| タイトル | Combining Through-Thickness Reinforcement and Self-Healing for Improved Damage Tolerance and Durability of Composites |
| 本文（外部サイト） | http://hdl.handle.net/2060/20130013399 |
| 著者（英） | Greenhalgh, Emile S.; O'Brien, T. Kevin; Czabaj, Michael W.; Hinkley, Jeffrey A.; Trask, Richard; Tsampas, Spiros; McCombe, Gregory; Bond, Ian P. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2013-05-01 |
| 言語 | eng |
| 内容記述 | A study was undertaken to develop a prototype method for adding through-thickness hollow glass tubes infused with uncured resin and hardener in a carbon Z-pin through-thickness reinforcement field embedded in a composite laminate. Two types of tube insertion techniques were attempted in an effort to ensure the glass tubes survived the panel manufacturing process. A self-healing resin was chosen with a very low viscosity, two component, liquid epoxy resin system designed to be mixed at a 2-to-1 ratio of epoxy to hardener. IM7/8552 carbon epoxy double cantilever beam (DCB) specimens were cut from the hybrid Z-pin and glass tube reinforced panels and tested. In-situ injection of resin and hardener directly into glass tubes, in a staggered pattern to allow for 2-to-1 ratio mixing, resulted in partial healing of the fracture plane, but only if the injection was performed while the specimen was held at maximum load after initial fracture. Hence, there is some potential for healing delamination via resin and hardener delivered through a network of through-thickness glass tubes, but only if the tubes are connected to a reservoir where additional material may be injected as needed. |
| NASA分類 | Composite Materials |
| レポートNO | NASA/TM-2013-217988
NF1676L-16561
L-20252 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
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