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FR2413542A1 - Amortisseur d'aube de turbomachine - Google Patents

Amortisseur d'aube de turbomachine

Info

Publication number
FR2413542A1
FR2413542A1 FR7827625A FR7827625A FR2413542A1 FR 2413542 A1 FR2413542 A1 FR 2413542A1 FR 7827625 A FR7827625 A FR 7827625A FR 7827625 A FR7827625 A FR 7827625A FR 2413542 A1 FR2413542 A1 FR 2413542A1
Authority
FR
France
Prior art keywords
shock absorber
radial
dawn
turbomachine
sense
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.)
Granted
Application number
FR7827625A
Other languages
English (en)
Other versions
FR2413542B1 (fr
Inventor
Frederick Charles Herzner
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 FR2413542A1 publication Critical patent/FR2413542A1/fr
Application granted granted Critical
Publication of FR2413542B1 publication Critical patent/FR2413542B1/fr
Granted 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
    • 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
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/10—Anti- vibration means
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/10—Suppression of vibrations in rotating systems by making use of members moving with the system
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

AMORTISSEUR RESISTANT AUX HAUTES TEMPERATURES. IL COMPREND UNE PARTIE INFERIEURE 87, RETENUE AUSSI BIEN DANS LE SENS RADIAL QUE DANS LE SENS AXIAL, DE FACON A POUVOIR TOURNER DANS UN PLAN AXIAL, ET UNE PARTIE SUPERIEURE 26 POSSEDANT UNE SURFACE D'APPUI 91 QUI PORTE SUR UNE AUBE, CET AMORTISSEUR AYANT UN CENTRE DE GRAVITE QUI SE TROUVE DANS UN PLAN RADIAL, AXIALEMENT DISTANT DE CELUI DU POINT DE RETENUE RADIALE, DANS LE SENS QUI S'ELOIGNE DU DISQUE. APPLICATION AUX AUBES DE TURBOMACHINE.
FR7827625A 1977-12-28 1978-09-27 Amortisseur d'aube de turbomachine Granted FR2413542A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/865,343 US4192633A (en) 1977-12-28 1977-12-28 Counterweighted blade damper

Publications (2)

Publication Number Publication Date
FR2413542A1 true FR2413542A1 (fr) 1979-07-27
FR2413542B1 FR2413542B1 (fr) 1985-04-26

Family

ID=25345292

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7827625A Granted FR2413542A1 (fr) 1977-12-28 1978-09-27 Amortisseur d'aube de turbomachine

Country Status (6)

Country Link
US (1) US4192633A (fr)
JP (1) JPS5491605A (fr)
DE (1) DE2841793A1 (fr)
FR (1) FR2413542A1 (fr)
GB (1) GB2012006B (fr)
IT (1) IT1098860B (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2523208A1 (fr) * 1982-03-12 1983-09-16 Snecma Dispositif d'amortissement des vibrations d'aubes mobiles de turbine
FR2586061A1 (fr) * 1985-08-08 1987-02-13 Snecma Disque porte labyrinthe multifonction pour rotor de turbomachine
EP0374079A1 (fr) * 1988-12-14 1990-06-20 United Technologies Corporation Dispositif de rétention et d'amortissage de vibrations pour aubes de turbine
EP0717170A1 (fr) * 1994-12-14 1996-06-19 United Technologies Corporation Dispositif d'étanchéité pour la plate-forme des aubes du rotor de turbine
FR2953554A1 (fr) * 2009-12-07 2011-06-10 Snecma Flasque de maintien d'un jonc de retenue comprenant une masse formant contrepoids
FR3020408A1 (fr) * 2014-04-24 2015-10-30 Snecma Ensemble rotatif pour turbomachine
FR3024491A1 (fr) * 2014-08-01 2016-02-05 Snecma Ensemble rotatif pour turbomachine a dispositif de mise en place d'aubes

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4480958A (en) * 1983-02-09 1984-11-06 The United States Of America As Represented By The Secretary Of The Air Force High pressure turbine rotor two-piece blade retainer
US4507052A (en) * 1983-03-31 1985-03-26 General Motors Corporation End seal for turbine blade bases
US4483661A (en) * 1983-05-02 1984-11-20 General Electric Company Blade assembly for a turbomachine
US4558988A (en) * 1983-12-22 1985-12-17 United Technologies Corporation Rotor disk cover plate attachment
US4645424A (en) * 1984-07-23 1987-02-24 United Technologies Corporation Rotating seal for gas turbine engine
US4669959A (en) * 1984-07-23 1987-06-02 United Technologies Corporation Breach lock anti-rotation key
US4659289A (en) * 1984-07-23 1987-04-21 United Technologies Corporation Turbine side plate assembly
JPS6217306A (ja) * 1985-07-12 1987-01-26 Mitsubishi Heavy Ind Ltd 回転機械翼
GB8705216D0 (en) * 1987-03-06 1987-04-08 Rolls Royce Plc Rotor assembly
US4784012A (en) * 1987-09-08 1988-11-15 United Technologies Corporation Rotor balance system
US4835827A (en) * 1987-09-08 1989-06-06 United Technologies Corporation Method of balancing a rotor
US4817455A (en) * 1987-10-15 1989-04-04 United Technologies Corporation Gas turbine engine balancing
US4890981A (en) * 1988-12-30 1990-01-02 General Electric Company Boltless rotor blade retainer
GB2228541B (en) * 1989-02-23 1993-04-14 Rolls Royce Plc Device for damping vibrations in turbomachinery blades
US5205714A (en) * 1990-07-30 1993-04-27 General Electric Company Aircraft fan blade damping apparatus
US5259728A (en) * 1992-05-08 1993-11-09 General Electric Company Bladed disk assembly
FR2695433B1 (fr) * 1992-09-09 1994-10-21 Snecma Joint annulaire d'étanchéité disposé à une extrémité axiale d'un rotor et recouvrant des brochages d'aubes.
GB2455431B (en) * 1994-11-30 2009-11-18 Rolls Royce Plc Split shank rotor blade
US6102664A (en) * 1995-12-14 2000-08-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Blading system and method for controlling structural vibrations
GB2311826B (en) * 1996-04-02 2000-05-10 Europ Gas Turbines Ltd Turbomachines
US5733103A (en) * 1996-12-17 1998-03-31 General Electric Company Vibration damper for a turbine engine
US6077035A (en) * 1998-03-27 2000-06-20 Pratt & Whitney Canada Corp. Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine
WO2000070509A1 (fr) 1999-05-13 2000-11-23 Rolls- Royce Corporation Procede de conception de structure a symetrie cyclique
FR2812906B1 (fr) * 2000-08-10 2002-09-20 Snecma Moteurs Bague de retention axiale d'un flasque sur un disque
US6796408B2 (en) * 2002-09-13 2004-09-28 The Boeing Company Method for vibration damping using superelastic alloys
US6884028B2 (en) * 2002-09-30 2005-04-26 General Electric Company Turbomachinery blade retention system
GB2405183A (en) * 2003-08-21 2005-02-23 Rolls Royce Plc Ring and channel arrangement for joining components
US7238008B2 (en) * 2004-05-28 2007-07-03 General Electric Company Turbine blade retainer seal
US7484936B2 (en) * 2005-09-26 2009-02-03 Pratt & Whitney Canada Corp. Blades for a gas turbine engine with integrated sealing plate and method
US8277191B2 (en) * 2009-02-25 2012-10-02 General Electric Company Apparatus for bucket cover plate retention
DE102009011964A1 (de) * 2009-03-05 2010-09-09 Mtu Aero Engines Gmbh Rotor für eine Strömungsmaschine
US20100254807A1 (en) * 2009-04-07 2010-10-07 Honeywell International Inc. Turbine rotor seal plate with integral flow discourager
US8353670B2 (en) * 2009-07-30 2013-01-15 Pratt & Whitney Canada Corp. Axial balancing clip weight for rotor assembly and method for balancing a rotor assembly
US8469670B2 (en) * 2009-08-27 2013-06-25 Rolls-Royce Corporation Fan assembly
DE102010015211B4 (de) * 2010-04-16 2013-06-20 Mtu Aero Engines Gmbh Dämpfungselement zur Dämpfung von Laufschaufelschwingungen, Laufschaufel sowie Rotor
US8727735B2 (en) * 2011-06-30 2014-05-20 General Electric Company Rotor assembly and reversible turbine blade retainer therefor
US9217334B2 (en) * 2011-10-26 2015-12-22 General Electric Company Turbine cover plate assembly
US10184345B2 (en) 2013-08-09 2019-01-22 United Technologies Corporation Cover plate assembly for a gas turbine engine
FR3010442B1 (fr) * 2013-09-09 2015-10-09 Snecma Disque aubage monobloc a contraintes reduites en pied d'aube, de preference pour soufflante de turbomachine d'aeronef
FR3011031B1 (fr) * 2013-09-25 2017-12-29 Herakles Ensemble rotatif pour turbomachine
EP3073052B1 (fr) * 2015-02-17 2018-01-24 Rolls-Royce Corporation Ensemble de soufflant
GB201506197D0 (en) * 2015-04-13 2015-05-27 Rolls Royce Plc Rotor damper
GB201514212D0 (en) * 2015-08-12 2015-09-23 Rolls Royce Plc Turbine disc assembly
US10724375B2 (en) * 2016-02-12 2020-07-28 General Electric Company Gas turbine engine with ring damper
FR3049645B1 (fr) * 2016-03-30 2019-06-28 Safran Aircraft Engines Ensemble rotatif pour turbomachine a jonc aval en u
US10323519B2 (en) * 2016-06-23 2019-06-18 United Technologies Corporation Gas turbine engine having a turbine rotor with torque transfer and balance features
GB2571176B (en) * 2017-12-14 2022-07-20 Safran Aircraft Engines Damping device
WO2019122691A1 (fr) * 2017-12-18 2019-06-27 Safran Aircraft Engines Dispositif amortisseur
US11035253B2 (en) * 2019-02-05 2021-06-15 Raytheon Technologies Corporation Face seal with damper
US11156110B1 (en) * 2020-08-04 2021-10-26 General Electric Company Rotor assembly for a turbine section of a gas turbine engine
US11686202B1 (en) 2021-12-20 2023-06-27 Rolls-Royce North American Technologies Inc. Rotor damper with contact biasing feature for turbine engines

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2990156A (en) * 1956-08-17 1961-06-27 Gen Electric Blade damping means
FR1319587A (fr) * 1961-04-10 1963-03-01 Thomson Houston Comp Francaise Dispositif d'étanchéité et de blocage d'aubes de turbine à longue queue
FR1362926A (fr) * 1962-07-11 1964-06-05 Thomson Houston Comp Francaise Plaque de recouvrement pour assurer l'obturation des intervalles entre des aubes de turbine
FR1384608A (fr) * 1963-07-05 1965-01-08 United Aircraft Corp Dispositif amortisseur pour aube
US3455537A (en) * 1967-09-27 1969-07-15 Continental Aviat & Eng Corp Air-cooled turbine rotor self-sustaining shroud plate
FR2324873A1 (fr) * 1975-09-17 1977-04-15 Snecma Perfectionnements aux flasques de rotors de turbomachines

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2836392A (en) * 1953-06-03 1958-05-27 United Aircraft Corp Disc vibration damping means
US2999668A (en) * 1958-08-28 1961-09-12 Curtiss Wright Corp Self-balanced rotor blade
US3129921A (en) * 1962-07-06 1964-04-21 United Aircraft Corp Blade damping device
NL295165A (fr) * 1962-07-11
US3181835A (en) * 1964-01-07 1965-05-04 Carroll C Davis Blade vibration damping device
US3700354A (en) * 1971-05-03 1972-10-24 Us Navy Compressor blade root seal
BE791375A (fr) * 1971-12-02 1973-03-01 Gen Electric Deflecteur et amortisseur pour ailettes de turbomachines
BE792286A (fr) * 1971-12-06 1973-03-30 Gen Electric Dispositif de retenue d'aubes sans boulon pour un rotor de turbomachin
US3814539A (en) * 1972-10-04 1974-06-04 Gen Electric Rotor sealing arrangement for an axial flow fluid turbine

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2990156A (en) * 1956-08-17 1961-06-27 Gen Electric Blade damping means
FR1319587A (fr) * 1961-04-10 1963-03-01 Thomson Houston Comp Francaise Dispositif d'étanchéité et de blocage d'aubes de turbine à longue queue
FR1362926A (fr) * 1962-07-11 1964-06-05 Thomson Houston Comp Francaise Plaque de recouvrement pour assurer l'obturation des intervalles entre des aubes de turbine
FR1384608A (fr) * 1963-07-05 1965-01-08 United Aircraft Corp Dispositif amortisseur pour aube
US3455537A (en) * 1967-09-27 1969-07-15 Continental Aviat & Eng Corp Air-cooled turbine rotor self-sustaining shroud plate
FR2324873A1 (fr) * 1975-09-17 1977-04-15 Snecma Perfectionnements aux flasques de rotors de turbomachines

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2523208A1 (fr) * 1982-03-12 1983-09-16 Snecma Dispositif d'amortissement des vibrations d'aubes mobiles de turbine
EP0089272A1 (fr) * 1982-03-12 1983-09-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Roue de rotor de turbine comportant un dispositif d'amortissement des vibrations d'aubes
US4480959A (en) * 1982-03-12 1984-11-06 S.N.E.C.M.A. Device for damping vibrations of mobile turbine blades
FR2586061A1 (fr) * 1985-08-08 1987-02-13 Snecma Disque porte labyrinthe multifonction pour rotor de turbomachine
EP0214876A1 (fr) * 1985-08-08 1987-03-18 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Disque porte labyrinthe multifonction pour rotor de turbomachine
US4668167A (en) * 1985-08-08 1987-05-26 Societe National D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Multifunction labyrinth seal support disk for a turbojet engine rotor
EP0374079A1 (fr) * 1988-12-14 1990-06-20 United Technologies Corporation Dispositif de rétention et d'amortissage de vibrations pour aubes de turbine
EP0717170A1 (fr) * 1994-12-14 1996-06-19 United Technologies Corporation Dispositif d'étanchéité pour la plate-forme des aubes du rotor de turbine
FR2953554A1 (fr) * 2009-12-07 2011-06-10 Snecma Flasque de maintien d'un jonc de retenue comprenant une masse formant contrepoids
FR3020408A1 (fr) * 2014-04-24 2015-10-30 Snecma Ensemble rotatif pour turbomachine
US9784114B2 (en) 2014-04-24 2017-10-10 Snecma Rotating assembly for a turbomachine
FR3024491A1 (fr) * 2014-08-01 2016-02-05 Snecma Ensemble rotatif pour turbomachine a dispositif de mise en place d'aubes

Also Published As

Publication number Publication date
IT1098860B (it) 1985-09-18
JPS5491605A (en) 1979-07-20
IT7827894A0 (it) 1978-09-20
GB2012006A (en) 1979-07-18
GB2012006B (en) 1982-10-13
DE2841793C2 (fr) 1988-04-21
JPS641642B2 (fr) 1989-01-12
FR2413542B1 (fr) 1985-04-26
US4192633A (en) 1980-03-11
DE2841793A1 (de) 1979-07-12

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