EP1457643A3 - Electronic safety system to avoid an over speed condition due to a shaft failure - Google Patents
Electronic safety system to avoid an over speed condition due to a shaft failure Download PDFInfo
- 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
- electronic safety
- avoid
- measuring
- speed condition
- 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
Links
- 230000003287 optical Effects 0.000 abstract 2
- 239000000446 fuels Substances 0.000 abstract 1
- 239000003365 glass fibers Substances 0.000 abstract 1
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
- 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
- F01D21/045—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 special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- F05D2270/09—Purpose of the control system to cope with emergencies
-
- 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
- F05D2270/09—Purpose of the control system to cope with emergencies
- F05D2270/091—Purpose of the control system to cope with emergencies in particular sudden load loss
-
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/614—Fibres or filaments
Abstract
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10310900 | 2003-03-13 | ||
DE2003110900 DE10310900A1 (en) | 2003-03-13 | 2003-03-13 | Electronic safety system to avoid an overspeed condition in the event of a shaft break |
Publications (3)
Publication Number | Publication Date |
---|---|
EP1457643A2 EP1457643A2 (en) | 2004-09-15 |
EP1457643A3 true EP1457643A3 (en) | 2007-03-21 |
EP1457643B1 EP1457643B1 (en) | 2009-07-08 |
Family
ID=32748218
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20040090043 Expired - Fee Related EP1457643B1 (en) | 2003-03-13 | 2004-02-11 | Electronic safety system to avoid an over speed condition due to a shaft failure |
Country Status (3)
Country | Link |
---|---|
US (1) | US7002172B2 (en) |
EP (1) | EP1457643B1 (en) |
DE (2) | DE10310900A1 (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102004009595A1 (en) * | 2004-02-27 | 2005-09-15 | Mtu Aero Engines Gmbh | Method and device for identifying a shaft break and / or an overspeed on a gas turbine |
WO2005093221A1 (en) * | 2004-03-23 | 2005-10-06 | Siemens Aktiengesellschaft | Array and method for detecting damages in a component of a jet engine |
DE102004026366A1 (en) * | 2004-05-29 | 2005-12-15 | Mtu Aero Engines Gmbh | Device for detecting a shaft fracture on a gas turbine and gas turbine |
DE102004033924A1 (en) * | 2004-07-14 | 2006-02-09 | Mtu Aero Engines Gmbh | Device for detecting a shaft fracture on a gas turbine and gas turbine |
DE102004047892A1 (en) * | 2004-10-01 | 2006-04-06 | Mtu Aero Engines Gmbh | Gas turbine and method of shutting down a gas turbine upon identification of a shaft break |
DE102005036879A1 (en) * | 2005-05-12 | 2006-11-16 | Logos-Innovationen Gmbh | Lifting device with a drive unit for lifting a load suspension |
US7536850B2 (en) * | 2005-09-27 | 2009-05-26 | Pratt & Whitney Canada Corp. | Emergency fuel shutoff system |
DE102006017790B3 (en) * | 2006-04-15 | 2007-07-26 | Mtu Aero Engines Gmbh | Shaft breakage detecting device for e.g. aircraft engine, has rotor-sided blade rim with section separating sensor unit to generate electrical signal that corresponds to shaft breakage, where sensor unit is designed as line replaceable unit |
US7581377B2 (en) * | 2006-06-14 | 2009-09-01 | Pratt & Whitney Canada Corp. | Low-cost frangible cable for gas turbine engine |
FR2907839B1 (en) * | 2006-10-25 | 2011-06-17 | Snecma | METHOD FOR REDUCING SPEED IN CASE OF TURBINE SHAFT BREAKAGE OF GAS TURBINE ENGINE |
FR2923540B1 (en) * | 2007-11-13 | 2010-01-29 | Snecma | DEVICE FOR DETECTING RUPTURE OF A TURBOMACHINE SHAFT |
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 (en) * | 2013-02-22 | 2014-08-28 | Rolls-Royce Deutschland Ltd & Co Kg | Aircraft gas turbine with a first rotatable shaft |
US10316689B2 (en) | 2016-08-22 | 2019-06-11 | Rolls-Royce Corporation | Gas turbine engine health monitoring system with shaft-twist sensors |
DE102017213094A1 (en) | 2017-07-28 | 2019-01-31 | Rolls-Royce Deutschland Ltd & Co Kg | Arrangement and method for detecting a shaft break |
Citations (2)
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 (en) * | 1997-06-27 | 1999-01-07 | Mtu Muenchen Gmbh | Device for the emergency shutdown of a gas turbine |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4712372A (en) * | 1985-09-18 | 1987-12-15 | Avco Corporation | Overspeed system redundancy monitor |
DE19857552A1 (en) * | 1998-12-14 | 2000-06-15 | Rolls Royce Deutschland | Method for detecting a shaft break in a fluid flow machine |
US6607349B2 (en) * | 2001-11-14 | 2003-08-19 | Honeywell International, Inc. | Gas turbine engine broken shaft detection system |
-
2003
- 2003-03-13 DE DE2003110900 patent/DE10310900A1/en not_active Withdrawn
-
2004
- 2004-02-11 DE DE200450009705 patent/DE502004009705D1/en active Active
- 2004-02-11 EP EP20040090043 patent/EP1457643B1/en not_active Expired - Fee Related
- 2004-03-12 US US10/798,367 patent/US7002172B2/en not_active Expired - Fee Related
Patent Citations (2)
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 (en) * | 1997-06-27 | 1999-01-07 | Mtu Muenchen Gmbh | Device for the emergency shutdown of a gas turbine |
Also Published As
Publication number | Publication date |
---|---|
US20050047913A1 (en) | 2005-03-03 |
EP1457643B1 (en) | 2009-07-08 |
DE502004009705D1 (en) | 2009-08-20 |
US7002172B2 (en) | 2006-02-21 |
EP1457643A2 (en) | 2004-09-15 |
DE10310900A1 (en) | 2004-09-23 |
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