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Sliding mechanism and levers retractable landing gear |
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Estructura del mecanismo |
| Función |
The element 2 rotates around a fixed axis A from the fuselage frame of the plane. The element 1 carrying the wheel a gives the couples of rotations B and C with elements 2 and 3. The element 3 rotates around a fixed axis D from the fuselage frame of the plane. The rod 5 of the actuating cylinder of the landing gear 4 constitutes a couple of rotation E with the element 2. The cylinder 4 rotates around a fixed axis F of the fuselage frame of the plane. When the rod 5 comes down in the actuating cylinder 4, elements 1, 2 and 3 revolve in the direction of arrows and the mechanism takes the position indicated in dotted lines, assuring the lifting of the landing gear of the plane. |
| Comment |
Authors : OPPENHAUSER Bastien 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 1428.
The mechanism is shown here.
The model and all attached items were made within this context. |
| Dimensión del mecanismo |
plano |
| Número de elementos |
7 |
| 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 |
planes |
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IFMA (French Institute for Advanced Mechanics) |
| Persons |
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editor: Perez-Borrajo, Miguel (Ed.)
creator: Oppenhauser, Bastien |
| Fecha de producción |
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September 2011 - January 2012 |
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