1) 2091 Al-Li alloy
2091Al-Li合金
2) Al-Li-Cu-Mg-Zr alloy 2091
2091Al-Li-Cu-Mg-Zr合金
3) 1420Al-Li alloy
1420Al-Li合金
1.
Corrosion behavior of 1420Al-Li alloy under tensile stress;
应力作用下1420Al-Li合金的腐蚀行为研究
4) Al-Li alloys
Al-Li合金
1.
The phase transformations in Al-Li alloys were studied by DSC (differential scanning calorimetry).
以Al-Li合金为对象,通过DSC技术研究了合金的相变。
2.
This paper has analyzed the reasons of the brittleness of rapid solidification Al-Li alloys and introduced some main toughening methods in manufacturing,forming and heat treatment of the alloys.
通过对快速冷凝 (RS)Al-Li合金低塑韧性原因的分析 ,介绍了Al-Li合金制备、成材、热处理等过程中一些主要韧化途径 ,并简单讨论了获得较好综合性能的Al-Li合金制品的工艺方法及大致工艺参数范
3.
Low cycle fatigue property, cyclic hardening and softening of 8090 Al-Li alloys at various aging conditions were studied.
研究了不同热处理状态8090Al－Li合金的循环疲劳与断裂行为。
5) Mg-Li alloy
Mg-Li合金
1.
Research on properties of Mg-Li alloys;
Mg-Li合金的性能研究
2.
Creep Resistance of Mg-Li Alloy and Its Composites;
Mg-Li合金及复合材料的抗蠕变性能
3.
Study on the Homogenizing Treatment of Mg-Li Alloy;
Mg-Li合金的均化制度研究
6) 2195 alloy
2195Al-Li合金
1.
Effects of T6I6 temper on the microstructure and mechanical properties of 2195 alloy were investigated.
研究了热处理工艺T6I6对2195Al-Li合金组织和性能的影响,结果表明:2195Al-Li合金的断裂韧性与析出相的密度、尺寸及分布有关,而以T1相的密度、尺寸和分布影响最大;T6I6热处理工艺抑制T1相在亚晶界析出并促进T1和θ′相在晶内细小弥散析出,从而使2195合金在强度没有降低的条件下相对T6工艺提高合金塑性及断裂韧性。
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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