FIELD: transport.
SUBSTANCE: invention relates to aircraft and spacecraft engineering. Proposed connector comprises base and heat parts, base connection element and head connection element. Base connection element one side mates the shape of the first reinforcing element while its opposite side is adapted to second reinforcing element base and rigidly jointed thereto. Head connection element one side mates the shape of the first reinforcing element while its opposite side is adapted to second reinforcing element base and rigidly jointed thereto. Skin component comprises two reinforcing elements with different profiles of cross-section jointed together in their lengthwise direction by proposed connector. Reinforcing elements are jointed together by connector in their lengthwise direction with lateral shift or with extra spacers for compensation of allowance.
EFFECT: decreased weight.
17 cl, 9 dwg
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