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Sliding mechanism and levers retractable landing gear |
  | Premi per ingrandire |
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Struttura del meccanismo |
Funzione |
The element 1 which turns around a fixed axis A of the frame of the plane trains a couple of rotation B with the element 4 carrying the wheel has. The element 4 establishes a couple of rotation C with the element 2 which turns around a fixed axis D of the frame of the plane. Elements 5 and 6, of equal length, train together a couple of rotation G and couples of rotation F and E with elements 2 and 4. The stalk 7 of the jack of command of the train 3 trains a couple of rotation G with elements 5 and 6. The cylinder of jack 3, the element 1 revolves in the sense of the arrow and the mechanism takes the position indicated in intermittent lines, so assuring the lifting of the landing gear of the plane. |
Comment |
Authors : DUBREUIL ROUS DE FENEYROLS Jean-Philippe 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 1442. The mechanism is shown here. The model and all attached items were made within this context. |
Dimensione del meccanismo |
planare |
Numero di membri |
8 |
Movimento del movente |
Traslazione rettilinea |
Gradi di libertà |
1 |
Numero di membri moventi |
1 |
Numero di membri cedenti |
6 |
Capacità di rotazione del membro movente |
no |
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Applicazione |
Area di applicazione |
Transport/Traffic |
Esempi di applicazione |
Mechanism with foldaway wing and control levers of the landing gear |
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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: Dubreuil-Rous-De-Feneyrols, Jean-Philippe |
Data di produzione |
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September 2011 - January 2012 |
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