The present disclosure provides an aircraft (10), as well as systems and methods for reducing current flow to electrical systems onboard an aircraft (10). A signal return network (220) is spaced from a composite structure (210) and first and second non-conductive components (240) are attached between the signal return network (220) and the composite structure (210) at first and second attachment points (242, 244), respectively. A conductive component (250) is attached between the signal return network (220) and the composite structure (210) at a third attachment point (246) for electrically coupling the signal return network (220) to the composite structure (210).
SIGNAL RETURN NETWORK FOR COMPOSITE AIRCRAFT
SIGNALRÜCKLAUFNETZWERK FÜR COMPOSITE-FLUGZEUG
RÉSEAU DE RETOUR DE SIGNAL POUR AÉRONEF COMPOSITE
2020-07-15
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT FUSELAGE WITH INTERNAL CURRENT RETURN NETWORK
Europäisches Patentamt | 2021
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