AIRCRAFT LOADING FRAME OF COMPOSITE MATERIAL

摘要

Aircraft loading frame (1) made of composite material characterised in that it comprises two side elements (2, 3) and a base element (7), wherein the side elements (2, 3) are joined by the inner portion of the frame (1) by means of the base element (7) and each of the side elements (2, 3) comprises a foot (4) attaching the frame (1) to the covering of the aircraft fuselage, a core (5) and inner skirt (6) attaching the core (5) to the base element (7).