| 摘要 |
<p>An aircraft fuselage structure is shown and described, comprising a plurality of ribs (5) extending at intervals from one another in planes perpendicular to the longitudinal axis (X), comprising a floor (7) extending in a plane parallel to the longitudinal axis (X), which has retaining rails (9) between which floor plates (11) are arranged, comprising support elements (15) which extend in the plane of the ribs (5) between the floor (7) and the ribs (5), wherein the retaining rails (9) extend across a plurality of support elements (15), wherein the lashing devices (35) are connected to the support elements (15), wherein the retaining rails (9) and the floor plates (11) are fixedly connected together for transmitting loads in the plane of the floor (7), wherein the support elements (15) have transverse profiles (17) extending directly below the floor (7) in the plane of the ribs (5), said transverse profiles extending in a linear manner between the ribs (5) between connecting points (19) therewith, on which the retaining rails (9) bear, and to which the lashing devices (35) are connected, wherein the transverse profiles (17) are at intervals from the ribs (5) between the connecting points (19) on the side thereof facing away from the floor (7) and wherein on the side of the transverse profiles (17) facing away from the floor (7), struts (27, 29) extend between the transverse profiles (17) and the ribs (5) in the plane thereof.</p> |
