JP2004220614A5 - - Google Patents

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Publication number
JP2004220614A5
JP2004220614A5 JP2004006361A JP2004006361A JP2004220614A5 JP 2004220614 A5 JP2004220614 A5 JP 2004220614A5 JP 2004006361 A JP2004006361 A JP 2004006361A JP 2004006361 A JP2004006361 A JP 2004006361A JP 2004220614 A5 JP2004220614 A5 JP 2004220614A5
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JP
Japan
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JP2004006361A
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JP4619008B2 (ja
JP2004220614A (ja
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Priority claimed from US10/342,931 external-priority patent/US7200538B2/en
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Publication of JP2004220614A publication Critical patent/JP2004220614A/ja
Publication of JP2004220614A5 publication Critical patent/JP2004220614A5/ja
Application granted granted Critical
Publication of JP4619008B2 publication Critical patent/JP4619008B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2004006361A 2003-01-15 2004-01-14 ガスタービンエンジンをモデリングするための方法及び装置 Expired - Fee Related JP4619008B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/342,931 US7200538B2 (en) 2003-01-15 2003-01-15 Methods and apparatus for modeling gas turbine engines

Publications (3)

Publication Number Publication Date
JP2004220614A JP2004220614A (ja) 2004-08-05
JP2004220614A5 true JP2004220614A5 (ja) 2007-03-01
JP4619008B2 JP4619008B2 (ja) 2011-01-26

Family

ID=32655469

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2004006361A Expired - Fee Related JP4619008B2 (ja) 2003-01-15 2004-01-14 ガスタービンエンジンをモデリングするための方法及び装置

Country Status (4)

Country Link
US (1) US7200538B2 (ja)
EP (1) EP1445464B1 (ja)
JP (1) JP4619008B2 (ja)
CN (1) CN100487712C (ja)

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CN101303702B (zh) * 2007-05-09 2011-07-06 通用汽车环球科技运作公司 发动机快速台试及建模法
US7681440B2 (en) * 2007-10-31 2010-03-23 Pratt & Whitney Canada Corp. Method and apparatus for turbine engine dynamic characterization
US8457936B2 (en) * 2008-11-24 2013-06-04 Honeywell International Inc. Apparatus and methods for simulating a system steady state devoid of performing full transient operating conditions
FR2939509B1 (fr) * 2008-12-09 2011-03-04 Snecma Procede et systeme d'estimation d'une temperature de veine dans un turboreacteur.
FR2939508B1 (fr) * 2008-12-09 2011-01-07 Snecma Procede et systeme de correction d'un signal de mesure d'une temperature.
US20110047962A1 (en) * 2009-08-28 2011-03-03 General Electric Company Pulse detonation combustor configuration for deflagration to detonation transition enhancement
GB0921660D0 (en) * 2009-12-10 2010-01-27 Zettner Michael Method for increasing the efficiency of a heat exchanger
CN101806260B (zh) * 2010-03-04 2012-01-11 西北工业大学 一种多管并联脉冲爆震燃烧室及其点火起爆方法
US9140456B2 (en) * 2011-12-01 2015-09-22 General Electric Company Variable initiation location system for pulse detonation combustor
US9718562B1 (en) * 2016-01-29 2017-08-01 General Electric Company System and method of evaluating the effect of dust on aircraft engines
WO2017194240A1 (de) * 2016-05-13 2017-11-16 Siemens Aktiengesellschaft Verfahren und system zur bestimmung von zustandsgrössen eines betriebsfluids
CN107945615A (zh) * 2017-12-08 2018-04-20 中国航空工业集团公司成都飞机设计研究所 一种实时仿真模拟发动机的方法

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