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A multilayer structural element, such as a skin panel for an aircraft fuselage, comprises a plurality of metal webs and a plurality of fiber webs arranged as layers in a sandwich structure, where the metal webs of neighbouring layers form stepped connecting regions. A material strip is provided on a

A multilayer structural element, such as a skin panel for an aircraft fuselage, comprises a plurality of metal webs and a plurality of fiber webs arranged as layers in a sandwich structure, where the metal webs of neighbouring layers form stepped connecting regions. A material strip is provided on an outer surface of the sandwich structure for at least partially covering an outlying connecting region, and the material strip enables the placement of rivets at uniform spacing for fastening a structure to the structural element.

대표청구항 ▼

What is claimed is: 1. A structural element, comprising:a plurality of metal sheets;a plurality of fiber sheets, wherein the plurality of metal sheets and the plurality of fiber sheets are arranged as layers of a sandwich structure, the sandwich structure having a plurality of connecting regions dis

What is claimed is: 1. A structural element, comprising:a plurality of metal sheets;a plurality of fiber sheets, wherein the plurality of metal sheets and the plurality of fiber sheets are arranged as layers of a sandwich structure, the sandwich structure having a plurality of connecting regions disposed along a face of the sandwich structure and oriented in a first direction across the face of the sandwich structure, the plurality of connecting regions corresponding to mutually overlapping edge sections of neighboring metal sheets of the plurality of metal sheets; anda plurality of material strips placed on the face of the sandwich structure and which traverse across the plurality of connecting regions, wherein each material strip is substantially narrower than the connecting regions along the first direction.