1) Mg-11Li-3Al-0.5RE alloy
Mg-11Li-3Al-0.5RE合金
2) Mg-3Al-1Zn alloy
Mg-3Al-1Zn合金
1.
In this paper the effects of Sr on the as-cast microstructure of Mg-3Al-1Zn alloy are investigated,and the results indicate that there are no obvious effects of adding 0.
结果表明:在Mg-3Al-1Zn合金中加入0。
2.
In this paper the effects of Y on the as-cast microstructure of Mg-3Al-1Zn alloy were investigated,and results indicated that the effects of 0.
结果表明,在Mg-3Al-1Zn合金中加入w(Y)=0。
3.
3%Y to Mg-3Al-1Zn alloy can refine the grains of the alloy, and adding Sr can obtain higher efficiency than adding Y.
Sr和Y以及不同Sr加入量对Mg-3Al-1Zn合金晶粒的细化效果差异与不同条件下Mg-3Al-1Zn合金的开始结晶温度不同有关。
3) AZ31(Mg-3AI-1.0Zn)magnesium alloy
AZ31(Mg-3Al-1.0Zn)镁合金
5) Ti 10V 2Fe 3Al Alloy
Ti10V-2Fe-3Al合金
6) Ti-10V-2Fe-3Al alloy
Ti-10V-2Fe-3Al合金
1.
The hot deformation behavior of two different microstructures of Ti-10V-2Fe-3Al alloy at temperature in the range of 650～900℃ and with strain rates from 0.
利用Gleeble3500热模拟试验机对Ti-10V-2Fe-3Al合金两种状态在不同变形温度及不同变形速率条件下的热变形行为进行了研究。
2.
Effect of β-fleck on properties of tensile elongation and low cycle fatigue life at room temperature for Ti-10V-2Fe-3Al alloy has been investigated.
研究了β斑点对Ti-10V-2Fe-3Al合金的室温拉伸性能和低周疲劳性能的影响,发现在β斑点区内,裂纹沿原始β晶界扩展形成沿晶脆性断裂,在交变应力作用下,β斑点往往成为疲劳源点,在高应变下,β斑区内的原始β晶界和晶界α处萌生裂纹并导致早期断裂。
补充资料：Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al—Ll合金构件——歼7一I 1机舱口盖及副翼扰流片 张自供稿
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
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