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2-dimensional thrust vectoring |
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Estructura del mecanismo |
| Función |
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. |
| Dimensión del mecanismo |
plano |
| Número de elementos |
12 |
| movimiento motor |
Traslación rectilínea |
| Grados de libertad |
2 |
| Número de entradas |
2 |
| Número de seguidores |
2 |
| Capacidad de rotabilidad |
no |
| Capacidad de rotabilidad del elemento de entrada |
no |
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Función de guía |
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Aplicación |
| Área de aplicación |
Transport/Traffic |
| Ejemplos de aplicación |
Fighter aircraft |
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IFMA (French Institute for Advanced Mechanics) |
| Persons |
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editor: Cousturier, Richard (Ed.)
creator: Ovide, Franck |
| Fecha de producción |
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September 2010 - January 2011 |
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