FIELD: internal combustion engines.
SUBSTANCE: fluid-draining device for an aircraft engine, comprising: a collector configured to collect fluids drained from the engine, comprising means for pumping fluids contained in the collector, and removing said fluids, and monitoring means configured to signal abnormal collection of fluids by the collector, said monitoring means being configured to be activated when the flow of the collected fluids exceeds the capacity of the pumping means. Aircraft engine comprising said draining device and a method of controlling such an aircraft engine are also described.
EFFECT: technical result of the invention is an increase in the efficiency of draining fluids from an aircraft engine.
10 cl, 10 dwg
