DE60203214D1 - Turbinenschaufel mit Labyrinthschneidendichtung - Google Patents

Turbinenschaufel mit Labyrinthschneidendichtung

Info

Publication number
DE60203214D1
DE60203214D1 DE60203214T DE60203214T DE60203214D1 DE 60203214 D1 DE60203214 D1 DE 60203214D1 DE 60203214 T DE60203214 T DE 60203214T DE 60203214 T DE60203214 T DE 60203214T DE 60203214 D1 DE60203214 D1 DE 60203214D1
Authority
DE
Germany
Prior art keywords
turbine blade
cutting gasket
labyrinth
labyrinth cutting
gasket
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
DE60203214T
Other languages
English (en)
Other versions
DE60203214T2 (de
Inventor
Chantal Giot
Jean-Luc Soupizon
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
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 SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Application granted granted Critical
Publication of DE60203214D1 publication Critical patent/DE60203214D1/de
Publication of DE60203214T2 publication Critical patent/DE60203214T2/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
    • F01D11/08—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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
DE60203214T 2001-05-31 2002-05-30 Turbinenschaufel mit Labyrinthschneidendichtung Expired - Lifetime DE60203214T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0107122 2001-05-31
FR0107122A FR2825411B1 (fr) 2001-05-31 2001-05-31 Aube de turbine avec lechette d'etancheite

Publications (2)

Publication Number Publication Date
DE60203214D1 true DE60203214D1 (de) 2005-04-21
DE60203214T2 DE60203214T2 (de) 2006-03-23

Family

ID=8863806

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60203214T Expired - Lifetime DE60203214T2 (de) 2001-05-31 2002-05-30 Turbinenschaufel mit Labyrinthschneidendichtung

Country Status (9)

Country Link
US (1) US6939104B2 (de)
EP (1) EP1262633B1 (de)
JP (1) JP4074244B2 (de)
CA (1) CA2448802C (de)
DE (1) DE60203214T2 (de)
ES (1) ES2240670T3 (de)
FR (1) FR2825411B1 (de)
RU (1) RU2296226C2 (de)
WO (1) WO2002097241A1 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004025321A1 (de) 2004-05-19 2005-12-08 Alstom Technology Ltd Strömungsmaschinenschaufel
US7549841B1 (en) 2005-09-03 2009-06-23 Florida Turbine Technologies, Inc. Pressure balanced centrifugal tip seal
FR2893268B1 (fr) * 2005-11-15 2008-02-08 Snecma Sa Procede de realisation d'un rebord situe a l'extremite libre d'une aube, aube obtenue par ce procede et turbomachine equipee de cette aube
US20090097979A1 (en) * 2007-07-31 2009-04-16 Omer Duane Erdmann Rotor blade
FR2923524B1 (fr) * 2007-11-12 2013-12-06 Snecma Aube metallique fabriquee par moulage et procede de fabrication de l'aube
DE102008061800A1 (de) * 2008-12-11 2010-06-17 Rolls-Royce Deutschland Ltd & Co Kg Segmentierte Dichtlippen für Labyrinthdichtungsringe
FR2950104B1 (fr) * 2009-09-11 2011-12-09 Snecma Roue de turbomachine
US8613596B2 (en) * 2009-12-28 2013-12-24 Rolls-Royce Corporation Vane assembly having a vane end seal
US9151166B2 (en) 2010-06-07 2015-10-06 Rolls-Royce North American Technologies, Inc. Composite gas turbine engine component
EP2412927A1 (de) * 2010-07-29 2012-02-01 Alstom Technology Ltd Turbinenschaufel
RU2010150602A (ru) * 2010-12-09 2012-06-20 Альстом Текнолоджи Лтд (Ch) Бандаж лопатки ротора
EP2604797B1 (de) * 2011-12-13 2020-01-22 MTU Aero Engines GmbH Laufschaufel mit einer Rippenanordnung mit abrasiver Beschichtung
FR2985759B1 (fr) * 2012-01-17 2014-03-07 Snecma Aube mobile de turbomachine
US20130230379A1 (en) * 2012-03-01 2013-09-05 General Electric Company Rotating turbomachine component having a tip leakage flow guide
CN102926819A (zh) * 2012-10-23 2013-02-13 如皋透平叶片制造有限公司 一种汽轮机叶片防窜动叶冠
FR3001759B1 (fr) 2013-02-07 2015-01-16 Snecma Rouge aubagee de turbomachine
US10167729B2 (en) 2013-03-15 2019-01-01 United Technologies Corporation Knife edge with increased crack propagation life
FR3072121B1 (fr) * 2017-10-06 2021-07-30 Safran Aircraft Engines Dispositif d'etancheite entre rotor et stator de turbomachine
FR3073595B1 (fr) 2017-11-15 2020-02-07 Safran Helicopter Engines Joint a labyrinthe comprenant une lechette dotee d'un deflecteur
GB201801296D0 (en) * 2018-01-26 2018-03-14 Rolls Royce Plc Circumferental seal
FR3095025B1 (fr) * 2019-04-12 2021-03-05 Safran Aircraft Engines Joint d’étanchéité à labyrinthe comportant un élément abradable à densité variable de cellules
FR3128970A1 (fr) 2021-11-05 2023-05-12 Safran Aircraft Engines Dispositif d’etancheite a labyrinthe pour une turbomachine d’aeronef
FR3139856B1 (fr) * 2022-09-21 2024-09-06 Safran Aircraft Engines Roue de turbomachine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1159965B (de) * 1961-08-10 1963-12-27 Bbc Brown Boveri & Cie Einrichtung zur Schwingungsdaempfung an einem Turbinen- oder Verdichter-Schaufelkranz
US3339933A (en) * 1965-02-24 1967-09-05 Gen Electric Rotary seal
GB1194061A (en) * 1968-01-17 1970-06-10 Rolls Royce Improvements relating to Pressure Exchanger Rotors
SU792014A1 (ru) * 1978-12-13 1980-12-30 Предприятие П/Я М-5906 Лабиринтное уплотнение
US4576551A (en) * 1982-06-17 1986-03-18 The Garrett Corporation Turbo machine blading
US4822248A (en) * 1987-04-15 1989-04-18 Metallurgical Industries, Inc. Rebuilt shrouded turbine blade and method of rebuilding the same
FR2615254A1 (fr) * 1987-05-13 1988-11-18 Snecma Aube mobile de soufflante comportant une depouille en extremite
DE4015206C1 (de) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
JP2001055902A (ja) * 1999-08-18 2001-02-27 Toshiba Corp タービン動翼
DE10047307A1 (de) * 2000-09-25 2002-08-01 Alstom Switzerland Ltd Dichtungsanordnung

Also Published As

Publication number Publication date
CA2448802A1 (fr) 2002-12-05
DE60203214T2 (de) 2006-03-23
EP1262633A1 (de) 2002-12-04
US6939104B2 (en) 2005-09-06
EP1262633B1 (de) 2005-03-16
RU2296226C2 (ru) 2007-03-27
JP2004526899A (ja) 2004-09-02
RU2003134537A (ru) 2005-05-10
ES2240670T3 (es) 2005-10-16
FR2825411A1 (fr) 2002-12-06
FR2825411B1 (fr) 2003-09-19
US20040146404A1 (en) 2004-07-29
WO2002097241A1 (fr) 2002-12-05
CA2448802C (fr) 2009-01-13
JP4074244B2 (ja) 2008-04-09

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SNECMA, PARIS, FR