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Non-Destructive Evaluation Measurements and Fracture Effects in Carbon/Epoxy Laminates Containing Porosity

机译:含孔隙的碳/环氧层压板的无损评估测量和断裂效应

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摘要

Carbon fiber composites have been increasingly used in aerospace, military, sports, automotive and other fields due to their excellent properties, including high specific strength, high specific modulus, corrosion resistance, fatigue resistance, and low thermal expansion coefficient.;Delamination, or interlaminar fracture, is a serious failure mode leading to a loss in composite stiffness and strength. Manufacturing process defects degrade the fatigue life and delamination resistance of the composite. This study investigates the effect of porosity on fatigue interlaminar fracture behavior of carbon fiber composites.;Carbon fiber reinforced epoxy samples with different vacuum levels: 0%, 50% and 100% of full vacuum were fabricated using the hand layup vacuum bagging manufacturing process. Porosity was evaluated using eight different NDE methods: X-Ray laminography, X-Ray refraction, ultrasonic testing, high frequency eddy current imaging, pulse thermography, pulse phase thermography and lock-in-thermography, and thermal conductivity measurements. Then, the static interlaminar fracture behavior under Mode I was conducted, as well as Mode I in fatigue. Fractography was implemented on the samples tested by static and fatigue Mode I. Finally, the destructive technique of serial sectioning (SS) was undertaken in two orientations: through-thickness (planar sectioning), and cross-thickness (cross sectioning).;The results of X-Ray Refraction and thermal conductivity measurements were the most successful NDE technique for quantifying porosity in the carbon fiber composite materials, because both methods gave specific fixed values with the porosity. The results of X-Ray laminography, pulse thermography, pulse phase thermography and ultrasonic were also successful NDE techniques for evaluating porosity shape, area fractions, size and distribution since they gave images for the porosity. Lock-in-Thermography showed the depth of porosity in the carbon fiber composite material, and eddy current showed how the carbon fibers were oriented in the composite material.;Serial sectioning magnified images showed the features of internal microstructure such as porosity type, morphology, distribution and location. Results of static Mode I interlaminar fracture tests showed that porosity could lead to a decrease in interlaminar fracture toughness. In addition, the presence of porosity leads to a decrease in Mode I cyclic strain energy release rate fatigue life.;Finally, all approaches conducted were correlated: the resulting NDE percentages and parameters were correlated with the features revealed by the destructive test of serial sectioning and static and fatigue values and fractographic images in order to quantify delamination and porosity.
机译:碳纤维复合材料由于其优异的性能,包括高比强度,高比模量,耐腐蚀性,耐疲劳性和低热膨胀系数,而在航空航天,军事,体育,汽车和其他领域得到越来越多的使用。断裂是导致复合材料刚度和强度损失的严重破坏模式。制造过程中的缺陷会降低复合材料的疲劳寿命和抗分层性。这项研究调查了孔隙率对碳纤维复合材料疲劳层间断裂行为的影响。;不同真空度的碳纤维增强环氧树脂样品:采用手工叠层真空包装工艺制造了全真空度的0%,50%和100%。使用八种不同的NDE方法评估孔隙率:X射线分层成像,X射线折射,超声测试,高频涡流成像,脉冲热成像,脉冲相位热成像和锁定热成像以及热导率测量。然后,进行了模式I下的静态层间断裂行为以及疲劳状态下的模式I。在通过静态和疲劳模式I测试的样品上实施了分形照相术。最后,在两个方向上进行了连续切片(SS)的破坏性技术:贯穿厚度(平面切片)和交叉厚度(横截面)。 X射线折射和热导率测量的结果是定量碳纤维复合材料中孔隙率最成功的NDE技术,因为这两种方法都给出了特定的孔隙率固定值。 X射线分层成像,脉冲热成像,脉冲相位热成像和超声技术的结果也是成功的NDE技术,可用于评估孔隙形状,面积分数,尺寸和分布,因为它们给出了孔隙率图像。锁定热像仪显示碳纤维复合材料中的孔隙深度,涡流显示碳纤维在复合材料中的取向。串行截面放大图像显示了内部微观结构的特征,如孔隙类型,形态,分布和位置。静态I型层间断裂试验结果表明,孔隙度可能导致层间断裂韧性降低。此外,孔隙的存在会导致I型循环应变能释放速率疲劳寿命的降低。最后,所有进行的方法都相互关联:所得的NDE百分比和参数与连续切片破坏性试验所揭示的特征相关静态和疲劳值以及分形图像以量化分层和孔隙率。

著录项

  • 作者

    Hakim, Issa A.;

  • 作者单位

    University of Dayton.;

  • 授予单位 University of Dayton.;
  • 学科 Mechanical engineering.
  • 学位 Ph.D.
  • 年度 2017
  • 页码 166 p.
  • 总页数 166
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 人类学;
  • 关键词

  • 入库时间 2022-08-17 11:54:27

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