| 摘要 |
<p>The present invention relates to a turbofan engine nacelle having a downstream section including at least one front frame (2) which is to be attached to a stationary portion of the nacelle, said downstream section being provided with at least one rail or slide (3) extending in a substantially longitudinal direction of the nacelle and capable of engaging with at least one corresponding slide or rail (3') of an attachment pylon of the turbofan engine, characterised in that the front frame is connected to the rail or slide (3) of the downstream section by means of at least one pivoted connecting rod (7a, 7b).</p> |
