CN100487712C - 用于模拟燃气涡轮发动机的方法和装置 - Google Patents

用于模拟燃气涡轮发动机的方法和装置 Download PDF

Info

Publication number
CN100487712C
CN100487712C CNB2004100067046A CN200410006704A CN100487712C CN 100487712 C CN100487712 C CN 100487712C CN B2004100067046 A CNB2004100067046 A CN B2004100067046A CN 200410006704 A CN200410006704 A CN 200410006704A CN 100487712 C CN100487712 C CN 100487712C
Authority
CN
China
Prior art keywords
deflagration
pulse
engine
processor
simulation system
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.)
Expired - Fee Related
Application number
CNB2004100067046A
Other languages
English (en)
Chinese (zh)
Other versions
CN1538341A (zh
Inventor
F·D·帕森斯
T·M·莫伊尼汗
K·S·文卡塔马尼
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN1538341A publication Critical patent/CN1538341A/zh
Application granted granted Critical
Publication of CN100487712C publication Critical patent/CN100487712C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Classifications

    • 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

Landscapes

  • 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)
CNB2004100067046A 2003-01-15 2004-01-15 用于模拟燃气涡轮发动机的方法和装置 Expired - Fee Related CN100487712C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/342931 2003-01-15
US10/342,931 US7200538B2 (en) 2003-01-15 2003-01-15 Methods and apparatus for modeling gas turbine engines

Publications (2)

Publication Number Publication Date
CN1538341A CN1538341A (zh) 2004-10-20
CN100487712C true CN100487712C (zh) 2009-05-13

Family

ID=32655469

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2004100067046A Expired - Fee Related CN100487712C (zh) 2003-01-15 2004-01-15 用于模拟燃气涡轮发动机的方法和装置

Country Status (4)

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

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7610179B2 (en) * 2004-09-24 2009-10-27 United Technologies Corporation Coupled parametric design of flow control and duct shape
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
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

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
DE2046079B1 (de) 1970-09-18 1971-12-23 Messerschmitt Bolkow Blohm GmbH, 8000 München Luftatmendes strahlrohr
US4215412A (en) * 1978-07-13 1980-07-29 The Boeing Company Real time performance monitoring of gas turbine engines
ES8800981A1 (es) 1985-06-28 1987-12-01 Univ Minnesota Un procedimiento para tratar celulas efectoras que tienen receptores de superficie para la region fc de un anticuerpo
GB8927377D0 (en) * 1989-12-04 1990-01-31 Univ Edinburgh Improvements in and relating to amperometric assays
US5694768A (en) * 1990-02-23 1997-12-09 General Electric Company Variable cycle turbofan-ramjet engine
US5080496A (en) * 1990-06-25 1992-01-14 General Electric Company Method and apparatus for compensated temperature prediction
US5280756A (en) * 1992-02-04 1994-01-25 Stone & Webster Engineering Corp. NOx Emissions advisor and automation system
US5402333A (en) * 1992-06-15 1995-03-28 E. I. Du Pont De Nemours & Co., Inc. System and method for improving model product property estimates
JP3196390B2 (ja) * 1992-12-25 2001-08-06 富士電機株式会社 パラメータ同定器
US5873240A (en) * 1993-04-14 1999-02-23 Adroit Systems, Inc. Pulsed detonation rocket engine
US5345758A (en) 1993-04-14 1994-09-13 Adroit Systems, Inc. Rotary valve multiple combustor pulse detonation engine
US5726891A (en) * 1994-01-26 1998-03-10 Sisson; Patterson B. Surge detection system using engine signature
US5689066A (en) * 1995-08-15 1997-11-18 Stevenson; Dennis B. Method and apparatus for analyzing gas turbine pneumatic fuel system
GB2321720A (en) 1997-02-04 1998-08-05 Secr Defence Modelling a system with more parameters than sensors
US5983624A (en) * 1997-04-21 1999-11-16 Anderson; J. Hilbert Power plant having a U-shaped combustion chamber with first and second reflecting surfaces
US7020595B1 (en) * 1999-11-26 2006-03-28 General Electric Company Methods and apparatus for model based diagnostics
US6442930B1 (en) * 2000-03-31 2002-09-03 General Electric Company Combined cycle pulse detonation turbine engine
US6477829B1 (en) * 2000-05-09 2002-11-12 Lockheed Martin Corporation Combined cycle pulse combustion/gas turbine engine
US6582183B2 (en) * 2000-06-30 2003-06-24 United Technologies Corporation Method and system of flutter control for rotary compression systems
GB0027288D0 (en) * 2000-11-08 2000-12-27 Rolls Royce Plc Overthrust protection system and method
US6505462B2 (en) * 2001-03-29 2003-01-14 General Electric Company Rotary valve for pulse detonation engines
US6457938B1 (en) * 2001-03-30 2002-10-01 General Electric Company Wide angle guide vane
US20020177985A1 (en) * 2001-04-23 2002-11-28 Kraft Joseph Anthony Computer system and method for radial cooled bucket optimization
KR20030053596A (ko) * 2001-12-22 2003-07-02 남궁영 피스톤 압축형 터빈기관 및 이의 제어방법
US7296411B2 (en) * 2002-06-21 2007-11-20 Darko Segota Method and system for regulating internal fluid flow within an enclosed or semi-enclosed environment
US6782703B2 (en) * 2002-09-11 2004-08-31 Siemens Westinghouse Power Corporation Apparatus for starting a combined cycle power plant
US6796123B2 (en) * 2002-11-01 2004-09-28 George Lasker Uncoupled, thermal-compressor, gas-turbine engine

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
爆震波在爆震燃烧室内传播过程的数值模拟. 何立明，严传俊，范玮，王建峰.推进技术，第19卷第6期. 1998 *
脉冲爆震发动机基本尺寸的确定. 范玮，严传俊，汪林全，张群，黄希桥.西北工业大学学报，第20卷第2期. 2002 *

Also Published As

Publication number Publication date
JP2004220614A (ja) 2004-08-05
EP1445464B1 (en) 2016-03-23
US20060282242A1 (en) 2006-12-14
US7200538B2 (en) 2007-04-03
EP1445464A1 (en) 2004-08-11
CN1538341A (zh) 2004-10-20
JP4619008B2 (ja) 2011-01-26

Similar Documents

Publication Publication Date Title
CN100487712C (zh) 用于模拟燃气涡轮发动机的方法和装置
Sousa et al. Thermodynamic analysis of a gas turbine engine with a rotating detonation combustor
Seldner Generalized simulation technique for turbojet engine system analysis
Mark et al. Design and analysis of annular combustion chamber of a low bypass turbofan engine in a jet trainer aircraft
Lolis Development of a preliminary weight estimation method for advanced turbofan engines
Grönstedt et al. First and second law analysis of future aircraft engines
Duran et al. Combustion noise in modern aero-engines
Gobran Off-design performance of solar Centaur-40 gas turbine engine using Simulink
Pellegrini et al. On the performance simulation of inter-stage turbine reheat
Perkins et al. Summary of pressure gain combustion research at NASA
Turan Energy and entropy analyses of an experimental turbojet engine for target drone application
Carter et al. The development of an NPSS engine cycle model to match engine cycle data, using a multi-design-point method
Yarlagadda Performance analysis of J85 turbojet engine matching thrust with reduced inlet pressure to the compressor
Bennett et al. An Approach to Evaluating the Impact of Small-core Turbofan Technologies on Engine and Aircraft Performance
Khalid Role of dynamic simulation in fighter engine design and development
Kishalov et al. Modeling and computer-aided design of combustion chambers for aircraft engines and gas turbine plants using an expert system
Dewanji et al. Feasibility study of some novel concepts for high bypass ratio turbofan engines
Eidelman et al. Pulsed detonation engine: Key issues
Sanghi et al. Preliminary estimation of engine gas-flow-path size and weight
Gro¨ nstedt et al. Low-pressure system component advancements and its influence on future turbofan engine emissions
Arif et al. Analytical modelling and validation of a turbofan engine at design conditions
Smith et al. Numerical simulation of enhanced mixing in jet plumes using pulsed blowing
Pakanati et al. High fidelity engine performance models for windmill relight predictions
Kavvalos et al. On the Performance of Common-Core Turboprops
Davis Jr A Post-Stall Compression System Modeling Technique

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090513

Termination date: 20170115