日本複合材料学会誌
Online ISSN : 1884-8559
Print ISSN : 0385-2563
ISSN-L : 0385-2563
研究論文
CFRPの構成要素が飛翔体衝突変形挙動とエネルギー散逸に与える影響
田邊 靖博山田 昌義小林 信介佐藤 成道橋本 雅弘
著者情報
ジャーナル フリー

2013 年 39 巻 1 号 p. 16-23

詳細
抄録
Carbon fiber reinforced plastic (CFRP) is widely used in making structural components of aircraft because of its high specific strength and high specific elasticity. Since aircrafts are inevitable risks from foreign object damage (FOD), it is important to understand the effects of elements, i.e., fiber, matrix resin and interface, in CFRP on the impact phenomena of CFRP by projectile’s impact. In this study, we conducted impact tests and investigated the effects of the elements on its impact phenomena and dissipated energy by using three-dimensional (3D) measurements in the deformation process under high-velocity projectile impact. It was estimated that deformation of CFRP was dissipated more than 30%, ever 70% in a greater case, of the kinetic energy of a projectile. It was also revealed that the CFRP, consisting of carbon fiber with high-strength and large-failure-strain and deformable resin, could dissipate large kinetic energy of a projectile.
著者関連情報
© 2013 日本複合材料学会
前の記事 次の記事
feedback
Top