铝锂合金的发展概况及其应用

本文简略地介绍了国外Al-Li合金的发展概况、最新进展,以及在航空航天领域中的应用,并对我国发展Al-Li合金提供了建议。     

Oxidation Properties in CO2 of Inconel Alloy 600 Coated by Simultaneous Aluminizing-Chromizing Process

IN 600 alloy was coated with two different types of coatings, Cr-modified aluminide coating this is called aluminizing-chromizing and Y-doped chromium modified aluminide coating this is called aluminizing-chromizing-yttriumizing. Diffusion coating was carried at 1 050 ℃ for 8 h under Ar atmosphere by simultaneous aluminizing-chromizing process and by simultaneous aluminizing-chromizing- yttriumizing. Cyclic oxidation tests were conducted on the uncoated and on the coated Inconel 600 alloy in the temperature range 800- 1 000 ℃ in CO2 for 100 h at 10 h cycle.The results showed that the oxidation kinetics for uncoated Inconel 600 alloy in CO2 is parabolic and the phases present are NiO, (Fe, Cr)2O3 , NiFe2O4 and NiCrO4. The oxidation kinetics for both coated systems in CO2 was found to be parabolic and the value of kP for both coated systems were found to be lower than that for uncoated Inconel 600 alloy. Oxide phases that formed on coated systems are Al2O3 and NiCrO4. The role of yttrium can be attributed to its ability to improve the adherence of the oxide scale.     

5wt％YAl2p／Mg-Li复合材料的组织与性能的研究

采用搅拌铸造法制备了5wt% YAl2p颗粒增强Mg-14Li-1Al合金基复合材料,研究了YAl2p/Mg-14Li-1Al复合材料的界面、组织特征,并对基体合金和复合材料的室温力学性能进行了测试.组织分析表明,YAl2p增强颗粒在基体合金中分布均匀,界面结合良好,未发现明显的团聚现象,也未观察到化学反应或明显的原子扩散.复合材料的室温拉伸强度为189 Mpa,较基体合金提高了约45.3%,而塑性得到了良好的保持(7%).     

Al-TiO2-C系原位合成铝基复合材料高温拉伸性能及断裂机理

讨论了Al-TiO2-C反应系原位反应合成铝基复合材料的常温和高温拉伸性能及其断裂机理.当C/TiO2摩尔比为0时,增强相由α-Al2O3和Al3Ti组成,随C/TiO2摩尔比的增加,Al3Ti逐渐减少,在C/TiO2摩尔比为1时,Al3Ti基本消失.室温抗拉强度和延伸率随C/TiO2摩尔比的增加而同步提高,分别由250.4 MPa和4.0%上升到350.8 MPa和6.0%.SEM观察发现有的Al3Ti自身解理开裂,并在四周形成较大韧窝,拉伸时裂纹核可在Al3Ti棒中和基体中α-Al2O3的聚集处形成,并分别在棒的解理面和基体中扩展引起断裂.高温时,热错配应力促使裂纹核先于基体在Al3Ti棒与基体的界面萌生扩展,Al3Ti从基体中脱离,断口出现洞坑,C/TiO2摩尔比为1的复合材料在727K时,拉伸强度降为93.3MPa,延伸率升为11.0%.     

纯铝累积叠轧焊界面及其性能

通过室温下L2纯铝的累积叠轧焊试验,利用光学显微镜观察研究了叠轧道次对连接界面的影响;利用常温拉伸试验研究了叠轧道次和退火温度对其力学性能的影响.研究表明:随着叠轧道次的增加,试样的连接效果越来越好,材料的强度提高,但延伸率却急剧下降.此外,退火温度对叠轧材料的性能影响显著.     

飞机机体和部件维修中铝件的粘接方法

本文总结了在飞机维修中铝件粘接的应用经验，阐述了铝件的粘接方法。     

定向凝固铸造Ni3Al基合金IC6—高性能燃气涡轮导向叶片材料

介绍了一种最近研制的可用作燃气涡轮发动机涡轮导向叶片的高温结构材料-定向凝固铸造Ni3Al基合金IC6，对其工作温度、主要成份、工艺方法、力学性能、微观组织和强化机理做了具体说明。     

金属基复合材料的连接技术

综述了铝基复合材料的各种连接技术，包括扩散焊、钎焊、电阻焊和熔化焊，并提出今后应解决的问题。     

铝锂合金复合材料

随着铝锂合金材料的发展，近年来铝锂合金基复合材料的研究也不断深入，其多种力学性能优于前者的优点将显示出用作航天材料的前途。本文简单地介绍了某些铝锂合金复合材料的制备、时效特性和力学性能。