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Aircraft landing gear |
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Estructura del mecanismo |
| Función |
This mechanism is used for the deployment and the fold of an aircraft landing gear.
It is composed of a set of rods that transform the translation movement of a commanded jack into a rotation of the landing gear wheel around the point A. It may be noted that A, D and F are points of the aircraft structure. |
| Comment |
Authors : Mickael COURTOI based on a model of I Artobolevski book.
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 1424.
The mechanism is shown here.
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 |
1 |
| Número de entradas |
1 |
| Número de seguidores |
4 |
| Capacidad de rotabilidad del elemento de entrada |
no |
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Aplicación |
| Área de aplicación |
Transport/Traffic |
| Ejemplos de aplicación |
The aircraft industry |
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IFMA (French Institute for Advanced Mechanics) |
| Persons |
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editor: Perez-Borrajo, Miguel (Ed.)
creator: Lecourtois, Mickaël |
| Fecha de producción |
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September 2011 - January 2012 |
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