RU2418965C2 - Способ и устройство для уменьшения скорости вращения ротора в случае разрушения вала турбины газотурбинного двигателя - Google Patents

Способ и устройство для уменьшения скорости вращения ротора в случае разрушения вала турбины газотурбинного двигателя Download PDF

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Publication number
RU2418965C2
RU2418965C2 RU2007139450/06A RU2007139450A RU2418965C2 RU 2418965 C2 RU2418965 C2 RU 2418965C2 RU 2007139450/06 A RU2007139450/06 A RU 2007139450/06A RU 2007139450 A RU2007139450 A RU 2007139450A RU 2418965 C2 RU2418965 C2 RU 2418965C2
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RU
Russia
Prior art keywords
rotor
temperature
turbine
stator
sensor
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RU2007139450/06A
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English (en)
Russian (ru)
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RU2007139450A (ru
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Клод Марсель МОН (FR)
Клод Марсель МОН
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Снекма
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Publication of RU2007139450A publication Critical patent/RU2007139450A/ru
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Publication of RU2418965C2 publication Critical patent/RU2418965C2/ru

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    • 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
    • F01D21/12—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to temperature
    • 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
    • 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
    • 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
    • F01D21/06—Shutting-down
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • 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
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • F05D2270/3032—Temperature excessive temperatures, e.g. caused by overheating
    • 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

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
RU2007139450/06A 2006-10-25 2007-10-24 Способ и устройство для уменьшения скорости вращения ротора в случае разрушения вала турбины газотурбинного двигателя RU2418965C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0654537A FR2907839B1 (fr) 2006-10-25 2006-10-25 Methode pour reduire la vitesse en cas de rupture d'arbre de turbine de moteur a turbine a gaz
FR0654537 2006-10-25

Publications (2)

Publication Number Publication Date
RU2007139450A RU2007139450A (ru) 2009-04-27
RU2418965C2 true RU2418965C2 (ru) 2011-05-20

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007139450/06A RU2418965C2 (ru) 2006-10-25 2007-10-24 Способ и устройство для уменьшения скорости вращения ротора в случае разрушения вала турбины газотурбинного двигателя

Country Status (6)

Country Link
US (1) US7934367B2 (enExample)
EP (1) EP1916391B1 (enExample)
JP (1) JP4759765B2 (enExample)
CA (1) CA2607244C (enExample)
FR (1) FR2907839B1 (enExample)
RU (1) RU2418965C2 (enExample)

Cited By (1)

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Publication number Priority date Publication date Assignee Title
RU2629854C2 (ru) * 2012-03-29 2017-09-04 АНСАЛДО ЭНЕРДЖИА АйПи ЮКей ЛИМИТЕД Способ управления турбинным двигателем после погасания пламени

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US8221057B2 (en) 2008-06-25 2012-07-17 General Electric Company Method, system and controller for establishing a wheel space temperature alarm in a turbomachine
CA2713316C (en) * 2009-08-17 2017-09-26 Pratt & Whitney Canada Corp. Turbine section architecture for gas turbine engine
GB201110116D0 (en) 2011-06-16 2011-07-27 Rolls Royce Plc Surge margin control
US10190440B2 (en) 2015-06-10 2019-01-29 Rolls-Royce North American Technologies, Inc. Emergency shut-down detection system for a gas turbine
US9982607B2 (en) 2015-07-20 2018-05-29 Rolls-Royce North American Technologies, Inc. Shaft failure detection using passive control methods
US10514065B2 (en) * 2015-12-14 2019-12-24 Hamilton Sundstrand Corporation Bearing thermal management system and method
GB201611674D0 (en) * 2016-07-05 2016-08-17 Rolls Royce Plc A turbine arrangement
US10738646B2 (en) * 2017-06-12 2020-08-11 Raytheon Technologies Corporation Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section
CN110926819A (zh) * 2019-12-05 2020-03-27 中国航发四川燃气涡轮研究院 一种转子内腔流动特性测试结构
IT202000028520A1 (it) 2020-11-26 2022-05-26 Ge Avio Srl Sistema e metodo per la mitigazione di velocita' eccessiva di rotore

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GB877127A (en) * 1959-04-15 1961-09-13 Napier & Son Ltd Gas turbines
EP0374003A1 (fr) * 1988-12-15 1990-06-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine comportant un dispositif de freinage entre rotor de turbine et carter d'échappement
RU2168044C2 (ru) * 1994-08-08 2001-05-27 Компрессор Контролз Корпорейшн Способ предотвращения отклонения параметров в газовых турбинах и устройство для его осуществления (варианты)
RU2193671C2 (ru) * 1996-11-08 2002-11-27 Сименс Акциенгезелльшафт Устройство управления турбины и способ регулирования цикла нагружения турбины
US6494046B1 (en) * 1998-12-14 2002-12-17 Rolls-Royce Deutschland Ltd & Co Kg Method and apparatus for recognition of a shaft rupture in a turbo-engine
RU2225945C2 (ru) * 2002-04-10 2004-03-20 Открытое акционерное общество "Авиадвигатель" Способ предотвращения отклонения параметров силовой турбины турбомашинного агрегата при внезапном полном или частичном сбросе нагрузки
EP1455054A1 (de) * 2003-03-07 2004-09-08 Rolls-Royce Deutschland Ltd & Co KG Abschaltsystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch

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US4595298A (en) * 1985-05-01 1986-06-17 The United States Of America As Represented By The Secretary Of The Air Force Temperature detection system for use on film cooled turbine airfoils
FR2630792B1 (fr) * 1988-04-29 1992-03-06 Mecanique Magnetique Sa Palier auxiliaire a stator en graphite pour arbre tournant monte sur paliers magnetiques
GB9111906D0 (en) * 1991-06-04 1991-07-24 Lucas Ind Plc Shaft breakage detection system
US5363317A (en) * 1992-10-29 1994-11-08 United Technologies Corporation Engine failure monitor for a multi-engine aircraft having partial engine failure and driveshaft failure detection
US6176074B1 (en) * 1998-06-05 2001-01-23 Pratt & Whitney Canada Corp. Shaft decouple logic for gas turbine
US6607349B2 (en) * 2001-11-14 2003-08-19 Honeywell International, Inc. Gas turbine engine broken shaft detection system
DE10310900A1 (de) * 2003-03-13 2004-09-23 Rolls-Royce Deutschland Ltd & Co Kg Elekronisches Sicherheitssystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch
US6923048B2 (en) * 2003-09-24 2005-08-02 Siemens Aktiengesellschaft Method and apparatus of monitoring temperature and strain by using fiber Bragg grating (FBG) sensors
WO2005112140A2 (en) * 2004-04-12 2005-11-24 The Board Of Governors For Higher Education, State Of Rhode Island And Providence Plantations Thin film ceramic thermocouples
JP4474989B2 (ja) * 2004-04-26 2010-06-09 株式会社Ｉｈｉ タービンノズル及びタービンノズルセグメント
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DE102005042271A1 (de) * 2005-09-06 2007-03-08 Mtu Aero Engines Gmbh Einrichtung zur Detektion eines Wellenbruchs an einer Gasturbine sowie Gasturbine

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB877127A (en) * 1959-04-15 1961-09-13 Napier & Son Ltd Gas turbines
EP0374003A1 (fr) * 1988-12-15 1990-06-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine comportant un dispositif de freinage entre rotor de turbine et carter d'échappement
RU2168044C2 (ru) * 1994-08-08 2001-05-27 Компрессор Контролз Корпорейшн Способ предотвращения отклонения параметров в газовых турбинах и устройство для его осуществления (варианты)
RU2193671C2 (ru) * 1996-11-08 2002-11-27 Сименс Акциенгезелльшафт Устройство управления турбины и способ регулирования цикла нагружения турбины
US6494046B1 (en) * 1998-12-14 2002-12-17 Rolls-Royce Deutschland Ltd & Co Kg Method and apparatus for recognition of a shaft rupture in a turbo-engine
RU2225945C2 (ru) * 2002-04-10 2004-03-20 Открытое акционерное общество "Авиадвигатель" Способ предотвращения отклонения параметров силовой турбины турбомашинного агрегата при внезапном полном или частичном сбросе нагрузки
EP1455054A1 (de) * 2003-03-07 2004-09-08 Rolls-Royce Deutschland Ltd & Co KG Abschaltsystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2629854C2 (ru) * 2012-03-29 2017-09-04 АНСАЛДО ЭНЕРДЖИА АйПи ЮКей ЛИМИТЕД Способ управления турбинным двигателем после погасания пламени

Also Published As

Publication number Publication date
US20080178603A1 (en) 2008-07-31
FR2907839A1 (fr) 2008-05-02
JP4759765B2 (ja) 2011-08-31
CA2607244C (fr) 2015-03-10
US7934367B2 (en) 2011-05-03
CA2607244A1 (fr) 2008-04-25
JP2008106745A (ja) 2008-05-08
RU2007139450A (ru) 2009-04-27
FR2907839B1 (fr) 2011-06-17
EP1916391B1 (fr) 2018-02-21
EP1916391A1 (fr) 2008-04-30

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