FR2619158B1 - - Google Patents

Info

Publication number
FR2619158B1
FR2619158B1 FR8810364A FR8810364A FR2619158B1 FR 2619158 B1 FR2619158 B1 FR 2619158B1 FR 8810364 A FR8810364 A FR 8810364A FR 8810364 A FR8810364 A FR 8810364A FR 2619158 B1 FR2619158 B1 FR 2619158B1
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
FR8810364A
Other versions
FR2619158A1 (fr
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
Publication of FR2619158A1 publication Critical patent/FR2619158A1/fr
Application granted granted Critical
Publication of FR2619158B1 publication Critical patent/FR2619158B1/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
    • 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
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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
FR8810364A 1987-08-05 1988-08-01 Dispositif d'etancheification et d'amortissement des vibrations de la plate-forme d'une aube de turbine Granted FR2619158A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/081,773 US4872812A (en) 1987-08-05 1987-08-05 Turbine blade plateform sealing and vibration damping apparatus

Publications (2)

Publication Number Publication Date
FR2619158A1 FR2619158A1 (fr) 1989-02-10
FR2619158B1 true FR2619158B1 (fr) 1993-02-26

Family

ID=22166300

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8810364A Granted FR2619158A1 (fr) 1987-08-05 1988-08-01 Dispositif d'etancheification et d'amortissement des vibrations de la plate-forme d'une aube de turbine

Country Status (6)

Country Link
US (1) US4872812A (fr)
CA (1) CA1279017C (fr)
DE (1) DE3825951C2 (fr)
FR (1) FR2619158A1 (fr)
GB (1) GB2208529B (fr)
IT (1) IT1226368B (fr)

Families Citing this family (100)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4936749A (en) * 1988-12-21 1990-06-26 General Electric Company Blade-to-blade vibration damper
US5226784A (en) * 1991-02-11 1993-07-13 General Electric Company Blade damper
US5156528A (en) * 1991-04-19 1992-10-20 General Electric Company Vibration damping of gas turbine engine buckets
US5205713A (en) * 1991-04-29 1993-04-27 General Electric Company Fan blade damper
US5108261A (en) * 1991-07-11 1992-04-28 United Technologies Corporation Compressor disk assembly
US5183389A (en) * 1992-01-30 1993-02-02 General Electric Company Anti-rock blade tang
US5242270A (en) * 1992-01-31 1993-09-07 Westinghouse Electric Corp. Platform motion restraints for freestanding turbine blades
US5302085A (en) * 1992-02-03 1994-04-12 General Electric Company Turbine blade damper
US5261790A (en) * 1992-02-03 1993-11-16 General Electric Company Retention device for turbine blade damper
US5415526A (en) * 1993-11-19 1995-05-16 Mercadante; Anthony J. Coolable rotor assembly
FR2716502B1 (fr) * 1994-02-23 1996-04-05 Snecma Garniture d'étanchéité entre des aubes et des plates-formes intermédiaires.
US5478207A (en) * 1994-09-19 1995-12-26 General Electric Company Stable blade vibration damper for gas turbine engine
FR2726323B1 (fr) * 1994-10-26 1996-12-13 Snecma Ensemble d'un disque rotatif et d'aubes, notamment utilise dans une turbomachine
US5573375A (en) * 1994-12-14 1996-11-12 United Technologies Corporation Turbine engine rotor blade platform sealing and vibration damping device
US5513955A (en) * 1994-12-14 1996-05-07 United Technologies Corporation Turbine engine rotor blade platform seal
US5827047A (en) * 1996-06-27 1998-10-27 United Technologies Corporation Turbine blade damper and seal
US5820348A (en) * 1996-09-17 1998-10-13 Fricke; J. Robert Damping system for vibrating members
US5820346A (en) * 1996-12-17 1998-10-13 General Electric Company Blade damper for a turbine engine
US5785499A (en) * 1996-12-24 1998-07-28 United Technologies Corporation Turbine blade damper and seal
US5924699A (en) * 1996-12-24 1999-07-20 United Technologies Corporation Turbine blade platform seal
US6273683B1 (en) 1999-02-05 2001-08-14 Siemens Westinghouse Power Corporation Turbine blade platform seal
DE10014198A1 (de) * 2000-03-22 2001-09-27 Alstom Power Nv Beschaufelung mit Dämpfungselementen
GB0109033D0 (en) 2001-04-10 2001-05-30 Rolls Royce Plc Vibration damping
US6579065B2 (en) 2001-09-13 2003-06-17 General Electric Co. Methods and apparatus for limiting fluid flow between adjacent rotor blades
US6752594B2 (en) 2002-02-07 2004-06-22 The Boeing Company Split blade frictional damper
US6699015B2 (en) 2002-02-19 2004-03-02 The Boeing Company Blades having coolant channels lined with a shape memory alloy and an associated fabrication method
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
GB0304329D0 (en) * 2003-02-26 2003-04-02 Rolls Royce Plc Damper seal
US6851932B2 (en) * 2003-05-13 2005-02-08 General Electric Company Vibration damper assembly for the buckets of a turbine
JP4254352B2 (ja) * 2003-06-04 2009-04-15 株式会社Ｉｈｉ タービンブレード
US6932575B2 (en) 2003-10-08 2005-08-23 United Technologies Corporation Blade damper
JP2005233141A (ja) 2004-02-23 2005-09-02 Mitsubishi Heavy Ind Ltd 動翼およびその動翼を用いたガスタービン
GB2412699A (en) * 2004-03-30 2005-10-05 Rolls Royce Plc Heat shield for rotor blade hub
DE102004023130A1 (de) * 2004-05-03 2005-12-01 Rolls-Royce Deutschland Ltd & Co Kg Dichtungs- und Dämpfungssystem für Turbinenschaufeln
US7121802B2 (en) * 2004-07-13 2006-10-17 General Electric Company Selectively thinned turbine blade
US20060029500A1 (en) * 2004-08-04 2006-02-09 Anthony Cherolis Turbine blade flared buttress
US7217081B2 (en) * 2004-10-15 2007-05-15 Siemens Power Generation, Inc. Cooling system for a seal for turbine vane shrouds
GB2420162A (en) * 2004-11-16 2006-05-17 Cross Mfg Company A seal arrangement for sealing between turbine blades
GB0523106D0 (en) 2005-11-12 2005-12-21 Rolls Royce Plc A cooliing arrangement
US7322797B2 (en) * 2005-12-08 2008-01-29 General Electric Company Damper cooled turbine blade
FR2896289B1 (fr) * 2006-01-13 2008-03-28 Snecma Sa Masselotte d'equilibrage, disque de rotor en etant equipe, rotor et moteur d'aeronef les comportant
EP1818506A1 (fr) 2006-02-08 2007-08-15 Siemens Aktiengesellschaft Réduction de la fatigue répétitive dans un pied de sapin
DE102006026968A1 (de) 2006-06-09 2008-01-24 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Rotoren hoher spezifischer Energieabgabe
US7534090B2 (en) * 2006-06-13 2009-05-19 General Electric Company Enhanced bucket vibration system
US7488157B2 (en) * 2006-07-27 2009-02-10 Siemens Energy, Inc. Turbine vane with removable platform inserts
US7581924B2 (en) * 2006-07-27 2009-09-01 Siemens Energy, Inc. Turbine vanes with airfoil-proximate cooling seam
DE102006041322A1 (de) * 2006-09-01 2008-04-24 Rolls-Royce Deutschland Ltd & Co Kg Dämpfungs- und Dichtungssystem für Turbinenschaufeln
US7762773B2 (en) * 2006-09-22 2010-07-27 Siemens Energy, Inc. Turbine airfoil cooling system with platform edge cooling channels
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
GB2446812A (en) * 2007-02-21 2008-08-27 Rolls Royce Plc Damping member positioned between blades of an aerofoil assembly
BRPI0818386A2 (pt) * 2007-10-25 2015-04-22 Siemens Ag Montagem de pá de turbina e tira de vedação
GB0814018D0 (en) 2008-08-01 2008-09-10 Rolls Royce Plc Vibration damper
US8096758B2 (en) * 2008-09-03 2012-01-17 Siemens Energy, Inc. Circumferential shroud inserts for a gas turbine vane platform
US8070448B2 (en) * 2008-10-30 2011-12-06 Honeywell International Inc. Spacers and turbines
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
DE102009004792B4 (de) * 2009-01-13 2019-10-31 Rolls-Royce Deutschland Ltd & Co Kg Dämpfungselement (Reibdämpfer) mit Dichtungsfunktion für Turbinenlaufschaufeln
US8419370B2 (en) * 2009-06-25 2013-04-16 Rolls-Royce Corporation Retaining and sealing ring assembly
US8469670B2 (en) * 2009-08-27 2013-06-25 Rolls-Royce Corporation Fan assembly
US8435006B2 (en) * 2009-09-30 2013-05-07 Rolls-Royce Corporation Fan
US8834123B2 (en) * 2009-12-29 2014-09-16 Rolls-Royce Corporation Turbomachinery component
US8820754B2 (en) 2010-06-11 2014-09-02 Siemens Energy, Inc. Turbine blade seal assembly
FR2963381B1 (fr) * 2010-07-27 2015-04-10 Snecma Etancheite inter-aubes pour une roue de turbine ou de compresseur de turbomachine
US8790086B2 (en) 2010-11-11 2014-07-29 General Electric Company Turbine blade assembly for retaining sealing and dampening elements
US9022727B2 (en) * 2010-11-15 2015-05-05 Mtu Aero Engines Gmbh Rotor for a turbo machine
US8684695B2 (en) * 2011-01-04 2014-04-01 General Electric Company Damper coverplate and sealing arrangement for turbine bucket shank
US8641368B1 (en) * 2011-01-25 2014-02-04 Florida Turbine Technologies, Inc. Industrial turbine blade with platform cooling
US8662849B2 (en) * 2011-02-14 2014-03-04 General Electric Company Component of a turbine bucket platform
US8905715B2 (en) * 2011-03-17 2014-12-09 General Electric Company Damper and seal pin arrangement for a turbine blade
US10287897B2 (en) * 2011-09-08 2019-05-14 General Electric Company Turbine rotor blade assembly and method of assembling same
US10024177B2 (en) * 2012-05-15 2018-07-17 United Technologies Corporation Detachable fan blade platform and method of repairing same
WO2014004098A1 (fr) 2012-06-30 2014-01-03 General Electric Company Structure d'étanchéité de pale de turbine
US9309782B2 (en) 2012-09-14 2016-04-12 General Electric Company Flat bottom damper pin for turbine blades
US20140271206A1 (en) * 2013-03-12 2014-09-18 Solar Turbines Incorporated Turbine blade with a pin seal slot
US20140271205A1 (en) * 2013-03-12 2014-09-18 Solar Turbines Incorporated Turbine blade pin seal
RU2529279C1 (ru) * 2013-04-11 2014-09-27 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Рабочее колесо компрессора турбомашины
FR3006366B1 (fr) * 2013-05-28 2018-03-02 Safran Aircraft Engines Roue de turbine dans une turbomachine
WO2015080781A2 (fr) 2013-09-11 2015-06-04 General Electric Company Architecture de pli pour une plate-forme intégrée et des éléments de retenue d'amortisseur dans des pales de turbine en composite à matrice céramique
EP2881544A1 (fr) 2013-12-09 2015-06-10 Siemens Aktiengesellschaft Profilé d'aube de turbine à gaz et agencement associé
US9797270B2 (en) 2013-12-23 2017-10-24 Rolls-Royce North American Technologies Inc. Recessable damper for turbine
US10030530B2 (en) 2014-07-31 2018-07-24 United Technologies Corporation Reversible blade rotor seal
FR3025563B1 (fr) * 2014-09-04 2019-04-05 Safran Aircraft Engines Aube a plateforme et excroissance creusee
FR3025553B1 (fr) * 2014-09-08 2019-11-29 Safran Aircraft Engines Aube a becquet amont
EP3073052B1 (fr) * 2015-02-17 2018-01-24 Rolls-Royce Corporation Ensemble de soufflant
US9810075B2 (en) 2015-03-20 2017-11-07 United Technologies Corporation Faceted turbine blade damper-seal
US10385701B2 (en) 2015-09-03 2019-08-20 General Electric Company Damper pin for a turbine blade
US10443408B2 (en) 2015-09-03 2019-10-15 General Electric Company Damper pin for a turbine blade
US10472975B2 (en) 2015-09-03 2019-11-12 General Electric Company Damper pin having elongated bodies for damping adjacent turbine blades
US10584597B2 (en) 2015-09-03 2020-03-10 General Electric Company Variable cross-section damper pin for a turbine blade
US10100648B2 (en) 2015-12-07 2018-10-16 United Technologies Corporation Damper seal installation features
EP3489464B1 (fr) * 2016-07-25 2021-09-08 IHI Corporation Structure de joint d'étanchéité pour aube de rotor de turbine à gaz
US10370996B2 (en) 2016-08-23 2019-08-06 United Technologies Corporation Floating, non-contact seal with offset build clearance for load imbalance
US10385715B2 (en) 2016-08-29 2019-08-20 United Technologies Corporation Floating, non-contact seal with angled beams
US10550708B2 (en) 2016-08-31 2020-02-04 United Technologies Corporation Floating, non-contact seal with at least three beams
US10683765B2 (en) * 2017-02-14 2020-06-16 General Electric Company Turbine blades having shank features and methods of fabricating the same
EP3438410B1 (fr) 2017-08-01 2021-09-29 General Electric Company Système d'étanchéité pour machine rotative
US10890081B2 (en) * 2018-04-23 2021-01-12 Rolls-Royce Corporation Turbine disk with platforms coupled to disk
US10934874B2 (en) * 2019-02-06 2021-03-02 Pratt & Whitney Canada Corp. Assembly of blade and seal for blade pocket
US11299992B2 (en) * 2020-03-25 2022-04-12 General Electric Company Rotor blade damping structures
JP2023093088A (ja) * 2021-12-22 2023-07-04 三菱重工業株式会社 回転機械

Family Cites Families (16)

* Cited by examiner, † Cited by third party
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
US2999631A (en) * 1958-09-05 1961-09-12 Gen Electric Dual airfoil
US3295825A (en) * 1965-03-10 1967-01-03 Gen Motors Corp Multi-stage turbine rotor
US3666376A (en) * 1971-01-05 1972-05-30 United Aircraft Corp Turbine blade damper
US3709631A (en) * 1971-03-18 1973-01-09 Caterpillar Tractor Co Turbine blade seal arrangement
US3689177A (en) * 1971-04-19 1972-09-05 Gen Electric Blade constraining structure
US3728041A (en) * 1971-10-04 1973-04-17 Gen Electric Fluidic seal for segmented nozzle diaphragm
SU418618A1 (fr) * 1972-01-25 1974-03-05
GB1460714A (en) * 1973-06-26 1977-01-06 Rolls Royce Bladed rotor for a gas turbine engine
US3936222A (en) * 1974-03-28 1976-02-03 United Technologies Corporation Gas turbine construction
US4111603A (en) * 1976-05-17 1978-09-05 Westinghouse Electric Corp. Ceramic rotor blade assembly for a gas turbine engine
US4101245A (en) * 1976-12-27 1978-07-18 United Technologies Corporation Interblade damper and seal for turbomachinery rotor
GB1549152A (en) * 1977-01-11 1979-08-01 Rolls Royce Rotor stage for a gas trubine engine
US4455122A (en) * 1981-12-14 1984-06-19 United Technologies Corporation Blade to blade vibration damper
US4505642A (en) * 1983-10-24 1985-03-19 United Technologies Corporation Rotor blade interplatform seal
US4743164A (en) * 1986-12-29 1988-05-10 United Technologies Corporation Interblade seal for turbomachine rotor

Also Published As

Publication number Publication date
US4872812A (en) 1989-10-10
DE3825951A1 (de) 1989-02-16
GB8818579D0 (en) 1988-09-07
IT1226368B (it) 1991-01-11
CA1279017C (fr) 1991-01-15
GB2208529A (en) 1989-04-05
IT8821642A0 (it) 1988-08-04
FR2619158A1 (fr) 1989-02-10
DE3825951C2 (de) 1999-05-27
GB2208529B (en) 1992-03-18

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20080430