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Dynamic deformation and failure of Gamma-Met PX at room and elevated temperatures.

机译:Gamma-Met PX在室温和高温下的动态变形和破坏。

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摘要

Recently, a new generation of gamma-TiAl alloys, Gamma-Met PX, has been developed. The lack of data on this material and its potential use for aerospace application makes it important to understand its response under different conditions, especially its behavior under dynamic loading capabilities. Studies of bird strike, hard particle impact damage, and fan blade containment within the jet engine during normal and abnormal operations and proper simulations of these events require material properties not only at high strain rates but also coupled with high temperatures. Such materials properties can be obtained from simple geometry laboratory experiments such as those performed in the present study. These experiments include evaluation of material response under dynamic uniaxial loading, dynamic fracture initiation toughness, and shock compression properties.; The compression and tensile tests are conducted using a split-Hopkinson bar apparatus at test temperatures up to 900°C and strain rates of up to 3500s-1. Under uniaxial compression, at temperatures higher than 600°C, thermal softening is observed at all strain rates employed in the present study with the rate of thermal softening increasing dramatically between 800°C and 900°C. The room temperature tensile tests show negligible strain-rate dependence on both yield stress and flow stress. However, the material shows a drop in both yield and flow stress at elevated temperatures. No anomaly in yield stress is observed up to 900°C.; The dynamic fracture toughness initiation study was performed using the modified Hopkinson Pressure Bar. The dynamic fracture initiation toughness was found to decrease with an increase in test temperatures. Moreover, long term elevated temperature exposures were found to be detrimental to fracture toughness.; Normal plate impact experiments were conducted using single stage gas gun to obtain shock properties under uniaxial strain compression. Gamma-Met PX has a Hugoniot Elastic Limit (HEL) of 1.88 GPa at target thickness of 3.86 mm. The decay in the elastic precursor is continuous without showing an asymptotic to a constant value within the range of target thicknesses studied. Under shock compression, Gamma-Met PX showed post yield hardening, however, the impact velocity has little or no effect on the rate of strain hardening. The measured spall strength of Gamma-Met PX was 1.8 +/- 0.09 GPa.
机译:最近,已经开发了新一代的γ-TiAl合金,即Gamma-Met PX。这种材料的数据缺乏及其在航空航天应用中的潜在用途,因此了解其在不同条件下的响应,尤其是其在动态载荷能力下的性能非常重要。在正常和异常运行过程中,对鸟击,硬质颗粒撞击损伤和喷气发动机内的风扇叶片密闭性的研究以及对这些事件的正确模拟,不仅需要在高应变速率下而且还要在高温下具有材料特性。可以从简单的几何实验室实验(例如本研究中执行的实验)获得此类材料的性能。这些实验包括评估动态单轴载荷下的材料响应,动态断裂起始韧性和冲击压缩性能。使用分裂霍普金森棒设备在最高900°C的测试温度和最高3500s-1的应变速率下进行压缩和拉伸测试。在单轴压缩下,在高于600°C的温度下,在本研究中采用的所有应变速率下均观察到热软化,并且在800°C至900°C之间热软化速率急剧增加。室温拉伸试验表明,应变率对屈服应力和流动应力的影响可忽略不计。然而,该材料在高温下显示出屈服应力和流应力的下降。高达900°C时未观察到屈服应力异常。使用改进的霍普金森压力棒进行动态断裂韧性的初始研究。发现动态断裂起始韧性随测试温度的升高而降低。此外,发现长期高温暴露不利于断裂韧性。使用单级气枪进行正常的板冲击实验,以获得单轴应变压缩下的冲击性能。 Gamma-Met PX的目标厚度为3.86 mm时,其Hugoniot弹性极限(HEL)为1.88 GPa。弹性前驱体的衰减是连续的,并且在所研究的目标厚度范围内未显示渐近线至恒定值。在冲击压缩下,Gamma-Met PX表现出屈服后硬化,但是,冲击速度对应变硬化速率几乎没有影响。测得的Gamma-Met PX的剥落强度为1.8 +/- 0.09 GPa。

著录项

  • 作者

    Shazly, Mostafa.;

  • 作者单位

    Case Western Reserve University.;

  • 授予单位 Case Western Reserve University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2005
  • 页码 263 p.
  • 总页数 263
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

  • 入库时间 2022-08-17 11:42:05

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