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Ballistic impact performance of multi-phase STF-impregnated Kevlar fabrics in aero-engine containment

机译:气孔发动机遏制中多相STF浸渍Kevlar织物的弹道冲击性能

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摘要

The current study focus on the multi-phase Shear thickening fluid (STF) treated high-strength fabrics which is an promising material for soft-wall containment casing. Three types of multi-phase STF were manufactured by adding graphene oxide (GO) and carbon nanotubes (CNTs) to a nanosilica suspension system. Steady rheological property tests and yarn pull-out tests were conducted to determine the shear thickening behavior of the multiphase STFs and inter-yarn friction of their compound fabrics. Ballistic impact tests were conducted using titanium blade-like projectiles. The energy absorption, deformation evolution and damage patterns were investigated. Tests show that the addition of GO and CNTs resulted in a higher initial viscosity, a lower shear rate for onset of shear thickening and a lower thickening ratio. The enhancement of the frictional force is more striking for multi-phase STFs. The GO additives have the highest deformation in the ballistic impact tests, corresponding to the greatest energy absorption with a ballistic performance index 78.3% higher than that of neat fabrics. The results show great potential for reducing the weight of containment casing.
机译:目前的研究集中在多相剪切增稠流体(STF)处理的高强度织物,其是用于软壁容纳外壳的有前途的材料。三种类型的多相STF的通过添加氧化石墨烯(GO)和碳纳米管(CNT),以一个纳米二氧化硅悬架系统制造。稳定的流变性能试验和纱线拉出测试以确定它们的化合物织物的多相STFS和纱间摩擦的剪切增稠行为。弹道冲击测试使用钛刀锋般的弹丸进行。能量吸收,变形的演变和损坏模式进行了研究。测试表明,加入GO和CNT的导致更高的初始粘度,剪切增稠的发作的较低剪切速率和较低的增粘率。摩擦力的增强是多阶段STFS更引人注目。该GO添加剂必须在弹道冲击试验最高变形,对应最大的能量吸收具有防弹性能指标比纯面料高78.3%。结果表明,减少容纳外壳的重量很大的潜力。

著录项

  • 来源
    《Thin-Walled Structures》 |2020年第2期|107103.1-107103.14|共14页
  • 作者单位

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;

    Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;

  • 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

    Containment casing; Kevlar fabric; Shear thickening fluid; Ballistic impact; Rheological behavior; Yarn pull-out;

    机译:遏制套管;Kevlar织物;剪切增厚液;弹道撞击;流变行为;纱线拉出;

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