Aircraft fuselage structure has skin field, where diagonal stiffening elements are formed by skin-field polygons, and stiffening frames are designed for limiting fuselage section

摘要

The aircraft fuselage structure (1a) has a skin field (2), where diagonal stiffening elements (6) are formed by skin-field polygons (4). Stiffening frames (8) are designed for limiting a fuselage section (10), where the stiffening elements are connected with one of the stiffening frames. The stiffening element is connected at a corner area (12) of the stiffening frame.