Structural panel component for aircraft fuselage, includes longitudinally extending and crosswise or transverse stiffening elements comprising the skin sheet of the component

摘要

Longitudinally extending and crosswise or transverse stiffening elements (3,4) comprise the skin sheet (2) of the structural panel component (1). The component is formed by performing a material chip removing process on a semi-finished starting material. An independent claim is also included for a method in fabricating a structural panel component.