To provide an integrated, multi-functional surface protection system that is suitable for placement on composite structures or composite parts, such as aircraft and aerospace composite structures and composite parts.SOLUTION: An integrated surface protection system (22) comprises: a single layer (24) comprising an electrically conductive network (26) and a fiber reinforcement material (28). The electrically conductive network (26) comprises a metal, which is, e.g., copper or aluminum. The electrically conductive network (26) may comprise an electrically conductive non-metal, which is, e.g., graphene or carbon nanotubes. The fiber reinforcement material (28) comprises at least one of glass fiber and carbon fiber. The single layer (24) further comprises a matrix material (27) supporting the electrically conductive network (26) and the fiber reinforcement material (28).SELECTED DRAWING: Figure 2
【課題】航空機や航空宇宙用の複合材構造及び複合材部品などの複合材構造及び複合材部品への配置に適した多機能一体型表面保護システムを提供する。【解決手段】一体型表面保護システム(22)は、導電性の網目構造(26)と繊維強化材料(28)とを含む単層レイヤ(24)を含む。導電性網目構造(26)は、金属を含み、この金属は、例えば、銅又はアルミニウムである。また、導電性網目構造(26)は、導電性の非金属を含むことができ、この非金属は、例えば、グラフェン又はカーボンナノチューブである。繊維強化材料(28)は、ガラス繊維と炭素繊維とのうちの少なくとも1つを含む。単層レイヤ(24)は、さらに、導電性網目構造(26)と繊維強化材料(28)とを担うマトリックス材料(27)を含む。【選択図】図2
INTEGRATED SURFACE PROTECTION SYSTEM, COMPOSITE STRUCTURE, AND METHOD FOR PROTECTING THE SAME
一体型表面保護システム、複合材構造、及び、その保護方法
2020-04-16
Patent
Electronic Resource
Japanese
IPC: | C08J Verarbeitung , WORKING-UP / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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