CAPOT D'AERONEF INCORPORANT DES MOYENS POUR LIMITER LES PHENOMENES D'ECOPE DE TYPE PNEUMATIQUE

摘要

The aircraft nacelle (10) has limiting element (19) with at least one lock that is integral with the rest of nacelle or respectively the cowl (14). One part of lock occupies locked state in which lock interferes with the cowl and prevents deformation that includes radial component of cowl and another free state in which lock no longer interferes with the cowl and allows the opening movement of cowl.