electric Company Collar support assembly for airfoils
US20190345833A1 (en) * 2018-05-11 2019-11-14 United Technologies Corporation Vane including internal radiant heat shield
US11181005B2 (en) * 2018-05-18 2021-11-23 Raytheon Technologies Corporation Gas turbine engine assembly with mid-vane outer platform gap
US10876416B2 (en) * 2018-07-27 2020-12-29 Pratt & Whitney Canada Corp. Vane segment with ribs
US10774665B2 (en) * 2018-07-31 2020-09-15 General Electric Company Vertically oriented seal system for gas turbine vanes
FR3101665B1 (fr) * 2019-10-07 2022-04-22 Safran Aircraft Engines Distributeur de turbine à aubage en composite à matrice céramique traversé par un circuit de ventilation métallique
US11255204B2 (en) * 2019-11-05 2022-02-22 Rolls-Royce Plc Turbine vane assembly having ceramic matrix composite airfoils and metallic support spar
US10975709B1 (en) 2019-11-11 2021-04-13 Rolls-Royce Plc Turbine vane assembly with ceramic matrix composite components and sliding support
US11519280B1 (en) 2021-09-30 2022-12-06 Rolls-Royce Plc Ceramic matrix composite vane assembly with compliance features
DE102022207874A1 (de) 2022-07-29 2024-02-01 Siemens Energy Global GmbH & Co. KG Dichtsegment mit Lasche und Tasche

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914300A (en) 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US4645217A (en) * 1985-11-29 1987-02-24 United Technologies Corporation Finger seal assembly
FR2610673B1 (fr) * 1987-02-05 1991-03-15 Snecma Turboreacteur multiflux a couronne externe de redresseur de soufflante frettee sur le carter
US5657998A (en) 1994-09-19 1997-08-19 General Electric Company Gas-path leakage seal for a gas turbine
US5509669A (en) 1995-06-19 1996-04-23 General Electric Company Gas-path leakage seal for a gas turbine
US5630700A (en) 1996-04-26 1997-05-20 General Electric Company Floating vane turbine nozzle
US5915697A (en) 1997-09-22 1999-06-29 General Electric Company Flexible cloth seal assembly
US6200092B1 (en) 1999-09-24 2001-03-13 General Electric Company Ceramic turbine nozzle
US6502825B2 (en) * 2000-12-26 2003-01-07 General Electric Company Pressure activated cloth seal
US6464456B2 (en) * 2001-03-07 2002-10-15 General Electric Company Turbine vane assembly including a low ductility vane
US6609885B2 (en) 2001-12-28 2003-08-26 General Electric Company Supplemental seal for the chordal hinge seal in a gas turbine
US6609886B2 (en) 2001-12-28 2003-08-26 General Electric Company Composite tubular woven seal for gas turbine nozzle and shroud interface
US6719295B2 (en) 2001-12-28 2004-04-13 General Electric Company Supplemental seal for the chordal hinge seals in a gas turbine
US6599089B2 (en) 2001-12-28 2003-07-29 General Electric Company Supplemental seal for the chordal hinge seal in a gas turbine
US6637751B2 (en) 2001-12-28 2003-10-28 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
US6655913B2 (en) 2002-01-15 2003-12-02 General Electric Company Composite tubular woven seal for an inner compressor discharge case
US6652231B2 (en) 2002-01-17 2003-11-25 General Electric Company Cloth seal for an inner compressor discharge case and methods of locating the seal in situ

Also Published As

Publication number Publication date
CN1712674B (zh) 2011-06-08
EP1609952A1 (de) 2005-12-28
US20050287002A1 (en) 2005-12-29
CA2509743A1 (en) 2005-12-23
CA2509743C (en) 2012-07-24
JP2006009800A (ja) 2006-01-12
SG118372A1 (en) 2006-01-27
MXPA05006608A (es) 2006-01-11
EP1609952B1 (de) 2008-01-23
CN1712674A (zh) 2005-12-28
DE602005004447T2 (de) 2009-01-15
JP4781017B2 (ja) 2011-09-28
BRPI0502751A (pt) 2006-02-07
MY138366A (en) 2009-05-29
US7052234B2 (en) 2006-05-30

Similar Documents

Publication Publication Date Title
DE602005004447D1 (de) Manschettendichtung für Turbinenleitschaufeln
NO20070239L (no) System for a vaske en gassturbinmotor
DE602005007408D1 (de) Dichtungsanordnung für eine Turbomaschine
DK1903188T3 (da) Gasturbine
DE602005007391D1 (de) Gasturbinentriebwerk
DE112005002877A5 (de) Leitapparat für Abgasturbine
DE502005006817D1 (de) Freistromturbinenanlage
FR2908152B1 (fr) Aube en fleche de turbomachine
DE602007008001D1 (de) Dichtung für segmentierte Gasturbinenkomponenten
DE602005001528D1 (de) Gasturbinentriebwerk
DE602005000026D1 (de) Dichtungsanordnung für die Hochdruckturbine einer Turbomaschine
DE602007007334D1 (de) Gasturbinenanordnung
GB0523469D0 (en) Blades for gas turbine engines
DE602005003759D1 (de) Gegenläufiges Turbinentriebwerk
DE602005014079D1 (de) Auswuchtvorrichtung für Gasturbinentriebwerke
DE502005010604D1 (de) Strömungsarbeitsmaschine
DE502006003548D1 (de) Beschichtete Turbinenschaufel
DE602006020376D1 (de) ugehörige Gasturbine
DE502005000209D1 (de) Dichtungs- und Dämpfungssystem für Turbinenschaufeln
DE502006002383D1 (de) Turbinenrad
DE602005014314D1 (de) Auswuchtvorrichtung für Gasturbinentriebwerke
FR2924155B1 (fr) Aube de turbomachine
DE502004003477D1 (de) Filmgekühlte Turbinenschaufel
NO20054322D0 (no) Rotorblad for forste trinn i en gassturbin
DE502007005310D1 (de) Klappendichtung für eine Strömungsmaschine

Legal Events

Date Code Title Description
8364 No opposition during term of opposition