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Aircraft landing gear |
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Structura mecanismului |
Funcţie |
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. |
Dimensiunea mecanismului |
plan |
Numărul de elemente |
12 |
mişcarea de antrenare |
Translaţie rectilinie |
Grad de libertate |
1 |
Numǎrul elementelor de intrare |
1 |
Numǎrul tacheţilor |
4 |
Posibilitatea unei relaţii complete a elementului de intrare |
nu |
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Aplicaţie |
Domeniul de aplicaţie |
Transport/Traffic |
Exemple de aplicare |
The aircraft industry |
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Administraţie |
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Loc |
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IFMA (French Institute for Advanced Mechanics) |
Persons |
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editor: Perez-Borrajo, Miguel (Ed.) creator: Lecourtois, Mickaël |
Data fabricaţiei |
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September 2011 - January 2012 |
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