JP2015038346A5 - - Google Patents

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Publication number
JP2015038346A5
JP2015038346A5 JP2014151058A JP2014151058A JP2015038346A5 JP 2015038346 A5 JP2015038346 A5 JP 2015038346A5 JP 2014151058 A JP2014151058 A JP 2014151058A JP 2014151058 A JP2014151058 A JP 2014151058A JP 2015038346 A5 JP2015038346 A5 JP 2015038346A5
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JP
Japan
Prior art keywords
apu
lubricating oil
threshold
decline
period
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JP2014151058A
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English (en)
Japanese (ja)
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JP6205318B2 (ja
JP2015038346A (ja
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Priority claimed from CN201310313876.7A external-priority patent/CN104340369B/zh
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Publication of JP2015038346A5 publication Critical patent/JP2015038346A5/ja
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JP2014151058A 2013-07-24 2014-07-24 飛行機の補助動力単元の潤滑油冷却器の性能の監視方法 Active JP6205318B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201310313876.7 2013-07-24
CN201310313876.7A CN104340369B (zh) 2013-07-24 2013-07-24 飞机辅助动力单元滑油冷却器性能监控方法及装置

Publications (3)

Publication Number Publication Date
JP2015038346A JP2015038346A (ja) 2015-02-26
JP2015038346A5 true JP2015038346A5 (enExample) 2017-08-10
JP6205318B2 JP6205318B2 (ja) 2017-09-27

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JP2014151058A Active JP6205318B2 (ja) 2013-07-24 2014-07-24 飛行機の補助動力単元の潤滑油冷却器の性能の監視方法

Country Status (9)

Country Link
US (1) US9689311B2 (enExample)
EP (1) EP2829696B1 (enExample)
JP (1) JP6205318B2 (enExample)
KR (1) KR102003896B1 (enExample)
CN (1) CN104340369B (enExample)
AU (1) AU2014206180B2 (enExample)
CA (1) CA2857795C (enExample)
SG (1) SG10201404347SA (enExample)
TW (1) TWI619645B (enExample)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106741978B (zh) * 2016-12-30 2023-09-29 重庆驼航科技有限公司 一种直升机用一体化复合式冷却系统
US10082243B1 (en) 2017-06-13 2018-09-25 Pratt & Whitney Canada Corp. Method and system for inlet blockage detection
CN109738195B (zh) * 2018-12-28 2020-12-08 成都国营锦江机器厂 Safir辅助动力装置起动试验模拟器及控制方法
TWI841671B (zh) * 2019-01-24 2024-05-11 日商第一三共股份有限公司 具有取代基之脲化合物
US11518545B2 (en) * 2019-04-17 2022-12-06 The Boeing Company Supplemental cooling unit prediction system
CN111056024B (zh) * 2019-11-25 2022-07-19 中国南方航空股份有限公司 一种飞机辅助动力单元运行状态监控装置
CN110925096A (zh) * 2019-12-05 2020-03-27 中国航发四川燃气涡轮研究院 一种发动机滑油冷却系统
US11551484B2 (en) 2020-02-07 2023-01-10 The Boeing Company Vapor cycle machine management system
CN113311886A (zh) * 2021-04-26 2021-08-27 中国船舶重工集团公司第七0三研究所 一种自适应滑油温度控制方法
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
CN113624505B (zh) * 2021-08-24 2022-10-28 中国航发湖南动力机械研究所 一种压气机出口流场模拟装置
CN115200883A (zh) * 2022-05-12 2022-10-18 观典防务技术股份有限公司 一种监测无人机发动机熄火控制装置
CN118733086A (zh) * 2024-06-27 2024-10-01 大卓智能科技有限公司 车辆ota软件升级系统、车辆及控制方法
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
CN119756873B (zh) * 2024-12-03 2025-10-21 中国航发沈阳发动机研究所 一种航空发动机空气滑油散热器故障监测方法
CN119717936B (zh) * 2024-12-06 2025-08-12 中维化纤股份有限公司 一种熔体输送过程的工艺参数优化方法
CN120141639B (zh) * 2025-05-16 2025-09-16 洛阳乾禾仪器有限公司 一种基于人工智能的光纤振动传感器运行性能监测系统

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5343778A (en) * 1992-11-09 1994-09-06 Alliedsignal Inc. Multifunction secondary power system
US6470735B1 (en) 2000-02-22 2002-10-29 Meritor Heavy Vehicle Systems, Llc Simple driveline condition sensing system
US7168254B2 (en) * 2004-02-17 2007-01-30 Honeywell International Inc. Control logic for fuel controls on APUs
US7062370B2 (en) * 2004-03-30 2006-06-13 Honeywell International Inc. Model-based detection, diagnosis of turbine engine faults
US7693643B2 (en) * 2005-02-14 2010-04-06 Honeywell International Inc. Fault detection system and method for turbine engine fuel systems
US7805947B2 (en) * 2005-05-19 2010-10-05 Djamal Moulebhar Aircraft with disengageable engine and auxiliary power unit components
US7369932B2 (en) * 2006-05-04 2008-05-06 Honeywell International, Inc. System and method for turbine engine fault detection using discrete event system modeling
US8532865B2 (en) * 2007-08-09 2013-09-10 Hitachi Construction Machinery Co., Ltd. Apparatus and system for diagnosing devices included in working machine
US20090048730A1 (en) * 2007-08-17 2009-02-19 General Electric Company Method and system for planning repair of an engine
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
US20120312023A1 (en) * 2011-06-08 2012-12-13 Honeywell International Inc. Thermal management systems and methods for auxiliary power units
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
US10094292B2 (en) * 2012-03-02 2018-10-09 Hamilton Sundstrand Corporation Method of acceleration control during APU starting
CN104345273B (zh) * 2013-07-24 2017-11-24 中国国际航空股份有限公司 飞机辅助动力单元起动机性能检测方法和装置
CN104348670B (zh) * 2013-07-24 2018-01-30 中国国际航空股份有限公司 飞机辅助动力单元燃油组件性能检测方法和装置

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