Aircraft wheel having driving lugs

An aircraft wheel comprising two half-wheels assembled together by bolts, each of the half wheels comprising a half-rim, a half-hub defining an axis of rotation of the aircraft wheel, and a half-web securing the half-rim and the half-hub coaxially with each other, the bolts being arranged in facing orifices formed in the half-webs, the aircraft wheel comprising:

• a first driving dog held in position on one of the half-hubs by screws screwed into holes provided on said one of the half-hubs, and
• at least one driving pin that extends from said one of the half-hubs, projecting in a direction substantially parallel to the axis of rotation of the aircraft wheel so as to cooperate with first driving dog so that a rotational driving torque input into the aircraft wheel wheel via the first driving dog does not pass through the screws.