Compact steering device for the landing gear of an aircraft

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/50 (2006.01)

Patent

CA 2611970

The invention relates to a steering device for the landing gear (1) of an aircraft, said steering device being characterised in that it comprises at least one means which is used to rotate (2, 3, 4, 5) the wheels (6) of the landing gear and is arranged along the strut (13) of the landing gear.

- L'objet de l'invention est un dispositif de direction pour atterrisseur (1 ) d'aéronef caractérisé en ce qu'il comporte au moins un moyen de manAEuvre en rotation (2, 3, 4, 5) des roues (6) de l'atterrisseur disposé le long de la jambe (13) de l'atterrisseur

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