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Modelling of High Temperature Multi-Axial Creep Rupture Behaviour of #gamma#-Titanium Aluminide

机译:高温多轴蠕变破裂行为的建模#γ-硝酸铝

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The creep behaviour of the intermetallic#gamma#-TiAl under conditions of multi-axial stress isconsidered. The particular alloy tested is known as 4722XD (Ti-47A1-2Mn-2Nb+0.8 percent vol. TiB_2) alloy as produced bythe Howmet Corporation. Tests on plain and round bar doublenotched tensile test pieces with different notch sharpness werecarried out on this alloy at 750 deg C. The creep stressdistributions generated across the notch throats were calculatedby finite element analysis. For each notch geometry a skeletalpoint has been identified where the stress slate is insensitive tothe creep law assumed. Metallographic observations have beenmade of the creep damage developed in the notch throats. It hasbeen found that the location of ibis damage can be correlatedwith the finite clement results using models for the influence ofstate of stress on the creep ductility of materials.
机译:在多轴应力的条件下,金属间组合#Gamma#的蠕变行为。所测试的特定合金被称为4722xd(Ti-47a1-2mn-2nb + 0.8%Vol。Tib_2)合金,由Howfore Corporation产生。在普通和圆形条的测试中,在750℃下,在该合金上载于不同的缺口锐度,在750℃下呈上载于凹口喉部产生的蠕变胁迫下划线。有限元分析。对于每个凹口几何形状,已经识别了骨骼点,其中应力板岩不敏感,所以蠕变律假定。金相观测已经是在凹口喉咙中产生的蠕变损坏。它已经发现,可以将宜必思损坏的位置与有限的Clement结果相反,使用模型对于对材料的蠕变延性的蠕变延展性的影响。

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