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Structural component with improved conductivity and mechanical strength, and a method for its manufacture

  • US 8,864,072 B2
  • Filed: 05/12/2011
  • Issued: 10/21/2014
  • Est. Priority Date: 05/12/2010
  • Status: Active Grant
First Claim
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1. A structural component of an aircraft fuselage structure, the structural component comprising:

  • a fiber composite material structure designed as at least one of a frame or stringer comprising a web portion extending upwards relative to a skin of the aircraft, the fiber composite material structure being arranged on the skin of the aircraft fuselage and having an outer surface; and

    at least one electrically conductive metal profile attached to the outer surface of the fiber composite material structure so as to provide improved electrical conductivity of the structural component and component protection.

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