AU2014206179B2 - 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
AU2014206179B2
AU2014206179B2 AU2014206179A AU2014206179A AU2014206179B2 AU 2014206179 B2 AU2014206179 B2 AU 2014206179B2 AU 2014206179 A AU2014206179 A AU 2014206179A AU 2014206179 A AU2014206179 A AU 2014206179A AU 2014206179 B2 AU2014206179 B2 AU 2014206179B2
Authority
AU
Australia
Prior art keywords
apu
malfunction
phase
turbine vane
start time
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.)
Active
Application number
AU2014206179A
Other languages
English (en)
Other versions
AU2014206179A1 (en
Inventor
Lei Chen
Huifeng Ding
Zhuping Gu
Lei Huang
Jiaju Wu
Qihe YUE
Hailong Zhang
Fengliang Zheng
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.)
Air China Ltd
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 AU2014206179A1 publication Critical patent/AU2014206179A1/en
Application granted granted Critical
Publication of AU2014206179B2 publication Critical patent/AU2014206179B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Analytical Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Control Of Turbines (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
AU2014206179A 2013-07-24 2014-07-24 Method and device for monitoring the malfunction of APU turbine vane fracture and rotor shaft jam Active AU2014206179B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201310313840.9A CN104344946B (zh) 2013-07-24 2013-07-24 Apu涡轮叶片断裂与转轴卡阻故障的监控方法和装置
CN201310313840.9 2013-07-24

Publications (2)

Publication Number Publication Date
AU2014206179A1 AU2014206179A1 (en) 2015-02-12
AU2014206179B2 true AU2014206179B2 (en) 2017-12-21

Family

ID=51224787

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2014206179A Active AU2014206179B2 (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 (9)

Country Link
US (1) US9632010B2 (enExample)
EP (1) EP2829688B1 (enExample)
JP (1) JP6205321B2 (enExample)
KR (1) KR101998188B1 (enExample)
CN (1) CN104344946B (enExample)
AU (1) AU2014206179B2 (enExample)
CA (1) CA2857748C (enExample)
SG (1) SG10201404370SA (enExample)
TW (1) TWI625273B (enExample)

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* Cited by examiner, † Cited by third party
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
WO2017055975A1 (en) 2015-09-30 2017-04-06 Bombardier Inc. Method of and system for presenting an operating status of an aircraft engine
US10895496B2 (en) * 2016-04-26 2021-01-19 University Of Pretoria Method and system for monitoring rotor blades of a turbomachine using blade tip timing (BTT)
CN106226060B (zh) * 2016-08-30 2019-02-05 成都飞亚航空设备应用研究所有限公司 飞机辅助动力装置测试系统
KR20190021640A (ko) 2017-08-23 2019-03-06 한화에어로스페이스 주식회사 인렛 가이드 베인 어셈블리
CN110510147B (zh) * 2019-08-02 2022-11-22 西安飞机工业（集团）有限责任公司 一种飞机结构裂纹检测方法
CN110617115B (zh) * 2019-10-29 2021-11-02 北京动力机械研究所 利用增材制造方式生产的涡轮发动机导流环组件
CN111038714B (zh) * 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 一种辅助动力装置超转检测装置及方法
CN113291488B (zh) * 2021-04-30 2022-01-04 浙江长龙航空有限公司 一种整体驱动发电机性能监控方法及装置
US12394252B2 (en) 2022-02-11 2025-08-19 Honeywell International Inc. Prognostic and health monitoring system for a device with a rotating component
CN114859845A (zh) * 2022-06-09 2022-08-05 中用科技有限公司 基于物联网控制器的智能工业数据管理系统
CN115610642A (zh) * 2022-10-17 2023-01-17 中国商用飞机有限责任公司 用于飞行器的舵面卡阻装置以及舵面卡阻测试方法和系统
CN115523179B (zh) * 2022-10-21 2025-07-04 宁波方太厨具有限公司 水泵及其卡死修复方法
CN115539431B (zh) * 2022-10-21 2025-08-12 宁波方太厨具有限公司 水泵
CN116398257B (zh) * 2023-04-12 2024-05-03 中国航发湖南动力机械研究所 一种航空涡轴发动机转子卡滞诊断方法及系统
CN116899164B (zh) * 2023-06-14 2025-10-28 湘潭大学 具有监测告警功能的消防供水软管及其监测告警方法
CN118424686B (zh) * 2024-05-21 2024-11-22 长江大学 涡轮性能测试装置及测试方法

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US20060195248A1 (en) * 2005-02-14 2006-08-31 Honeywell International, Inc. Fault detection system and method for turbine engine fuel systems
US20130179028A1 (en) * 2011-07-07 2013-07-11 Air China Limited Method for detecting whether performance of aircraft components is in the deterioration period

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US6122575A (en) * 1999-06-30 2000-09-19 Hamilton Sundstrand Corporation APU troubleshooting system
JP2005033559A (ja) * 2003-07-14 2005-02-03 Fuji Xerox Co Ltd 故障診断装置
US7364116B2 (en) * 2004-09-27 2008-04-29 The Boeing Company Automatic control systems for aircraft auxiliary power units, and associated methods
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
CN102343983A (zh) * 2011-07-07 2012-02-08 中国国际航空股份有限公司 飞机apu性能检测方法
CN102416821A (zh) * 2011-07-27 2012-04-18 中国国际航空股份有限公司 飞机系统数据处理方法
ITCO20120008A1 (it) * 2012-03-01 2013-09-02 Nuovo Pignone Srl Metodo e sistema per monitorare la condizione di un gruppo di impianti

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Publication number Priority date Publication date Assignee Title
US20060195248A1 (en) * 2005-02-14 2006-08-31 Honeywell International, Inc. Fault detection system and method for turbine engine fuel systems
US20130179028A1 (en) * 2011-07-07 2013-07-11 Air China Limited Method for detecting whether performance of aircraft components is in the deterioration period

Also Published As

Publication number Publication date
TWI625273B (zh) 2018-06-01
TW201515933A (zh) 2015-05-01
EP2829688A1 (en) 2015-01-28
SG10201404370SA (en) 2015-02-27
KR20150012217A (ko) 2015-02-03
AU2014206179A1 (en) 2015-02-12
KR101998188B1 (ko) 2019-07-09
JP2015038348A (ja) 2015-02-26
CN104344946B (zh) 2017-12-05
CA2857748C (en) 2019-08-20
JP6205321B2 (ja) 2017-09-27
US9632010B2 (en) 2017-04-25
CN104344946A (zh) 2015-02-11
HK1202330A1 (en) 2015-09-25
CA2857748A1 (en) 2015-01-24
EP2829688B1 (en) 2019-01-16
US20150068293A1 (en) 2015-03-12

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