Procédé d'installation d'un système électrique dans un fuselage d'avion

摘要

Described an illustrated is a method for installing an electric system (1) into an aircraft fuselage. The object to provide a method for simply and quickly installing an electric system into an aircraft fuselage, wherein the electric system is as little heavy and space consuming as possible, and wherein a wide range of customized alternatives of the electric system is possible, is achieved by the steps of providing a fuselage element (3) extending along an aircraft longitudinal axis (5) and comprising an outer skin (7) and an interior surface, providing a foil sheet (11) of an electrically insulating substrate material, attaching said foil sheet (11) on the inner side (17) of said fuselage element (3), applying particles of electrically conductive material (19) onto the inner surface (21) of said attached foil sheet (11) opposite the outer skin (7) in a predetermined pattern, such that the accumulated particles of electrically conductive material (19) form electric conductor elements (23) along said inner surface (21) of said foil sheet (11).