FR2869069A1 - Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine roue aubagee presentant un desaccordage volontaire - Google Patents

Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine roue aubagee presentant un desaccordage volontaire

Info

Publication number
FR2869069A1
FR2869069A1 FR0404130A FR0404130A FR2869069A1 FR 2869069 A1 FR2869069 A1 FR 2869069A1 FR 0404130 A FR0404130 A FR 0404130A FR 0404130 A FR0404130 A FR 0404130A FR 2869069 A1 FR2869069 A1 FR 2869069A1
Authority
FR
France
Prior art keywords
wheel
voluntary
turbomachine
introducing
aubed
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.)
Granted
Application number
FR0404130A
Other languages
English (en)
Other versions
FR2869069B1 (fr
Inventor
Jerome Dupeux
Christian Dupont
Jean Pierre Francois Lombard
Eric Pierre Seinturier
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 Moteurs SA
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 Moteurs SA filed Critical SNECMA Moteurs SA
Priority to FR0404130A priority Critical patent/FR2869069B1/fr
Priority to CA2503659A priority patent/CA2503659C/fr
Priority to US11/107,877 priority patent/US7500299B2/en
Priority to RU2005111685/06A priority patent/RU2372492C2/ru
Priority to DE602005023373T priority patent/DE602005023373D1/de
Priority to EP05103148A priority patent/EP1589191B1/fr
Priority to ES05103148T priority patent/ES2351507T3/es
Publication of FR2869069A1 publication Critical patent/FR2869069A1/fr
Application granted granted Critical
Publication of FR2869069B1 publication Critical patent/FR2869069B1/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
    • F01D5/02—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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04—Antivibration arrangements
    • 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
    • F01D5/14—Form or construction
    • F01D5/16—Form or construction for counteracting blade vibration
    • 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
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49318—Repairing or disassembling
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49764—Method of mechanical manufacture with testing or indicating
    • Y10T29/49771—Quantitative measuring or gauging
    • Y10T29/49774—Quantitative measuring or gauging by vibratory or oscillatory movement

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)

Abstract

Procédé pour introduire un désaccordage volontaire dans une roue aubagée d'une turbomachine déterminée de manière à réduire les niveaux vibratoires de la roue en réponse forcée, caractérisé par le fait qu'il consiste à déterminer, en fonction des conditions de fonctionnement de la roue à l'intérieur de la turbomachine, une valeur optimale d'écart type de désaccordage par rapport à la réponse maximale en amplitude de vibration voulue sur la roue, disposer sur ladite roue, au moins en partie, des aubes de fréquences propres différentes de telle sorte que la répartition des fréquences de l'ensemble des aubes présente un écart type au moins égal à la dite valeur de désaccordage.
FR0404130A 2004-04-20 2004-04-20 Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine roue aubagee presentant un desaccordage volontaire Expired - Fee Related FR2869069B1 (fr)

Priority Applications (7)

Application Number Priority Date Filing Date Title
FR0404130A FR2869069B1 (fr) 2004-04-20 2004-04-20 Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine roue aubagee presentant un desaccordage volontaire
US11/107,877 US7500299B2 (en) 2004-04-20 2005-04-18 Method for introducing a deliberate mismatch on a turbomachine bladed wheel and bladed wheel with a deliberate mismatch
CA2503659A CA2503659C (fr) 2004-04-20 2005-04-18 Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine. roue aubagee presentant un desaccordage volontaire
DE602005023373T DE602005023373D1 (de) 2004-04-20 2005-04-19 Verfahren zum Einstellen gezielter unterschiedlicher Eigenfrequenzen eines beschaufelten Rotors einer Turbomachine sowie Rotor
RU2005111685/06A RU2372492C2 (ru) 2004-04-20 2005-04-19 Способ установки заданного рассогласования на лопастном колесе турбомашины и лопастное колесо турбомашины с заданным рассогласованием (варианты)
EP05103148A EP1589191B1 (fr) 2004-04-20 2005-04-19 Procédé pour introduire un désaccordage volontaire sur une roue aubagée de turbomachine. Roue aubagée présentant un désaccordage volontaire
ES05103148T ES2351507T3 (es) 2004-04-20 2005-04-19 Procedimiento para introducir una desintonización voluntaria en una rueda alabeada de turbomáquina, rueda alabeada que presenta una desintonización voluntaria.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0404130A FR2869069B1 (fr) 2004-04-20 2004-04-20 Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine roue aubagee presentant un desaccordage volontaire

Publications (2)

Publication Number Publication Date
FR2869069A1 true FR2869069A1 (fr) 2005-10-21
FR2869069B1 FR2869069B1 (fr) 2008-11-21

Family

ID=34939389

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0404130A Expired - Fee Related FR2869069B1 (fr) 2004-04-20 2004-04-20 Procede pour introduire un desaccordage volontaire sur une roue aubagee de turbomachine roue aubagee presentant un desaccordage volontaire

Country Status (7)

Country Link
US (1) US7500299B2 (fr)
EP (1) EP1589191B1 (fr)
CA (1) CA2503659C (fr)
DE (1) DE602005023373D1 (fr)
ES (1) ES2351507T3 (fr)
FR (1) FR2869069B1 (fr)
RU (1) RU2372492C2 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2112326A1 (fr) 2008-04-23 2009-10-28 Snecma Carter de turbomachine comportant un dispositif empêchant une instabilité lors d'un contact entre le carter et le rotor
WO2017072469A1 (fr) 2015-10-28 2017-05-04 Safran Aircraft Engines Procede pour introduire un desaccordage volontaire dans une roue aubagee de turbomachine
WO2017216480A1 (fr) 2016-06-16 2017-12-21 Safran Aircraft Engines Roue aubagee volontairement desaccordee

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GB0601837D0 (en) 2006-01-31 2006-03-08 Rolls Royce Plc An aerofoil assembly and a method of manufacturing an aerofoil assembly
FR2913074B1 (fr) * 2007-02-27 2009-05-22 Snecma Sa Methode de reduction des niveaux vibratoires d'une roue aubagee de turbomachine.
DE102007016369A1 (de) * 2007-04-03 2008-10-09 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Ermittlung der Schaufelverstimmung bei Laufrädern in Integralbauweise
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
US8167540B2 (en) * 2008-01-30 2012-05-01 Hamilton Sundstrand Corporation System for reducing compressor noise
FR2935350B1 (fr) * 2008-08-27 2011-05-20 Snecma Methode de reduction des niveaux vibratoires d'une helice de turbomoteur.
WO2010022739A2 (fr) * 2008-08-29 2010-03-04 Vestas Wind Systems A/S Générateur d’éolienne comprenant un rotor ayant des propriétés d’absorption de vibrations
US8043063B2 (en) * 2009-03-26 2011-10-25 Pratt & Whitney Canada Corp. Intentionally mistuned integrally bladed rotor
FR2944050B1 (fr) * 2009-04-02 2014-07-11 Turbomeca Roue de turbine a pales desaccordees comportant un dispositif d'amortissement
US8172511B2 (en) * 2009-05-04 2012-05-08 Hamilton Sunstrand Corporation Radial compressor with blades decoupled and tuned at anti-nodes
US8172510B2 (en) * 2009-05-04 2012-05-08 Hamilton Sundstrand Corporation Radial compressor of asymmetric cyclic sector with coupled blades tuned at anti-nodes
US8419370B2 (en) 2009-06-25 2013-04-16 Rolls-Royce Corporation Retaining and sealing ring assembly
DE102009033618A1 (de) * 2009-07-17 2011-01-20 Mtu Aero Engines Gmbh Verfahren zur Frequenzverstimmung eines Rotorkörpers einer Gasturbine und ein Rotor einer Gasturbine
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
DE102009053247A1 (de) * 2009-11-13 2011-05-19 Mtu Aero Engines Gmbh Verfahren zum Verändern einer Eigenfrequenz einer Schaufel für eine Strömungsmaschine
US20110274537A1 (en) * 2010-05-09 2011-11-10 Loc Quang Duong Blade excitation reduction method and arrangement
DE102011076790B4 (de) * 2011-05-31 2023-07-13 Zf Friedrichshafen Ag Antriebssystem für ein Fahrzeug
US8834098B2 (en) 2011-12-02 2014-09-16 United Technologies Corporation Detuned vane airfoil assembly
US9097125B2 (en) 2012-08-17 2015-08-04 Mapna Group Intentionally frequency mistuned turbine blades
EP2762678A1 (fr) * 2013-02-05 2014-08-06 Siemens Aktiengesellschaft Procédé de désaccordage d'une matrice d'aube directrice
EP2986822B8 (fr) * 2013-04-16 2021-04-07 Raytheon Technologies Corporation Rotors à aubes désaccordées par modification du module de young
WO2015057544A1 (fr) 2013-10-16 2015-04-23 United Technologies Corporation Aube de roue de groupe auxiliaire de puissance
US10400606B2 (en) 2014-01-15 2019-09-03 United Technologies Corporation Mistuned airfoil assemblies
EP2942481B1 (fr) 2014-05-07 2019-03-27 Rolls-Royce Corporation Rotor pour un moteur à turbine à gaz
EP3073052B1 (fr) 2015-02-17 2018-01-24 Rolls-Royce Corporation Ensemble de soufflant
US11041388B2 (en) 2015-03-30 2021-06-22 Pratt & Whitney Canada Corp. Blade cutback distribution in rotor for noise reduction
EP3176369B1 (fr) * 2015-12-04 2019-05-29 MTU Aero Engines GmbH Compresseur de turbines a gaz
US10837287B2 (en) * 2017-01-20 2020-11-17 Pratt & Whitney Canada Corp. Mistuned bladed rotor and associated manufacturing method
GB201702698D0 (en) * 2017-02-20 2017-04-05 Rolls Royce Plc Fan
US11255345B2 (en) 2017-03-03 2022-02-22 Elliott Company Method and arrangement to minimize noise and excitation of structures due to cavity acoustic modes
JP2019108822A (ja) * 2017-12-15 2019-07-04 三菱日立パワーシステムズ株式会社 回転機械
CN108254144A (zh) * 2017-12-25 2018-07-06 中国航发四川燃气涡轮研究院 一种用于高周疲劳极限测量的分体式叶片降频结构
GB201808651D0 (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
GB201808646D0 (en) 2018-05-25 2018-07-11 Rolls Royce Plc Rotor Blade Arrangement
US11220913B2 (en) 2019-10-23 2022-01-11 Rolls-Royce Corporation Gas turbine engine blades with airfoil plugs for selected tuning
FR3119642B1 (fr) * 2021-02-10 2024-03-01 Safran Aircraft Engines Rotor de turbomachine présentant un comportement vibratoire amélioré

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WO1998036966A1 (fr) * 1997-02-21 1998-08-27 California Institute Of Technology Rotors a pales desaccordees
EP1211382A2 (fr) * 2000-11-30 2002-06-05 United Technologies Corporation Rotor de turbomachine avec des aubes à fréquence propre différente

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US4097192A (en) * 1977-01-06 1978-06-27 Curtiss-Wright Corporation Turbine rotor and blade configuration
US6428278B1 (en) * 2000-12-04 2002-08-06 United Technologies Corporation Mistuned rotor blade array for passive flutter control
US6854959B2 (en) * 2003-04-16 2005-02-15 General Electric Company Mixed tuned hybrid bucket and related method
US7082371B2 (en) * 2003-05-29 2006-07-25 Carnegie Mellon University Fundamental mistuning model for determining system properties and predicting vibratory response of bladed disks

Patent Citations (3)

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WO1998036966A1 (fr) * 1997-02-21 1998-08-27 California Institute Of Technology Rotors a pales desaccordees
US5993161A (en) * 1997-02-21 1999-11-30 California Institute Of Technology Rotors with mistuned blades
EP1211382A2 (fr) * 2000-11-30 2002-06-05 United Technologies Corporation Rotor de turbomachine avec des aubes à fréquence propre différente

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2112326A1 (fr) 2008-04-23 2009-10-28 Snecma Carter de turbomachine comportant un dispositif empêchant une instabilité lors d'un contact entre le carter et le rotor
WO2017072469A1 (fr) 2015-10-28 2017-05-04 Safran Aircraft Engines Procede pour introduire un desaccordage volontaire dans une roue aubagee de turbomachine
FR3043131A1 (fr) * 2015-10-28 2017-05-05 Snecma Procede pour introduire un desaccordage volontaire dans une roue aubagee de turbomachine
US10267155B2 (en) 2015-10-28 2019-04-23 Safran Aircraft Engines Method for intentionally mistuning a turbine blade of a turbomachine
WO2017216480A1 (fr) 2016-06-16 2017-12-21 Safran Aircraft Engines Roue aubagee volontairement desaccordee

Also Published As

Publication number Publication date
CA2503659A1 (fr) 2005-10-20
FR2869069B1 (fr) 2008-11-21
RU2372492C2 (ru) 2009-11-10
EP1589191A1 (fr) 2005-10-26
EP1589191B1 (fr) 2010-09-08
DE602005023373D1 (de) 2010-10-21
CA2503659C (fr) 2013-01-29
US20050249586A1 (en) 2005-11-10
US7500299B2 (en) 2009-03-10
RU2005111685A (ru) 2006-10-27
ES2351507T3 (es) 2011-02-07

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Effective date: 20121228