(EN) The invention relates to an aircraft pylon for mounting a dual- or triple-flow jet engine (1), said pylon comprising an upper surface for connection to the aircraft, two side flanks, and a flange on the lower portion of the pylon. Said pylon includes at least one portion that extends downstream from the cold flow nozzle (5) of said jet engine and lies in the cold flow. Said pylon is characterized in that it comprises, on the portion thereof extending into the cold flow beyond said nozzle, at least one opening (8), positioned on one of the flanks of said pylon, by means of which an air stream is injected into or drawn from the gas flow that flows along the flanks of the pylon.
(ZH) 本发明涉及一种用于支撑双流或三流涡轮喷气引擎(1)的飞机外挂架，包含一用于连接到该飞机的上面，两个侧面和一在该外挂架下面部分的底面。所述外挂架包含至少一个向所述喷气引擎的冷流排气管(5)的下游延伸，并在所述冷流中的部分。该外挂架在其延伸到超过所述排气管的冷流中的部分上包括至少一个定位在所述外挂架的一个侧面上的孔(8)，空气流通过该孔从沿该外挂架侧面流动的气流喷入或吸入。
