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The Effect of Thermomechanical Processing on the Tensile, Fatigue, and Creep Behavior of Magnesium Alloy AM60

机译:热机械加工对镁合金AM60的拉伸,疲劳和蠕变行为的影响

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摘要

Tensile, fatigue, fracture toughness, and creep experiments were performed on a commercially available magnesium-aluminum alloy (AM60) after three processing treatments: (1) as-THIXOMOLDED (as-molded), (2) THIXOMOLDED then thermomechanically processed (TTMP), and (3) THIXOMOLDED then TTMP then annealed (annealed). The TTMP procedure resulted in a significantly reduced grain size and a tensile yield strength greater than twice that of the as-molded material without a debit in elongation to failure (ε f ). The as-molded material exhibited the lowest strength, while the annealed material exhibited an intermediate strength but the highest ε f (>1 pct). The TTMP and annealed materials exhibited fracture toughness values almost twice that of the as-molded material. The as-molded material exhibited the lowest fatigue threshold values and the lowest fatigue resistance. The annealed material exhibited the greatest fatigue resistance, and this was suggested to be related to its balance of tensile strength and ductility. The fatigue lives of each material were similar at both room temperature (RT) and 423 K (150 °C). The tensile-creep behavior was evaluated for applied stresses ranging between 20 and 75 MPa and temperatures between 373 and 473 K (100 and 200 °C). During both the fatigue and creep experiments, cracking preferentially occurred at grain boundaries. Overall, the results indicate that thermomechanical processing of AM60 dramatically improves the tensile, fracture toughness, and fatigue behavior, making this alloy attractive for structural applications. The reduced creep resistance after thermomechanical processing offers an opportunity for further research and development.
机译:在以下三种加工处理之后,对市售的镁铝合金(AM60)进行了拉伸,疲劳,断裂韧性和蠕变实验:(1)触变模制(模制),(2)触变模制然后进行热机械加工(TTMP) ,以及(3)进行THOMOMOLDED之后再进行TTMP退火(退火)。 TTMP程序可导致晶粒尺寸显着减小,拉伸屈服强度大于成型材料的两倍,而断裂伸长率不降低(ε f )。刚成型的材料表现出最低的强度,而退火的材料表现出中等强度,但最高ε f (> 1 pct)。 TTMP和退火材料的断裂韧性值几乎是成型材料的断裂韧性值的两倍。成型材料表现出最低的疲劳阈值和最低的抗疲劳性。退火材料表现出最大的抗疲劳性,这被认为与其抗拉强度和延展性的平衡有关。在室温(RT)和423 K(150°C)下,每种材料的疲劳寿命相似。在20至75 MPa之间的施加应力和373至473 K(100至200°C)的温度范围内评估了拉伸蠕变行为。在疲劳和蠕变实验中,裂纹优先发生在晶界处。总体而言,结果表明,AM60的热机械加工可显着改善拉伸强度,断裂韧性和疲劳性能,从而使该合金对结构应用具有吸引力。热机械加工后降低的抗蠕变性为进一步的研究和开发提供了机会。

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