CPC B64D 11/0647 (2014.12) [B64D 45/02 (2013.01); H01P 1/203 (2013.01); H05F 1/00 (2013.01); H05F 3/00 (2013.01)] | 23 Claims |
13. A system for reducing electromagnetic interference (EMI) in an aircraft, the system comprising:
a seat assembly of a first plurality of seat assemblies configured in one or more rows, the seat assembly comprising:
a frame including a base electrically coupled to an electric ground of the aircraft and a support member operatively coupled to the base; and
a seat coupled to the base and the support member, the seat including a conductive substrate layer configured to limit transmission of EMI between a forward area and a rear area relative to the seat assembly, the conductive substrate layer electrically coupled to the base; and
wherein the seat further comprises a first portion coupled to the base and a first side of the support member, and a second portion coupled to a second side of the support member opposite the first side, the conductive substrate layer covering the first portion and the second portion.
|