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Dynamic Fracture Toughness of Magnesium Alloy under Impact Loading Conditions

机译:冲击载荷条件下镁合金动态断裂韧性

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In the present study, three-point bend impact experiments on AZ61 magnesium alloy were conducted using an instrumented impact testing machine by Charpy V notch in accordance to ASTM E24.03.03. This test method is to determine dynamic fracture toughness at sharp crack for five different thickness of 2,4, 6, 8 and 10 mm. A sharp fatigue pre-crack was initiated and propagated to half of specimen width at a constant crack propagation rate of about 1 x 10~(-8) m/cycle before the specimen was loaded by the impact force until the maximum force is reached and then rapid fracture occurred. The Charpy V notch test was conducted at an impact velocity of 3.85 m/s. The dynamics fracture toughness at sharp crack was determined from the force-displacement history of the load point obtained from measurements of input and reflected strain profiles on the incident specimen. The dynamic fracture toughness K_d values obtained for different thicknesses showed that K_d value decreased with increasing specimen thickness. Scanning electron microscopy was used to elucidate the micro and macro failure mechanism operation during the dynamic fracture event. In particular two micro-mechanisms of failure were of primary interest: (a) fatigue and rapid fracture surface and (b) the development of shear lips at the surface of the specimen follow by fracture.
机译:在本研究中,根据ASTM E24.03.03,使用仪表式冲击试验机进行三点弯曲镁合金对AZ61镁合金的实验。该测试方法是在尖锐裂缝中测定5种不同厚度的2,4,6,8和10mm的动态断裂韧性。在达到抗冲击力的恒定裂纹传播速率下以恒定的裂纹传播速率引发尖锐的疲劳前裂纹并在标本宽度的一半以约1×10〜(-8)m /循环。然后发生快速骨折。 Charpy V Notch测试在冲击速度为3.85 m / s。从入射标本上的输入和反射应变型材的测量结果获得的负载点的力 - 位移历史确定了尖锐裂缝处的动力断裂韧性。用于不同厚度的动态断裂韧性K_D值显示K_D值随着样品厚度的增加而降低。扫描电子显微镜用于在动态骨折事件期间阐明微型和宏观故障机构操作。特别是两种微型失败机制是主要的兴趣:(a)疲劳和快速骨折表面和(b)裂缝在样本表面的剪切嘴唇的发育。

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