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Sliding mechanism and levers retractable landing gear |
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Estructura del mecanismo |
| Función |
The element 1 carrying the wheel "a" turns around a fixed axis of the frame of the plane. The element 2 trains the torque B and C with the element 1 and the rod 4 of the jack of command of the train 3 which is mobile around a fixed axis D of the frame of the plane. The element 2 carries a roller “d” which slides freely in the groove e of the frame of the plane. When the stalk 4 comes down in the cylinder of jack 3, elements 1 and 2 revolve in direction of the arrow and the mechanism takes the position indicated in intermittent lines, so assuring the lifting of the landing gear of the plane. In extreme position, the element 2 makes a commitment by its roller d in the bights of the groove "e", and the jack of command is free from all encumbrances. |
| Comment |
Authors : DEMEULENAERE Mickaël 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 1441.
The mechanism is shown here.
The model and all attached items were made within this context. |
| Dimensión del mecanismo |
plano |
| Número de elementos |
4 |
| movimiento motor |
Traslación rectilínea |
| Grados de libertad |
1 |
| Número de entradas |
1 |
| Número de seguidores |
2 |
| Capacidad de rotabilidad del elemento de entrada |
no |
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Aplicación |
| Área de aplicación |
Transport/Traffic |
| Ejemplos de aplicación |
Aeronautics |
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IFMA (French Institute for Advanced Mechanics) |
| Persons |
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editor: Perez-Borrajo, Miguel (Ed.)
creator: Demeulenaere, Mickaël |
| Fecha de producción |
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September 2011 - January 2012 |
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