BREATHING SYSTEM OF TURBOJET ENGINE

摘要

FIELD: engines and pumps.SUBSTANCE: invention relates to turbojet double-circuit engines used in the field of aviation. A breathing system of a turbojet engine includes a breathing pipeline connected with a breathing pipe installed onto a nozzle. The outlet end of the breathing pipe is made as bent to form a reservoir for oil condensate. The outlet section of the nozzle is made as perpendicular to the axis of the pipe.EFFECT: elimination of oil ingress to a landing strip after switching off an engine.3 dwg