TURBO ENGINE ATTACHMENT PYLON

摘要

A turbo engine attachment pylon, configured to connect a turbo engine to a structural element of an aircraft, said pylon (30) having an aerodynamic profile defined by two opposing lateral faces and delimited longitudinally between a leading edge (31) and a trailing edge (33). The pylon (30) comprises, on each of the lateral faces (36) thereof, a series of deflectors (40) spaced transversely apart from one another and between them defining two converging curved channels (60) configured to accelerate the air flow circulating inside the channels (60) when the aircraft is taking off or during flight, and to divert said air flow towards the jet of the turbo engine.