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Mechanism with foldaway slide and control levers of the landing gear |
  | Click to enlarge |
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Structure of mechanism |
Function |
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. |
Dimension of mechanism |
planar |
Number of links |
5 |
Drive movement |
Rectilinear translation |
Degree of freedom |
1 |
Fundamental mechanism |
Link containing mechanism
Mechanism, containing pressurizing medium |
Number of inputs |
2 |
Number of followers |
3 |
Revolution ability of input link |
no |
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Application |
Application area |
Transport/Traffic and Other fields |
Examples of application |
airplane |
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Collections |
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Permanent links |
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Data provider |
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Administration |
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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: Ruangdajanan, Pairach |
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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