FIELD: transport.
SUBSTANCE: invention relates to structural component for aircraft or spacecraft including component core passing through component area, the first and the second coatings which are made on two opposite boundary surfaces of component core and pass through component area, a number of squeezed elements which are distributed throughout component area and interconnect the first and the second coatings via component core, and reinforcing strip which passes between coatings along reinforcement line which is virtually parallel to component area.
EFFECT: design improvement.
13 cl, 7 dwg
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