FR2674569B1 - - Google Patents

Info

Publication number
FR2674569B1
FR2674569B1 FR9103688A FR9103688A FR2674569B1 FR 2674569 B1 FR2674569 B1 FR 2674569B1 FR 9103688 A FR9103688 A FR 9103688A FR 9103688 A FR9103688 A FR 9103688A FR 2674569 B1 FR2674569 B1 FR 2674569B1
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 - Fee Related
Application number
FR9103688A
Other versions
FR2674569A1 (fr
Inventor
Gerard Miraucourt
Gabriel
Jacky Naudet
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 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR9103688A priority Critical patent/FR2674569A1/fr
Priority to GB9203017A priority patent/GB2255138B/en
Publication of FR2674569A1 publication Critical patent/FR2674569A1/fr
Application granted granted Critical
Publication of FR2674569B1 publication Critical patent/FR2674569B1/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
    • F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • 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
    • F01D5/12—Blades
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR9103688A 1991-03-27 1991-03-27 Disque ailete monobloc avec amortissement des vibrations pour turbomachine. Granted FR2674569A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9103688A FR2674569A1 (fr) 1991-03-27 1991-03-27 Disque ailete monobloc avec amortissement des vibrations pour turbomachine.
GB9203017A GB2255138B (en) 1991-03-27 1992-02-13 Unitary bladed disc with vibration damping means

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9103688A FR2674569A1 (fr) 1991-03-27 1991-03-27 Disque ailete monobloc avec amortissement des vibrations pour turbomachine.

Publications (2)

Publication Number Publication Date
FR2674569A1 FR2674569A1 (fr) 1992-10-02
FR2674569B1 true FR2674569B1 (fr) 1994-12-16

Family

ID=9411166

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9103688A Granted FR2674569A1 (fr) 1991-03-27 1991-03-27 Disque ailete monobloc avec amortissement des vibrations pour turbomachine.

Country Status (2)

Country Link
FR (1) FR2674569A1 (fr)
GB (1) GB2255138B (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2712037B1 (fr) * 1993-11-03 1995-12-08 Snecma Turbomachine à compresseur dont le rotor a un étage amont amovible.
FR2716931B1 (fr) * 1994-03-03 1996-04-05 Snecma Système d'équilibrage et d'amortissement d'un dique de turbomachine.
FR2726323B1 (fr) * 1994-10-26 1996-12-13 Snecma Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine
US6375428B1 (en) 2000-08-10 2002-04-23 The Boeing Company Turbine blisk rim friction finger damper
US6354780B1 (en) * 2000-09-15 2002-03-12 General Electric Company Eccentric balanced blisk
US6969239B2 (en) * 2002-09-30 2005-11-29 General Electric Company Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine
FR2870309B1 (fr) * 2004-05-17 2006-07-07 Snecma Moteurs Sa Procede d'assemblage de disques aubages monoblocs et dispositif d'amortissement des vibrations des aubes de ces disques
FR2905413B1 (fr) * 2006-08-31 2012-02-17 Snecma Zone de raccordement entre deux parties d'une piece
EP2019188A1 (fr) * 2007-07-25 2009-01-28 Siemens Aktiengesellschaft Etage de rotor comprenant un dispositif d'amortissement
JP5030813B2 (ja) * 2008-02-20 2012-09-19 三菱重工業株式会社 ブリスク
US9151170B2 (en) * 2011-06-28 2015-10-06 United Technologies Corporation Damper for an integrally bladed rotor
JP2013253522A (ja) * 2012-06-06 2013-12-19 Ihi Corp ブリスク
FR3001402B1 (fr) * 2013-01-31 2015-07-03 Snecma Dispositif auxiliaire de soudage de disques broches, comprenant une ceinture amortissante, et procede de soudage par friction
GB201506196D0 (en) 2015-04-13 2015-05-27 Rolls Royce Plc Rotor damper
GB201506197D0 (en) * 2015-04-13 2015-05-27 Rolls Royce Plc Rotor damper
GB201506195D0 (en) * 2015-04-13 2015-05-27 Rolls Royce Plc Rotor damper
DE102016101427A1 (de) * 2016-01-27 2017-07-27 Rolls-Royce Deutschland Ltd & Co Kg Rotor in BLISK- oder BLING-Bauweise eines Flugtriebwerks
DE102016120346A1 (de) 2016-10-25 2018-04-26 Rolls-Royce Deutschland Ltd & Co Kg Verdichterrotor einer Strömungsmaschine
JP2022148852A (ja) * 2021-03-24 2022-10-06 三菱重工航空エンジン株式会社 タービン動翼及びタービン

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3881844A (en) * 1974-05-28 1975-05-06 Gen Electric Blade platform vibration dampers
US4088421A (en) * 1976-09-30 1978-05-09 General Electric Company Coverplate damping arrangement
US4182598A (en) * 1977-08-29 1980-01-08 United Technologies Corporation Turbine blade damper
GB2172060A (en) * 1985-03-09 1986-09-10 Rolls Royce Bladed rotor
US4621976A (en) * 1985-04-23 1986-11-11 United Technologies Corporation Integrally cast vane and shroud stator with damper
DE3706170C2 (de) * 1987-02-26 1997-08-14 Pierburg Ag Seitenkanalpumpe
US4784572A (en) * 1987-10-14 1988-11-15 United Technologies Corporation Circumferentially bonded rotor

Also Published As

Publication number Publication date
FR2674569A1 (fr) 1992-10-02
GB2255138B (en) 1994-04-20
GB2255138A (en) 1992-10-28
GB9203017D0 (en) 1992-03-25

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Legal Events

Date Code Title Description
CL Concession to grant licenses
CD Change of name or company name
TP Transmission of property
CD Change of name or company name
ST Notification of lapse

Effective date: 20101130