Floor structure for a fuselage

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/18 (2006.01) B64C 1/00 (2006.01)

Patent

CA 2646005

The present invention provides a floor structure for a fuselage containing a plurality of cross beams (6) to which respectively at least one first strut (11) and at least one second strut (12) are associated for connecting the respective cross beam to the fuselage; the at least one first strut (11) is aligned in a corresponding first direction vector and the at least second strut (12) is aligned corresponding to a second direction vector; and the projections of the first direction vector and of the second direction vector onto the longitudinal direction of the fuselage being different for absorbing a force acting in the longitudinal direction of the fuselage on the floor structure, through the first (11) and second (12) struts.

La présente invention propose une structure de plancher pour fuselage contenant une pluralité de poutres transversales (6) auxquelles au moins une première entretoise (11) et au moins une seconde entretoise (12) sont respectivement associées pour relier la poutre transversale respective au fuselage ; la ou les premières entretoises (11) sont alignées dans un premier vecteur de direction correspondant et la ou les secondes entretoises (12) sont alignées suivant un deuxième vecteur de direction ; les projections du premier vecteur de direction et du deuxième vecteur de direction sur la direction longitudinale du fuselage sont différentes afin d'absorber une force agissant dans la direction longitudinale du fuselage sur la structure de plancher par l'intermédiaire des première (11) et seconde (12) entretoises.

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