tuyere of ejection of hot gases for a turbojet, comprising, on the packaging a deflector of these gases

摘要

Ejection nozzle of hot gases to an aircraft turboreactor, provided to be installed in a pod supported by a pylon comprising a cowling (8) disposed in the vicinity of the outer surface of this nozzle (12), the space between the fairing and the nozzle forming a substantially longitudinal channel (10), characterized in that it comprises on its outer wall (12), a deflector (20) arranged in a transverse plane, covering an angular sector lying in the channel (10), which is designed to come close to the cowling (8) without touching it.