Method for producing an aircraft structure component having an outer skin provided with electric conductor elements

摘要

A method for producing an aircraft structure component is disclosed the component having an outer skin provided with electric conductor elements. The method includes providing an aircraft structure component having an outer skin, applying particles of electrically conductive material onto the outer surface of the outer skin of said aircraft structure component in a predetermined pattern, such that the accumulated particles of electrically conductive material form electric conductor elements along the outer surface of the outer skin, and applying particles of electrically insulating material onto the outer surface of the outer skin of said aircraft structure component in a predetermined pattern, such that the accumulated particles of electrically isolating material form an insulating layer for the electric conductor elements.

主权项

1. A method for producing an aircraft structure component having an outer skin provided with electric conductor elements, the method comprising:
a. providing the aircraft structure component having the outer skin, b. applying particles of electrically conductive material onto an outer surface of the outer skin of the aircraft structure component in a predetermined pattern, such that accumulated particles of the electrically conductive material form electric conductor elements along the outer surface of the outer skin, and c. applying particles of electrically insulating material onto the outer surface of the outer skin of the aircraft structure component in a predetermined pattern, such that accumulated particles of the electrically insulating material form an insulating layer for the electric conductor elements,
wherein the electric conductor elements are formed along the outer skin of the aircraft structure component such that the electric conductor elements contact rivets received in the outer skin of the aircraft structure component, so that an electric signal may be guided through the rivets to an inner surface of the outer skin of the aircraft structure component and into an inside of the aircraft structure component,wherein the rivets are connected to a computer or to a controlling device.