...
首页> 外文期刊>Materials Science and Technology: MST: A publication of the Institute of Metals >Low cycle fatigue and creep-fatigue interaction in short fibre reinforced aluminium alloy composite
【24h】

Low cycle fatigue and creep-fatigue interaction in short fibre reinforced aluminium alloy composite

机译:短纤维增强铝合金复合材料的低周疲劳和蠕变疲劳相互作用

获取原文
获取原文并翻译 | 示例
           

摘要

The high temperature low cycle fatigue resistance and the creep-fatigue interaction (CFI) behaviour in terms of the effects of prior fatigue exposure on the subsequent creep behaviour are evaluated and reported for a short alumina fibre (Saffil) reinforced aluminium alloy (AI-12Si-CuMgNi) matrix composite at 623 K. The prior fatigue to study the CFI behaviour was imparted in the form of low cycle fatigue loading in a fully reversed, total strain controlled loading up to a quarter of fatigue life at a total strain amplitude of 0-006 (the plastic strain amplitude at half-life is 0-004), corresponding to a plastic strain energy per cycle value of 0-46 MJ m~(-3). Subsequently, isothermal tensile creep tests were conducted at 623 K to evaluate the minimum creep rate, rupture time and strain to failure as a function of applied creep stress. Also examined were the fracture features as well as the nature and extent of damage that occurs during low cycle fatigue and creep-fatigue loading. The results obtained on the composite material are compared with those of the matrix aluminium alloy to bring out the effects of reinforcement. The results showed that the reinforcement causes significant loss in high temperature low cycle fatigue resistance in terms of fatigue ductility and cyclic energy parameters. Prior fatigue loading was seen to cause a small but consistent decrease in the creep resistance, which is attributed to the combined effects of mechanical loading and microstructural damage from prior fatigue loading.
机译:就短氧化铝纤维(Saffil)增强铝合金(AI-12Si)而言,评估并报告了高温,低周疲劳强度和蠕变疲劳相互作用(CFI)行为(根据先前的疲劳暴露对随后的蠕变行为的影响)。 -CuMgNi)基复合材料在623K。研究CFI行为的先前疲劳是以低循环疲劳载荷的形式给出的,该载荷在完全反向,总应变控制的载荷下达到完全疲劳振幅的四分之一,总应变幅度为0。 -006(半衰期的塑性应变幅度为0-004),对应于每个循环的塑性应变能值为0-46 MJ m〜(-3)。随后,在623 K下进行了等温拉伸蠕变试验,以评估最小蠕变速率,断裂时间和断裂应变与所施加蠕变应力的关系。还检查了在低周疲劳和蠕变疲劳载荷过程中发生的断裂特征以及损伤的性质和程度。将在复合材料上获得的结果与基体铝合金的结果进行比较,以得出增强效果。结果表明,就疲劳延展性和循环能量参数而言,这种增强材料会导致高温低周疲劳强度的显着降低。先前的疲劳载荷被认为会引起抗蠕变性能的微小但持续的下降,这归因于机械载荷和先前疲劳载荷对微观结构的损害。

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