FR2726323B1 - Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine - Google Patents

Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine

Info

Publication number
FR2726323B1
FR2726323B1 FR9412785A FR9412785A FR2726323B1 FR 2726323 B1 FR2726323 B1 FR 2726323B1 FR 9412785 A FR9412785 A FR 9412785A FR 9412785 A FR9412785 A FR 9412785A FR 2726323 B1 FR2726323 B1 FR 2726323B1
Authority
FR
France
Prior art keywords
turbomachine
blades
assembly
rotary disc
especially used
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
FR9412785A
Other languages
English (en)
Other versions
FR2726323A1 (fr
Inventor
Marc Roger Marchi
Jean Claude Christian Taillant
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR9412785A priority Critical patent/FR2726323B1/fr
Priority to US08/544,019 priority patent/US5599170A/en
Priority to DE69505085T priority patent/DE69505085T2/de
Priority to EP95402376A priority patent/EP0709549B1/fr
Publication of FR2726323A1 publication Critical patent/FR2726323A1/fr
Application granted granted Critical
Publication of FR2726323B1 publication Critical patent/FR2726323B1/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
    • 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
    • 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
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR9412785A 1994-10-26 1994-10-26 Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine Expired - Fee Related FR2726323B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR9412785A FR2726323B1 (fr) 1994-10-26 1994-10-26 Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine
US08/544,019 US5599170A (en) 1994-10-26 1995-10-17 Seal for gas turbine rotor blades
DE69505085T DE69505085T2 (de) 1994-10-26 1995-10-25 Beschaufelter Rotor besonders für eine Turbomaschine
EP95402376A EP0709549B1 (fr) 1994-10-26 1995-10-25 Ensemble d'un disque rotatif et d'aubes, notamment utilisé dans un turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9412785A FR2726323B1 (fr) 1994-10-26 1994-10-26 Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine

Publications (2)

Publication Number Publication Date
FR2726323A1 FR2726323A1 (fr) 1996-05-03
FR2726323B1 true FR2726323B1 (fr) 1996-12-13

Family

ID=9468217

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9412785A Expired - Fee Related FR2726323B1 (fr) 1994-10-26 1994-10-26 Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine

Country Status (4)

Country Link
US (1) US5599170A (fr)
EP (1) EP0709549B1 (fr)
DE (1) DE69505085T2 (fr)
FR (1) FR2726323B1 (fr)

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FR2739135B1 (fr) * 1995-09-21 1997-10-31 Snecma Agencement amortisseur monte entre des aubes de rotor
FR2758855B1 (fr) * 1997-01-30 1999-02-26 Snecma Systeme de ventilation des plates-formes des aubes mobiles
US5836744A (en) * 1997-04-24 1998-11-17 United Technologies Corporation Frangible fan blade
US5873702A (en) * 1997-06-20 1999-02-23 Siemens Westinghouse Power Corporation Apparatus and method for sealing gas turbine blade roots
US6273683B1 (en) 1999-02-05 2001-08-14 Siemens Westinghouse Power Corporation Turbine blade platform seal
JP2002544432A (ja) 1999-05-14 2002-12-24 シーメンス アクチエンゲゼルシヤフト ロータに対する漏れ止め装置付き流体機械
JP2002544430A (ja) 1999-05-14 2002-12-24 シーメンス アクチエンゲゼルシヤフト ロータに対する漏れ止め装置付き流体機械特にガスタービン
GB9915637D0 (en) * 1999-07-06 1999-09-01 Rolls Royce Plc A rotor seal
FR2810365B1 (fr) * 2000-06-15 2002-10-11 Snecma Moteurs Systeme de ventilation d'une paire de plates-formes d'aubes juxtaposees
US6431835B1 (en) * 2000-10-17 2002-08-13 Honeywell International, Inc. Fan blade compliant shim
SE0103002D0 (sv) * 2001-09-10 2001-09-10 Trelleborg Ab Vibration damping material
US6579065B2 (en) * 2001-09-13 2003-06-17 General Electric Co. Methods and apparatus for limiting fluid flow between adjacent rotor blades
US6916154B2 (en) * 2003-04-29 2005-07-12 Pratt & Whitney Canada Corp. Diametrically energized piston ring
US6932575B2 (en) * 2003-10-08 2005-08-23 United Technologies Corporation Blade damper
US7217081B2 (en) * 2004-10-15 2007-05-15 Siemens Power Generation, Inc. Cooling system for a seal for turbine vane shrouds
US20070048140A1 (en) * 2005-08-24 2007-03-01 General Electric Company Methods and apparatus for assembling gas turbine engines
US7762780B2 (en) * 2007-01-25 2010-07-27 Siemens Energy, Inc. Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies
GB0802834D0 (en) * 2008-02-18 2008-03-26 Rolls Royce Plc Annulus filler
US8215914B2 (en) * 2008-07-08 2012-07-10 General Electric Company Compliant seal for rotor slot
US8210823B2 (en) * 2008-07-08 2012-07-03 General Electric Company Method and apparatus for creating seal slots for turbine components
US8210821B2 (en) * 2008-07-08 2012-07-03 General Electric Company Labyrinth seal for turbine dovetail
US8038405B2 (en) * 2008-07-08 2011-10-18 General Electric Company Spring seal for turbine dovetail
US8210820B2 (en) * 2008-07-08 2012-07-03 General Electric Company Gas assisted turbine seal
US8011894B2 (en) * 2008-07-08 2011-09-06 General Electric Company Sealing mechanism with pivot plate and rope seal
US8393869B2 (en) 2008-12-19 2013-03-12 Solar Turbines Inc. Turbine blade assembly including a damper
US8820754B2 (en) 2010-06-11 2014-09-02 Siemens Energy, Inc. Turbine blade seal assembly
FR2970033B1 (fr) * 2011-01-04 2015-10-16 Turbomeca Procede d'amortissement de pale de turbine a gaz et amortisseur de vibration de mise en oeuvre
US9366142B2 (en) * 2011-10-28 2016-06-14 General Electric Company Thermal plug for turbine bucket shank cavity and related method
US9297263B2 (en) 2012-10-31 2016-03-29 Solar Turbines Incorporated Turbine blade for a gas turbine engine
US9347325B2 (en) 2012-10-31 2016-05-24 Solar Turbines Incorporated Damper for a turbine rotor assembly
US9228443B2 (en) 2012-10-31 2016-01-05 Solar Turbines Incorporated Turbine rotor assembly
US9303519B2 (en) 2012-10-31 2016-04-05 Solar Turbines Incorporated Damper for a turbine rotor assembly
WO2014160641A1 (fr) 2013-03-25 2014-10-02 United Technologies Corporation Pale de rotor à languette d'étanchéité en forme de l
US9765625B2 (en) * 2013-05-23 2017-09-19 MTU Aero Engines AG Turbomachine blade
EP2806106A1 (fr) 2013-05-23 2014-11-26 MTU Aero Engines GmbH Aube de turbomachine avec corps d'impulsion
ES2632939T3 (es) * 2013-12-12 2017-09-18 MTU Aero Engines AG Disposición de álabes móviles para turbinas de gas
US9797270B2 (en) 2013-12-23 2017-10-24 Rolls-Royce North American Technologies Inc. Recessable damper for turbine
US9920627B2 (en) * 2014-05-22 2018-03-20 United Technologies Corporation Rotor heat shield
US9995162B2 (en) * 2014-10-20 2018-06-12 United Technologies Corporation Seal and clip-on damper system and device
EP3078808A1 (fr) * 2015-04-07 2016-10-12 Siemens Aktiengesellschaft Rangée d'aubes pour une turbomachine
US10472975B2 (en) * 2015-09-03 2019-11-12 General Electric Company Damper pin having elongated bodies for damping adjacent turbine blades
EP3438410B1 (fr) 2017-08-01 2021-09-29 General Electric Company Système d'étanchéité pour machine rotative
JP7039355B2 (ja) * 2018-03-28 2022-03-22 三菱重工業株式会社 回転機械
US10641111B2 (en) * 2018-08-31 2020-05-05 Rolls-Royce Corporation Turbine blade assembly with ceramic matrix composite components
FR3109403B1 (fr) * 2020-04-16 2022-08-12 Safran Aircraft Engines Aube avec organes d’étanchéités améliorés
US11066936B1 (en) * 2020-05-07 2021-07-20 Rolls-Royce Corporation Turbine bladed disc brazed sealing plate with flow metering and axial retention features

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Publication number Priority date Publication date Assignee Title
US2912223A (en) * 1955-03-17 1959-11-10 Gen Electric Turbine bucket vibration dampener and sealing assembly
US3119595A (en) * 1961-02-23 1964-01-28 Gen Electric Bladed rotor and baffle assembly
US3112915A (en) * 1961-12-22 1963-12-03 Gen Electric Rotor assembly air baffle
US3887298A (en) * 1974-05-30 1975-06-03 United Aircraft Corp Apparatus for sealing turbine blade damper cavities
US4183720A (en) * 1978-01-03 1980-01-15 The United States Of America As Represented By The Secretary Of The Air Force Composite fan blade platform double wedge centrifugal seal
FR2503247B1 (fr) * 1981-04-07 1985-06-14 Snecma Perfectionnements aux etages de turbine a gaz de turboreacteurs munis de moyens de refroidissement par air du disque de la roue de la turbine
GB2112466A (en) * 1981-12-30 1983-07-20 Rolls Royce Rotor blade vibration damping
US4473337A (en) * 1982-03-12 1984-09-25 United Technologies Corporation Blade damper seal
FR2523208A1 (fr) * 1982-03-12 1983-09-16 Snecma Dispositif d'amortissement des vibrations d'aubes mobiles de turbine
GB2127104A (en) * 1982-08-11 1984-04-04 Rolls Royce Sealing means for a turbine rotor blade in a gas turbine engine
US4872812A (en) * 1987-08-05 1989-10-10 General Electric Company Turbine blade plateform sealing and vibration damping apparatus
FR2665726B1 (fr) * 1990-08-08 1993-07-02 Snecma Soufflante de turbomachine a amortisseur dynamique a cames.
FR2674569A1 (fr) * 1991-03-27 1992-10-02 Snecma Disque ailete monobloc avec amortissement des vibrations pour turbomachine.
US5156528A (en) * 1991-04-19 1992-10-20 General Electric Company Vibration damping of gas turbine engine buckets
US5261790A (en) * 1992-02-03 1993-11-16 General Electric Company Retention device for turbine blade damper
US5313786A (en) * 1992-11-24 1994-05-24 United Technologies Corporation Gas turbine blade damper
US5284421A (en) * 1992-11-24 1994-02-08 United Technologies Corporation Rotor blade with platform support and damper positioning means
US5478207A (en) * 1994-09-19 1995-12-26 General Electric Company Stable blade vibration damper for gas turbine engine
US5513955A (en) * 1994-12-14 1996-05-07 United Technologies Corporation Turbine engine rotor blade platform seal

Also Published As

Publication number Publication date
EP0709549A1 (fr) 1996-05-01
EP0709549B1 (fr) 1998-09-30
DE69505085D1 (de) 1998-11-05
FR2726323A1 (fr) 1996-05-03
US5599170A (en) 1997-02-04
DE69505085T2 (de) 1999-05-06

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Legal Events

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