1) Al-Cu-Li alloy
Al-Cu-Li合金
1.
Microstructures and mechanical properties of friction-stir welding joint of Al-Cu-Li alloy;
Al-Cu-Li合金搅拌摩擦焊接头的微观组织和力学性能
2.
The effects of trace element Ce,Ag on the microstructure and mechanical properties of Al-Cu-Li alloy after thermal exposure have been investigated.
研究了微量Ce、Ag对一种Al-Cu-Li合金热暴露后显微组织和性能的影响。
3.
The Al-Cu-Li alloys with addition of trace elements of Mg and Zn,treated by T6(solution treatment+artificial aging)and T8(solution treatment+pre-deformation+artificial aging),were studied.
对一种含少量Mg、Zn的Al-Cu-Li合金经过T6(固溶+人工时效)和T8(固溶+预变形+人工时效)热处理后的显微组织进行研究。
2) Al-Li-Cu alloy
Al-Li-Cu合金
1.
Effect of Sc on microstructure and properties of 2197 Al-Li-Cu alloy;
微量Sc对Al-Li-Cu合金组织和性能的影响
2.
Effect of heat treatment on microstructures and mechanical properties of Al-Li-Cu alloy TIG welded joint;
热处理对Al-Li-Cu合金TIG焊接头组织及力学性能的影响
3) Al-Li-Cu-Mg-Zr alloy
Al-Li-Cu-Mg-Zr合金
1.
Equal-channel angular pressed (ECAP) Al-Li-Cu-Mg-Zr alloy mainly consists of near equi-axial grains with size smaller than 1μm.
等通道转角挤压(ECAP)方法制备的Al-LI-Cu-Mg-Zr合金主要由晶粒小于1μm的等轴晶组成,循环形变时,ECAP Al-Li-Cu-Mg-Zr合金在应变幅较小时先出现短暂软化,然后持续硬化;在应变幅较大时持续软化直至断裂,ECAPAl-Li-Cu-Mg-Zr合金的Coffin-Manson曲线近似一条直线,这些特性均与文献报道的峰时效Al-Li-Cu-Mg-Zr合金有所不同。
2.
An Al-Li-Cu-Mg-Zr alloy 8090 was heat treated in different aging condition.
对Al-Li-Cu-Mg-Zr合金8090热轧板材进行了不同的时效处理,测试了该合金在不同时效状态下的力学性能和阻尼特性。
3.
The residual strength and relation to the cavitation of as-warm rolledAl-Li-Cu-Mg-Zr alloy have been investigated after superplastic deformation under differ-ent tensile conditions.
研究了温轧态Al-Li-Cu-Mg-Zr合金经不同拉伸条件超塑变形后残余强度及其与空洞行为的关系结果表明在一定应变量范围内,以高的应变速率变形的试样比以低的应变速率变形的试样空洞少,残余强度高;在变形到较大的应变量时,先快后慢的两段速率拉伸变形与一段速率拉伸相比,试样中空洞少,残余强度高结合该合金变形初期发生的形变促使连续再结晶过程,讨论了拉伸条件与空洞行为及残余强度的关
4) Al Li Cu Zr alloy
Al-Li-Cu-Zr合金
5) Al Li Mg Cu alloys
Al-Li-Cu-Mg合金
6) Al-Zn-Li-Mg-Cu alloy
Al-Zn-Li-Mg-Cu合金
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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