PROBLEM TO BE SOLVED: To provide an inexpensive and robust technique for temporarily repairing outer composite aircraft skins that utilize copper foil along fastener rows for lightning strike protection that have been altered by lightning strikes or in some other way.SOLUTION: A repair apparatus for an electrically conductive layer 110 of a composite structure includes a conductive layer secured over a dielectric layer 104 and to the structure around the entirety of the perimeter of the dielectric layer, the conductive layer treated along a perimeter region 120 thereof to improve a conductive path between the conductive layer and the structure.
【課題】落雷又は別の方法で変えられた落雷保護用の留め具列に沿って、銅箔を用いる外側の複合航空機外板を、一時的に修復するための、低価格かつ強固な技術を提供する。【解決手段】複合構造の導電層110のための修復装置は、誘電体層104上に固定され、誘電体層の境界全体の周囲で構造に固定される導電層であって、導電層と構造との間の導電性パスを改良するために、その境界領域120に沿って処理される導電層を備える。【選択図】図4
REPAIR APPARATUS AND METHOD FOR COMPOSITE PANELS HAVING CONDUCTIVE LAYER
導電層を有する複合パネルのための修復装置及び方法
2015-09-28
Patent
Elektronische Ressource
Japanisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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