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Mechanisms with wings and control levers of landing gear |
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Estructura del mecanismo |
| Función |
The element 1 carrying the wheel a turns around the fixed axis D of the frame of the plane. The element 2 forms the couples of rotation C and D with elements 1 and 3. The element 3 turns around the fixed axis A of the frame of the plane. The stalk of the command’s jack of the train 4 constitutes a couple of rotation E with the element 3. The command’s jack 4 turns around the fixed axis F of the plane’s frame. When the stalk 5 goes back up in the cylinder of the jack 4, elements 1,2 and 3 revolve in the direction of arrows and mechanism take the position indicated in intermittent lines, so assuring the lifting of the landing gear of the plane. |
| Comment |
Authors : Simon RENARD from I Artobolevski model
Modified by : Miguel PEREZ BORRAJO
IFMA (French Institute for Advanced Mechanics) - http://www.ifma.fr
Clermont-Ferrand, FRANCE
This model is based on a mechanism described by Artobolevskij under number 1423.
The mechanism is shown here.
The model and all attached items were made within this context. |
| Dimensión del mecanismo |
plano |
| Número de elementos |
6 |
| movimiento motor |
Traslación rectilínea |
| Grados de libertad |
1 |
| Número de entradas |
1 |
| Número de seguidores |
1 |
| Capacidad de rotabilidad del elemento de entrada |
no |
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Aplicación |
| Área de aplicación |
Transport/Traffic |
| Ejemplos de aplicación |
Use possible as front wheel on light passenger aircraft. |
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IFMA (French Institute for Advanced Mechanics) |
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editor: Perez-Borrajo, Miguel (Ed.)
creator: Renard, Simon |
| Fecha de producción |
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September 2011 - January 2012 |
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