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Aircraft landing gear |
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Struttura del meccanismo |
Funzione |
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. |
Dimensione del meccanismo |
planare |
Numero di membri |
12 |
Movimento del movente |
Traslazione rettilinea |
Gradi di libertà |
1 |
Numero di membri moventi |
1 |
Numero di membri cedenti |
4 |
Capacità di rotazione del membro movente |
no |
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Applicazione |
Area di applicazione |
Transport/Traffic |
Esempi di applicazione |
The aircraft industry |
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Collections |
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Permanent links |
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Data provider |
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Amministrazione |
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Luogo di origine |
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IFMA (French Institute for Advanced Mechanics) |
Persons |
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editore: Perez-Borrajo, Miguel (Ed.) produttore: Lecourtois, Mickaël |
Data di produzione |
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September 2011 - January 2012 |
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Further media formats |
Animations |
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CAX files |
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Documents |
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Videos |
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Images |
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