RIGID FRAMEWORK FOR AIRCRAFT ENGINE MOUNTING STRUCTURE AND ENGINE MOUNTING STRUCTURE COMPRISING SAME

摘要

The invention concerns a rigid framework (8) for aircraft engine mounting structure, in the form of a structure box closed by first and second structure box side panels (34a, 34b), said framework comprising inter-rib spaces (38<SUB>1</SUB> à 38<SUB>8</SUB>) each delimited by two directly consecutive transverse ribs (36) of the structure box. The invention is characterized in that for each inter-rib space pertaining to a group comprising at least any three directly consecutive inter-rib spaces, a single access opening(42<SUB>1</SUB> à 42<SUB>8</SUB>) is provided on the side panels, said openings being arranged alternately on the first and second side panels.