首页> 外文会议>Symposium on Lightweight Alloys for Aerospace Application, Feb 12-14, 2001, New Orleans, LA, USA >DEFORMATION, FRACTURE AND FATIGUE IN A DISPERSION STRENGTHENED ALUMINUM ALLOY
【24h】

DEFORMATION, FRACTURE AND FATIGUE IN A DISPERSION STRENGTHENED ALUMINUM ALLOY

机译:弥散强化铝合金的变形,断裂和疲劳

获取原文
获取原文并翻译 | 示例

摘要

Numerous attempts to produce aluminum alloys that retain useful property levels after extended exposure to elevated temperatures have been made in the past two decades. The typical approach has been to create a fine grain material that is stabilized against grain growth by the presence of numerous dispersoids. The dispersoid composition is generally tailored so as to inhibit coarsening (either oxide dispersion or transition metal bearing intermetallics). This paper reports the fatigue, fracture, and tensile behavior of a dispersion strengthened alloy consisting of a nearly pure aluminum matrix reinforced by a few volume percent of Al_2O_3. The behavior of this alloy is compared to that of previously developed dispersion strengthened aluminum alloys. While the properties of the new material are reasonably good, it suffers from drawbacks similar to those exhibited by other DS-A1 alloys, notably reduced ductility with increasing temperature, low uniform elongation, minimal work hardening, and relatively low fatigue crack growth threshold at low stress ratio.
机译:在过去的二十年中,已经进行了许多尝试来生产铝合金,这些铝合金在长时间暴露于高温下仍保持有用的性能水平。典型的方法是创建一种细晶粒材料,该材料由于存在大量分散质而稳定,可防止晶粒长大。通常调整分散体的组成以抑制变粗(氧化物分散体或带有过渡金属的金属间化合物)。本文报道了一种弥散强化合金的疲劳,断裂和拉伸行为,该弥散强化合金由几乎纯的铝基体组成,并由少量体积的Al_2O_3增强。将该合金的性能与先前开发的弥散强化铝合金的性能进行了比较。尽管新材料的性能相当不错,但它也具有与其他DS-A1合金相似的缺点,尤其是随着温度的升高而延展性降低,均匀伸长率低,加工硬化最小以及在低温下疲劳裂纹扩展阈值相对较低应力比。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号