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| 1 | 镍基合金超声疲劳裂纹扩展寿命预测研究显示文摘针对发动机结构材料承受高频循环载荷的特点,应用超声疲劳试验技术开展了镍基合金材料的疲劳裂纹扩展试验研究。考虑高频载荷下疲劳裂纹扩展过程中的温升效应,测试了超声疲劳裂纹扩展过程中的温度变化,基于温度变化对材料弹性模量的影响和热膨胀效应,数值计算了疲劳裂纹扩展应力强度因子。研究了温度变化对超声疲劳裂纹扩展的影响机制,并在现有模型基础上,建立了考虑温度影响的超声疲劳裂纹扩展模型,完善疲劳裂纹扩展寿命预测方法。 | 薛红前 姜祎君 封硕 | 2014 | 材料工程2014，42，3： | 8 |
| 2 | DZ125镍基合金的显微组织与蠕变行为显示文摘通过蠕变性能测试及组织形貌观察,研究DZ125合金的高温蠕变行为。结果表明:经完全热处理后,合金在枝晶干/间区域存在明显的组织不均匀性,粗大γ′相存在于枝晶问,细小γ′相存在于枝晶干。蠕变初期合金中γ′相已转变成筏状结构,稳态蠕变期间合金的变形机制是位错攀移越过γ′相,其中,位错攀移期间,易形成位错的割阶,空位的形成和扩散是位错攀移的控制环节。而蠕变后期合金的变形机制是位错在基体中滑移和剪切进入筏状γ′相。在高温蠕变后期,合金中裂纹首先在晶界处萌生与扩展,且不同形态晶界具有不同的损伤特征,其中,沿应力轴成45°角晶界承受蠕变损伤的较大剪切应力可使其发生较大几率的蠕变损伤;而加入的元素Hf促进细小粒状相沿晶界的析出,可抑制晶界滑移,提高晶界强度,是合金蠕变断裂后晶界呈现非光滑表面的主要原因。 | 田宁 田素贵 于慧臣 孟宪林 | 2014 | 中国有色金属学报2014，24，5： | 6 |
| 3 | Stress Relaxation Behavior of GH4169 Superalloy显示文摘GH4169 superalloy stress relaxation test was investigated to study its characteristics of stress relaxation curves at various temperatures( 550,650,and 750 ℃). These curves presented jointly two distinct stages,the stage of inner stress relaxing quickly,and the stage of inner stress relaxing slowly and closing to the stress relaxation limit. And these curves obtained could be fitted by second order exponential decay function well. Based on the experimental stress relaxation curves,the relationship between stress relaxation rate and time were derived, which showed that the higher relaxation temperature and the greater initial rate of stress relaxation. The whole process presented two different stages,the stage of stress relaxation rate falling rapidly and the stage of stress relaxation rate slowing down and tending to be constant. The relation curve between creep strain rate and stress of GH4169 superalloy can be divided into three stages,low stress stage,transition stage,and high stress stage.Both the high stage and the low stage present linear correlation. | 常鹏鹏 孔永华 陈国胜 谢黎雄 朱世根 | 2015 | Journal of Donghua University(English Edition)2015，32，1： | 0 |
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