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Landing Gear |
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Structura mecanismului |
| Funcţie |
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. |
| Dimensiunea mecanismului |
plan |
| Numărul de elemente |
7 |
| mişcarea de antrenare |
Translaţie rectilinie |
| Grad de libertate |
1 |
| Numǎrul elementelor de intrare |
2 |
| Numǎrul tacheţilor |
2 |
| Posibilitatea unei relaţii complete a elementului de intrare |
da |
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Aplicaţie |
| Domeniul de aplicaţie |
Transport/Traffic |
| Exemple de aplicare |
Design of aircrafts |
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IFMA (French Institute for Advanced Mechanics) |
| Producǎtor |
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Estelle Chouteau |
| Persons |
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editor: Arrouk, Khaled (Ed.)
creator: Chouteau, Estelle |
| Data fabricaţiei |
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September 2011 - January 2012 |
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