B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01)
Patent
CA 2624385
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 (381 à 388) 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(421 à 428) is provided on the side panels, said openings being arranged alternately on the first and second side panels.
L'invention se rapporte à une structure rigide (8) d'un mât d'accrochage de moteur d'aéronef, se présentant sous la forme d'un caisson fermé par un premier et un second panneau latéral de caisson (34a, 34b), cette structure comportant des espaces inter-nervures (381 à 388) chacun délimité par deux nervures transversales (36) directement consécutives du caisson. Selon l'invention, pour chaque espace inter-nervures appartenant à un groupe comportant au moins trois espaces inter-nervures quelconques et directement consécutifs, une unique ouverture d'accès (421 à 428) est prévue sur les panneaux latéraux, ces ouvertures étant disposées en alternance sur les premier et second panneaux latéraux.
Bernardi Lionel
Huguet Thierry
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
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