IT7827417A0 - Simulatore di propulsione compatto per areoplano multimissione. - Google Patents

Simulatore di propulsione compatto per areoplano multimissione.

Info

Publication number
IT7827417A0
IT7827417A0 IT7827417A IT2741778A IT7827417A0 IT 7827417 A0 IT7827417 A0 IT 7827417A0 IT 7827417 A IT7827417 A IT 7827417A IT 2741778 A IT2741778 A IT 2741778A IT 7827417 A0 IT7827417 A0 IT 7827417A0
Authority
IT
Italy
Prior art keywords
mission aircraft
simulator
compact propulsion
propulsion simulator
compact
Prior art date
Application number
IT7827417A
Other languages
English (en)
Other versions
IT1098830B (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT7827417A0 publication Critical patent/IT7827417A0/it
Application granted granted Critical
Publication of IT1098830B publication Critical patent/IT1098830B/it

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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Engines (AREA)
IT27417/78A 1977-12-12 1978-09-07 Simulatore di propulsione compatto per areoplano multimissione IT1098830B (it)

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 (2)

Publication Number Publication Date
IT7827417A0 true IT7827417A0 (it) 1978-09-07
IT1098830B IT1098830B (it) 1985-09-18

Family

ID=25332349

Family Applications (1)

Application Number Title Priority Date Filing Date
IT27417/78A IT1098830B (it) 1977-12-12 1978-09-07 Simulatore di propulsione compatto per areoplano multimissione

Country Status (7)

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

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CA3071172A1 (en) * 2005-12-15 2008-04-17 Gulfstream Aerospace Corporation Isentropic compression inlet for supersonic aircraft
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
EP2510289A4 (en) * 2009-12-08 2018-03-21 Fusion HVAC Pty Limited 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
US10480416B2 (en) 2013-03-15 2019-11-19 United Technologies Corporation Compact aero-thermo model based control system estimator starting algorithm
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
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
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
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
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
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
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
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
US12162618B2 (en) * 2021-10-11 2024-12-10 Boom Technology, Inc. Dissimilarly shaped aircraft nozzles with tandem mixing devices, and associated systems and methods
CN114720086A (zh) * 2022-04-06 2022-07-08 付柏山 一种涡轮动力模拟器
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
DE2839599A1 (de) 1979-06-13
FR2411400A1 (fr) 1979-07-06
US4189939A (en) 1980-02-26
IT1098830B (it) 1985-09-18
SE7809544L (sv) 1979-06-13
JPS5453494A (en) 1979-04-26
GB2009857A (en) 1979-06-20

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