| 摘要 |
This aircraft engine nacelle air intake assembly comprises an air intake structure comprising an air intake lip (7) and an acoustic shroud (5) extending downstream of this air intake lip (7) and designed to be mounted on a fixed structure (2), the said air intake structure being designed to be able to move with respect to the said fixed structure (2) between an operating position in which the said lip (7) is in contact with the said shroud (5), and a maintenance position in which the said lip (7) is set apart in the upstream direction away from the said shroud (5). This assembly is notable in that it comprises runway means (19) designed to centre this lip (7) with respect to this shroud (5).
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