FR2739136B1 - Agencement amortissant pour des aubes de rotor - Google Patents

Agencement amortissant pour des aubes de rotor

Info

Publication number
FR2739136B1
FR2739136B1 FR9511080A FR9511080A FR2739136B1 FR 2739136 B1 FR2739136 B1 FR 2739136B1 FR 9511080 A FR9511080 A FR 9511080A FR 9511080 A FR9511080 A FR 9511080A FR 2739136 B1 FR2739136 B1 FR 2739136B1
Authority
FR
France
Prior art keywords
rotor blades
damping arrangement
damping
arrangement
blades
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
FR9511080A
Other languages
English (en)
Other versions
FR2739136A1 (fr
Inventor
Jacques Marie Pierre Stenneler
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 FR9511080A priority Critical patent/FR2739136B1/fr
Priority to US08/714,976 priority patent/US5791877A/en
Priority to EP96401990A priority patent/EP0764765A1/fr
Publication of FR2739136A1 publication Critical patent/FR2739136A1/fr
Application granted granted Critical
Publication of FR2739136B1 publication Critical patent/FR2739136B1/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
    • 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
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • 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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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)
FR9511080A 1995-09-21 1995-09-21 Agencement amortissant pour des aubes de rotor Expired - Fee Related FR2739136B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR9511080A FR2739136B1 (fr) 1995-09-21 1995-09-21 Agencement amortissant pour des aubes de rotor
US08/714,976 US5791877A (en) 1995-09-21 1996-09-17 Damping disposition for rotor vanes
EP96401990A EP0764765A1 (fr) 1995-09-21 1996-09-19 Agencement amortissant pour des aubes de rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9511080A FR2739136B1 (fr) 1995-09-21 1995-09-21 Agencement amortissant pour des aubes de rotor

Publications (2)

Publication Number Publication Date
FR2739136A1 FR2739136A1 (fr) 1997-03-28
FR2739136B1 true FR2739136B1 (fr) 1997-10-31

Family

ID=9482789

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9511080A Expired - Fee Related FR2739136B1 (fr) 1995-09-21 1995-09-21 Agencement amortissant pour des aubes de rotor

Country Status (3)

Country Link
US (1) US5791877A (fr)
EP (1) EP0764765A1 (fr)
FR (1) FR2739136B1 (fr)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2776012B1 (fr) * 1998-03-12 2000-04-07 Snecma Joint d'etancheite d'un etage d'aubes circulaire
US6431835B1 (en) 2000-10-17 2002-08-13 Honeywell International, Inc. Fan blade compliant shim
FR2831207B1 (fr) * 2001-10-24 2004-06-04 Snecma Moteurs Plates-formes pour aubes d'un ensemble rotatif
US6857856B2 (en) * 2002-09-27 2005-02-22 Florida Turbine Technologies, Inc. Tailored attachment mechanism for composite airfoils
US7300255B2 (en) * 2002-09-27 2007-11-27 Florida Turbine Technologies, Inc. Laminated turbomachine airfoil with jacket and method of making the airfoil
GB0806171D0 (en) * 2008-04-07 2008-05-14 Rolls Royce Plc Aeroengine fan assembly
GB0814718D0 (en) * 2008-08-13 2008-09-17 Rolls Royce Plc Annulus filler
CH700001A1 (de) 2008-11-20 2010-05-31 Alstom Technology Ltd Laufschaufelanordnung, insbesondere für eine gasturbine.
US8616849B2 (en) * 2009-02-18 2013-12-31 Pratt & Whitney Canada Corp. Fan blade platform
US8568102B2 (en) 2009-02-18 2013-10-29 Pratt & Whitney Canada Corp. Fan blade anti-fretting insert
DE102009011964A1 (de) * 2009-03-05 2010-09-09 Mtu Aero Engines Gmbh Rotor für eine Strömungsmaschine
EP2295722B1 (fr) * 2009-09-09 2019-11-06 Ansaldo Energia IP UK Limited Pale de turbine
FR2959527B1 (fr) * 2010-04-28 2012-07-20 Snecma Piece anti-usure pour echasse d'aube de soufflante de turboreacteur
US8794925B2 (en) 2010-08-24 2014-08-05 United Technologies Corporation Root region of a blade for a gas turbine engine
US8734101B2 (en) * 2010-08-31 2014-05-27 General Electric Co. Composite vane mounting
GB2489222A (en) * 2011-03-21 2012-09-26 Rolls Royce Plc Bladed rotor with annulus filler
GB2490858B (en) 2011-03-22 2014-01-01 Rolls Royce Plc A bladed rotor
GB201106050D0 (en) * 2011-04-11 2011-05-25 Rolls Royce Plc A retention device for a composite blade of a gas turbine engine
US20130011271A1 (en) * 2011-07-05 2013-01-10 United Technologies Corporation Ceramic matrix composite components
US9140132B2 (en) 2012-05-31 2015-09-22 Solar Turbines Incorporated Turbine blade support
US9017033B2 (en) * 2012-06-07 2015-04-28 United Technologies Corporation Fan blade platform
GB201217257D0 (en) * 2012-09-27 2012-11-07 Rolls Royce Plc Annulus filler for axial flow machine
US9353629B2 (en) 2012-11-30 2016-05-31 Solar Turbines Incorporated Turbine blade apparatus
US9650902B2 (en) * 2013-01-11 2017-05-16 United Technologies Corporation Integral fan blade wear pad and platform seal
WO2014163709A2 (fr) * 2013-03-13 2014-10-09 Uskert Richard C Plate-forme pour aubes de turbine composites à matrice céramique
US9958113B2 (en) * 2013-03-15 2018-05-01 United Technologies Corporation Fan blade lubrication
US9896946B2 (en) * 2013-10-31 2018-02-20 General Electric Company Gas turbine engine rotor assembly and method of assembling the same
FR3037097B1 (fr) * 2015-06-03 2017-06-23 Snecma Aube composite comprenant une plateforme munie d'un raidisseur
US10753368B2 (en) * 2016-08-23 2020-08-25 Raytheon Technologies Corporation Multi-piece non-linear airfoil
US10767498B2 (en) 2018-04-03 2020-09-08 Rolls-Royce High Temperature Composites Inc. Turbine disk with pinned platforms
US10890081B2 (en) 2018-04-23 2021-01-12 Rolls-Royce Corporation Turbine disk with platforms coupled to disk
US10577961B2 (en) 2018-04-23 2020-03-03 Rolls-Royce High Temperature Composites Inc. Turbine disk with blade supported platforms
FR3085415B1 (fr) * 2018-09-05 2021-04-16 Safran Aircraft Engines Aube comprenant une structure en materiau composite et une coque metallique
FR3087831B1 (fr) * 2018-10-30 2022-06-24 Safran Aircraft Engines Aube comprenant une structure en materiau composite et une piece de raidissement metallique
FR3087830B1 (fr) * 2018-10-30 2020-10-16 Safran Aircraft Engines Aube comprenant une structure en materiau composite et une piece de raidissement metallique
RU191667U1 (ru) * 2019-03-15 2019-08-15 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Рабочее колесо осевого турбокомпрессора
FR3099520B1 (fr) * 2019-07-31 2021-07-23 Safran Aircraft Engines Roue de turbomachine
US11280202B2 (en) 2020-04-06 2022-03-22 Raytheon Technologies Corporation Balanced composite root region for a blade of a gas turbine engine
FR3121171B1 (fr) * 2021-03-25 2023-04-14 Safran Aircraft Engines Rotor de soufflante pour une turbomachine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3119595A (en) * 1961-02-23 1964-01-28 Gen Electric Bladed rotor and baffle assembly
US3640640A (en) * 1970-12-04 1972-02-08 Rolls Royce Fluid flow machine
DE2108176A1 (de) * 1971-02-20 1972-08-31 Motoren Turbinen Union Befestigung von keramischen Turbinenschaufeln
US4019832A (en) * 1976-02-27 1977-04-26 General Electric Company Platform for a turbomachinery blade
FR2419389A1 (fr) * 1978-03-08 1979-10-05 Snecma Perfectionnements aux flasques de rotors de turbomachines
US4417854A (en) * 1980-03-21 1983-11-29 Rockwell International Corporation Compliant interface for ceramic turbine blades
FR2523208A1 (fr) * 1982-03-12 1983-09-16 Snecma Dispositif d'amortissement des vibrations d'aubes mobiles de turbine
GB2171151B (en) * 1985-02-20 1988-05-18 Rolls Royce Rotors for gas turbine engines
US4790723A (en) * 1987-01-12 1988-12-13 Westinghouse Electric Corp. Process for securing a turbine blade
FR2669686B1 (fr) * 1990-11-28 1994-09-02 Snecma Rotor de soufflante avec aubes sans plates-formes et sabots reconstituant le profil de veine.
US5160243A (en) * 1991-01-15 1992-11-03 General Electric Company Turbine blade wear protection system with multilayer shim
US5205713A (en) * 1991-04-29 1993-04-27 General Electric Company Fan blade damper
US5240375A (en) * 1992-01-10 1993-08-31 General Electric Company Wear protection system for turbine engine rotor and blade

Also Published As

Publication number Publication date
FR2739136A1 (fr) 1997-03-28
EP0764765A1 (fr) 1997-03-26
US5791877A (en) 1998-08-11

Similar Documents

Publication Publication Date Title
FR2739136B1 (fr) Agencement amortissant pour des aubes de rotor
BR9707910A (pt) Unidade de equilíbrio
BR9600312A (pt) Amortecedor de vibrações de rotação
FR2731466B1 (fr) Stator de turbomachine
DE69614794D1 (de) Betätigungseinrichtung für verstellbare Statorschaufeln
GB2310463B (en) Rotor blade
DE59600750D1 (de) Schwingungsdämpfung für Turbinenschaufeln
DE69606692D1 (de) Welleneinheit
BR9604371A (pt) Macrobiomembrana biossintética indutora de neoformação
ATE228237T1 (de) Rotor
DE69521787D1 (de) Vordämpfungsanlage für rotationsschwingungen
DE69517284D1 (de) Zentrifugenrotor
DE69528281D1 (de) Hochgeschwindigkeitsrotoranordnung
FR2742274B1 (fr) Rotor de magneto-generateur
DE69817257D1 (de) Schwingungsdämpfung bei Rotorblättern
FR2741775B1 (fr) Rotor pour la coupe des vegetaux
DE69620091D1 (de) Giesspapier
FR2742603B1 (fr) Rotor de magneto-generateur
FR2742275B1 (fr) Rotor de magneto-generateur
NO961026D0 (no) Skaft
NO973436D0 (no) Rotor
IT1283542B1 (it) Antivibratore per albero rotante
KR950029045U (ko) 로터베이터용 경운날
KR970000535U (ko) 연속식 진동분쇄기
KR960027168U (ko) 가정용 간이주조기

Legal Events

Date Code Title Description
ST Notification of lapse