FIELD: transport.
SUBSTANCE: invention relates to aircraft structural support element, to aircraft design and aircraft. Proposed element has X-like cross section and comprises a zone that stays in mechanical contact with the element to be supported, features closed cross section and ensures stability. Said zone comprises first and second struts jointed in some connecting zone that forms a bulge. First strut is a long strut. Second strut is a short strut. Support element has vertical wall arranged perpendicular to the element to be supported and provided with support surface to take up load of other structural elements. Vertical wall if formed by one of said two struts.
EFFECT: higher structural strength.
10 cl, 11 dwg
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