Patent ID: 8925864
Filing Date: 2015-01-06
Classification: B29C,B29L,B32B,B64C,B64D,Y02T,Y10T

Abstract:
1. A component for building a fuselage section of an aircraft, comprising: a first component including a first border area connectable to a second border area of a second component so as to form an electrically conductive joint between the first border area and the second border area, wherein the component includes a composite structure, wherein the first border area includes a layer structure comprising a plurality of electrically conductive metal layers disposed one on top of another, wherein the electrically conductive metal layers extend outward from the first border area, and wherein the electrically conductive metal layers of the first component alternately engage metal layers of the second component in each case at the electrically conductive joint so as to fill any cavities between the first and the second components, leaving no void.