| 摘要 |
The fireproof seal is intended for an assembly comprising a turbojet engine pylon and nacelle, in particular an O-duct type. The nacelle comprises a fixed internal nacelle structure (4) and a primary exhaust nozzle (5) for combustion gas, which can be driven at least partially in a relative longitudinal linear movement in the direction of the longitudinal axis of the nacelle (A). The seal comprises a plurality of baffles (10-15) arranged longitudinally such as not to interfere during a longitudinal linear movement (B) between the primary combustion gas exhaust nozzle and the fixed internal nacelle structure. |
