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Effects of fine porosity on the fatigue behavior of a powder metallurgy superalloy

机译:细孔对粉末冶金高温合金疲劳性能的影响

摘要

Hot isostatically pressed powder metallurgy Astroloy was obtained which contained 1.4 percent fine porosity at the grain boundaries produced by argon entering the powder container during pressing. This material was tested at 650 C in fatigue, creep fatigue, tension, and stress-rupture and the results compared with previous data on sound Astroloy. The pores averaged about 2 micrometers diameter and 20 micrometers spacing. They did influence fatigue crack initiation and produced a more intergranular mode of propagation. However, fatigue life was not drastically reduced. A large 25 micrometers pore in one specimen resulting from a hollow particle did not reduce life by 60 percent. Fatigue behavior of the porous material showed typical correlation with tensile behavior. The plastic strain range life relation was reduced proportionately with the reduction in tensile ductility, but the elastic strain range-life relation was little changed reflecting the small reduction in sigma sub u/E for the porous material.
机译:获得了热等静压粉末冶金Astroloy,其在氩气压制过程中进入粉末容器所产生的晶界处含有1.4%的细孔。对该材料进行了650 C的疲劳,蠕变疲劳,拉伸和应力断裂测试,并将结果与​​以前的Astroloy合理数据进行了比较。孔的平均直径约为2微米,间距平均为20微米。它们确实影响了疲劳裂纹的萌生并产生了更多的晶间传播模式。但是,疲劳寿命并未大大降低。一个中空颗粒在一个样品中产生了25微米的大孔,使用寿命并未降低60%。多孔材料的疲劳行为显示出与拉伸行为的典型相关性。塑性应变范围-寿命关系随着拉伸延展性的降低而成比例地减小,但是弹性应变范围-寿命关系几乎没有变化,这反映了多孔材料的σsub u / E减小很小。

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