Pivot pin for a turbine engine comprising a ring for recovering a flow of lubricating oil with a plurality of lubricating oil discharge ports

A journal configured to be driven in rotation in a housing of a turbine engine, or for an aircraft, the journal comprising:

• a circumferential main body comprising a plurality of angularly distributed ventilation openings configured to allow a plurality of axial airflows to circulate from upstream to downstream in the turbine engine, two consecutive ventilation openings being connected by a connecting segment;
• and
• a circumferential ring for recovering a flow of lubrication oil, which ring is rigidly connected to the main body and is radially inside the ventilation openings, the recovery ring extending longitudinally and comprising a plurality of radial discharge openings for allowing a plurality of radial flows of oil to be discharged towards the outside, of the circumferential ring;
• wherein each discharge opening is radially aligned with a connecting segment of the main body to allow each flow of oil to be discharged between the airflows.