JP4619008B2 - 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 - Google Patents

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 Download PDF

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JP4619008B2
JP4619008B2 JP2004006361A JP2004006361A JP4619008B2 JP 4619008 B2 JP4619008 B2 JP 4619008B2 JP 2004006361 A JP2004006361 A JP 2004006361A JP 2004006361 A JP2004006361 A JP 2004006361A JP 4619008 B2 JP4619008 B2 JP 4619008B2
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Prior art keywords
detonation
engine
pulse
gas turbine
tube
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JP2004006361A
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Japanese (ja)
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JP2004220614A (ja
JP2004220614A5 (https=
Inventor
フランクリン・ディー・パーソンズ
トマス・エム・モイニハン
カッタライシェリ・エス・ベンカタラマニ
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General Electric Co
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General Electric Co
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)
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 JP2004220614A5 (https=) 2007-03-01
JP4619008B2 true JP4619008B2 (ja) 2011-01-26

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ID=32655469

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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

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

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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
FR2939508B1 (fr) * 2008-12-09 2011-01-07 Snecma Procede et systeme de correction d'un signal de mesure d'une temperature.
FR2939509B1 (fr) * 2008-12-09 2011-03-04 Snecma Procede et systeme d'estimation d'une temperature de veine dans un turboreacteur.
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
CN117418964B (zh) * 2023-09-21 2026-02-06 中国航发沈阳发动机研究所 一种采用爆震燃烧室的航空发动机及其性能设计方法

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Also Published As

Publication number Publication date
JP2004220614A (ja) 2004-08-05
EP1445464B1 (en) 2016-03-23
US20060282242A1 (en) 2006-12-14
CN100487712C (zh) 2009-05-13
US7200538B2 (en) 2007-04-03
EP1445464A1 (en) 2004-08-11
CN1538341A (zh) 2004-10-20

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