Fixing pylon for connecting turbojet to wing of airplane, has air foil defined by two opposite faces and delimited longitudinally between leading edge and trailing edge, where portion of trailing edge is provided with brackets

摘要

The pylon (30) has an air foil defined by two opposite faces (36) and delimited longitudinally between a leading edge (31) and a trailing edge (33), where the pylon is transversely delimited between a distal end (35) to be fixed at a turboshaft engine and a proximal end (34) to be fixed at a structure element of the aircraft. A portion of the trailing edge is provided with brackets (40). The brackets extend longitudinally without deviation in a thickness direction of the pylon and penetrate a shearing zone (Z1) between a primary flow and a secondary flow.