PL2588718T3 - Wykrywanie nadmiernej prędkości turbiny swobodnej w wyniku pomiaru momentometrem - Google Patents

Wykrywanie nadmiernej prędkości turbiny swobodnej w wyniku pomiaru momentometrem

Info

Publication number
PL2588718T3
PL2588718T3 PL11741633T PL11741633T PL2588718T3 PL 2588718 T3 PL2588718 T3 PL 2588718T3 PL 11741633 T PL11741633 T PL 11741633T PL 11741633 T PL11741633 T PL 11741633T PL 2588718 T3 PL2588718 T3 PL 2588718T3
Authority
PL
Poland
Prior art keywords
torquemeter
free turbine
overspeed detection
overspeed
detection
Prior art date
Application number
PL11741633T
Other languages
English (en)
Inventor
Jean-Luc Charles Gilbert Frealle
Alain Michel Perbos
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL2588718T3 publication Critical patent/PL2588718T3/pl

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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • 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
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • 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
    • F01D21/02—Shutting-down responsive to overspeed
    • 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
    • F01D21/04—Shutting-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
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/329—Application in turbines in gas turbines in helicopters
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/02—Purpose of the control system to control rotational speed (n)
    • F05D2270/021—Purpose of the control system to control rotational speed (n) to prevent overspeed
    • 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
    • F05D2270/01—Purpose of the control system
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/052—Torque
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Control Of Turbines (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Eletrric Generators (AREA)
PL11741633T 2010-07-02 2011-07-01 Wykrywanie nadmiernej prędkości turbiny swobodnej w wyniku pomiaru momentometrem PL2588718T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1055350A FR2962165B1 (fr) 2010-07-02 2010-07-02 Detection de survitesse d'une turbine libre par mesure sur couplemetre
PCT/FR2011/051558 WO2012001334A1 (fr) 2010-07-02 2011-07-01 Detection de survitesse d'une turbine libre par mesure sur couplemetre
EP11741633.9A EP2588718B1 (fr) 2010-07-02 2011-07-01 Detection de survitesse d'une turbine libre par mesure sur couplemetre

Publications (1)

Publication Number Publication Date
PL2588718T3 true PL2588718T3 (pl) 2018-03-30

Family

ID=43608848

Family Applications (1)

Application Number Title Priority Date Filing Date
PL11741633T PL2588718T3 (pl) 2010-07-02 2011-07-01 Wykrywanie nadmiernej prędkości turbiny swobodnej w wyniku pomiaru momentometrem

Country Status (11)

Country Link
US (1) US20130098042A1 (pl)
EP (1) EP2588718B1 (pl)
JP (1) JP2013530348A (pl)
KR (1) KR20130094285A (pl)
CN (1) CN102971495B (pl)
CA (1) CA2804089A1 (pl)
ES (1) ES2654348T3 (pl)
FR (1) FR2962165B1 (pl)
PL (1) PL2588718T3 (pl)
RU (1) RU2564159C2 (pl)
WO (1) WO2012001334A1 (pl)

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FR2987085B1 (fr) * 2012-02-20 2014-03-21 Snecma Procede de securisation du fonctionnement d'une turbomachine
ITCO20120008A1 (it) 2012-03-01 2013-09-02 Nuovo Pignone Srl Metodo e sistema per monitorare la condizione di un gruppo di impianti
FR2998058B1 (fr) * 2012-11-13 2016-02-05 Microturbo Dispositif et procede de protection d'un calculateur de turbo-machine d'aeronef contre les erreurs de mesure de vitesse
US9771167B2 (en) * 2013-01-16 2017-09-26 Airbus Helicopters Monitor system for monitoring the starting of a rotary wing aircraft, an aircraft, and a method using the system
FR3000989A1 (fr) * 2013-01-16 2014-07-18 Eurocopter France Systeme de surveillance du demarrage d'un aeronef a voilure tournante, aeronef et procede mettant en oeuvre ce systeme
FR3007787B1 (fr) 2013-06-27 2015-06-26 Eurocopter France Procede et dispositif de protection dun moteur de giravion en survitesse
EP2848771A1 (de) * 2013-09-17 2015-03-18 Siemens Aktiengesellschaft Verfahren zum Prüfen einer Überdrehzahlschutzeinrichtung einer Einwellenanlage
EP2848772A1 (de) * 2013-09-17 2015-03-18 Siemens Aktiengesellschaft Verfahren zum Testen einer Überdrehzahlschutzeinrichtung einer Einwellenanlage
CN105765172B (zh) * 2013-09-30 2018-03-27 西门子公司 用于操作具有超载保护的涡轮机的方法以及包括用于执行所述方法的装置的涡轮机
FR3013390B1 (fr) 2013-11-19 2019-01-25 Safran Helicopter Engines Turbomachine et procede de regulation
GB201403178D0 (en) * 2014-02-24 2014-04-09 Rolls Royce Plc Electrical power generator for a gas turbine engine
FR3026437A1 (fr) 2014-09-26 2016-04-01 Airbus Helicopters Procede pour arreter un moteur de giravion en survitesse, systeme et giravion associes
FR3026438B1 (fr) 2014-09-26 2019-03-15 Airbus Helicopters Procede pour arreter un moteur de giravion en survitesse, systeme et giravion associes
US10180078B2 (en) * 2016-06-17 2019-01-15 Pratt & Whitney Canada Corp. Shaft shear detection in gas turbine engines
DE102016217690A1 (de) 2016-09-15 2018-03-15 Rolls-Royce Deutschland Ltd & Co Kg Vorrichtung und Verfahren zur Messung einer Rotationsbewegung, insbesondere einer Rotationsrichtung, sowie zur Erkennung eines Wellenbruchs
US10006375B1 (en) * 2017-07-11 2018-06-26 General Electric Company Propulsion system for an aircraft
US20190155318A1 (en) 2017-11-23 2019-05-23 Pratt & Whitney Canada Corp. Torque signal dynamic compensation based on sensor location
JP2021523664A (ja) 2018-05-09 2021-09-02 アーベーベー・シュバイツ・アーゲーＡＢＢ Ｓｃｈｗｅｉｚ ＡＧ ブレーカ自動同期装置
GB201901113D0 (en) * 2019-01-28 2019-03-13 Rolls Royce Plc Shaft monitoring system
US11168621B2 (en) * 2019-03-05 2021-11-09 Pratt & Whitney Canada Corp. Method and system for operating an engine in a multi-engine aircraft
RU2703581C1 (ru) * 2019-04-11 2019-10-21 Публичное Акционерное Общество "Одк-Сатурн" Способ останова двигателя при обрыве ротора турбины
US11352900B2 (en) * 2019-05-14 2022-06-07 Pratt & Whitney Canada Corp. Method and system for operating a rotorcraft engine
US11333035B2 (en) 2019-07-24 2022-05-17 Pratt & Whitney Canada Corp. Shaft shear detection in a gas turbine engine
GB201914042D0 (en) 2019-09-30 2019-11-13 Rolls Royce Plc Gas turbine engine
RU198844U1 (ru) * 2019-12-18 2020-07-31 федеральное государственное бюджетное образовательное учреждение высшего образования "Московский политехнический университет" (Московский Политех) Устройство ограничения частоты вращения турбогенератора
US20210332765A1 (en) * 2020-04-27 2021-10-28 Hamilton Sundstrand Corporation Detecting condition of a shaft of a gas turbofan aircraft engine
FR3111668B1 (fr) * 2020-06-17 2023-04-07 Airbus Helicopters Procédé pour arrêter un moteur en survitesse, système et giravion associés
CN113719359B (zh) * 2021-09-28 2022-11-01 中国航发湖南动力机械研究所 一种预防航空涡轴发动机涡轮超转破裂的保护方法和系统
US20230251165A1 (en) * 2022-02-04 2023-08-10 Pratt & Whitney Canada Corp. Method and system for detecting a shaft shear event
US11965424B2 (en) * 2022-06-21 2024-04-23 General Electric Company Electronic overspeed protection system and method

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RU2376487C2 (ru) * 2008-01-09 2009-12-20 Государственное предприятие "Запорожское машиностроительное конструкторское бюро "Прогресс" имени академика А.Г. Ивченко" Способ защиты газотурбинного двигателя
FR2931552B1 (fr) * 2008-05-21 2010-07-30 Turbomeca Dispositif de mesure de couple transmis par un arbre de puissance

Also Published As

Publication number Publication date
JP2013530348A (ja) 2013-07-25
CA2804089A1 (fr) 2012-01-05
RU2013101569A (ru) 2014-08-10
CN102971495A (zh) 2013-03-13
EP2588718B1 (fr) 2017-11-22
RU2564159C2 (ru) 2015-09-27
ES2654348T3 (es) 2018-02-13
EP2588718A1 (fr) 2013-05-08
FR2962165A1 (fr) 2012-01-06
FR2962165B1 (fr) 2014-05-02
KR20130094285A (ko) 2013-08-23
US20130098042A1 (en) 2013-04-25
CN102971495B (zh) 2016-06-01
WO2012001334A1 (fr) 2012-01-05

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