WO2013004951A3 - Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine - Google Patents

Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine Download PDF

Info

Publication number
WO2013004951A3
WO2013004951A3 PCT/FR2012/051478 FR2012051478W WO2013004951A3 WO 2013004951 A3 WO2013004951 A3 WO 2013004951A3 FR 2012051478 W FR2012051478 W FR 2012051478W WO 2013004951 A3 WO2013004951 A3 WO 2013004951A3
Authority
WO
WIPO (PCT)
Prior art keywords
turbomachine
blade tip
passage times
tip passage
measuring blade
Prior art date
Application number
PCT/FR2012/051478
Other languages
English (en)
Other versions
WO2013004951A2 (fr
Inventor
André LEROUX
Original Assignee
Snecma
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 filed Critical Snecma
Priority to CN201280031373.4A priority Critical patent/CN103620355B/zh
Priority to BR112013033935A priority patent/BR112013033935A2/pt
Priority to RU2014103480/28A priority patent/RU2593427C2/ru
Priority to CA2839815A priority patent/CA2839815A1/fr
Priority to EP12738537.5A priority patent/EP2726829A2/fr
Priority to US14/130,382 priority patent/US20140126993A1/en
Publication of WO2013004951A2 publication Critical patent/WO2013004951A2/fr
Publication of WO2013004951A3 publication Critical patent/WO2013004951A3/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
    • G01B7/14—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring distance or clearance between spaced objects or spaced apertures
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/003—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
    • G01H1/006—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines of the rotor of turbo machines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/80—Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
    • F05D2270/821—Displacement measuring means, e.g. inductive

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)
  • Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)

Abstract

L'invention concerne la mesure des temps de passage des sommets d'aubes dans une turbomachine, au moyen d'un capteur capacitif monté sur un carter au droit de la trajectoire de passage des sommets (80) des aubes d'une roue de compresseur de la turbomachine. Le capteur comprend au moins une électrode longiligne (70) fixée sur la face interne du carter et orientée en oblique par rapport à la trajectoire des sommets d'aubes (80).
PCT/FR2012/051478 2011-07-01 2012-06-27 Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine WO2013004951A2 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
CN201280031373.4A CN103620355B (zh) 2011-07-01 2012-06-27 用于测量涡轮发动机中叶尖的通过时间的设备和方法
BR112013033935A BR112013033935A2 (pt) 2011-07-01 2012-06-27 dispositivo e processo de medida dos tempos de passagem de pontas de pás em uma turbomáquina
RU2014103480/28A RU2593427C2 (ru) 2011-07-01 2012-06-27 Устройство и способ измерения времени прохождения вершин лопаток в турбомашине
CA2839815A CA2839815A1 (fr) 2011-07-01 2012-06-27 Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine
EP12738537.5A EP2726829A2 (fr) 2011-07-01 2012-06-27 Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine
US14/130,382 US20140126993A1 (en) 2011-07-01 2012-06-27 Device and a method for measuring the times of passage of blade tips in a turbine engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1155983A FR2977316B1 (fr) 2011-07-01 2011-07-01 Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine
FR1155983 2011-07-01

Publications (2)

Publication Number Publication Date
WO2013004951A2 WO2013004951A2 (fr) 2013-01-10
WO2013004951A3 true WO2013004951A3 (fr) 2013-10-24

Family

ID=46579198

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2012/051478 WO2013004951A2 (fr) 2011-07-01 2012-06-27 Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine

Country Status (8)

Country Link
US (1) US20140126993A1 (fr)
EP (1) EP2726829A2 (fr)
CN (1) CN103620355B (fr)
BR (1) BR112013033935A2 (fr)
CA (1) CA2839815A1 (fr)
FR (1) FR2977316B1 (fr)
RU (1) RU2593427C2 (fr)
WO (1) WO2013004951A2 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201004559D0 (en) * 2010-03-19 2010-05-05 Rolls Royce Plc Rotating blade analysis
FR3037135B1 (fr) * 2015-06-03 2020-04-17 Safran Aircraft Engines Dispositif de determination du positionnement d'un arbre dans son logement et turbomachine comportant un tel dispositif
JP6792050B2 (ja) * 2016-07-21 2020-11-25 シーメンス・ヘルスケア・ダイアグノスティックス・インコーポレーテッドＳｉｅｍｅｎｓ Ｈｅａｌｔｈｃａｒｅ Ｄｉａｇｎｏｓｔｉｃｓ Ｉｎｃ． 槽および高速空気ソリューション
FR3071919B1 (fr) * 2017-10-03 2019-09-20 Safran Aircraft Engines Systeme et procede de mesure de decalage
FR3095507B1 (fr) * 2019-04-29 2021-04-16 Safran Aircraft Engines Procede de controle dimensionnel d’une piece de turbomachine
CN111043949B (zh) * 2019-12-31 2021-04-30 电子科技大学 一种用于涡轮叶片叶尖间隙检测的装置
CN114485894B (zh) * 2021-12-17 2023-10-27 武汉科技大学 一种基于叶尖定时的旋转叶片振动测试系统及测试方法

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2204693A (en) * 1987-05-14 1988-11-16 Rolls Royce Plc Turbomachine tip clearance sensor
US20100268509A1 (en) * 2007-10-25 2010-10-21 Michael Zielinski Turbomachine, gap-measuring system, and method for determining a rotor gap

Family Cites Families (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1009979A (en) * 1960-10-21 1965-11-17 Bristol Siddeley Engines Ltd Means for measuring the superimposed oscillation of part of a rotating member
US4049644A (en) * 1976-06-23 1977-09-20 Wennerstrom Arthur J Device for measuring tip deflection of rotating blades
US4247247A (en) * 1979-05-29 1981-01-27 General Motors Corporation Blade tip clearance control
US4509332A (en) * 1984-04-30 1985-04-09 Westinghouse Electric Corp. Apparatus for monitoring corrosive salt solutions in a low pressure steam turbine
GB2181246B (en) * 1985-10-02 1989-09-27 Rolls Royce Apparatus for measuring axial movement of a rotating member
US4955269A (en) * 1988-02-04 1990-09-11 Westinghouse Electric Corp. Turbine blade fatigue monitor
US4934192A (en) * 1988-07-11 1990-06-19 Westinghouse Electric Corp. Turbine blade vibration detection system
GB2229004B (en) * 1989-03-07 1993-09-29 Rolls Royce Plc Improvements in or relating to gas turbine engine tip clearance sensors
US4951500A (en) * 1989-07-26 1990-08-28 Westinghouse Electric Corp. Method for determining the untwist of turbine blades
US5119036A (en) * 1990-05-29 1992-06-02 General Electric Company Electrical capacitance clearanceometer
US5166626A (en) * 1990-05-29 1992-11-24 General Electric Company Electrical capacitance clearanceometer
US5101165A (en) * 1990-05-29 1992-03-31 General Electric Company Electrical capacitance clearanceometer
US5450760A (en) * 1993-10-18 1995-09-19 Lew; Hyok S. Turbine flowmeter with capacitive transducer
US5545007A (en) * 1994-11-25 1996-08-13 United Technologies Corp. Engine blade clearance control system with piezoelectric actuator
FR2811422B1 (fr) * 2000-07-06 2002-08-30 Snecma Moteurs Capteur de mesure de jeux par abrasion multiprofondeur
GB2374123B (en) * 2001-04-05 2004-09-08 Rolls Royce Plc Gas turbine engine system
US6700393B2 (en) * 2001-10-17 2004-03-02 Delphi Technologies, Inc. Capacitive sensor assembly for use in a non-contact obstacle detection system
US7582359B2 (en) * 2002-09-23 2009-09-01 Siemens Energy, Inc. Apparatus and method of monitoring operating parameters of a gas turbine
US6955461B2 (en) * 2003-01-24 2005-10-18 Dow Global Technologies, Inc. Tickler for slurry reactors and tanks
US8742944B2 (en) * 2004-06-21 2014-06-03 Siemens Energy, Inc. Apparatus and method of monitoring operating parameters of a gas turbine
US7341428B2 (en) * 2005-02-02 2008-03-11 Siemens Power Generation, Inc. Turbine blade for monitoring torsional blade vibration
RU2280238C1 (ru) * 2005-02-24 2006-07-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Способ измерения и контроля радиально-осевых зазоров в турбомашинах и устройство для его осуществления
US8591188B2 (en) * 2005-04-26 2013-11-26 General Electric Company Displacement sensor system and method of operation
GB0513654D0 (en) * 2005-07-02 2005-08-10 Rolls Royce Plc Variable displacement turbine liner
US7215129B1 (en) * 2006-03-30 2007-05-08 General Electric Company Multi tip clearance measurement system and method of operation
US7891938B2 (en) * 2007-03-20 2011-02-22 General Electric Company Multi sensor clearance probe
GB2455968B (en) * 2007-11-21 2010-06-09 Rolls Royce Plc Turbomachine having an apparatus to measure the clearance between a rotor blade tip and a stator liner of a stator casing
US20090142194A1 (en) * 2007-11-30 2009-06-04 General Electric Company Method and systems for measuring blade deformation in turbines
US8151647B2 (en) * 2008-09-24 2012-04-10 Siemens Energy, Inc. Apparatus for monitoring blade vibration with an imaging fiber optic ribbon probe
US8126662B2 (en) * 2008-09-24 2012-02-28 Siemens Energy, Inc. Method and apparatus for monitoring blade vibration with a fiber optic ribbon probe
FR2986864B1 (fr) * 2012-02-14 2014-02-28 Snecma Methode de mesure de la deformation d'une aube de turbomachine au cours du fonctionnement de la turbomachine
US8687206B2 (en) * 2012-05-29 2014-04-01 United Technologies Corporation Optical detection of airfoil axial position with NSMS
EP2728128A1 (fr) * 2012-10-31 2014-05-07 Siemens Aktiengesellschaft Procédé de mesure destiné à détecter les dommages sur une aube de turbine et turbine
GB201309622D0 (en) * 2013-05-30 2013-07-10 Rolls Royce Plc Blade tip timing
GB2520247B (en) * 2013-11-12 2015-12-09 Rolls Royce Plc Edge Detector

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2204693A (en) * 1987-05-14 1988-11-16 Rolls Royce Plc Turbomachine tip clearance sensor
US20100268509A1 (en) * 2007-10-25 2010-10-21 Michael Zielinski Turbomachine, gap-measuring system, and method for determining a rotor gap

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
ALI ABDUL-AZIZ ET AL.: "Propulsion health monitoring of a turbine engine disk using spin test data", HEALTH MONITORING OF STRUCTURAL AND BIOLOGICAL SYSTEMS, 2010, pages 1 - 10, XP002674174 *
LAWSON C P ET AL: "Tubomachinery blade vibration amplitude measurement through tip timing with capacitance tip clearance probes", SENSORS AND ACTUATORS A, ELSEVIER SEQUOIA S.A., LAUSANNE, CH, vol. 118, no. 1, 31 January 2005 (2005-01-31), pages 14 - 24, XP025325191, ISSN: 0924-4247, [retrieved on 20050131], DOI: 10.1016/S0924-4247(04)00482-0 *
TYCO THERMAL CONTROLS LLC: "High temperature clearance and vibration monitoring systems", CAPACISENSE, 2010, XP002674175 *

Also Published As

Publication number Publication date
BR112013033935A2 (pt) 2017-02-14
CN103620355A (zh) 2014-03-05
CN103620355B (zh) 2015-09-09
US20140126993A1 (en) 2014-05-08
EP2726829A2 (fr) 2014-05-07
RU2014103480A (ru) 2015-08-10
WO2013004951A2 (fr) 2013-01-10
FR2977316A1 (fr) 2013-01-04
CA2839815A1 (fr) 2013-01-10
RU2593427C2 (ru) 2016-08-10
FR2977316B1 (fr) 2014-02-21

Similar Documents

Publication Publication Date Title
WO2013004951A3 (fr) Dispositif et procede de mesure des temps de passage de sommets d'aubes dans une turbomachine
GB201110141D0 (en) A method of detecting shaft break
EP2551517A3 (fr) Pale de turbine éolienne et système de mesure des éclairs
PL2099582T3 (pl) Urządzenie i sposób naprawy lub wytwarzania końców łopatek turbiny gazowej, w szczególności silnika lotniczego
EP2375004A3 (fr) Procédés, systèmes et appareil relatif à des calculs de jeux d'aubes dans des moteurs de turbine
WO2012068055A3 (fr) Détection de capacité dans un organe de commande de gouttelettes
GB2455968B (en) Turbomachine having an apparatus to measure the clearance between a rotor blade tip and a stator liner of a stator casing
EP2597258A3 (fr) Procédé et système de surveillance pour turbine à gaz
ATE513221T1 (de) Messanordnung zur erfassung eines umdrehungsimpulses eines triebwerkrotors sowie verfahren hierzu
EP2557271A3 (fr) Procédé de mesure d'érosion d'extrémité d'aube de turbine
WO2010054644A3 (fr) Procédé et dispositif de détection de fissures sur des aubes mobiles d'un compresseur
ATE552484T1 (de) Verfahren und vorrichtung zum messen, prüfen und/oder überwachen einer turbinenleistung
RU2012134278A (ru) Турбоустановка
GB201301604D0 (en) System For Detecting An Impact On An Aircraft Engine Impeller Wheel
WO2010122348A3 (fr) Débitmètre pour fluide
WO2012103541A3 (fr) Système d'interprétation de dégâts d'une canalisation
EP2600130A3 (fr) Dispositif de mesure de pression et procédé de mesure de pression pour une turbomachine
MX359001B (es) Metodo para medir el angulo de una pala de rotor.
WO2014099937A8 (fr) Système de sonde à synchronisation de pointe optique interrompue à faisceau intégré pour aube de moteur à turbine à gaz
WO2012066107A3 (fr) Procédé de détermination d'états de fonctionnement d'une éolienne
EP2505985A3 (fr) Sonde de chambre de combustion pour turbine à gaz
EP2781897A3 (fr) Synchronisation de pointe d'aube
WO2015105547A3 (fr) Pale de ventilateur comportant un couvercle de pale de ventilateur segmenté
WO2012141846A3 (fr) Boîtier de palier d'un turbocompresseur à gaz d'échappement
EP2730749A3 (fr) Appareil et procédé pour mesurer l'écoulement gazeux à travers un joint rotatif

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 12738537

Country of ref document: EP

Kind code of ref document: A2

ENP Entry into the national phase

Ref document number: 2839815

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 2012738537

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 14130382

Country of ref document: US

ENP Entry into the national phase

Ref document number: 2014103480

Country of ref document: RU

Kind code of ref document: A

REG Reference to national code

Ref country code: BR

Ref legal event code: B01A

Ref document number: 112013033935

Country of ref document: BR

ENP Entry into the national phase

Ref document number: 112013033935

Country of ref document: BR

Kind code of ref document: A2

Effective date: 20131230