1) microstructure/Al-Li allays
微观结构/Al-Li合金
2) microstructure/Al-Li alloys
显微结构/Al-Li合金
3) 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。
4) Al-Li alloy
Al-Li合金
1.
Calculation on valence electronic structures of Al-Li alloy under earlier aging condition;
Al-Li合金时效初期的价键分析
2.
Study on no-interlayer diffusion welding technology of Al-Li alloy;
Al-Li合金无中间层扩散焊接工艺研究
3.
Preparation and Evaluation of Spectral Al-Li Alloy Reference Material;
Al-Li合金光谱标准样品制备和定值
6) Al-Li alloy
Al-Li 合金
1.
The solidification and segregation behaviors of 8090 Al-Li alloy have been in-vestigated with differential thermal analysis and metallographic-electron microprobe method.
研究了8090Al-Li 合金在缓慢冷却时的凝固过程,结果表明:L→α-Al+L′反应是基本凝固过程,贯彻始终。
2.
The experimental results of superplastic tensile test carried out according to orthonormal designshow that,for cold-rolled Al-Li alloy,better superplasticity can be obtained by usingthree-stage tension process.
研究了未经预处理的冷轧态 Al-Li 合金超塑变形工艺,根据三段拉伸设想,按正交试验设计方案,进行了超塑拉伸试验。
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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