EP1457643A3 - Elektronisches Sicherheitssystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch - Google Patents

Elektronisches Sicherheitssystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch Download PDF

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Publication number
EP1457643A3
EP1457643A3 EP04090043A EP04090043A EP1457643A3 EP 1457643 A3 EP1457643 A3 EP 1457643A3 EP 04090043 A EP04090043 A EP 04090043A EP 04090043 A EP04090043 A EP 04090043A EP 1457643 A3 EP1457643 A3 EP 1457643A3
Authority
EP
European Patent Office
Prior art keywords
shaft
safety system
electronic safety
avoid
measuring
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
EP04090043A
Other languages
English (en)
French (fr)
Other versions
EP1457643B1 (de
EP1457643A2 (de
Inventor
Detlef Rensch
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.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
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 Rolls Royce Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Publication of EP1457643A2 publication Critical patent/EP1457643A2/de
Publication of EP1457643A3 publication Critical patent/EP1457643A3/de
Application granted granted Critical
Publication of EP1457643B1 publication Critical patent/EP1457643B1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • 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
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/09Purpose of the control system to cope with emergencies
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/09Purpose of the control system to cope with emergencies
    • F05D2270/091Purpose of the control system to cope with emergencies in particular sudden load loss
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/614Fibres or filaments

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Monitoring And Testing Of Nuclear Reactors (AREA)
  • Optical Transform (AREA)

Abstract

Ein elektronisches Sicherheitssystem zur Detektion eines Wellenbruchs und zur Unterbrechung der Antriebsenergiezufuhr umfasst mindestens einen in Wellenlängsrichtung fest verlegten, mit der Welle (1) rotierenden und an der Eintrittsseite (14) mit einem mit der Lichtquelle (18) verbundenen Mess-Lichtleiter (13). Bei einem Wellenbruch wird der Mess-Lichtleiter durchtrennt, wobei das Ausbleiben des Lichts an der Austrittsseite (15) von einem optischen Sensor (19) registriert und über eine Auswerte- und Steuerelektronik (20, 21) als Signal zur Abschaltung der weiteren Energiezufuhr an einem Kraftstoff-Absperrventil (22) dient. Der Mess-Lichtleiter ist an einer an beiden Enden mit der Welle verbundenen Messhülse (4) fixiert.
EP04090043A 2003-03-13 2004-02-11 Elektronisches Sicherheitssystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch Expired - Fee Related EP1457643B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10310900A DE10310900A1 (de) 2003-03-13 2003-03-13 Elekronisches Sicherheitssystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch
DE10310900 2003-03-13

Publications (3)

Publication Number Publication Date
EP1457643A2 EP1457643A2 (de) 2004-09-15
EP1457643A3 true EP1457643A3 (de) 2007-03-21
EP1457643B1 EP1457643B1 (de) 2009-07-08

Family

ID=32748218

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04090043A Expired - Fee Related EP1457643B1 (de) 2003-03-13 2004-02-11 Elektronisches Sicherheitssystem zur Vermeidung eines Überdrehzahlzustandes bei einem Wellenbruch

Country Status (3)

Country Link
US (1) US7002172B2 (de)
EP (1) EP1457643B1 (de)
DE (2) DE10310900A1 (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004009595A1 (de) * 2004-02-27 2005-09-15 Mtu Aero Engines Gmbh Verfahren und Vorrichtung zur Identifikation eines Wellenbruchs und/oder einer Überdrehzahl an einer Gasturbine
DE502005001831D1 (de) * 2004-03-23 2007-12-13 Siemens Ag Anordnung und verfahren zur beschädigungsdetektion an einer komponente einer strömungsmaschine
DE102004026366A1 (de) * 2004-05-29 2005-12-15 Mtu Aero Engines Gmbh Einrichtung zur Detektion eines Wellenbruchs an einer Gasturbine sowie Gasturbine
DE102004033924A1 (de) * 2004-07-14 2006-02-09 Mtu Aero Engines Gmbh Einrichtung zur Detektion eines Wellenbruchs an einer Gasturbine sowie Gasturbine
DE102004047892A1 (de) 2004-10-01 2006-04-06 Mtu Aero Engines Gmbh Gasturbine und Verfahren zum Abschalten einer Gasturbine bei Identifikation eines Wellenbruchs
DE102005036879A1 (de) * 2005-05-12 2006-11-16 Logos-Innovationen Gmbh Hebevorrichtung mit einer Antriebseinheit zum Heben einer Lastaufnahme
US7536850B2 (en) * 2005-09-27 2009-05-26 Pratt & Whitney Canada Corp. Emergency fuel shutoff system
DE102006017790B3 (de) * 2006-04-15 2007-07-26 Mtu Aero Engines Gmbh Einrichtung zur Detektion eines Wellenbruchs an einer Gasturbine sowie Gasturbine
US7581377B2 (en) * 2006-06-14 2009-09-01 Pratt & Whitney Canada Corp. Low-cost frangible cable for gas turbine engine
FR2907839B1 (fr) * 2006-10-25 2011-06-17 Snecma Methode pour reduire la vitesse en cas de rupture d'arbre de turbine de moteur a turbine a gaz
FR2923540B1 (fr) * 2007-11-13 2010-01-29 Snecma Dispositif de detection de rupture d'un arbre de turbomachine
US9169742B2 (en) * 2010-02-26 2015-10-27 Pratt & Whitney Canada Corp. Electronic shaft shear detection conditioning circuit
US10167784B2 (en) 2012-10-26 2019-01-01 Pratt & Whitney Canada Corp. System for detecting shaft shear event
DE102013101791A1 (de) * 2013-02-22 2014-08-28 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbine mit einer ersten drehbaren Welle
US10316689B2 (en) 2016-08-22 2019-06-11 Rolls-Royce Corporation Gas turbine engine health monitoring system with shaft-twist sensors
DE102017213094A1 (de) * 2017-07-28 2019-01-31 Rolls-Royce Deutschland Ltd & Co Kg Anordnung und Verfahren zur Erkennung eines Wellenbruchs
IT202000028520A1 (it) 2020-11-26 2022-05-26 Ge Avio Srl Sistema e metodo per la mitigazione di velocita' eccessiva di rotore

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5411364A (en) * 1993-12-22 1995-05-02 Allied-Signal Inc. Gas turbine engine failure detection system
DE19727296A1 (de) * 1997-06-27 1999-01-07 Mtu Muenchen Gmbh Einrichtung zur Notabschaltung einer Gasturbine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4712372A (en) * 1985-09-18 1987-12-15 Avco Corporation Overspeed system redundancy monitor
DE19857552A1 (de) * 1998-12-14 2000-06-15 Rolls Royce Deutschland Verfahren zum Erkennen eines Wellenbruches in einer Strömungskraftmaschine
US6607349B2 (en) * 2001-11-14 2003-08-19 Honeywell International, Inc. Gas turbine engine broken shaft detection system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5411364A (en) * 1993-12-22 1995-05-02 Allied-Signal Inc. Gas turbine engine failure detection system
DE19727296A1 (de) * 1997-06-27 1999-01-07 Mtu Muenchen Gmbh Einrichtung zur Notabschaltung einer Gasturbine

Also Published As

Publication number Publication date
EP1457643B1 (de) 2009-07-08
EP1457643A2 (de) 2004-09-15
US20050047913A1 (en) 2005-03-03
US7002172B2 (en) 2006-02-21
DE10310900A1 (de) 2004-09-23
DE502004009705D1 (de) 2009-08-20

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