FR1579923A - - Google Patents

Info

Publication number
FR1579923A
FR1579923A FR1579923DA FR1579923A FR 1579923 A FR1579923 A FR 1579923A FR 1579923D A FR1579923D A FR 1579923DA FR 1579923 A FR1579923 A FR 1579923A
Authority
FR
France
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
Application number
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 filed Critical
Application granted granted Critical
Publication of FR1579923A publication Critical patent/FR1579923A/fr
Expired legal-status Critical Current

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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00Fluid reaction surfaces, i.e. impellers
    • Y10S416/50Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Electric Vacuum Cleaners (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1579923D 1968-08-09 1968-09-13 Expired FR1579923A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1201168A CH494896A (de) 1968-08-09 1968-08-09 Halterung von Laufschaufeln im Rotor einer Turbomaschine

Publications (1)

Publication Number Publication Date
FR1579923A true FR1579923A (fr) 1969-08-29

Family

ID=4379003

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1579923D Expired FR1579923A (fr) 1968-08-09 1968-09-13

Country Status (7)

Country Link
US (1) US3610778A (fr)
BE (1) BE737251A (fr)
CH (1) CH494896A (fr)
DE (1) DE1800817B1 (fr)
FR (1) FR1579923A (fr)
GB (1) GB1280701A (fr)
NL (1) NL6812195A (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2376958A1 (fr) * 1977-01-11 1978-08-04 Rolls Royce Etage mobile de compresseur
FR2451452A1 (fr) * 1979-03-10 1980-10-10 Rolls Royce Rotor aube, a amortisseur de vibrations, pour moteur a turbine a gaz
FR2523209A1 (fr) * 1982-03-12 1983-09-16 United Technologies Corp Amortisseur d'aube et assemblage d'amortissement d'aubes dans un rotor
FR2669686A1 (fr) * 1990-11-28 1992-05-29 Snecma Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.
EP0490522A1 (fr) * 1990-12-10 1992-06-17 General Electric Company Pièce d'étanchéité pour roue d'aubes de turbine
FR3126446A1 (fr) * 2021-09-01 2023-03-03 Safran Aircraft Engines Amortisseur déformable pour roue mobile de turbomachine

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE791375A (fr) * 1971-12-02 1973-03-01 Gen Electric Deflecteur et amortisseur pour ailettes de turbomachines
US3887298A (en) * 1974-05-30 1975-06-03 United Aircraft Corp Apparatus for sealing turbine blade damper cavities
US4088421A (en) * 1976-09-30 1978-05-09 General Electric Company Coverplate damping arrangement
US4101245A (en) * 1976-12-27 1978-07-18 United Technologies Corporation Interblade damper and seal for turbomachinery rotor
US4182598A (en) * 1977-08-29 1980-01-08 United Technologies Corporation Turbine blade damper
US4626169A (en) * 1983-12-13 1986-12-02 United Technologies Corporation Seal means for a blade attachment slot of a rotor assembly
US4645425A (en) * 1984-12-19 1987-02-24 United Technologies Corporation Turbine or compressor blade mounting
US5313786A (en) * 1992-11-24 1994-05-24 United Technologies Corporation Gas turbine blade damper
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
US5827047A (en) * 1996-06-27 1998-10-27 United Technologies Corporation Turbine blade damper and seal
US5924699A (en) * 1996-12-24 1999-07-20 United Technologies Corporation Turbine blade platform seal
US5785499A (en) * 1996-12-24 1998-07-28 United Technologies Corporation Turbine blade damper and seal
US6929453B2 (en) * 2003-12-11 2005-08-16 Siemens Westinghouse Power Corporation Locking spacer assembly for slotted turbine component
US7125225B2 (en) * 2004-02-04 2006-10-24 United Technologies Corporation Cooled rotor blade with vibration damping device
GB0814018D0 (en) * 2008-08-01 2008-09-10 Rolls Royce Plc Vibration damper
US8240987B2 (en) * 2008-08-15 2012-08-14 United Technologies Corp. Gas turbine engine systems involving baffle assemblies
US8137072B2 (en) * 2008-10-31 2012-03-20 Solar Turbines Inc. Turbine blade including a seal pocket
US8393869B2 (en) 2008-12-19 2013-03-12 Solar Turbines Inc. Turbine blade assembly including a damper
DE102009011879A1 (de) * 2009-03-05 2010-09-16 Mtu Aero Engines Gmbh Integral beschaufelter Rotor und Verfahren zur Herstellung eines integral beschaufelten Rotors
US9650901B2 (en) 2012-05-31 2017-05-16 Solar Turbines Incorporated Turbine damper
US9279332B2 (en) 2012-05-31 2016-03-08 Solar Turbines Incorporated Turbine damper
FR2991372B1 (fr) * 2012-06-04 2014-05-16 Snecma Roue de turbine dans une turbomachine
US9297263B2 (en) * 2012-10-31 2016-03-29 Solar Turbines Incorporated Turbine blade for a gas turbine engine
US9896946B2 (en) * 2013-10-31 2018-02-20 General Electric Company Gas turbine engine rotor assembly and method of assembling the same
US11193376B2 (en) * 2020-02-10 2021-12-07 Raytheon Technologies Corporation Disk supported damper for a gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2669383A (en) * 1951-02-06 1954-02-16 A V Roe Canada Ltd Rotor blade
BE540433A (fr) * 1954-08-12
US2942842A (en) * 1956-06-13 1960-06-28 Gen Motors Corp Turbine blade lock
US3037741A (en) * 1958-12-29 1962-06-05 Gen Electric Damping turbine buckets
US3001760A (en) * 1959-08-07 1961-09-26 Gen Motors Corp Turbine blade lock
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
US3294364A (en) * 1962-01-02 1966-12-27 Gen Electric Rotor assembly
GB996729A (en) * 1963-12-16 1965-06-30 Rolls Royce Improvements relating to turbines and compressors

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2376958A1 (fr) * 1977-01-11 1978-08-04 Rolls Royce Etage mobile de compresseur
FR2451452A1 (fr) * 1979-03-10 1980-10-10 Rolls Royce Rotor aube, a amortisseur de vibrations, pour moteur a turbine a gaz
FR2523209A1 (fr) * 1982-03-12 1983-09-16 United Technologies Corp Amortisseur d'aube et assemblage d'amortissement d'aubes dans un rotor
FR2669686A1 (fr) * 1990-11-28 1992-05-29 Snecma Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.
EP0488874A1 (fr) * 1990-11-28 1992-06-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine
US5161949A (en) * 1990-11-28 1992-11-10 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.M.C.A." Rotor fitted with spacer blocks between the blades
EP0490522A1 (fr) * 1990-12-10 1992-06-17 General Electric Company Pièce d'étanchéité pour roue d'aubes de turbine
FR3126446A1 (fr) * 2021-09-01 2023-03-03 Safran Aircraft Engines Amortisseur déformable pour roue mobile de turbomachine
WO2023031556A1 (fr) * 2021-09-01 2023-03-09 Safran Aircraft Engines Dispositif d'amortissement pour roue mobile de turbomachine d'aéronef, roue mobile pour turbomachine d'aéronef, turbomachine pour aéronef et procédé de fabrication d'un dispositif d'amortissement

Also Published As

Publication number Publication date
GB1280701A (en) 1972-07-05
US3610778A (en) 1971-10-05
CH494896A (de) 1970-08-15
DE1800817B1 (de) 1970-03-12
BE737251A (fr) 1970-02-09
NL6812195A (fr) 1970-02-11

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Legal Events

Date Code Title Description
ST Notification of lapse