A current return network assembly, for an aircraft having a predetermined potential lightning strike zone, is mounted within the predetermined potential lightning strike zone. The current return network assembly includes an electrically conductive honeycomb central core (102) that conducts electrical current both through the assembly and through the predetermined potential lightning strike zone. The electrical current is caused by a lightning strike on the aircraft at the predetermined potential lightning strike zone.
Method for providing a current return network in an aircraft structure
Verfahren zur Erstellung eines Stromrücklaufnetzwerkes in einer Flugzeugstruktur
Méthode pour l'institution d'un réseau de retour de courant dans une structure d'aéronef
2016-10-12
Patent
Elektronische Ressource
Englisch
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