DE60142426D1 - Turbomaschinenrotor mit Schaufeln unterschiedlicher Eigenfrequenz - Google Patents

Turbomaschinenrotor mit Schaufeln unterschiedlicher Eigenfrequenz

Info

Publication number
DE60142426D1
DE60142426D1 DE60142426T DE60142426T DE60142426D1 DE 60142426 D1 DE60142426 D1 DE 60142426D1 DE 60142426 T DE60142426 T DE 60142426T DE 60142426 T DE60142426 T DE 60142426T DE 60142426 D1 DE60142426 D1 DE 60142426D1
Authority
DE
Germany
Prior art keywords
blades
natural frequency
different natural
turbomachine rotor
turbomachine
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 - Lifetime
Application number
DE60142426T
Other languages
English (en)
Inventor
Matthew Montgomery
Marc Samit
John A Orosa
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE60142426D1 publication Critical patent/DE60142426D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/668Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04Antivibration arrangements
    • F01D25/06Antivibration arrangements for preventing blade vibration
    • 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
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/10Anti- vibration means
    • 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
    • F01D5/14Form or construction
    • F01D5/16Form or construction for counteracting blade vibration
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
    • 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
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • 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
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • F05D2260/961Preventing, counteracting or reducing vibration or noise by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • 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
DE60142426T 2000-11-30 2001-11-28 Turbomaschinenrotor mit Schaufeln unterschiedlicher Eigenfrequenz Expired - Lifetime DE60142426D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/728,238 US6471482B2 (en) 2000-11-30 2000-11-30 Frequency-mistuned light-weight turbomachinery blade rows for increased flutter stability

Publications (1)

Publication Number Publication Date
DE60142426D1 true DE60142426D1 (de) 2010-08-05

Family

ID=24926000

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60142426T Expired - Lifetime DE60142426D1 (de) 2000-11-30 2001-11-28 Turbomaschinenrotor mit Schaufeln unterschiedlicher Eigenfrequenz

Country Status (4)

Country Link
US (1) US6471482B2 (de)
EP (1) EP1211382B1 (de)
JP (1) JP2002188404A (de)
DE (1) DE60142426D1 (de)

Families Citing this family (91)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6814543B2 (en) 2002-12-30 2004-11-09 General Electric Company Method and apparatus for bucket natural frequency tuning
FR2851285B1 (fr) * 2003-02-13 2007-03-16 Snecma Moteurs Realisation de turbines pour turbomachines ayant des aubes a frequences de resonance ajustees differentes et procede d'ajustement de la frequence de resonance d'une aube de turbine
GB2401683B (en) * 2003-05-16 2006-02-08 Rolls Royce Plc Method for monitoring engine order forcing frequency
FR2869069B1 (fr) * 2004-04-20 2008-11-21 Snecma Moteurs Sa Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine roue aubagee presentant un desaccordage volontaire
US7147437B2 (en) * 2004-08-09 2006-12-12 General Electric Company Mixed tuned hybrid blade related method
US20060073022A1 (en) * 2004-10-05 2006-04-06 Gentile David P Frequency tailored thickness blade for a turbomachine wheel
US20070036658A1 (en) * 2005-08-09 2007-02-15 Morris Robert J Tunable gas turbine engine fan assembly
US7497664B2 (en) * 2005-08-16 2009-03-03 General Electric Company Methods and apparatus for reducing vibrations induced to airfoils
ITMI20060340A1 (it) 2006-02-27 2007-08-28 Nuovo Pignone Spa Pala di un rotore di un secondo stadio di un compressore
ITMI20060341A1 (it) * 2006-02-27 2007-08-28 Nuovo Pignone Spa Pala di un rotore di un non stadio di un compressore
US7874794B2 (en) * 2006-03-21 2011-01-25 General Electric Company Blade row for a rotary machine and method of fabricating same
US7866949B2 (en) * 2006-08-24 2011-01-11 General Electric Company Methods and apparatus for fabricating a rotor for a steam turbine
US7753652B2 (en) 2006-12-15 2010-07-13 Siemens Energy, Inc. Aero-mixing of rotating blade structures
US20080273961A1 (en) * 2007-03-05 2008-11-06 Rosenkrans William E Flutter sensing and control system for a gas turbine engine
US8204701B2 (en) * 2007-06-15 2012-06-19 United Technologies Corporation Aeroelastic model using the principal shapes of modes (AMPS)
US8402742B2 (en) 2007-12-05 2013-03-26 United Technologies Corporation Gas turbine engine systems involving tip fans
US8590286B2 (en) * 2007-12-05 2013-11-26 United Technologies Corp. Gas turbine engine systems involving tip fans
DE102007059155A1 (de) * 2007-12-06 2009-06-10 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung von in Integralbauweise ausgebildeten Laufrädern für Verdichter und Turbinen
US20090155082A1 (en) * 2007-12-18 2009-06-18 Loc Duong Method to maximize resonance-free running range for a turbine blade
US8167540B2 (en) * 2008-01-30 2012-05-01 Hamilton Sundstrand Corporation System for reducing compressor noise
US7870929B2 (en) * 2008-04-29 2011-01-18 The Boeing Company Engine assembly, acoustical liner and associated method of fabrication
US8100641B2 (en) * 2008-09-09 2012-01-24 General Electric Company Steam turbine having stage with buckets of different materials
US8043063B2 (en) * 2009-03-26 2011-10-25 Pratt & Whitney Canada Corp. Intentionally mistuned integrally bladed rotor
FR2944049B1 (fr) * 2009-04-02 2014-06-27 Turbomeca Roue a aubes dont les pales sont desaccordees
US8172510B2 (en) * 2009-05-04 2012-05-08 Hamilton Sundstrand Corporation Radial compressor of asymmetric cyclic sector with coupled blades tuned at anti-nodes
US8172511B2 (en) * 2009-05-04 2012-05-08 Hamilton Sunstrand Corporation Radial compressor with blades decoupled and tuned at anti-nodes
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
US8573945B2 (en) * 2009-11-13 2013-11-05 Alstom Technology Ltd. Compressor stator vane
GB2483061A (en) 2010-08-23 2012-02-29 Rolls Royce Plc A method of damping aerofoil structure vibrations
EP2505780B1 (de) 2011-04-01 2016-05-11 MTU Aero Engines GmbH Schaufelanordnung für eine Turbomaschine
US8834098B2 (en) 2011-12-02 2014-09-16 United Technologies Corporation Detuned vane airfoil assembly
US9394852B2 (en) 2012-01-31 2016-07-19 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
US8375699B1 (en) * 2012-01-31 2013-02-19 United Technologies Corporation Variable area fan nozzle with wall thickness distribution
EP2653658A1 (de) * 2012-04-16 2013-10-23 Siemens Aktiengesellschaft Leitschaufelkranz für eine Axialströmungsmaschine und Verfahren zum Auslegen des Leitschaufelkranzes
ITTO20120517A1 (it) * 2012-06-14 2013-12-15 Avio Spa Schiera di profili aerodinamici per un impianto di turbina a gas
US9097125B2 (en) * 2012-08-17 2015-08-04 Mapna Group Intentionally frequency mistuned turbine blades
US10982551B1 (en) 2012-09-14 2021-04-20 Raytheon Technologies Corporation Turbomachine blade
EP3653838A1 (de) * 2012-09-25 2020-05-20 United Technologies Corporation Schaufelreihe mit schaufeln unterschiedlicher geometrie und merkmalen zum fehlerfreien einbau
ES2546992T3 (es) 2012-10-24 2015-09-30 MTU Aero Engines AG Método para desintonizar los álabes de un motor de turbina de gas
WO2014105533A1 (en) 2012-12-28 2014-07-03 United Technologies Corporation Shrouded turbine blade with cut corner
EP2762678A1 (de) * 2013-02-05 2014-08-06 Siemens Aktiengesellschaft Verfahren zum Verstimmen eines Laufschaufelgitters
EP2959108B1 (de) 2013-02-21 2021-04-21 Raytheon Technologies Corporation Gasturbinenmotor mit verstimmter stufe
US10808543B2 (en) 2013-04-16 2020-10-20 Raytheon Technologies Corporation Rotors with modulus mistuned airfoils
EP2860347B1 (de) 2013-10-08 2017-04-12 MTU Aero Engines GmbH Gasturbinen-Verdichter-Schaufelgitter
WO2015057544A1 (en) 2013-10-16 2015-04-23 United Technologies Corporation Auxiliary power unit impeller blade
WO2015112305A1 (en) 2014-01-24 2015-07-30 United Technologies Corporation Gas turbine engine stator vane mistuning
EP2942481B1 (de) 2014-05-07 2019-03-27 Rolls-Royce Corporation Rotor für einen gasturbinenmotor
US10443391B2 (en) 2014-05-23 2019-10-15 United Technologies Corporation Gas turbine engine stator vane asymmetry
DE102014214271A1 (de) * 2014-07-22 2016-01-28 MTU Aero Engines AG Turbomaschinenschaufel
US9879539B2 (en) 2014-11-18 2018-01-30 Honeywell International Inc. Engine airfoils and methods for reducing airfoil flutter
US20160160874A1 (en) * 2014-12-04 2016-06-09 Solar Turbines Incorporated Airfoil for inlet guide vane (igv) of multistage compressor
FR3038341B1 (fr) * 2015-07-03 2017-07-28 Snecma Procede d'alteration de la loi de vrillage de la surface aerodynamique d'une pale de soufflante de moteur a turbine a gaz
FR3043131B1 (fr) * 2015-10-28 2017-11-03 Snecma Procede pour introduire un desaccordage volontaire dans une roue aubagee de turbomachine
EP3176369B1 (de) 2015-12-04 2019-05-29 MTU Aero Engines GmbH Gasturbinen-verdichter
US10823192B2 (en) 2015-12-18 2020-11-03 Raytheon Technologies Corporation Gas turbine engine with short inlet and mistuned fan blades
US10215194B2 (en) * 2015-12-21 2019-02-26 Pratt & Whitney Canada Corp. Mistuned fan
US10670041B2 (en) 2016-02-19 2020-06-02 Pratt & Whitney Canada Corp. Compressor rotor for supersonic flutter and/or resonant stress mitigation
US10294965B2 (en) 2016-05-25 2019-05-21 Honeywell International Inc. Compression system for a turbine engine
US10641281B2 (en) 2016-08-08 2020-05-05 United Technologies Corporation Mistuned laminate airfoil
US20180080450A1 (en) * 2016-09-19 2018-03-22 Rolls-Royce Corporation Flutter avoidance through control of texture and modulus of elasticity in adjacent fan blades
US10533581B2 (en) 2016-12-09 2020-01-14 United Technologies Corporation Stator with support structure feature for tuned airfoil
US11261737B1 (en) 2017-01-17 2022-03-01 Raytheon Technologies Corporation Turbomachine blade
US10677266B1 (en) * 2017-01-17 2020-06-09 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
US10774651B1 (en) * 2017-01-17 2020-09-15 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
US10808544B1 (en) * 2017-01-17 2020-10-20 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
US11199096B1 (en) 2017-01-17 2021-12-14 Raytheon Technologies Corporation Turbomachine blade
US10844727B1 (en) * 2017-01-17 2020-11-24 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
US10801330B1 (en) * 2017-01-17 2020-10-13 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
US10683761B1 (en) * 2017-01-17 2020-06-16 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
US10865809B1 (en) * 2017-01-17 2020-12-15 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
GB201702698D0 (en) 2017-02-20 2017-04-05 Rolls Royce Plc Fan
US10480535B2 (en) 2017-03-22 2019-11-19 Pratt & Whitney Canada Corp. Fan rotor with flow induced resonance control
US10458436B2 (en) 2017-03-22 2019-10-29 Pratt & Whitney Canada Corp. Fan rotor with flow induced resonance control
US10823203B2 (en) 2017-03-22 2020-11-03 Pratt & Whitney Canada Corp. Fan rotor with flow induced resonance control
US10480527B2 (en) 2017-05-05 2019-11-19 Robert Bosch Gmbh Axial fan with unbalanced blade spacing
US10954804B2 (en) * 2017-07-05 2021-03-23 Raytheon Technologies Corporation Rotary machines including a hybrid rotor with hollow and solid rotor blade sets
US10876417B2 (en) 2017-08-17 2020-12-29 Raytheon Technologies Corporation Tuned airfoil assembly
US11002293B2 (en) 2017-09-15 2021-05-11 Pratt & Whitney Canada Corp. Mistuned compressor rotor with hub scoops
US10865806B2 (en) 2017-09-15 2020-12-15 Pratt & Whitney Canada Corp. Mistuned rotor for gas turbine engine
US10443411B2 (en) 2017-09-18 2019-10-15 Pratt & Whitney Canada Corp. Compressor rotor with coated blades
US10837459B2 (en) * 2017-10-06 2020-11-17 Pratt & Whitney Canada Corp. Mistuned fan for gas turbine engine
GB201808651D0 (en) 2018-05-25 2018-07-11 Rolls Royce Plc Rotor blade arrangement
GB201808646D0 (en) 2018-05-25 2018-07-11 Rolls Royce Plc Rotor Blade Arrangement
GB201808650D0 (en) 2018-05-25 2018-07-11 Rolls Royce Plc Rotor Blade Arrangement
US10876409B2 (en) * 2018-11-07 2020-12-29 Honeywell International Inc. Mistuned rotors and methods for manufacture
FR3089553B1 (fr) * 2018-12-11 2021-01-22 Safran Aircraft Engines Aube de turbomachine a loi de fleche a forte marge au flottement
CN110529402A (zh) * 2019-08-14 2019-12-03 湖南伟玛集团有限公司 一种中速多级离心风机
US20230349297A1 (en) * 2022-04-29 2023-11-02 Pratt & Whitney Canada Corp. Method of manufacturing a mistuned rotor
US11959395B2 (en) * 2022-05-03 2024-04-16 General Electric Company Rotor blade system of turbine engines

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1177277B (de) * 1954-02-06 1964-09-03 Bbc Brown Boveri & Cie Axial- oder Radialgeblaese, insbesondere fuer elektrische Generatoren und Motoren
DE1503520A1 (de) * 1965-09-22 1970-02-26 Daimler Benz Ag Schaufelrad von Axial- oder Radialverdichtern
SU411214A1 (de) * 1968-05-12 1974-01-15
GB1293553A (en) * 1969-02-18 1972-10-18 Cav Ltd Radial flow fans
US4097192A (en) * 1977-01-06 1978-06-27 Curtiss-Wright Corporation Turbine rotor and blade configuration
JPS5644495A (en) * 1979-09-20 1981-04-23 Nissan Motor Co Ltd Impeller for centrifugal compressor
US4332525A (en) * 1979-12-03 1982-06-01 United Technologies Corporation Matched stiffness rotor flexbeam and blade system
US4878810A (en) * 1988-05-20 1989-11-07 Westinghouse Electric Corp. Turbine blades having alternating resonant frequencies
US4919593A (en) * 1988-08-30 1990-04-24 Westinghouse Electric Corp. Retrofitted rotor blades for steam turbines and method of making the same
US5299914A (en) * 1991-09-11 1994-04-05 General Electric Company Staggered fan blade assembly for a turbofan engine
US5286168A (en) 1992-01-31 1994-02-15 Westinghouse Electric Corp. Freestanding mixed tuned blade
DE4324960A1 (de) * 1993-07-24 1995-01-26 Mtu Muenchen Gmbh Laufrad einer Turbomaschine, insbesondere einer Turbine eines Gasturbinentriebwerks
US5524341A (en) * 1994-09-26 1996-06-11 Westinghouse Electric Corporation Method of making a row of mix-tuned turbomachine blades
US5667361A (en) 1995-09-14 1997-09-16 United Technologies Corporation Flutter resistant blades, vanes and arrays thereof for a turbomachine
US5988982A (en) * 1997-09-09 1999-11-23 Lsp Technologies, Inc. Altering vibration frequencies of workpieces, such as gas turbine engine blades
US6042338A (en) * 1998-04-08 2000-03-28 Alliedsignal Inc. Detuned fan blade apparatus and method
US6195982B1 (en) * 1998-12-30 2001-03-06 United Technologies Corporation Apparatus and method of active flutter control
US6379112B1 (en) * 2000-11-04 2002-04-30 United Technologies Corporation Quadrant rotor mistuning for decreasing vibration

Also Published As

Publication number Publication date
EP1211382A2 (de) 2002-06-05
US6471482B2 (en) 2002-10-29
EP1211382A3 (de) 2004-01-02
JP2002188404A (ja) 2002-07-05
EP1211382B1 (de) 2010-06-23
US20020064458A1 (en) 2002-05-30

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