A system of protection against electrical shock, especially rays, of structural components of aircraft, particularly deposits or fuel tanks manufactured from composite materials. (Machine-translation by Google Translate, not legally binding)

摘要

A system of protection against electrical shock for parts and structural parts of aircraft, particularly of deposits or fuel tanks, made of composite materials, which consists of a layer of metal mesh (1) that covers the outer face of the whole surface exposed to the impact of rays; a first layer of insulating material (2) placed between the mesh (1) and the outer cover (r.e.) made of composite material; a second layer of insulating material (3) placed inside the internal piece (p.i.) to be fastened, if this internal piece contains or consists of carbon fiber; a third layer of insulating material (5) placed between the outer cladding (r.e.) and the internal piece (p.i.) to be subjected; a strip of insulating material (6); a double strip of self-adhesive aluminum sheet (4) that covers the strip of aising material (6) and finally, on all the surface, an organic finish. (Machine-translation by Google Translate, not legally binding)