ATE337471T1 - Nachgiebiges zwischenstück für eine fanschaufel - Google Patents

Nachgiebiges zwischenstück für eine fanschaufel

Info

Publication number
ATE337471T1
ATE337471T1 AT01977744T AT01977744T ATE337471T1 AT E337471 T1 ATE337471 T1 AT E337471T1 AT 01977744 T AT01977744 T AT 01977744T AT 01977744 T AT01977744 T AT 01977744T AT E337471 T1 ATE337471 T1 AT E337471T1
Authority
AT
Austria
Prior art keywords
fan blade
shim
intermediate piece
flexible intermediate
compliant
Prior art date
Application number
AT01977744T
Other languages
English (en)
Inventor
Michael Kolodziej
Bruce D Wilson
Original Assignee
Honeywell Int Inc
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 Honeywell Int Inc filed Critical Honeywell Int Inc
Application granted granted Critical
Publication of ATE337471T1 publication Critical patent/ATE337471T1/de

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
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • F01D5/3092Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/04Heavy metals
    • F05C2201/0433Iron group; Ferrous alloys, e.g. steel
    • F05C2201/0463Cobalt
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/90Coating; Surface treatment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/70Shape
    • F05D2250/71Shape curved
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/611Coating

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Filters For Electric Vacuum Cleaners (AREA)
AT01977744T 2000-10-17 2001-10-15 Nachgiebiges zwischenstück für eine fanschaufel ATE337471T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/690,216 US6431835B1 (en) 2000-10-17 2000-10-17 Fan blade compliant shim

Publications (1)

Publication Number Publication Date
ATE337471T1 true ATE337471T1 (de) 2006-09-15

Family

ID=24771589

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01977744T ATE337471T1 (de) 2000-10-17 2001-10-15 Nachgiebiges zwischenstück für eine fanschaufel

Country Status (7)

Country Link
US (2) US6431835B1 (de)
EP (1) EP1327056B1 (de)
AT (1) ATE337471T1 (de)
CA (1) CA2426135C (de)
DE (1) DE60122550T2 (de)
TW (1) TW567276B (de)
WO (1) WO2002033224A1 (de)

Families Citing this family (87)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20020005034A (ko) * 1999-05-14 2002-01-16 칼 하인쯔 호르닝어 회전자용 밀봉 시스템을 갖는 터보 머신
FR2831207B1 (fr) * 2001-10-24 2004-06-04 Snecma Moteurs Plates-formes pour aubes d'un ensemble rotatif
US6733234B2 (en) 2002-09-13 2004-05-11 Siemens Westinghouse Power Corporation Biased wear resistant turbine seal assembly
US6883807B2 (en) 2002-09-13 2005-04-26 Seimens Westinghouse Power Corporation Multidirectional turbine shim seal
US6773234B2 (en) * 2002-10-18 2004-08-10 General Electric Company Methods and apparatus for facilitating preventing failure of gas turbine engine blades
US6860722B2 (en) * 2003-01-31 2005-03-01 General Electric Company Snap on blade shim
GB2408295A (en) * 2003-11-14 2005-05-25 Rolls Royce Plc An assembly with a plastic insert between two metal components
EP1557534A1 (de) * 2004-01-20 2005-07-27 Siemens Aktiengesellschaft Turbinenschaufel und Gasturbine mit einer solchen Turbinenschaufel
GB0427083D0 (en) * 2004-12-10 2005-01-12 Rolls Royce Plc Platform mounted components
US7329101B2 (en) * 2004-12-29 2008-02-12 General Electric Company Ceramic composite with integrated compliance/wear layer
WO2006080055A1 (ja) * 2005-01-26 2006-08-03 Ishikawajima-Harima Heavy Industries Co., Ltd. ターボファンエンジン
GB2426301B (en) 2005-05-19 2007-07-18 Rolls Royce Plc A seal arrangement
FR2890684B1 (fr) * 2005-09-15 2007-12-07 Snecma Clinquant pour aube de turboreacteur
JP4528721B2 (ja) * 2005-12-28 2010-08-18 株式会社東芝 発電機ロータのき裂進展予測システムと運転条件決定支援システム、方法およびプログラム、並びに運転制御システム
US7721526B2 (en) * 2006-06-28 2010-05-25 Ishikawajima-Harima Heavy Industries Co., Ltd. Turbofan engine
JP4911344B2 (ja) * 2006-07-04 2012-04-04 株式会社Ihi ターボファンエンジン
US7806655B2 (en) * 2007-02-27 2010-10-05 General Electric Company Method and apparatus for assembling blade shims
US20080273982A1 (en) * 2007-03-12 2008-11-06 Honeywell International, Inc. Blade attachment retention device
FR2913735B1 (fr) * 2007-03-16 2013-04-19 Snecma Disque de rotor d'une turbomachine
US8568101B2 (en) * 2007-03-27 2013-10-29 Ihi Corporation Fan rotor blade support structure and turbofan engine having the same
US8016565B2 (en) * 2007-05-31 2011-09-13 General Electric Company Methods and apparatus for assembling gas turbine engines
FR2918703B1 (fr) * 2007-07-13 2009-10-16 Snecma Sa Ensemble de rotor de turbomachine
FR2918702B1 (fr) * 2007-07-13 2009-10-16 Snecma Sa Clinquant pour aube de turbomachine
US7878764B2 (en) 2007-07-23 2011-02-01 Caterpillar Inc. Adjustable fan and method
GB2452515B (en) * 2007-09-06 2009-08-05 Siemens Ag Seal coating between rotor blade and rotor disk slot in gas turbine engine
FR2921409B1 (fr) * 2007-09-25 2009-12-18 Snecma Clinquant pour aube de turbomachine.
US8210819B2 (en) * 2008-02-22 2012-07-03 Siemens Energy, Inc. Airfoil structure shim
FR2934873B1 (fr) * 2008-08-06 2011-07-08 Snecma Dispositif amortisseur de vibrations pour attaches d'aubes.
GB2462810B (en) * 2008-08-18 2010-07-21 Rolls Royce Plc Sealing means
US8075280B2 (en) * 2008-09-08 2011-12-13 Siemens Energy, Inc. Composite blade and method of manufacture
US20100077612A1 (en) * 2008-09-30 2010-04-01 Courtney James Tudor Method of manufacturing a fairing with an integrated seal
FR2938872B1 (fr) * 2008-11-26 2015-11-27 Snecma Dispositif anti-usure pour aubes d'un distributeur de turbine d'une turbomachine aeronautique
FR2945074B1 (fr) * 2009-04-29 2011-06-03 Snecma Cale d'aube de soufflante renforcee
US8734089B2 (en) 2009-12-29 2014-05-27 Rolls-Royce Corporation Damper seal and vane assembly for a gas turbine engine
FR2959527B1 (fr) * 2010-04-28 2012-07-20 Snecma Piece anti-usure pour echasse d'aube de soufflante de turboreacteur
US8616850B2 (en) 2010-06-11 2013-12-31 United Technologies Corporation Gas turbine engine blade mounting arrangement
FR2963383B1 (fr) * 2010-07-27 2016-09-09 Snecma Aube de turbomachine, rotor, turbine basse pression et turbomachine equipes d'une telle aube
US8672634B2 (en) * 2010-08-30 2014-03-18 United Technologies Corporation Electroformed conforming rubstrip
GB2477825B (en) * 2010-09-23 2015-04-01 Rolls Royce Plc Anti fret liner assembly
JP5416072B2 (ja) * 2010-10-26 2014-02-12 株式会社日立産機システム スクリュー圧縮機
US8985960B2 (en) * 2011-03-30 2015-03-24 General Electric Company Method and system for sealing a dovetail
GB201106050D0 (en) * 2011-04-11 2011-05-25 Rolls Royce Plc A retention device for a composite blade of a gas turbine engine
GB201106276D0 (en) * 2011-04-14 2011-05-25 Rolls Royce Plc Annulus filler system
GB201106278D0 (en) 2011-04-14 2011-05-25 Rolls Royce Plc Annulus filler system
GB201119655D0 (en) 2011-11-15 2011-12-28 Rolls Royce Plc Annulus filler
US9840917B2 (en) 2011-12-13 2017-12-12 United Technologies Corporation Stator vane shroud having an offset
US9085989B2 (en) 2011-12-23 2015-07-21 General Electric Company Airfoils including compliant tip
US8899914B2 (en) 2012-01-05 2014-12-02 United Technologies Corporation Stator vane integrated attachment liner and spring damper
US8920112B2 (en) 2012-01-05 2014-12-30 United Technologies Corporation Stator vane spring damper
US9810077B2 (en) * 2012-01-31 2017-11-07 United Technologies Corporation Fan blade attachment of gas turbine engine
US9611746B2 (en) * 2012-03-26 2017-04-04 United Technologies Corporation Blade wedge attachment
FR2994216B1 (fr) * 2012-08-02 2014-09-05 Snecma Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaire
US9410439B2 (en) 2012-09-14 2016-08-09 United Technologies Corporation CMC blade attachment shim relief
US9500083B2 (en) * 2012-11-26 2016-11-22 U.S. Department Of Energy Apparatus and method to reduce wear and friction between CMC-to-metal attachment and interface
US20140169979A1 (en) * 2012-12-14 2014-06-19 United Technologies Corporation Gas turbine engine fan blade platform seal
CN103985407A (zh) 2013-02-07 2014-08-13 辉达公司 采用分段式页面配置的dram
WO2014143318A1 (en) 2013-03-13 2014-09-18 United Technologies Corporation Blade wear pads and manufacture methods
WO2014163709A2 (en) 2013-03-13 2014-10-09 Uskert Richard C Platform for ceramic matrix composite turbine blades
EP2971551B1 (de) * 2013-03-14 2019-06-12 United Technologies Corporation Lüfter mit niedriger geschwindigkeit für gasturbinenmotoren
US9958113B2 (en) * 2013-03-15 2018-05-01 United Technologies Corporation Fan blade lubrication
US9470098B2 (en) * 2013-03-15 2016-10-18 General Electric Company Axial compressor and method for controlling stage-to-stage leakage therein
CA2913055A1 (en) 2013-05-29 2015-02-19 General Electric Company Composite airfoil metal patch
US20160281515A1 (en) * 2013-11-18 2016-09-29 United Technologies Corporation Method of attaching a ceramic matrix composite article
EP3094825A1 (de) 2014-01-16 2016-11-23 General Electric Company Belastungsreduzierende unterlegscheibe für verbundschaufelfuss
US20160024946A1 (en) * 2014-07-22 2016-01-28 United Technologies Corporation Rotor blade dovetail with round bearing surfaces
FR3027071B1 (fr) * 2014-10-13 2019-08-23 Safran Aircraft Engines Procede d'intervention sur un rotor et clinquant associe
US10087948B2 (en) * 2015-03-30 2018-10-02 United Technologies Corporation Fan blade and method of covering a fan blade root portion
US10036503B2 (en) 2015-04-13 2018-07-31 United Technologies Corporation Shim to maintain gap during engine assembly
US10099323B2 (en) 2015-10-19 2018-10-16 Rolls-Royce Corporation Rotating structure and a method of producing the rotating structure
DE102017207445A1 (de) 2017-05-03 2018-11-08 MTU Aero Engines AG Verschleißschutzblech für eine Laufschaufel einer Gasturbine
US10907491B2 (en) 2017-11-30 2021-02-02 General Electric Company Sealing system for a rotary machine and method of assembling same
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
JP7269029B2 (ja) * 2019-02-27 2023-05-08 三菱重工業株式会社 動翼及び回転機械
US11242761B2 (en) 2020-02-18 2022-02-08 Raytheon Technologies Corporation Tangential rotor blade slot spacer for a gas turbine engine
FR3107922B1 (fr) * 2020-03-03 2023-06-16 Safran Aircraft Engines Clinquant pour aube mobile de turbomachine
US11486261B2 (en) 2020-03-31 2022-11-01 General Electric Company Turbine circumferential dovetail leakage reduction
CN113833691A (zh) * 2020-06-08 2021-12-24 中国航发商用航空发动机有限责任公司 一种风扇组件及涡轮风扇发动机
FR3113421B1 (fr) * 2020-08-11 2022-11-04 Safran Aircraft Engines Clinquant pour aube de rotor
FR3114347B1 (fr) * 2020-09-24 2022-08-12 Safran Aircraft Engines Aube de soufflante comprenant un système anti-pivotement amélioré
US11591919B2 (en) * 2020-12-16 2023-02-28 Integran Technologies Inc. Gas turbine blade and rotor wear-protection system
GB2607886A (en) * 2021-06-11 2022-12-21 Siemens Energy Global Gmbh & Co Kg Rotor assembly and method of assembling a rotor assembly for a gas turbine engine
FR3124218A1 (fr) * 2021-06-21 2022-12-23 Safran Aircraft Engines Clinquant a languette longue pour pied d’aube de rotor de turbomachine
FR3127986A1 (fr) * 2021-10-11 2023-04-14 Safran Aircraft Engines Aube de turbine avec un pied comprenant un bloquage du clinquant
US20230175416A1 (en) * 2021-12-03 2023-06-08 General Electric Company Apparatuses for deicing fan blades and methods of forming the same

Family Cites Families (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2686656A (en) 1950-04-04 1954-08-17 United Aircraft Corp Blade locking device
DE1251338B (de) 1962-12-14 1967-10-05 Aktiengesellschaft Brown, Boveri &. Cie , Baden (Schweiz) Verfahren zum Befestigen von Schaufeln in Turbmenlaufern
GB996729A (en) 1963-12-16 1965-06-30 Rolls Royce Improvements relating to turbines and compressors
IL36770A (en) 1970-09-25 1973-07-30 Gen Electric Turbomachinery blade wear insert
US4019832A (en) 1976-02-27 1977-04-26 General Electric Company Platform for a turbomachinery blade
US4169694A (en) 1977-07-20 1979-10-02 Electric Power Research Institute, Inc. Ceramic rotor blade having root with double curvature
US4183720A (en) 1978-01-03 1980-01-15 The United States Of America As Represented By The Secretary Of The Air Force Composite fan blade platform double wedge centrifugal seal
US4326835A (en) 1979-10-29 1982-04-27 General Motors Corporation Blade platform seal for ceramic/metal rotor assembly
US4417854A (en) 1980-03-21 1983-11-29 Rockwell International Corporation Compliant interface for ceramic turbine blades
FR2503247B1 (fr) 1981-04-07 1985-06-14 Snecma Perfectionnements aux etages de turbine a gaz de turboreacteurs munis de moyens de refroidissement par air du disque de la roue de la turbine
US4422827A (en) 1982-02-18 1983-12-27 United Technologies Corporation Blade root seal
US4875830A (en) 1985-07-18 1989-10-24 United Technologies Corporation Flanged ladder seal
US4820126A (en) 1988-02-22 1989-04-11 Westinghouse Electric Corp. Turbomachine rotor assembly having reduced stress concentrations
DE3815977A1 (de) 1988-05-10 1989-11-30 Mtu Muenchen Gmbh Folienzwischenlage zur fuegung von reibkorrosionsgefaehrdeten maschinenbauteilen
US5087174A (en) 1990-01-22 1992-02-11 Westinghouse Electric Corp. Temperature activated expanding mineral shim
US5137420A (en) * 1990-09-14 1992-08-11 United Technologies Corporation Compressible blade root sealant
US5139389A (en) * 1990-09-14 1992-08-18 United Technologies Corporation Expandable blade root sealant
US5160243A (en) 1991-01-15 1992-11-03 General Electric Company Turbine blade wear protection system with multilayer shim
US5312696A (en) 1991-09-16 1994-05-17 United Technologies Corporation Method for reducing fretting wear between contacting surfaces
US5240375A (en) 1992-01-10 1993-08-31 General Electric Company Wear protection system for turbine engine rotor and blade
US5281097A (en) 1992-11-20 1994-01-25 General Electric Company Thermal control damper for turbine rotors
US5368444A (en) 1993-08-30 1994-11-29 General Electric Company Anti-fretting blade retention means
AU7771394A (en) 1993-12-03 1995-06-08 Westinghouse Electric Corporation Gas turbine blade alloy
US5558500A (en) 1994-06-07 1996-09-24 Alliedsignal Inc. Elastomeric seal for axial dovetail rotor blades
GB2293628B (en) 1994-09-27 1998-04-01 Europ Gas Turbines Ltd Turbines
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
FR2739136B1 (fr) 1995-09-21 1997-10-31 Snecma Agencement amortissant pour des aubes de rotor
GB9602129D0 (en) 1996-02-02 1996-04-03 Rolls Royce Plc Rotors for gas turbine engines
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
US5820338A (en) * 1997-04-24 1998-10-13 United Technologies Corporation Fan blade interplatform seal
US5836744A (en) 1997-04-24 1998-11-17 United Technologies Corporation Frangible fan blade
US6132175A (en) * 1997-05-29 2000-10-17 Alliedsignal, Inc. Compliant sleeve for ceramic turbine blades
US6202273B1 (en) * 1999-07-30 2001-03-20 General Electric Company Shim removing tool
EP1295252B1 (de) 2000-06-30 2006-12-27 BRITISH TELECOMMUNICATIONS public limited company Anordnung zur generierung von elementensequenzen

Also Published As

Publication number Publication date
EP1327056A1 (de) 2003-07-16
TW567276B (en) 2003-12-21
DE60122550D1 (de) 2006-10-05
US6431835B1 (en) 2002-08-13
WO2002033224A1 (en) 2002-04-25
CA2426135A1 (en) 2002-04-25
US6398499B1 (en) 2002-06-04
US20020044870A1 (en) 2002-04-18
CA2426135C (en) 2008-01-08
EP1327056B1 (de) 2006-08-23
DE60122550T2 (de) 2007-09-20

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