FR2411400A1 - Simulateur de propulsion par moteur a turbine a gaz - Google Patents

Simulateur de propulsion par moteur a turbine a gaz

Info

Publication number
FR2411400A1
FR2411400A1 FR7826068A FR7826068A FR2411400A1 FR 2411400 A1 FR2411400 A1 FR 2411400A1 FR 7826068 A FR7826068 A FR 7826068A FR 7826068 A FR7826068 A FR 7826068A FR 2411400 A1 FR2411400 A1 FR 2411400A1
Authority
FR
France
Prior art keywords
simulated
motor
turbine
air
simulator
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.)
Withdrawn
Application number
FR7826068A
Other languages
English (en)
Inventor
Harrison West
Bobby Ray Delaney
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 FR2411400A1 publication Critical patent/FR2411400A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003—Arrangements for testing or measuring
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Engines (AREA)

Abstract

SIMULATEUR CAPABLE DE REPRODUIRE AVEC PRECISION LES CARACTERISTIQUES AERODYNAMIQUES EN VOL D'UNE GAMME ETENDUE DE MOTEURS. IL COMPREND: UNE ENTREE DE FLUX 42 REDUITE DANS UN RAPPORT D'ECHELLE LINEAIRE PAR RAPPORT A CELLE DU MOTEUR A SIMULER; UN COMPRESSEUR 44 COMPRIMANT UN FLUX D'AIR ISSU DE L'ENTREE A UNE VALEUR EGALE A CELUI DU MOTEUR A SIMULER MULTIPLIE PAR LE CARRE DU FACTEUR D'ECHELLE LINEAIRE; UNE TURBINE 48; UN DISPOSITIF 56 POUR ENVOYER DANS LA TURBINE UN FLUX D'AIR MOTEUR A HAUTE PRESSION PRODUIT A L'EXTERIEUR; UN DISPOSITIF 36 POUR MELANGER UNE PARTIE DE L'AIR MOTEUR DE LA TURBINE AVEC L'AIR MIS EN PRESSION PAR LE COMPRESSEUR, POUR PRODUIRE UN MELANGE POSSEDANT UN PROFIL DE PRESSION D'UN NIVEAU CAPABLE DE PRODUIRE A TRAVERS LE SIMULATEUR UN RAPPORT DE PRESSION PRATIQUEMENT IDENTIQUE A CELUI DU MOTEUR A SIMULER; ET UNE TUYERE 38, DE TAILLE PRATIQUEMENT IDENTIQUE AU PRODUIT DE CELLE DU MOTEUR A SIMULER PAR LE FACTEUR D'ECHELLE LINEAIRE, POUR DECHARGER LE MELANGE SOUS LA FORME D'UN JET PROPULSIF. APPLICATION A L'ETUDE DES MOTEURS A TURBINE A GAZ.
FR7826068A 1977-12-12 1978-09-12 Simulateur de propulsion par moteur a turbine a gaz Withdrawn FR2411400A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/860,032 US4189939A (en) 1977-12-12 1977-12-12 Compact multimission aircraft propulsion simulator

Publications (1)

Publication Number Publication Date
FR2411400A1 true FR2411400A1 (fr) 1979-07-06

Family

ID=25332349

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7826068A Withdrawn FR2411400A1 (fr) 1977-12-12 1978-09-12 Simulateur de propulsion par moteur a turbine a gaz

Country Status (7)

Country Link
US (1) US4189939A (fr)
JP (1) JPS5453494A (fr)
DE (1) DE2839599A1 (fr)
FR (1) FR2411400A1 (fr)
GB (1) GB2009857A (fr)
IT (1) IT1098830B (fr)
SE (1) SE7809544L (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
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GB8901417D0 (en) * 1989-01-23 1989-03-15 Jones Robert D Preparing metal for melt-coating
US7275025B2 (en) * 2000-12-27 2007-09-25 General Electric Company Method and system for analyzing performance of a turbine
JP3757269B2 (ja) * 2001-08-24 2006-03-22 独立行政法人 宇宙航空研究開発機構 回流式超音速風洞における風路内圧力変動低減方法及びその装置
BR0307340B8 (pt) 2002-01-30 2013-02-19 mÉtodo para configurar e operar um aviço para minimizar os efeitos de estampido sânico bem como mÉtodo e veÍculo aeroespacial configurado para reduzir os efeitos de estampido sânico.
US6698684B1 (en) 2002-01-30 2004-03-02 Gulfstream Aerospace Corporation Supersonic aircraft with spike for controlling and reducing sonic boom
US7174797B2 (en) * 2002-10-15 2007-02-13 Florida Turbine Technologies, Inc. High temperature and pressure testing facility
US7574904B1 (en) * 2005-11-01 2009-08-18 Florida Turbine Technologies, Inc. Advanced hot section materials and coatings test rig
JP4846808B2 (ja) 2005-12-15 2011-12-28 ガルフストリーム・エアロスペース・コーポレイション 超音速航空機のための等エントロピー圧縮インレット
FR2902838B1 (fr) * 2006-06-26 2013-03-15 Snecma Cone d'echappement pour la canalisation d'une veine de gaz a l'aval d'une turbine
GB0712980D0 (en) * 2007-07-04 2007-08-15 Rolls Royce Plc Engine performance model
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
DE102008041916B3 (de) * 2008-09-09 2010-01-21 Anecom Aerotest Gmbh Testvorrichtung für den Fan eines Flugzeugtriebwerks
DE102009002184B4 (de) * 2008-10-22 2016-12-29 Airbus Operations Gmbh Aufbau einer Triebwerk-Simulationseinrichtung und Verfahren zur Simulation
NZ601090A (en) * 2009-12-08 2014-05-30 Fusion Hvac Pty Ltd A system and method for delivering air
US8281649B1 (en) 2010-06-11 2012-10-09 Florida Turbine Technologies, Inc. Advanced hot section materials and coatings test rig
US10107204B2 (en) 2013-03-15 2018-10-23 United Technologies Corporation Compact aero-thermo model base point linear system based state estimator
CN103991558B (zh) * 2014-04-17 2016-03-30 中国航空工业集团公司沈阳飞机设计研究所 一种抗干扰力矩模拟器
US9909507B2 (en) 2015-01-27 2018-03-06 General Electric Company Control system for can-to-can variation in combustor system and related method
US9932985B2 (en) 2015-02-03 2018-04-03 Honeywell International Inc. Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereof
US9856796B2 (en) * 2015-12-07 2018-01-02 General Electric Company Application of probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods
US9879612B2 (en) * 2015-12-16 2018-01-30 General Electric Company Combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods
US9879615B2 (en) 2015-12-16 2018-01-30 General Electric Company Machine-specific probabilistic control in gas turbine tuning for power output-emissions parameters, related control systems, computer program products and methods
US9879614B2 (en) 2015-12-16 2018-01-30 General Electric Company Machine-specific combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods
US9882454B2 (en) * 2015-12-16 2018-01-30 General Electric Company Application of combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods
US9856797B2 (en) * 2015-12-16 2018-01-02 General Electric Company Application of combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods
US9879613B2 (en) 2015-12-16 2018-01-30 General Electric Company Application of combined probabilistic control in gas turbine tuning for power output-emissions parameters with scaling factor, related control systems, computer program products and methods
CN112412654B (zh) * 2020-11-05 2022-09-20 中国航发四川燃气涡轮研究院 一种螺杆调节式二元矢量喷管结构及调节方法
US20230112668A1 (en) * 2021-10-11 2023-04-13 Boom Technology, Inc. Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methods
CN115436010B (zh) * 2022-11-08 2023-02-03 中国空气动力研究与发展中心高速空气动力研究所 一种基于后体与喷管一体化设计的喷管推力测量试验方法

Also Published As

Publication number Publication date
IT1098830B (it) 1985-09-18
SE7809544L (sv) 1979-06-13
IT7827417A0 (it) 1978-09-07
JPS5453494A (en) 1979-04-26
DE2839599A1 (de) 1979-06-13
GB2009857A (en) 1979-06-20
US4189939A (en) 1980-02-26

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Legal Events

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