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Căutare avansată   Căutare mecanism

Aircraft landing gear

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Structura mecanismului

Funcţie 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.
Dimensiunea mecanismului plan
Numărul de elemente 12
mişcarea de antrenare Translaţie rectilinie
Grad de libertate 1
Numǎrul elementelor de intrare 1
Numǎrul tacheţilor 4
Posibilitatea unei relaţii complete a elementului de intrare nu
 

Aplicaţie

Domeniul de aplicaţie Transport/Traffic
Exemple de aplicare The aircraft industry
 
Collections
Mecanism articulat
Transport
IAO 2011
Permanent links
DMG-Lib FaviconDMG-Lib https://www.dmg-lib.org/dmglib/handler?mcdsc=3248025
Europeana FaviconEuropeana  http://www.europeana.eu/portal/record/2020801/dmglib_handler_mcdsc_3248025.html
Data provider
IFMIFMA  http://www.ifma.fr
Administraţie
Loc IFMA (French Institute for Advanced Mechanics)
Persons editor: Perez-Borrajo, Miguel (Ed.)
creator: Lecourtois, Mickaël
Data fabricaţiei September 2011 - January 2012
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