ACOUSTIC PANEL FOR A TURBOJET ENGINE NACELLE, WITH IN-BUILT FASTENERS

摘要

The present invention relates to an acoustic panel (5) comprising at least one cellular core arranged between at least an internal skin and an external skin (53), characterized in that said external skin incorporates at least one fastener (61) able to collaborate in a disconnectable fashion with a complementary fastener associated with a structure to which it is to be attached.