Collector for a drained liquid for an aircraft turbine engine and associated turbine engine

A collector for a drained liquid for an aircraft turbine engine, the collector comprising:

• an internal cavity comprising a first space for collecting the drained liquid and a second space for transferring the collected liquid to a recovery outlet;
• at least one inlet for the drained liquid, in fluid communication with the first space;
• and
• at least one recovery outlet, in fluid communication with the second space;
• wherein the first space and the second space are separated from each other by a liquid-tight partition in which is arranged a drained liquid passage restriction means which restricts the passage of the drained liquid from the first space to the second space, the air in the first space being in communication with the air in the second space such that the air pressure is identical in the first space and in the second space.