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Aircraft landing gear |
  | Click to enlarge |
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Structure of mechanism |
| Function |
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. |
| Dimension of mechanism |
planar |
| Number of links |
12 |
| Drive movement |
Rectilinear translation |
| Degree of freedom |
1 |
| Fundamental mechanism |
 Link containing mechanism |
| Number of inputs |
1 |
| Number of followers |
4 |
| Revolution ability of input link |
no |
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Application |
| Application area |
Transport/Traffic |
| Examples of application |
The aircraft industry |
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| Location |
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IFMA (French Institute for Advanced Mechanics) |
| Persons |
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editor: Perez-Borrajo, Miguel (Ed.)
creator: Lecourtois, Mickaël |
| Date of production |
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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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Newsletter
DMG-Lib
Europeana
IFMA
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