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 jam

Info

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
Application number
SG10201404370SA
Inventor
Huifeng Ding
Zhuping Gu
Qihe Yue
Lei Chen
Jiaju Wu
Hailong Zhang
Fengliang Zheng
Lei Huang
Original Assignee
Air China Ltd
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 Air China Ltd filed Critical Air China Ltd
Publication of SG10201404370SA publication Critical patent/SG10201404370SA/en

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M15/00Testing of engines
    • G01M15/14Testing gas-turbine engines or jet-propulsion engines
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60Testing or inspecting aircraft components or systems
    • 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
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N25/00Investigating or analyzing materials by the use of thermal means
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring
    • G05B23/0205Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
    • G05B23/0218Electric 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
    • G05B23/0224Process history based detection method, e.g. whereby history implies the availability of large amounts of data
    • G05B23/0227Qualitative 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
    • G05B23/0235Qualitative 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
    • 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
    • F05D2220/00Application
    • F05D2220/50Application for auxiliary power units (APU's)
    • 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
    • F05D2270/40Type of control system
    • F05D2270/44Type of control system active, predictive, or anticipative
SG10201404370SA 2013-07-24 2014-07-24 Method and device for monitoring the malfunction of apu turbine vane fracture and rotor shaft jam SG10201404370SA (en)

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)

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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)

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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

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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