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Temperature Effects on the Mechanical Behaviour of PAEK Thermoplastic Composites Subjected to High Strain Rates Under Compression Loading

机译:对压缩负荷高应变率进行高应变率的PAEK热塑性复合材料的温度效应

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摘要

This work presents an experimental study on the mechanical behaviour of thermoplastic polyarlyetherketone (PAEK) based composite laminates reinforced with woven carbon fibres, subjected to high strain rates under compression loading. The specimens were tested using a Split Hopkinson Pressure Bar (SHPB). The tests covered the working temperatures and stress envelopes of -54 degrees C, RT (25 degrees C), and 80 degrees C, each tested at six different off-axis angles. The high-speed imaging system was used to monitor the failure process. The strain on the loading direction was determined using Digital Image Correlation (DIC). Fractography analysis was performed to understand the influence of temperature on the damage aspects, using Scanning Electron Microscopy (SEM). The -54 degrees C and RT SHPB tests showed more intralaminar damage aspects than the ones tested at 80 degrees C, which presented a preference for the interlaminar damage aspect and exhibited the lowest strength. A new failure criterion dependent on temperature and strain rate was proposed, based on a phenomenological approach and experimental results. The fabric architecture at the ply level was idealised as a two-part mosaic model. The crystallinity of the PAEK thermoplastic matrix was analysed using Differential Scanning Calorimetry (DSC). Results showed no evidence of crystallinity degree variation induced by the high strain rate tests.
机译:该工作介绍了用织造碳纤维加固的热塑性聚甲醚酮(PAEK)复合层压板的力学行为的实验研究,在压缩负载下进行高应变率。使用分裂霍普金森压棒(SHPB)测试标本。该试验覆盖了-54摄氏度,RT(25℃)和80℃的工作温度和应力包络,每次在六个不同的离轴角度测试。高速成像系统用于监控故障过程。使用数字图像相关(DIC)确定加载方向上的应变。使用扫描电子显微镜(SEM)来进行Fractography分析以了解温度对损伤方面的影响。 -54℃和RT SHPB测试显示比在80℃下测试的胰蛋白酶损伤的损伤方面更多,这提出了对层间损伤方面的偏好并表现出最低强度。基于现象学方法和实验结果,提出了一种依赖于温度和应变速率的新故障标准。 PLY水平的织物架构是作为两部分马赛克模型的理想化。使用差示扫描量热法(DSC)分析了PAEK热塑性基质的结晶度。结果显示,没有通过高应变速率试验引起的结晶度变化的证据。

著录项

  • 来源
    《Composite Structures》 |2021年第4期|113299.1-113299.14|共14页
  • 作者单位

    Inst Tecnol Aeronaut Dept Aeronaut Praca Marechal Eduardo Gomes 50 BR-12228900 Sao Jose Dos Campos SP Brazil;

    Inst Tecnol Aeronaut Dept Aeronaut Praca Marechal Eduardo Gomes 50 BR-12228900 Sao Jose Dos Campos SP Brazil;

    Ctr Univ Fundacao Educ Inaciana Pe Saboia de Mede Dept Mat Engn Ave Humberto de Alencar Castelo Branco 3972 BR-09850901 Sao Bernardo Do Campo SP Brazil;

    Inst Tecnol Aeronaut Dept Aeronaut Praca Marechal Eduardo Gomes 50 BR-12228900 Sao Jose Dos Campos SP Brazil|Technol Coll Sao Jose dos Campos Ave Cesare Mansueto Giulio Lattes 1350 BR-12247014 Sao Jose Dos Campos SP Brazil;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Thermoplastic resin; Fabrics/textiles; Impact behaviour; Analytical modelling; Fractography; Thermal analysis;

    机译:热塑性树脂;织物/纺织品;影响行为;分析建模;Fractography;热分析;
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