FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed wing support structure comprises one or several rod elements 36 and one or several joint elements 37. Rod element 36 comprises transition area 9 to engage with one joint element 37. With transition area of rod element 37 engaged with one joint element 38, central transmission of force between rod element 36 and joint element 37 is actuated. Invention covers also joint elements, rod element, wing, aircraft, method of force transmission and method of joint element manufacture.
EFFECT: perfected design.
32 cl, 19 dwg
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