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Estructura del mecanismo |
| Función |
The lengths of the mechanism’s elements verify these conditions: AE=DF and EF=AD, that’s means AEFD is a parallelogram. The elements 4 and 3 turn around fixe axis A and D of the fuselage of the plane.
The element 1 composed of the wheel a form a rotation frame E with the element 4 and a rotation frame B with the elements 2 which form a rotation frame too (C) with the element 3.
The element 3 form a rotation frame G with the cylinder axis 5, mobil around of a fix axis H of the plane’s fuselage.
When the axis 5 mount in body of the cylinder (6), the elements 1 and 3 pivot to the fleche’s senses and the mechanism takes the indicated position, enabling the landing train lifting of the plane.
When the landing train is left, the elements 1, 4 and 2, 3 fix themselves in their extreme positions and form a stiff system. |
| Comment |
Authors : LICBARSKI Jonathan 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 1439.
The mechanism is shown here.
The model and all attached items were made within this context. |
| Dimensión del mecanismo |
plano |
| Número de elementos |
9 |
| movimiento motor |
Traslación rectilínea |
| Grados de libertad |
1 |
| Número de entradas |
1 |
| Número de seguidores |
7 |
| Capacidad de rotabilidad del elemento de entrada |
no |
| |
Aplicación |
| Ejemplos de aplicación |
planes |
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