SG10201404370SA - Method and device for monitoring the malfunction of apu turbine vane fracture and rotor shaft jam - Google Patents
Method and device for monitoring the malfunction of apu turbine vane fracture and rotor shaft jamInfo
- Publication number
- SG10201404370SA SG10201404370SA SG10201404370SA SG10201404370SA SG10201404370SA SG 10201404370S A SG10201404370S A SG 10201404370SA SG 10201404370S A SG10201404370S A SG 10201404370SA SG 10201404370S A SG10201404370S A SG 10201404370SA SG 10201404370S A SG10201404370S A SG 10201404370SA
- Authority
- SG
- Singapore
- Prior art keywords
- malfunction
- monitoring
- rotor shaft
- turbine vane
- apu turbine
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
- G01M15/14—Testing gas-turbine engines or jet-propulsion engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N25/00—Investigating or analyzing materials by the use of thermal means
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0218—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
- G05B23/0224—Process history based detection method, e.g. whereby history implies the availability of large amounts of data
- G05B23/0227—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions
- G05B23/0235—Qualitative history assessment, whereby the type of data acted upon, e.g. waveforms, images or patterns, is not relevant, e.g. rule based assessment; if-then decisions based on a comparison with predetermined threshold or range, e.g. "classical methods", carried out during normal operation; threshold adaptation or choice; when or how to compare with the threshold
-
- 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
- F05D2220/50—Application for auxiliary power units (APU's)
-
- 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
- F05D2270/40—Type of control system
- F05D2270/44—Type of control system active, predictive, or anticipative
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310313840.9A CN104344946B (en) | 2013-07-24 | 2013-07-24 | APU turbo blades are broken monitoring method and device with rotating shaft jamming failure |
Publications (1)
Publication Number | Publication Date |
---|---|
SG10201404370SA true SG10201404370SA (en) | 2015-02-27 |
Family
ID=51224787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG10201404370SA SG10201404370SA (en) | 2013-07-24 | 2014-07-24 | Method and device for monitoring the malfunction of apu turbine vane fracture and rotor shaft jam |
Country Status (10)
Country | Link |
---|---|
US (1) | US9632010B2 (en) |
EP (1) | EP2829688B1 (en) |
JP (1) | JP6205321B2 (en) |
KR (1) | KR101998188B1 (en) |
CN (1) | CN104344946B (en) |
AU (1) | AU2014206179B2 (en) |
CA (1) | CA2857748C (en) |
HK (1) | HK1202330A1 (en) |
SG (1) | SG10201404370SA (en) |
TW (1) | TWI625273B (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2518893B (en) * | 2013-10-07 | 2018-11-21 | Ge Aviat Systems Ltd | Method for predicting an auxiliary power unit fault |
CA3000595A1 (en) | 2015-09-30 | 2017-04-06 | Bombardier Inc. | Method of and system for presenting an operating status of an aircraft engine |
CN109313069B (en) * | 2016-04-26 | 2021-08-03 | 比勒陀利亚大学 | Method and system for monitoring turbine rotor blades using tip timing (BTT) |
CN106226060B (en) * | 2016-08-30 | 2019-02-05 | 成都飞亚航空设备应用研究所有限公司 | Aircraft auxiliary power plant test macro |
KR20190021640A (en) | 2017-08-23 | 2019-03-06 | 한화에어로스페이스 주식회사 | Inlet guide vane assembly |
CN110510147B (en) * | 2019-08-02 | 2022-11-22 | 西安飞机工业(集团)有限责任公司 | Airplane structure crack detection method |
CN110617115B (en) * | 2019-10-29 | 2021-11-02 | 北京动力机械研究所 | Turbine engine guide ring assembly produced by additive manufacturing mode |
CN111038714B (en) * | 2019-11-28 | 2021-02-26 | 中国航空工业集团公司西安航空计算技术研究所 | Over-rotation detection device and method for auxiliary power device |
CN113291488B (en) * | 2021-04-30 | 2022-01-04 | 浙江长龙航空有限公司 | Method and device for monitoring performance of integral drive generator |
CN116398257B (en) * | 2023-04-12 | 2024-05-03 | 中国航发湖南动力机械研究所 | Aviation turboshaft engine rotor clamping stagnation diagnosis method and system |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6122575A (en) * | 1999-06-30 | 2000-09-19 | Hamilton Sundstrand Corporation | APU troubleshooting system |
JP2005033559A (en) * | 2003-07-14 | 2005-02-03 | Fuji Xerox Co Ltd | Failure diagnostic device |
US7364116B2 (en) * | 2004-09-27 | 2008-04-29 | The Boeing Company | Automatic control systems for aircraft auxiliary power units, and associated methods |
US7693643B2 (en) * | 2005-02-14 | 2010-04-06 | Honeywell International Inc. | Fault detection system and method for turbine engine fuel systems |
US7369932B2 (en) * | 2006-05-04 | 2008-05-06 | Honeywell International, Inc. | System and method for turbine engine fault detection using discrete event system modeling |
US8116932B2 (en) * | 2009-02-25 | 2012-02-14 | GM Global Technology Operations LLC | Auxiliary pump diagnostic systems and methods |
US8471702B2 (en) * | 2010-12-22 | 2013-06-25 | General Electric Company | Method and system for compressor health monitoring |
CN102320382A (en) * | 2011-07-07 | 2012-01-18 | 中国国际航空股份有限公司 | Aircraft performance detection method |
CN102343983A (en) * | 2011-07-07 | 2012-02-08 | 中国国际航空股份有限公司 | Airplane APU (Auxiliary Power Unit) performance detecting method |
CN102416821A (en) * | 2011-07-27 | 2012-04-18 | 中国国际航空股份有限公司 | Aircraft system data processing method |
ITCO20120008A1 (en) * | 2012-03-01 | 2013-09-02 | Nuovo Pignone Srl | METHOD AND SYSTEM FOR MONITORING THE CONDITION OF A GROUP OF PLANTS |
-
2013
- 2013-07-24 CN CN201310313840.9A patent/CN104344946B/en active Active
-
2014
- 2014-07-23 US US14/339,350 patent/US9632010B2/en active Active
- 2014-07-23 CA CA2857748A patent/CA2857748C/en active Active
- 2014-07-24 TW TW103125397A patent/TWI625273B/en active
- 2014-07-24 AU AU2014206179A patent/AU2014206179B2/en active Active
- 2014-07-24 EP EP14178425.6A patent/EP2829688B1/en active Active
- 2014-07-24 KR KR1020140093939A patent/KR101998188B1/en active IP Right Grant
- 2014-07-24 SG SG10201404370SA patent/SG10201404370SA/en unknown
- 2014-07-24 JP JP2014151133A patent/JP6205321B2/en active Active
-
2015
- 2015-03-17 HK HK15102745.7A patent/HK1202330A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
EP2829688A1 (en) | 2015-01-28 |
KR20150012217A (en) | 2015-02-03 |
AU2014206179A1 (en) | 2015-02-12 |
CA2857748A1 (en) | 2015-01-24 |
CN104344946B (en) | 2017-12-05 |
TW201515933A (en) | 2015-05-01 |
CN104344946A (en) | 2015-02-11 |
TWI625273B (en) | 2018-06-01 |
JP2015038348A (en) | 2015-02-26 |
KR101998188B1 (en) | 2019-07-09 |
EP2829688B1 (en) | 2019-01-16 |
AU2014206179B2 (en) | 2017-12-21 |
JP6205321B2 (en) | 2017-09-27 |
US20150068293A1 (en) | 2015-03-12 |
HK1202330A1 (en) | 2015-09-25 |
CA2857748C (en) | 2019-08-20 |
US9632010B2 (en) | 2017-04-25 |
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