Assembly for a mechanical reducer of an aircraft

An assembly comprising planet gears and a planet carrier for a mechanical splash-lubricated reducer, in particular for an aircraft, this assembly having an annular shape about a longitudinal axis,

• the planet gears being evenly spaced around said axis and each comprising two cylindrical longitudinal ends,
• the planet carrier having an annular shape about said axis and comprising housings for receiving the planet gears, these housings being evenly distributed about said axis and each being axially delimited by two walls extending respectively in two planes perpendicular to said axis, and two lateral bulkheads extending between the walls these walls, comprising orifices for mounting said longitudinal ends of the planet gears,
• wherein the assembly further comprises oil scoops which are secured to the planet carrier and which are evenly distributed around said axis and interposed between the planet gears, each of these scoops comprising at least one curved bucket, the concavity of which extends partly around one of the planet gears and is separated from this planet gear by one of said bulkheads.