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Mechanical properties and durability of a composite material at cryogenic temperatures.

机译:复合材料在低温下的机械性能和耐久性。

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摘要

Several issues relevant to the use of a high-performance graphite-epoxy material in hydrogen storage tank applications have been examined. The tensile properties of IM7/977-2 were evaluated as a function of test temperature and thermal-mechanical load history. The temperature dependent coefficient of thermal expansion (CTE) of unidirectional specimens of the same material was measured between -200°C and 0°C. The effects of test temperature, mechanical loading, and damage state on the leak rate of hydrogen gas through IM7/977-2 laminates were evaluated using a novel test system. Finally, the mechanical properties of several commercially available polymer films, which might prove useful as leak-resistant liners for composite cryogenic fuel tanks, were evaluated at elevated and cryogenic temperatures.; The mechanical property study of IM7/977-2 showed that the effects of exposure to a cryogenic fuel tank environment varied significantly with test temperature and laminate schedule. Matrix dominated properties were found to be the most strongly affected by cryogenic test temperature exposure. Fiber-dominated properties were found to be comparatively insensitive to cryogenic test temperature.; The CTE measurements showed that the cryogenic conditioning did not have marked effects on the thermal expansion behavior of IM7/977-2. Transverse CTE was Coefficient of thermal expansion was calculated strongly temperature-dependent.; The leak rate study revealed that both mechanical loading and decreasing test temperatures increase the leak rate of gaseous hydrogen through the microcrack network within a damaged composite laminate. The effect of temperature on permeability was shown to be stronger than that of tensile loading. At low damage levels, proportionality was demonstrated between the number of crack junctions present within the laminate and the hydrogen gas leak rate. At higher damage levels this proportionality was not as clear, perhaps due to the greater role played by delaminations in gas leakage.; In the polymer film study, large differences were observed in tensile modulus and tensile strength at 23°C and 65°C. At -150°C, the differences were far smaller and the behavior of all of the films was uniformly brittle in nature.
机译:已经研究了与在储氢罐应用中使用高性能石墨环氧材料有关的几个问题。 IM7 / 977-2的拉伸性能根据测试温度和热机械负荷历史来评估。在-200°C至0°C之间测量了相同材料的单向试样的温度相关热膨胀系数(CTE)。使用新型测试系统评估了测试温度,机械负载和损坏状态对通过IM7 / 977-2层压板的氢气泄漏率的影响。最后,在高温和低温下评估了几种可商购的聚合物薄膜的机械性能,这些薄膜可能被证明可用作复合低温燃料箱的防漏衬里。 IM7 / 977-2的机械性能研究表明,暴露于低温燃料箱环境的影响随测试温度和层压时间表的不同而有很大不同。发现基体主导的性能受低温测试温度的影响最大。发现纤维主导的性能对低温测试温度相对不敏感。 CTE测量表明,低温调节对IM7 / 977-2的热膨胀行为没有明显影响。横向CTE为热膨胀系数,与温度高度相关。泄漏率研究表明,机械载荷和降低的测试温度都会增加损坏的复合层压板中通过微裂纹网络的气态氢的泄漏率。结果表明,温度对渗透率的影响要强于拉伸载荷。在低损伤水平下,层压板内存在的裂纹连接数与氢气泄漏率之间成比例。在较高的破坏水平下,这种比例性并不清楚,这可能是由于分层在气体泄漏中发挥了更大的作用。在聚合物膜研究中,在23°C和65°C下观察到拉伸模量和拉伸强度存在很大差异。在-150℃下,差异要小得多,并且所有薄膜的行为本质上都是均匀的脆性。

著录项

  • 作者

    Grenoble, Ray Walton.;

  • 作者单位

    Old Dominion University.;

  • 授予单位 Old Dominion University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2006
  • 页码 264 p.
  • 总页数 264
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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