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首页> 外文期刊>Metallurgical and Materials Transactions A >Effect of Loading History on Stress Corrosion Cracking of 7075-T651 Aluminum Alloy in Saline Aqueous Environment
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Effect of Loading History on Stress Corrosion Cracking of 7075-T651 Aluminum Alloy in Saline Aqueous Environment

机译:加载历史对盐水溶液环境下7075-T651铝合金应力腐蚀开裂的影响

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摘要

An experimental study of stress corrosion cracking (SCC) was conducted on 7075-T651 aluminum alloy in a chromate-inhibited, acidic 3.5 pct sodium chloride aqueous solution using compact tension specimens with a thickness of 3.8 mm under permanent immersion conditions. The effects of loading magnitude, overload, underload, and two-step high-low sequence loading on incubation time and crack growth behavior were investigated. The results show that the SCC process consists of three stages: incubation, transient crack growth, and stable crack growth. The incubation time is highly dependent on the load level. Tensile overload or compressive underload applied prior to SCC significantly altered the initiation time of corrosion cracking. Transition from a high to a low loading magnitude resulted in a second incubation but much shorter or disappearing transient stage. The stable crack growth rate is independent of stress intensity factor in the range of 10 to 22 MPa Ö{textm} . sqrt {text{m}} .
机译:在永久浸入条件下,使用厚度为3.8 mm的紧凑拉伸试样,在铬酸盐抑制的酸性3.5 pct氯化钠水溶液中对7075-T651铝合金进行了应力腐蚀开裂(SCC)的实验研究。研究了加载量,过载,欠载和两步高-低序列加载对保温时间和裂纹扩展行为的影响。结果表明,SCC过程包括三个阶段:保温,瞬时裂纹扩展和稳定裂纹扩展。孵育时间高度依赖于负载水平。在SCC之前施加的拉伸过载或压缩欠载显着改变了腐蚀裂纹的产生时间。从高负荷量到低负荷量的转变导致了第二次孵育,但过渡期更短或消失了。稳定的裂纹扩展速率与应力强度因子无关,在10至22 MPaÖ{textm}范围内。 sqrt {text {m}}。

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