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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
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
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.
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