An electromagnetic energy protection system for an aircraft component, the system including a plurality of conductive sheets (208A, 208B, 208C, 208D, 208E) ohmically connected by conductive interconnects (210A, 210B). The conductive interconnects are metal formed by a metal deposition process. The metal deposition process can include a plasma deposition process. The conductive interconnects prevent the formation of surface deformities such as bumps that may be caused when connecting, either physically or electrically, adjacent conductive sheets.
Electromagnetic energy surface protection
Elektromagnetischer Energieoberflächenschutz
Protection de surface d'énergie électromagnétique
2018-12-19
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Automobile electromagnetic energy absorption and protection device group
European Patent Office | 2020
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