JP2015025451A5 - - Google Patents

Download PDF

Info

Publication number
JP2015025451A5
JP2015025451A5 JP2014151067A JP2014151067A JP2015025451A5 JP 2015025451 A5 JP2015025451 A5 JP 2015025451A5 JP 2014151067 A JP2014151067 A JP 2014151067A JP 2014151067 A JP2014151067 A JP 2014151067A JP 2015025451 A5 JP2015025451 A5 JP 2015025451A5
Authority
JP
Japan
Prior art keywords
apu
period
threshold
turbine efficiency
npa
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
JP2014151067A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015025451A (ja
JP6205319B2 (ja
Filing date
Publication date
Priority claimed from CN201310313879.0A external-priority patent/CN104343476B/zh
Application filed filed Critical
Publication of JP2015025451A publication Critical patent/JP2015025451A/ja
Publication of JP2015025451A5 publication Critical patent/JP2015025451A5/ja
Application granted granted Critical
Publication of JP6205319B2 publication Critical patent/JP6205319B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2014151067A 2013-07-24 2014-07-24 飛行機の補助動力単元のタービン効率の監視方法と装置 Active JP6205319B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201310313879.0 2013-07-24
CN201310313879.0A CN104343476B (zh) 2013-07-24 2013-07-24 飞机辅助动力单元涡轮效率监控方法和装置

Publications (3)

Publication Number Publication Date
JP2015025451A JP2015025451A (ja) 2015-02-05
JP2015025451A5 true JP2015025451A5 (enExample) 2017-08-31
JP6205319B2 JP6205319B2 (ja) 2017-09-27

Family

ID=51224788

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014151067A Active JP6205319B2 (ja) 2013-07-24 2014-07-24 飛行機の補助動力単元のタービン効率の監視方法と装置

Country Status (9)

Country Link
US (1) US9696239B2 (enExample)
EP (1) EP2829686B1 (enExample)
JP (1) JP6205319B2 (enExample)
KR (1) KR101998187B1 (enExample)
CN (1) CN104343476B (enExample)
AU (1) AU2014206182B2 (enExample)
CA (1) CA2857787C (enExample)
SG (1) SG10201404368YA (enExample)
TW (1) TWI625271B (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014005070A1 (en) * 2012-06-28 2014-01-03 Alaska Airlines, Inc. Robust systems and methods for improving passenger jet aircraft fuel economy
CN105114977B (zh) * 2015-09-02 2017-05-24 哈尔滨工业大学 一种基于排温测点相关性的燃机燃烧系统在线监测方法
CN110341986B (zh) * 2019-07-16 2021-07-20 哈尔滨工业大学 基于rbm优化elm的飞机辅助动力装置性能参数多步预测方法
CN111693180B (zh) * 2020-05-27 2021-07-23 中国航空工业集团公司西安航空计算技术研究所 一种辅助动力系统排气温度超温故障检测方法
CN119429157B (zh) * 2024-11-13 2025-11-25 中国南方航空股份有限公司 一种航空滑油冷却器的维护方法、系统、设备和介质
CN120793187B (zh) * 2025-09-02 2025-11-11 商飞软件有限公司 一种民用辅助动力装置转速综合控制方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6466858B1 (en) * 2000-11-02 2002-10-15 General Electric Company Methods and apparatus for monitoring gas turbine engine operation
US6470258B1 (en) * 2001-05-18 2002-10-22 General Electric Company System and method for monitoring engine starting systems
US7487029B2 (en) * 2004-05-21 2009-02-03 Pratt & Whitney Canada Method of monitoring gas turbine engine operation
US7506517B2 (en) 2004-11-23 2009-03-24 Honeywell International, Inc. System and method for turbine engine startup profile characterization
US7369932B2 (en) 2006-05-04 2008-05-06 Honeywell International, Inc. System and method for turbine engine fault detection using discrete event system modeling
US8467949B2 (en) 2009-05-29 2013-06-18 Honeywell International Inc. Methods and systems for turbine line replaceable unit fault detection and isolation during engine startup
CN102095572A (zh) * 2010-12-06 2011-06-15 广州市熠芯节能服务有限公司 基于标杆产品比对的产品性能测试方法
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
CN102320382A (zh) 2011-07-07 2012-01-18 中国国际航空股份有限公司 飞机性能检测方法
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

Similar Documents

Publication Publication Date Title
JP2015025451A5 (enExample)
JP2015038347A5 (enExample)
He et al. Developments and thoughts on operational reliability assessment of mechanical equipment
Shah et al. The implementation of an IoT-based flood alert system
EP3557819A8 (en) Server failure detection method and system
WO2017185796A1 (zh) 一种温度预测方法及电子体温计
JP2013019413A5 (enExample)
WO2019165743A1 (zh) 确定对风角度偏差及修正对风角度的方法、装置和系统
CN105067262A (zh) 一种滚动轴承状态监测方法
KR20180137513A (ko) 감시 장치, 대상 장치의 감시 방법 및 프로그램
JP2015138864A5 (enExample)
CN111684314A (zh) 气象预测校正方法以及气象预测系统
CN107152376B (zh) 停止桨叶顺桨的方法及系统
CN108872666B (zh) 一种负载开关事件检测方法及系统
CN105277886A (zh) 一种蓄电池的剩余寿命的检测方法和装置
US11237547B2 (en) Information processing device, information processing method, and program
CN110848024A (zh) 一种发动机增压系统故障监测方法及装置
CN110762771B (zh) 一种空调外机共振控制方法、装置及空调器
JP2016201921A (ja) 太陽光発電設備の発電量の低下を検出する方法、装置、およびプログラム
CN110824361B (zh) 风电机组超级电容剩余寿命计算方法、装置、设备及介质
CN104242245B (zh) 发电机失步保护方法和装置
CN109085423B (zh) 一种负载开关事件检测方法及系统
CN103569191A (zh) 电动式动力转向器控制温度值计算装置及方法和控制系统
CN110501129B (zh) 井架的振动检测方法、设备及终端设备
JP2015038345A5 (enExample)