Patent ID: 9663246
Date: 2017-05-30
CPC Classifications: B64C,B64D,B64F,H05K,Y10T

Claim:
1. A method for installing an electric system into an aircraft fuselage, the method comprising: a. providing a fuselage element extending along an aircraft longitudinal axis and comprising an outer skin and a plurality of support elements extending along an interior surface of the outer skin, b. providing a foil sheet of an electrically insulating substrate material, c. attaching the foil sheet on an inner side of the fuselage element, and d. applying particles of electrically conductive material onto an inner surface of the attached foil sheet opposite the outer skin in a predetermined pattern, such that the applied particles of electrically conductive material form electric conductor elements along the inner surface of the foil sheet, wherein, prior to attaching the foil sheet on the inner side of the fuselage element, at least one power supply cable is attached to the inner side of the fuselage element at such a position that each of the at least one power supply cables is sandwiched between the foil sheet and the inner side of the fuselage element.