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High Temperature Fatigue of Carbon/Polyimide 8-harness Satin Woven Composites. Part I: Digital Image Correlation and Micro-Computed Tomography Damage Characterization
Composite Structures ( IF 6.3 ) Pub Date : 2020-07-01 , DOI: 10.1016/j.compstruct.2020.112255
Yannick Pannier , Federico Foti , Marco Gigliotti

Abstract This paper focuses on the experimental high temperature fatigue of Carbon/polyimide 8-harness satin woven composite materials. Traction-traction (R = 0.1) fatigue tests at 250 °C are carried out on Carbon/polyimide [45]6 8-harness satin woven composites under three different environments (air, 2 bar N2, 2 bar O2). Part I is specifically devoted to image based damage characterization by employment of Digital Image Correlation (DIC) and Micro-Computed Tomography (µ-CT) techniques. For the used samples, intra tow matrix cracks along fibres on the external plies are the first damage form at the ply-scale. Damage evolution on the sample surface can be followed during the test (in situ) by using 2D DIC. Moreover, fatigue tests are periodically interrupted to perform µ-CT scans to characterize and quantify the damage in the volume of the samples. The obtained results prove that the damage assessment methods presented in this work are suitable for environmentally-assisted fatigue tests on composite materials.

中文翻译:

碳/聚酰亚胺 8 线束缎纹编织复合材料的高温疲劳。第一部分:数字图像相关和微计算机断层扫描损伤表征

摘要 本文重点研究了碳/聚酰亚胺8线缎纹编织复合材料的高温疲劳试验。在三种不同环境(空气、2 bar N2、2 bar O2)下对碳/聚酰亚胺 [45]6 8 线束缎纹编织复合材料进行了 250 °C 的牵引-牵引 (R = 0.1) 疲劳测试。第一部分专门介绍通过使用数字图像相关 (DIC) 和微计算机断层扫描 (μ-CT) 技术进行基于图像的损伤表征。对于使用过的样品,外部层上沿纤维的丝束内基体裂纹是层级的第一种损伤形式。通过使用 2D DIC,可以在测试(原位)期间跟踪样品表面的损伤演变。此外,疲劳测试会定期中断以执行 µ-CT 扫描,以表征和量化样品体积中的损坏。
更新日期:2020-07-01
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