FIELD: transport.
SUBSTANCE: invention relates to structure composed of parts from composite materials to be used for aircraft working structures to accommodate electrical circuitry in aircraft. Stiff structural part 1 from laminar composite includes at least two conductors, two structural layers 11, 12 including fibers retained by thermosetting or thermoplastic matrix. Note here that at least one conducting circuit layer 15 is arranged between at least two structural layers. At least one conducting circuit layer comprises circuit of electric conductors 151a-151c. Note here that electric conductors are arranged in one structural parts, regularly and electrically isolated from two structural layers by dielectric material 150. Structural part 1 comprises electrical connectors 18 to connect said conductors 151a-151c and at least one circuit layer 15 to make electric circuit by assembly of several structural elements.
EFFECT: large structures with electric circuit formed by electrical connection of structural parts.
22 cl, 9 dwg
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