Patent ID: 8995108
Filing Date: 2015-03-31
Classification: B64C,B64D,F16B,H01R,H05H

Abstract:
1. A coupling structure for airframe components, comprising: a fastener member that fastens a first member and a second member adjacent to each other, the first member and the second member constituting an airframe of an aircraft and being placed on top of each other in an overlapped portion, the fastener member being inserted into a through-hole formed in the overlapped portion; a conductive area that is formed of a conductive material at an interface between the first member and the second member in a first part of the overlapped portion, the conductive area providing an electrical path from the first member through the conductive area to the second member; and an insulating area that is formed of an insulating material at the interface in a second part of the overlapped portion, wherein the insulating area is located in the overlapped portion between an end part of the first member and the conductive area.