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Landing Gear |
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Struttura del meccanismo |
| Funzione |
A semi-levered landing gear for an aircraft comprises a main shock absorber strut with upper and lower telescoping portions, with the upper portion connectable to the airframe, a bogie beam to extend fore and aft of the aircraft fuselage with at least one forward axle and one aft axle for respective forward and aft wheels and a main pivot between the forward and aft axle pivotally connected to the lower portion of the main shock absorber strut and an auxiliary actuator mechanism comprising a lever pivotally connected to the upper portion of the main shock absorber strut so as to pivot between an upper position fot take-off and a lower position. |
| Comment |
Author : Estelle Chouteau
Modified by : Khaled-Assad ARROUK
IFMA (French Institute for Advanced Mechanics) - http://www.ifma.fr
Clermont-Ferrand, France
This model was generated to explain a certain patent in more detail.
The model and all attached items were made within this context. |
| Dimensione del meccanismo |
planare |
| Numero di membri |
7 |
| Movimento del movente |
Traslazione rettilinea |
| Gradi di libertà |
1 |
| Numero di membri moventi |
2 |
| Numero di membri cedenti |
2 |
| Capacità di rotazione del membro movente |
sì |
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Applicazione |
| Area di applicazione |
Transport/Traffic |
| Esempi di applicazione |
Design of aircrafts |
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| Data provider |
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| Luogo di origine |
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IFMA (French Institute for Advanced Mechanics) |
| Produttore |
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Estelle Chouteau |
| Persons |
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editore: Arrouk, Khaled (Ed.)
produttore: Chouteau, Estelle |
| Data di produzione |
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September 2011 - January 2012 |
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