The invention relates to an aircraft landing gear comprising the wheel shaft (2) and the wheels (3,3'). The wheels (3, 3') comprises wheel hubs (4,4') and first masses (F,F '). The wheel hubs are installed in a manner of surrounding the first rotation axis (X) and rotating on the wheel shaft. The first masses (11,11') which are protrudingly projected from the one side of the wheel hubs (4,4'), the first mass is cooperated with the gear (8) of the driving braking device (8) loaded by the landing rack, and the gear rotates around the second rotation axis (Y) perpendicular to the first rotation axis and can be installed in a rotation manner.
Aircraft landing gear provided with means for rotating the wheels carried by the landing gear
29.04.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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