An aircraft radome includes a composite structure including, or according to the circumstances configured to define, at least one housing extending along the radome from a base of the radome. The housing receives an electrically conductive strip in contact with an inner surface of an outer wall, or according to the circumstances flush with the outer wall, of the composite structure. A conductive base is situated in the region of the radome base and connected to a ground of the aircraft. The composite structure of the radome is devoid of any perforations or through-passages in the region of the electrically conductive strip, and a first end of the electrically conductive strip is in contact with the conductive base.
RADÔME D'AÉRONEF INTÉGRANT UN SYSTÈME DE PROTECTION PARAFOUDRE ET AÉRONEF COMPRENANT UN TEL RADÔME
AIRCRAFT RADOME INCORPORATING A LIGHTNING PROTECTION SYSTEM, AND AIRCRAFT COMPRISING SUCH A RADOME
RADOM EINES LUFTFAHRZEUGS, DAS EIN BLITZSCHUTZSYSTEM UMFASST, UND LUFTFAHRZEUG, DAS EIN SOLCHES RADOM UMFASST
2025-03-05
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS / H02G INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES , Verlegen oder Installieren elektrischer Kabel oder Leitungen, Verlegen oder Installieren kombinierter optischer und elektrischer Kabel oder Leitungen |
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