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FR2810365B1 - Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees - Google Patents

Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees

Info

Publication number
FR2810365B1
FR2810365B1 FR0007611A FR0007611A FR2810365B1 FR 2810365 B1 FR2810365 B1 FR 2810365B1 FR 0007611 A FR0007611 A FR 0007611A FR 0007611 A FR0007611 A FR 0007611A FR 2810365 B1 FR2810365 B1 FR 2810365B1
Authority
FR
France
Prior art keywords
dawn
juxtaposed
platforms
ventilation
pair
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
FR0007611A
Other languages
English (en)
Other versions
FR2810365A1 (fr
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
Priority to FR0007611A priority Critical patent/FR2810365B1/fr
Priority to EP01401534A priority patent/EP1164253B1/fr
Priority to DE2001609093 priority patent/DE60109093T2/de
Priority to JP2001180380A priority patent/JP4047560B2/ja
Priority to US09/883,948 priority patent/US6457935B1/en
Publication of FR2810365A1 publication Critical patent/FR2810365A1/fr
Application granted granted Critical
Publication of FR2810365B1 publication Critical patent/FR2810365B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F01D11/005—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
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/80—Platforms for stationary or moving blades
    • F05B2240/801—Platforms for stationary or moving blades cooled platforms
    • 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
    • F05D2240/80—Platforms for stationary or moving blades
    • F05D2240/81—Cooled platforms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0007611A 2000-06-15 2000-06-15 Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees Expired - Fee Related FR2810365B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0007611A FR2810365B1 (fr) 2000-06-15 2000-06-15 Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees
EP01401534A EP1164253B1 (fr) 2000-06-15 2001-06-14 Système de ventilation d'une paire de plates-formes d'aubes juxtaposées
DE2001609093 DE60109093T2 (de) 2000-06-15 2001-06-14 Kühlungssystem für die Abdeckplatten von Rotorschaufelpaaren
JP2001180380A JP4047560B2 (ja) 2000-06-15 2001-06-14 並置された羽根のプラットフォーム対の通風システム
US09/883,948 US6457935B1 (en) 2000-06-15 2001-06-20 System for ventilating a pair of juxtaposed vane platforms

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0007611A FR2810365B1 (fr) 2000-06-15 2000-06-15 Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees
US09/883,948 US6457935B1 (en) 2000-06-15 2001-06-20 System for ventilating a pair of juxtaposed vane platforms

Publications (2)

Publication Number Publication Date
FR2810365A1 FR2810365A1 (fr) 2001-12-21
FR2810365B1 true FR2810365B1 (fr) 2002-10-11

Family

ID=26212467

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0007611A Expired - Fee Related FR2810365B1 (fr) 2000-06-15 2000-06-15 Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees

Country Status (4)

Country Link
US (1) US6457935B1 (fr)
EP (1) EP1164253B1 (fr)
JP (1) JP4047560B2 (fr)
FR (1) FR2810365B1 (fr)

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DE10332561A1 (de) * 2003-07-11 2005-01-27 Rolls-Royce Deutschland Ltd & Co Kg Gekühltes Turbinenlaufrad, insbesondere Hochdruckturbinenlaufrad für ein Flugtriebwerk
GB2411697B (en) * 2004-03-06 2006-06-21 Rolls Royce Plc A turbine having a cooling arrangement
US7198467B2 (en) * 2004-07-30 2007-04-03 General Electric Company Method and apparatus for cooling gas turbine engine rotor blades
US20060056968A1 (en) * 2004-09-15 2006-03-16 General Electric Company Apparatus and methods for cooling turbine bucket platforms
US7186089B2 (en) * 2004-11-04 2007-03-06 Siemens Power Generation, Inc. Cooling system for a platform of a turbine blade
GB2420162A (en) * 2004-11-16 2006-05-17 Cross Mfg Company A seal arrangement for sealing between turbine blades
US20060269409A1 (en) * 2005-05-27 2006-11-30 Mitsubishi Heavy Industries, Ltd. Gas turbine moving blade having a platform, a method of forming the moving blade, a sealing plate, and a gas turbine having these elements
GB0523106D0 (en) 2005-11-12 2005-12-21 Rolls Royce Plc A cooliing arrangement
ATE459447T1 (de) * 2006-10-16 2010-03-15 Siemens Ag Turbinenschaufel für eine turbine mit einem kühlmittelkanal
US8240981B2 (en) * 2007-11-02 2012-08-14 United Technologies Corporation Turbine airfoil with platform cooling
FR2927357B1 (fr) * 2008-02-12 2013-09-20 Snecma Dispositif d'amortissement des vibrations entre deux aubes de roue aubagee de turbomachine
JP5129633B2 (ja) * 2008-03-28 2013-01-30 三菱重工業株式会社 冷却通路用カバーおよび該カバーの製造方法ならびにガスタービン
GB0806893D0 (en) * 2008-04-16 2008-05-21 Rolls Royce Plc A damper
US8240987B2 (en) * 2008-08-15 2012-08-14 United Technologies Corp. Gas turbine engine systems involving baffle assemblies
US8292587B2 (en) * 2008-12-18 2012-10-23 Honeywell International Inc. Turbine blade assemblies and methods of manufacturing the same
US9121293B2 (en) 2009-03-09 2015-09-01 Avio S.P.A. Rotor for turbomachines
EP2282014A1 (fr) * 2009-06-23 2011-02-09 Siemens Aktiengesellschaft Section de canal d'écoulement annulaire pour une turbomachine
US8356978B2 (en) * 2009-11-23 2013-01-22 United Technologies Corporation Turbine airfoil platform cooling core
WO2011084040A2 (fr) * 2010-01-05 2011-07-14 Alibi Akhmejanov Procédé de blocage d'éléments mobiles et dispositif permettant de le réaliser
US8777568B2 (en) * 2010-09-30 2014-07-15 General Electric Company Apparatus and methods for cooling platform regions of turbine rotor blades
US8814517B2 (en) * 2010-09-30 2014-08-26 General Electric Company Apparatus and methods for cooling platform regions of turbine rotor blades
GB201016597D0 (en) 2010-10-04 2010-11-17 Rolls Royce Plc Turbine disc cooling arrangement
US8641368B1 (en) * 2011-01-25 2014-02-04 Florida Turbine Technologies, Inc. Industrial turbine blade with platform cooling
FR2974387B1 (fr) * 2011-04-19 2015-11-20 Snecma Roue de turbine pour une turbomachine
RU2460886C1 (ru) * 2011-04-26 2012-09-10 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Ротор турбины
US8734111B2 (en) * 2011-06-27 2014-05-27 General Electric Company Platform cooling passages and methods for creating platform cooling passages in turbine rotor blades
FR2981132B1 (fr) * 2011-10-10 2013-12-06 Snecma Ensemble pour turbomachine a refroidissement de disque
FR2981979B1 (fr) * 2011-10-28 2013-11-29 Snecma Roue de turbine pour une turbomachine
US8870525B2 (en) 2011-11-04 2014-10-28 General Electric Company Bucket assembly for turbine system
US8840370B2 (en) 2011-11-04 2014-09-23 General Electric Company Bucket assembly for turbine system
US8845289B2 (en) 2011-11-04 2014-09-30 General Electric Company Bucket assembly for turbine system
CN103982250B (zh) * 2014-05-12 2015-07-22 天津大学 具有冷却功能的金属橡胶减振器
JP6422308B2 (ja) * 2014-11-05 2018-11-14 三菱日立パワーシステムズ株式会社 シール構造を備えたガスタービン
US10030523B2 (en) * 2015-02-13 2018-07-24 United Technologies Corporation Article having cooling passage with undulating profile
US10066488B2 (en) * 2015-12-01 2018-09-04 General Electric Company Turbomachine blade with generally radial cooling conduit to wheel space
DE102016104957A1 (de) * 2016-03-17 2017-09-21 Rolls-Royce Deutschland Ltd & Co Kg Kühleinrichtung zur Kühlung von Plattformen eines Leitschaufelkranzes einer Gasturbine
RU2695160C2 (ru) * 2017-06-06 2019-07-22 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ БЮДЖЕТНОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Брянский государственный технический университет" Устройство демпфирования колебаний ротора газотурбинного двигателя
EP3438410B1 (fr) 2017-08-01 2021-09-29 General Electric Company Système d'étanchéité pour machine rotative
US20190085706A1 (en) * 2017-09-18 2019-03-21 General Electric Company Turbine engine airfoil assembly
FR3094034B1 (fr) * 2019-03-20 2021-03-19 Safran Aircraft Engines Chemise tubulaire de ventilation pour un distributeur de turbomachine

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Publication number Priority date Publication date Assignee Title
GB612097A (en) * 1946-10-09 1948-11-08 English Electric Co Ltd Improvements in and relating to the cooling of gas turbine rotors
GB1259750A (en) * 1970-07-23 1972-01-12 Rolls Royce Rotor for a fluid flow machine
JPS6022002A (ja) * 1983-07-18 1985-02-04 Hitachi Ltd タ−ボ機械の翼構造
GB2195403A (en) * 1986-09-17 1988-04-07 Rolls Royce Plc Improvements in or relating to sealing and cooling means
US4767260A (en) * 1986-11-07 1988-08-30 United Technologies Corporation Stator vane platform cooling means
US4902198A (en) * 1988-08-31 1990-02-20 Westinghouse Electric Corp. Apparatus for film cooling of turbine van shrouds
US5075621A (en) 1988-12-19 1991-12-24 International Business Machines Corporation Capacitor power probe
US5281097A (en) * 1992-11-20 1994-01-25 General Electric Company Thermal control damper for turbine rotors
GB2280935A (en) * 1993-06-12 1995-02-15 Rolls Royce Plc Cooled sealing strip for nozzle guide vane segments
FR2726323B1 (fr) * 1994-10-26 1996-12-13 Snecma Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine
US5513955A (en) * 1994-12-14 1996-05-07 United Technologies Corporation Turbine engine rotor blade platform seal
US5573375A (en) * 1994-12-14 1996-11-12 United Technologies Corporation Turbine engine rotor blade platform sealing and vibration damping device
FR2758855B1 (fr) 1997-01-30 1999-02-26 Snecma Systeme de ventilation des plates-formes des aubes mobiles

Also Published As

Publication number Publication date
EP1164253B1 (fr) 2005-03-02
US6457935B1 (en) 2002-10-01
JP4047560B2 (ja) 2008-02-13
FR2810365A1 (fr) 2001-12-21
EP1164253A1 (fr) 2001-12-19
JP2002021503A (ja) 2002-01-23

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Legal Events

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CL Concession to grant licences
CD Change of name or company name
ST Notification of lapse

Effective date: 20070228