航空用蜂窝复合材料夹层结构制造参数优化

2013 International Conference on Aerospace Science & Engineering (ICASE) Pub Date : 2013-08-01 DOI:10.1109/ICASE.2013.6785560

U. Farooq, A. A. Khurram, M. Ahmad, S. A. Rakha, N. Ali, A. Munir, T. Subhani

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引用次数: 2

摘要

由对芳纶纸蜂窝芯和碳纤维环氧基复合材料面板组成的夹层结构用于航空航天应用。采用两种不同类型的粘接膜对蜂窝芯和复合片材进行粘接。对胶膜的固化温度和固化时间进行了优化，以获得最大的粘接强度。

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Optimization of the manufacturing parameters of honeycomb composite sandwich structures for aerospace application

Sandwich structures comprising para-aramid paper honeycomb core and carbon fiber epoxy matrix composite facesheets were fabricated for aerospace applications. For the adhesion of honeycomb core and composite facesheets, two different types of adhesive films were used. The curing parameters for adhesive films, including temperature and time, were optimized for maximum bonding strength.

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2013 International Conference on Aerospace Science & Engineering (ICASE)

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