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The effect of microstructure on mechanical properties of directionally solidified intermetallic Ti-46Al-8Nb alloy

机译:显微组织对定向凝固金属间Ti-46Al-8Nb合金力学性能的影响

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The effect of microstructure on mechanical properties of directionally solidified (DS) intermetallic Ti-46Al-8Nb (at. percent ) alloy was studied. After directional solidification at constant growth rates V ranging from 5.56 X 10~(-6) to 1.18 X 10~(-4) m s~(-1) and constant temperature gradients in liquid at the solid liquid interface G_L from 3.5 X 10~3 to 8 X 10~3 K m~(-1), the DS samples contain several columnar grains aligned in a direction parallel or nearly parallel to the growth direction. The microstructure within the columnar grains is fully lamellar consisting of alpha_2(Ti_3Al) + gamma(TiAl) lamellae. Mean alpha_2-alpha_2 interlamellar spacing A decreases with increasing growth rate V and increasing cooling rate. Room temperature Vickers microhardness HV_m and compressive yield stress sigma_y at 700 deg C increase with decreasing interlamellar spacing A according to Hall-Petch relationship. High-temperature compressive yield stress depends on an angle & between lamellar boundaries and loading axis. Maximum values of the yield stress are measured at theta = 90 deg and minimum values at theta ranging from 30 deg to 60 deg . Columnar grain structure leading to a high anisotropy of mechanical properties can be transformed to fine equiaxed grains with convoluted type of alpha_2 + gamma microstructure by appropriate heat treatments. Compressive yield stress of the specimens with equiaxed grain structure continuously decreases with increasing test temperature. A simple relationship is proposed for a prediction of the compressive yield stress at temperatures ranging from 20 to 900 deg C.
机译:研究了显微组织对定向凝固(DS)金属间金属Ti-46Al-8Nb(at。%)合金力学性能的影响。在以5.56 X 10〜(-6)到1.18 X 10〜(-4)ms〜(-1)的恒定增长率进行定向凝固之后,固液界面G_L处的液体中的恒定温度梯度从3.5 X 10〜在3〜8×10〜3K m〜(-1)的范围内,DS样品包含沿与生长方向平行或大致平行的方向排列的多个圆柱状的晶粒。柱状晶粒内的微观结构是完全薄片状的,由α_2(Ti_3Al)+γ(TiAl)薄片组成。平均α_2-α_2层间间距A随着生长速率V和冷却速率的增加而减小。根据霍尔-帕奇关系,随着层间距A的减小,室温维氏显微硬度HV_m和700℃的压缩屈服应力σ_y增大。高温压缩屈服应力取决于层状边界与加载轴之间的夹角和夹角。屈服应力的最大值在θ= 90度时测量,而θ在30度至60度范围内的最小值。可以通过适当的热处理将导致较高机械性能各向异性的柱状晶粒结构转变为具有α_2+γ微结构卷积型的细等轴晶粒。等轴晶结构的试样的压缩屈服应力随着测试温度的升高而持续降低。提出了一种简单的关系来预测温度在20至900摄氏度之间的压缩屈服应力。

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