| 摘要 |
<p>Process for manufacturing a turbojet engine nacelle part. The present invention relates to a process for manufacturing a lip (4a) of an air intake (4) of a nacelle (1) comprising a plurality of constituent elements (41, 42, 43, 44, 421, 431), characterized in that it comprises the following steps that aim to: - place inside a mould at least one portion of the constituent elements within an assembly of fibrous layers (44, 45) completely or partly encompassing the constituent elements and thus forming a preform, - carry out an impregnation of the preform obtained in order to obtain the moulding of the part.</p> |
