JP2002115565A5 - - Google Patents

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Publication number
JP2002115565A5
JP2002115565A5 JP2001228813A JP2001228813A JP2002115565A5 JP 2002115565 A5 JP2002115565 A5 JP 2002115565A5 JP 2001228813 A JP2001228813 A JP 2001228813A JP 2001228813 A JP2001228813 A JP 2001228813A JP 2002115565 A5 JP2002115565 A5 JP 2002115565A5
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JP
Japan
Prior art keywords
engine
trim
aircraft engine
thrust
reference value
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
JP2001228813A
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English (en)
Japanese (ja)
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JP2002115565A (ja
JP4733309B2 (ja
Filing date
Publication date
Priority claimed from US09/629,529 external-priority patent/US6459963B1/en
Application filed filed Critical
Publication of JP2002115565A publication Critical patent/JP2002115565A/ja
Publication of JP2002115565A5 publication Critical patent/JP2002115565A5/ja
Application granted granted Critical
Publication of JP4733309B2 publication Critical patent/JP4733309B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2001228813A 2000-07-31 2001-07-30 エンジン制御システムをトリムする方法及び装置 Expired - Fee Related JP4733309B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/629,529 US6459963B1 (en) 2000-07-31 2000-07-31 Methods and apparatus for trimming engine control systems
US09/629529 2000-07-31

Publications (3)

Publication Number Publication Date
JP2002115565A JP2002115565A (ja) 2002-04-19
JP2002115565A5 true JP2002115565A5 (2) 2008-09-11
JP4733309B2 JP4733309B2 (ja) 2011-07-27

Family

ID=24523381

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001228813A Expired - Fee Related JP4733309B2 (ja) 2000-07-31 2001-07-30 エンジン制御システムをトリムする方法及び装置

Country Status (4)

Country Link
US (1) US6459963B1 (2)
EP (1) EP1178196B1 (2)
JP (1) JP4733309B2 (2)
DE (1) DE60139229D1 (2)

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US20040243284A1 (en) * 2003-05-28 2004-12-02 Caterpillar Inc. Methods and systems for modifying flash files
US7032388B2 (en) * 2003-11-17 2006-04-25 General Electric Company Method and system for incorporating an emission sensor into a gas turbine controller
US20050193739A1 (en) * 2004-03-02 2005-09-08 General Electric Company Model-based control systems and methods for gas turbine engines
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US7752833B2 (en) * 2006-01-10 2010-07-13 General Electric Company Methods and apparatus for gas turbine fuel control
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US20070260424A1 (en) * 2006-05-05 2007-11-08 Harold Brown Methods and apparatus for estimating engine thrust
WO2008097269A2 (en) * 2006-08-01 2008-08-14 Hal Gerard Wick Aircraft engine management for fuel conservation
US7739004B2 (en) * 2006-11-29 2010-06-15 The Boeing Company Automatic engine fuel flow monitoring and alerting fuel leak detection method
US20090226303A1 (en) * 2008-03-05 2009-09-10 Grabowski Zbigniew M Variable area fan nozzle fan flutter management system
US9074531B2 (en) 2008-03-05 2015-07-07 United Technologies Corporation Variable area fan nozzle fan flutter management system
US8381510B2 (en) * 2009-04-30 2013-02-26 General Electric Company Method and systems for controlling engine thrust using variable trim
US8682562B2 (en) * 2009-05-08 2014-03-25 Rolls-Royce Corporation Turbine engine thrust scheduling
WO2010132439A1 (en) 2009-05-12 2010-11-18 Icr Turbine Engine Corporation Gas turbine energy storage and conversion system
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WO2011109514A1 (en) 2010-03-02 2011-09-09 Icr Turbine Engine Corporatin Dispatchable power from a renewable energy facility
US8862433B2 (en) 2010-05-18 2014-10-14 United Technologies Corporation Partitioning of turbomachine faults
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
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US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US8490404B1 (en) 2012-02-28 2013-07-23 General Electric Company Sensor-based performance-seeking gas turbine engine control
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
GB201219815D0 (en) * 2012-11-05 2012-12-19 Rolls Royce Plc Engine control parameter trimming
US9243970B2 (en) 2012-11-30 2016-01-26 Pratt & Whitney Canada Corp. Method and system for integrating gas turbine trim balancing system into electronic engine controls
US10107197B2 (en) * 2012-11-30 2018-10-23 United Technologies Corporation Lubrication system for gas turbine engines
US20140244132A1 (en) * 2013-02-22 2014-08-28 Pratt & Whitney Canada Corp. System and method for 0n-wing engine trim verification
EP2972620B1 (en) 2013-03-15 2020-03-11 Rolls-Royce North American Technologies, Inc. Integrated health management approach to propulsion control system protection limiting
FR3029570B1 (fr) * 2014-12-05 2019-08-30 Safran Aircraft Engines Dispositif et procede de regulation d'un moteur exploitant une mesure de poussee
US10227933B2 (en) * 2015-02-12 2019-03-12 United Technologies Corporation Aircraft power setting trims for life extension
US9771878B2 (en) * 2015-10-19 2017-09-26 General Electric Company Thrust scheduling method for variable pitch fan engines and turbo-shaft, turbo-propeller engines
US10005561B2 (en) 2016-06-16 2018-06-26 Ge Aviation Systems Llc Controlling aircraft using thrust differential trim
US10604268B2 (en) * 2017-02-22 2020-03-31 Pratt & Whitney Canada Corp. Autothrottle control for turboprop engines
WO2019237320A1 (zh) * 2018-06-15 2019-12-19 大连理工大学 一种基于模型预测的航空发动机在线优化及多变量控制设计方法
US11236683B2 (en) * 2018-06-20 2022-02-01 Rolls-Royce Plc Control system
CN113969842B (zh) * 2021-10-22 2022-11-18 清华大学 一种航空发动机推力高动态响应控制方法
US12228085B2 (en) * 2022-10-28 2025-02-18 Pratt & Whitney Canada Corp. System and method for thrust linearization with thrust lever angle
US11821155B1 (en) 2022-11-17 2023-11-21 Frogparking Limited Vehicle barrier gate system

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