1) behavior of stress corrosion cracking
应力腐蚀特性
2) SCC
抗应力腐蚀性能
1.
As one of the key structure materials in aerospace industry, 7000 series super-high strength aluminium alloy has the superior mechanical properties in T6 condition,but it is prone to SCC.
7000系超高强铝合金是航空航天工业的主要结构材料之一,T6(峰时效)状态下该系合金强度最高但对应力腐蚀(SCC)十分敏感,RRA(回归再时效)工艺兼顾了合金的强度和抗应力腐蚀性能,适应目前航空航天工业对结构材料的要求。
2.
The effects of alloying elements and various heat treatments process on mechanical properties, stress corrosion crack (SCC) property, fracture toughness and microstructural evolution of 7475 high strength aluminum alloys were investigated by means of the tensile test, SCC test, optical microscopy (OM), scanning electron microscopy (SEM) and transmission electron microscopy (TEM).
采用室温拉伸、硬度、断裂韧性和抗应力腐蚀拉伸测试方法，金相(OM)和电子显微分析方法(SEM、TEM)研究了合金元素及热处理工艺对7475铝合金的力学性能、抗应力腐蚀性能、显微组织结构的影响及其变化规律，优化了热处理制度，并从理论上进行了分析和讨论。
3) Stress Corrosion Cracking Sensitivity
应力腐蚀敏感性
1.
Influence of Different Ageing Process on Stress Corrosion Cracking Sensitivity of 2519 Aluminum Alloy Hot Rolled Plate;
时效工艺对2519铝合金热轧板材抗应力腐蚀敏感性的影响
5) stress corrosion cracking
应力腐蚀性能
1.
Effect of high-temperature pre-precipitation on microstructure, mechanical property and stress corrosion cracking of Al-Zn-Mg aluminum alloy;
高温预析出对Al-Zn-Mg铝合金组织、力学性能和应力腐蚀性能的影响
6) stress corrosion sensitivity
应力腐蚀敏感性
1.
Influence of heat treatment on mechanical properties and stress corrosion sensitivity of 2519 aluminum alloy plate;
热处理制度对2519铝合金板材力学性能和应力腐蚀敏感性的影响
2.
The purpose of the research is to compare the effect of different alloying constituents on the stress corrosion sensitivity.
目的在于比较不同合金成分对应力腐蚀敏感性的影响。
补充资料：固定应力腐蚀
分子式：
分子量：
CAS号：
性质：见应力腐蚀。
分子量：
CAS号：
性质：见应力腐蚀。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条