IT1098830B - Simulatore di propulsione compatto per areoplano multimissione - Google Patents
Simulatore di propulsione compatto per areoplano multimissioneInfo
- Publication number
- IT1098830B IT1098830B IT27417/78A IT2741778A IT1098830B IT 1098830 B IT1098830 B IT 1098830B IT 27417/78 A IT27417/78 A IT 27417/78A IT 2741778 A IT2741778 A IT 2741778A IT 1098830 B IT1098830 B IT 1098830B
- Authority
- IT
- Italy
- Prior art keywords
- areoplan
- multimission
- simulator
- compact propulsion
- propulsion simulator
- Prior art date
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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Testing Of Engines (AREA)
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 IT7827417A0 (it) | 1978-09-07 |
IT1098830B true 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 (29)
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 |
WO2003064254A2 (en) * | 2002-01-30 | 2003-08-07 | Gulfstream Aerospace Corporation | Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom |
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 |
EP1960266B1 (en) | 2005-12-15 | 2019-02-20 | 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 |
AU2010330689B2 (en) * | 2009-12-08 | 2016-02-25 | 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 |
JP6466398B2 (ja) | 2013-03-15 | 2019-02-06 | ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation | コンパクトな空力熱モデルのリアルタイム線形化を用いた状態推定器 |
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 |
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 |
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 |
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 |
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 |
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 |
WO2023064215A1 (en) * | 2021-10-11 | 2023-04-20 | 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 |
-
1977
- 1977-12-12 US US05/860,032 patent/US4189939A/en not_active Expired - Lifetime
-
1978
- 1978-09-01 GB GB7835242A patent/GB2009857A/en not_active Withdrawn
- 1978-09-07 IT IT27417/78A patent/IT1098830B/it active
- 1978-09-11 SE SE7809544A patent/SE7809544L/xx unknown
- 1978-09-12 DE DE19782839599 patent/DE2839599A1/de not_active Withdrawn
- 1978-09-12 FR FR7826068A patent/FR2411400A1/fr not_active Withdrawn
- 1978-09-12 JP JP11136778A patent/JPS5453494A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US4189939A (en) | 1980-02-26 |
FR2411400A1 (fr) | 1979-07-06 |
SE7809544L (sv) | 1979-06-13 |
GB2009857A (en) | 1979-06-20 |
IT7827417A0 (it) | 1978-09-07 |
JPS5453494A (en) | 1979-04-26 |
DE2839599A1 (de) | 1979-06-13 |
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