BR112012019559A2 - metodo para a deteccao automatica da ingestao de pelo menos um corpo estraho por meio de um motor de turbina a gas - Google Patents

metodo para a deteccao automatica da ingestao de pelo menos um corpo estraho por meio de um motor de turbina a gas

Info

Publication number
BR112012019559A2
BR112012019559A2 BR112012019559A BR112012019559A BR112012019559A2 BR 112012019559 A2 BR112012019559 A2 BR 112012019559A2 BR 112012019559 A BR112012019559 A BR 112012019559A BR 112012019559 A BR112012019559 A BR 112012019559A BR 112012019559 A2 BR112012019559 A2 BR 112012019559A2
Authority
BR
Brazil
Prior art keywords
foreign body
gas turbine
turbine engine
ingestion
intake
Prior art date
Application number
BR112012019559A
Other languages
English (en)
Inventor
Bourget Sebastien
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
Publication of BR112012019559A2 publication Critical patent/BR112012019559A2/pt

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
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003Arrangements for testing or measuring

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Testing Of Engines (AREA)

Abstract

método para a detecção automática da ingestão de pelo menos um corpo estranho por meio de um motor de turbina a gás. a invenção se refere a um método para a detecção automática da ingestão de pelo menos um corpo estranho por meio de um motor de turbina a gás, de acordo coma qual: a velocidade instatânea do rotor (r(t) é medida; o sinal de velocidade do rotor (r(t) é filtrado a fim de separar o componente estático (rs(t) a partir do seu componente dinâmico (rd(t); o componente dinâmico filtrado (rd(r) é comparado a uma onda de ressonância padrão (e(t) do rotor a fim de se obter um indicador da ingestão (ting), a onda de ressonância padrão (e(t) correspondente à resposta ao impulso vibracional de um rotor; o indicaodr da ingestão obtido (ting) é comparado com um início da detecção (s); e um sinal de detecção de ingestão do corpo estranho é emitido quando o indicador da ingestão (ting) é maior do que o início da detecção (s).
BR112012019559A 2010-02-08 2011-02-02 metodo para a deteccao automatica da ingestao de pelo menos um corpo estraho por meio de um motor de turbina a gas BR112012019559A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1050870A FR2956159B1 (fr) 2010-02-08 2010-02-08 Methode de detection automatisee de l'ingestion d'au moins un corps etranger par un moteur a turbine a gaz
PCT/FR2011/050205 WO2011095737A1 (fr) 2010-02-08 2011-02-02 Méthode de détection automatisée de l'ingestion d'au moins un corps étranger par un moteur à turbine à gaz

Publications (1)

Publication Number Publication Date
BR112012019559A2 true BR112012019559A2 (pt) 2018-03-27

Family

ID=42697390

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012019559A BR112012019559A2 (pt) 2010-02-08 2011-02-02 metodo para a deteccao automatica da ingestao de pelo menos um corpo estraho por meio de um motor de turbina a gas

Country Status (9)

Country Link
US (1) US9366154B2 (pt)
EP (1) EP2534341B1 (pt)
JP (1) JP5698766B2 (pt)
CN (1) CN103026006B (pt)
BR (1) BR112012019559A2 (pt)
CA (1) CA2788901C (pt)
FR (1) FR2956159B1 (pt)
RU (1) RU2551252C2 (pt)
WO (1) WO2011095737A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2968038B1 (fr) * 2010-11-26 2012-12-28 Snecma Systeme de detection d'un evenement fugace sur une roue aubagee de moteur d'aeronef
EP2594912A1 (en) * 2011-11-21 2013-05-22 Eurocopter Deutschland GmbH Detection system for detection of damages on rotating components of aircraft and method of operating such a detection system
FR2986269B1 (fr) * 2012-01-30 2015-08-07 Snecma Systeme de detection d'un impact sur une roue aubagee de moteur d'aeronef
FR2988130B1 (fr) * 2012-03-13 2014-05-09 Snecma Systeme de detection de defaut sur une roue aubagee de moteur d'aeronef
US10228304B2 (en) 2016-01-18 2019-03-12 Pratt & Whitney Canada Corp. Shaft shear detection through shaft oscillation
RU2680770C1 (ru) * 2018-06-25 2019-02-26 Акционерное общество "Научно-исследовательский и конструкторский институт центробежных и роторных компрессоров им. В.Б. Шнеппа" Способ обнаружения попадания несжимаемых объектов в проточную часть турбокомпрессора и система для его реализации

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8707187D0 (en) 1987-03-25 1987-04-29 Hughes Ltd Stewart Monitoring of foreign object in engines
US6098022A (en) 1997-10-17 2000-08-01 Test Devices, Inc. Detecting anomalies in rotating components
JP2002540870A (ja) * 1999-03-30 2002-12-03 コーニンクレッカ フィリップス エレクトロニクス エヌ ヴィ 時間平均モーメントを導出する方法及びシステム
US6499350B1 (en) * 2000-04-04 2002-12-31 Swantech, L.L.C. Turbine engine foreign object damage detection system
US6668655B2 (en) * 2001-09-27 2003-12-30 Siemens Westinghouse Power Corporation Acoustic monitoring of foreign objects in combustion turbines during operation
GB0126706D0 (en) * 2001-11-07 2002-01-02 Rolls Royce Plc An apparatus and method for detecting an impact on a rotor blade
FR2840358B1 (fr) * 2002-05-28 2006-09-15 Snecma Moteurs Procede et systeme de detection d'endommagement de rotor d'un moteur d'aeronef
EP1574674A1 (de) * 2004-03-03 2005-09-14 Siemens Aktiengesellschaft Verfahren und Vorrichtung zur Detektierung von Verunreinigungen an Turbinenbauteilen
JP2006138756A (ja) * 2004-11-12 2006-06-01 Fanuc Ltd 衝撃検知装置
DE102005020900B3 (de) * 2005-05-04 2006-11-02 Siemens Ag Verfahren und System zur Diagnose von mechanischen, elektromechanischen oder fluidischen Komponenten
US8818683B2 (en) * 2006-04-21 2014-08-26 General Electric Company Method and apparatus for operating a gas turbine engine
RU2348911C1 (ru) * 2007-06-21 2009-03-10 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Способ диагностики газотурбинных двигателей при попадании посторонних предметов на их вход
RU2367811C2 (ru) * 2007-07-30 2009-09-20 Алексей Александрович Комов Способ регулирования величины обратной тяги газотурбинных двигателей на пробеге четырехдвигательного самолета при использовании реверса тяги двух внутренних двигателей
JP2009278757A (ja) * 2008-05-14 2009-11-26 Toshiba Corp 回転電機又は回転機械のリプレイス情報収集方法及び収集システム
FR2937079B1 (fr) * 2008-10-10 2011-08-26 Snecma Procede et systeme de surveillance d'un turboreacteur
US7855469B2 (en) * 2009-10-02 2010-12-21 General Electric Company Condition monitoring system for wind turbine generator and method for operating wind turbine generator

Also Published As

Publication number Publication date
JP2013519031A (ja) 2013-05-23
WO2011095737A1 (fr) 2011-08-11
JP5698766B2 (ja) 2015-04-08
EP2534341B1 (fr) 2013-11-13
CN103026006A (zh) 2013-04-03
RU2012138447A (ru) 2014-03-20
EP2534341A1 (fr) 2012-12-19
RU2551252C2 (ru) 2015-05-20
CA2788901A1 (fr) 2011-08-11
US20120303330A1 (en) 2012-11-29
CN103026006B (zh) 2015-04-01
FR2956159A1 (fr) 2011-08-12
FR2956159B1 (fr) 2012-02-10
US9366154B2 (en) 2016-06-14
CA2788901C (fr) 2017-01-03

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