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2-dimensional thrust vectoring |
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Structura mecanismului |
| Funcţie |
This device is placed directly to the output of the reactor. Exclusively for fighter aircraft, this vector thrust nozzle can direct exhaust gas and then increase the maneuverability of the aircraft regardless of its speed. We talk about hyper-maneuverability because with this technology an aircraft is capable to make turns at high angle of attack and to fly at very low speed. |
| Comment |
Authors : Franck Ovide
IFMA (French Institute of Advanced Mechanics) - http://www.ifma.fr
Clermont-Ferrand, France
This model was generated to explain a certain patent in more detail.
The model and all attached items were made within this context. |
| Dimensiunea mecanismului |
plan |
| Numărul de elemente |
12 |
| mişcarea de antrenare |
Translaţie rectilinie |
| Grad de libertate |
2 |
| Numǎrul elementelor de intrare |
2 |
| Numǎrul tacheţilor |
2 |
| Posibilitatea unei rotaţii complete |
nu |
| Posibilitatea unei relaţii complete a elementului de intrare |
nu |
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Funcţia de ghidare |
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Aplicaţie |
| Domeniul de aplicaţie |
Transport/Traffic |
| Exemple de aplicare |
Fighter aircraft |
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IFMA (French Institute for Advanced Mechanics) |
| Persons |
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editor: Cousturier, Richard (Ed.)
creator: Ovide, Franck |
| Data fabricaţiei |
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September 2010 - January 2011 |
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