METHOD AND APPARATUS FOR PROVIDING CURRENT RETURN NETWORK IN AIRCRAFT STRUCTURE
PROBLEM TO BE SOLVED: To provide a current return network assembly that does not add weight to an aircraft.SOLUTION: A current return network assembly 100 for an aircraft having a predetermined potential lightning strike zone is installed within the predetermined potential lightning strike zone. The...
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Sprache: | eng ; jpn |
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Zusammenfassung: | PROBLEM TO BE SOLVED: To provide a current return network assembly that does not add weight to an aircraft.SOLUTION: A current return network assembly 100 for an aircraft having a predetermined potential lightning strike zone is installed 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. The electrically conductive honeycomb central core 102 conducts electrical current, which is caused by a lightning strike on the aircraft at the zone, through the assembly and the zone.
【課題】航空機に重量を付加しない電流リターンネットワークアセンブリを提供する。【解決手段】所定の潜在的落雷ゾーンを有する航空機用の電流リターンネットワークアセンブリ100は、所定の潜在的落雷ゾーン内に取り付けられる。電流リターンネットワークアセンブリは、アセンブリと所定の潜在的落雷ゾーンとの両方を通して電流を伝導する導電性のハニカム中央コア102を含む。電流は、航空機の所定の潜在的落雷ゾーンへの落雷により生じる。導電性のハニカム中央コア102は、航空機の前記ゾーンへの落雷により生じた電流を、前記アセンブリおよび前記ゾーンを通して伝導する。【選択図】図3A |
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