| 摘要 |
The invention relates to a jet nozzle of a turbine engine, comprising an outer wall and an inner wall defining, between each other, a flow channel for the exhaust gas; the inner wall forming a central frustoconical body oriented in a longitudinal direction. The nozzle is characterised in that the central body (32) comprises means (44) for guiding the exhaust gas in the longitudinal direction over at least part of the length of the central body (32) in the direction of flow of the gas. |
