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Fracture Toughness and SCC Behavior of 7075 Aluminum Alloy under Mixed-Mode I-II Loading

机译:I-II混合模式下7075铝合金的断裂韧性和SCC行为

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Under mode I, II and mixed-mode I-II loading, the fracture toughness and SCC response of aluminum alloy 7075-T6 plate have been studied in the S-L and L-S orientations. The fracture toughness in S-L under mixed-mode loading coincides with K_(1c) for K_2/K_1 <1 and K_(2c) for K_2/K_1 >1, where K_(1c) and K_(2c) are the fracture toughness under mode I and mode II respectively, and K_2/K_1 is the stress intensity ratio. The former fracture occurs due to a preferential intergranular delamination controlled by a normal stress component on grain boundaries, while the latter fracture proceeds in a trangranular shear mode. The SCC growth rate under the mixed-mode loading decreases with an increase of K_2 component, and under the pure mode II loading SCC growth becomes more difficult. Based on the experimental results and discussions of stress-induced hydrogen accumulation at crack tip the intergranular SCC of 7075-T6 can assumed principally controlled by hydrogen embrittlement, and an anodic dissolution reaction involved in the mode II SCC process plays an assisting role in lamellar crack joining in transgranular fracture.
机译:在模式I,II和混合模式I-II下,研究了7075-T6铝合金板在S-L和L-S方向上的断裂韧性和SCC响应。混合模式载荷下SL的断裂韧性与K_2 / K_1 <1的K_(1c)和K_2 / K_1> 1的K_(2c)一致,其中K_(1c)和K_(2c)是模式下的断裂韧性分别为I和II,而K_2 / K_1为应力强度比。前者的断裂是由于晶界上的正应力分量所控制的优先的晶间分层而发生的,而后者的断裂则以三角形剪切模式进行。混合模式载荷下的SCC生长速率随着K_2组分的增加而降低,而在纯模式载荷下,SCC的生长变得更加困难。基于实验结果和应力引起的氢在裂纹尖端聚集的讨论,可以认为7075-T6的晶间SCC主要受氢脆控制,并且II型SCC过程中涉及的阳极溶解反应在层状裂纹中起辅助作用参加经晶状体骨折。

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