JP2003090232A5 - - Google Patents

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Publication number
JP2003090232A5
JP2003090232A5 JP2002140856A JP2002140856A JP2003090232A5 JP 2003090232 A5 JP2003090232 A5 JP 2003090232A5 JP 2002140856 A JP2002140856 A JP 2002140856A JP 2002140856 A JP2002140856 A JP 2002140856A JP 2003090232 A5 JP2003090232 A5 JP 2003090232A5
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JP
Japan
Prior art keywords
data
engine
performance
gas turbine
criteria
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Application number
JP2002140856A
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English (en)
Japanese (ja)
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JP4171610B2 (ja
JP2003090232A (ja
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Priority claimed from US09/861,336 external-priority patent/US6470258B1/en
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Publication of JP2003090232A publication Critical patent/JP2003090232A/ja
Publication of JP2003090232A5 publication Critical patent/JP2003090232A5/ja
Application granted granted Critical
Publication of JP4171610B2 publication Critical patent/JP4171610B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2002140856A 2001-05-18 2002-05-16 エンジン始動装置をモニタするシステム及び方法 Expired - Fee Related JP4171610B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/861,336 US6470258B1 (en) 2001-05-18 2001-05-18 System and method for monitoring engine starting systems
US09/861336 2001-05-18

Publications (3)

Publication Number Publication Date
JP2003090232A JP2003090232A (ja) 2003-03-28
JP2003090232A5 true JP2003090232A5 (https=) 2005-08-25
JP4171610B2 JP4171610B2 (ja) 2008-10-22

Family

ID=25335523

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002140856A Expired - Fee Related JP4171610B2 (ja) 2001-05-18 2002-05-16 エンジン始動装置をモニタするシステム及び方法

Country Status (4)

Country Link
US (1) US6470258B1 (https=)
EP (1) EP1260690B1 (https=)
JP (1) JP4171610B2 (https=)
DE (1) DE60234287D1 (https=)

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US7194866B1 (en) 2003-06-20 2007-03-27 Hamilton Sundstrand Corporation Static structure for an expendable gas turbine engine
US6943699B2 (en) 2003-07-23 2005-09-13 Harris Corporation Wireless engine monitoring system
US8438858B1 (en) 2003-08-20 2013-05-14 Hamilton Sundstrand Corporation Rotational system for an expendable gas turbine engine
US7072797B2 (en) 2003-08-29 2006-07-04 Honeywell International, Inc. Trending system and method using monotonic regression
US7231180B2 (en) * 2004-03-24 2007-06-12 Honeywell International, Inc. Aircraft engine sensor network using wireless sensor communication modules
US7216489B2 (en) * 2004-05-26 2007-05-15 Honeywell International, Inc. System and method for lightoff detection in turbine engines
US7140240B2 (en) * 2004-06-21 2006-11-28 Hamilton Sundstrand Electric engine start system with inspection mode
US7254491B2 (en) * 2004-06-28 2007-08-07 Honeywell International, Inc. Clustering system and method for blade erosion detection
US7506517B2 (en) * 2004-11-23 2009-03-24 Honeywell International, Inc. System and method for turbine engine startup profile characterization
US20060129301A1 (en) * 2004-12-14 2006-06-15 General Electric Company Method and apparatus for assessing gas turbine acceleration capability
US7693643B2 (en) * 2005-02-14 2010-04-06 Honeywell International Inc. Fault detection system and method for turbine engine fuel systems
US7191084B2 (en) * 2005-04-20 2007-03-13 General Electric Company Method and apparatus for gas turbine engine ignition systems
US7577549B2 (en) * 2005-07-18 2009-08-18 General Electric Company System and method for trending exhaust gas temperature in a turbine engine
US7369932B2 (en) * 2006-05-04 2008-05-06 Honeywell International, Inc. System and method for turbine engine fault detection using discrete event system modeling
CN104189968B (zh) 2008-06-26 2017-04-12 甘布罗伦迪亚股份公司 用于处理时间相关的测量信号的方法及装置
US9121769B2 (en) * 2008-08-20 2015-09-01 United Technologies Corporation Sensor and antenna arrangement
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
US8370045B2 (en) * 2009-08-14 2013-02-05 Lockheed Martin Corporation Starter control valve failure prediction machine to predict and trend starter control valve failures in gas turbine engines using a starter control valve health prognostic, program product and related methods
US9053468B2 (en) * 2011-04-07 2015-06-09 General Electric Company Methods and systems for monitoring operation of equipment
US20130212210A1 (en) * 2012-02-10 2013-08-15 General Electric Company Rule engine manager in memory data transfers
FR2998003B1 (fr) * 2012-11-12 2014-11-07 Snecma Procede de surveillance d'une sequence d'allumage d'un moteur de turbomachine
US10309317B2 (en) * 2013-06-21 2019-06-04 Hamilton Sundstrand Corporation Air turbine starter pressure monitor system
GB201313140D0 (en) * 2013-07-23 2013-09-04 Rolls Royce Engine Control Systems Ltd System for performing staging control of a multi-stage combustor
CN104343476B (zh) * 2013-07-24 2016-06-08 中国国际航空股份有限公司 飞机辅助动力单元涡轮效率监控方法和装置
BR112016007478A2 (pt) * 2013-10-07 2017-08-01 Ge Aviat Systems Ltd método para diagnosticar uma falha de unidade auxiliar de potência em uma aeronave
FR3018546B1 (fr) * 2014-03-13 2022-01-21 Snecma Procede de surveillance de l'etat d'un moteur par surveillance des gaz d'echappement
US10553120B2 (en) * 2014-09-15 2020-02-04 L3 Technologies, Inc. Fail safe aircraft monitoring and tracking
US9952612B2 (en) 2015-03-03 2018-04-24 Caterpillar Inc. Power system having zone-based load sharing
WO2017055975A1 (en) 2015-09-30 2017-04-06 Bombardier Inc. Method of and system for presenting an operating status of an aircraft engine
US10454525B2 (en) 2016-06-20 2019-10-22 Ge Aviation Systems Llc Communication of signals over fuel lines in a vehicle
US10587307B2 (en) 2016-06-20 2020-03-10 Ge Aviation Systems, Llc Transmission of power and communication of signals over fuel and hydraulic lines in a vehicle
US10598095B2 (en) 2016-10-11 2020-03-24 Unison Industries, Llc Integrated starter for aerial vehicle
US10266278B2 (en) 2016-10-11 2019-04-23 Unison Industries, Llc Starter issue detection
US20180209295A1 (en) * 2016-10-11 2018-07-26 General Electric Company Starter controller
US11225915B2 (en) 2017-11-16 2022-01-18 General Electric Company Engine core speed reducing method and system
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
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KR102713501B1 (ko) * 2024-02-23 2024-10-02 국방과학연구소 군용 무인항공기의 탑재장비 상태 분석방법 및 장치

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US6498978B2 (en) * 2001-05-18 2002-12-24 General Electric Company System and method for monitoring thermal state to normalize engine trending data

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