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Mechanism with foldaway slide and control levers of the landing gear |
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Structura mecanismului |
| Funcţie |
The element 1 carrying the wheel has turns around a fixed axis A of the frame of the plane. The slide 4 moving according to the axis of the element 1, forms a couple of rotation B with the element 2 turning around a fixed axis D of the frame of the plane. The element 2 constitutes a couple of rotation C with the stalk 5 of the cylinder of command of the train 3, which turns around a fixed axis G of the frame of the plane. When the stalk 5 comes down in the cylinder 3, elements 1 and 2 revolve in the direction of arrows and the mechanism takes the position indicated in intermittent lines, so 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 1440.
The mechanism is shown here.
The model and all attached items were made within this context. |
| Dimensiunea mecanismului |
plan |
| Numărul de elemente |
5 |
| mişcarea de antrenare |
Translaţie rectilinie |
| Grad de libertate |
1 |
| Numǎrul elementelor de intrare |
2 |
| Numǎrul tacheţilor |
3 |
| Posibilitatea unei relaţii complete a elementului de intrare |
nu |
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Aplicaţie |
| Domeniul de aplicaţie |
Transport/Traffic and Other fields |
| Exemple de aplicare |
airplane |
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IFMA (French Institute for Advanced Mechanics) |
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editor: Perez-Borrajo, Miguel (Ed.)
creator: Ruangdajanan, Pairach |
| Data fabricaţiei |
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September 2011 - January 2012 |
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