多向锻造7075铝合金的结构和性能

在440℃经多向锻造加工成7075铝合金锻件。研究了锻件的显微组织和力学性能随退火温度和T73回火的变化，TEM和SEM用于分析锻件的晶粒和第二相形态。多向和大变形锻造产生平均晶粒尺寸1．8μm的完全再结晶组织。390℃-450℃退火使晶粒长大到3μm，但位错和第二相分布没有明显改变，这时锻件展现出较低强度和较高延性。T73回火使锻件屈服强度和拉伸强度分别提高280％和210％，而延性同退火样相比并无明显下降，断裂韧性达到51MPam^1/2，可以认为这是沉淀强化的贡献。     

氢对Ti-2Al-2.5Zr钛合金疲劳性能的影响

研究了4种含量的氢对Ti-2Al-2.5Zr钛合金疲劳性能的影响。结果表明，自然含氢量的材料具有最好的疲劳性能。而当疲劳载荷大于材料的屈服强度时，氢含量对疲劳寿命基本没有影响；低于屈服强度后，疲劳寿命随着氢含量的升高而和。认为固溶的原子氢导致驻留滑移带软化，裂纹萌生提前，造成在较大△σ时充氢试样的疲劳寿命降低；而材料中氢化物对驻留滑移带（PSB）的阻碍作用导致氢化物与基体分离 而成为裂纹源，是小△σ下疲劳寿命降低扩要原因。     

变形Fe-Nb-C合金的室温至180℃内耗

测量了700℃，30min水冷后变形Fe－Nb-C合金室温至180℃的内耗，发现除Snoek峰外，合金在此温度区还有阻尼峰。测量了合金经过980℃，2h中间处理样品的内耗，并给出变形及室温原位时效的汽车钢ST14与GBPH340的内耗结果。认为Fe-Nb-C合金的变形“B”峰。是被饱和Cotterll气团碳原子团簇钉扎的位错段拖曳碳的稀Cottrell气团运动引起的，是合金在变形时碳原子稀Cottrell气团择优分布在位错上的结果。     

CuAlBi合金摩擦磨损性能的研究

采用MMU-5G摩擦磨损试验机测试了QuAlBi合金在不同载荷和摩擦速度下摩擦系数的变化规律，并测出各对应条件下的磨损量。结果表明：合金的摩擦系数随载荷的增加先减小再增大，随着速度的增加而减小；其磨损量随速度、载荷的增加而增大。犁沟是主要的磨损失效形式。     

锆在镁及镁合金中的作用

镁合金作为一种新型的工程材料具有许多独特的优点,锆作为微量元素加入到镁合金中,可以细化合金的微观组织,显著提高材料的力学性能,减少夹杂,改善镁合金的抗腐蚀性能等。论述了锆元素对镁合金各项性能的作用机理、锆元素细化镁合金晶粒的机制,提出合金制备过程中的加锆方式应是含锆镁合金今后研究的重点。     

冲击腐蚀磨损系统中影响因素的正交分析

用改进的MLD-10型冲击腐蚀磨损试验机，对不同条件下的冶金矿山用低碳高合金钢的冲击腐蚀磨损性能进行了试验。用正交分析法研究了磨粒，冲击功和pH值在低碳高合金钢冲击腐蚀磨损过程中的作用。结果表明，磨粒在冲击腐蚀磨损过程中对材料的影响最大，其次为冲击功，pH值的影响最小。     

钛基复合材料激光熔覆层显微组织及其强化机制

利用激光熔覆技术在Ti-6A1-4V合金表面制备了TiC增强钛基复合材料涂层，复合材料的硬度明显高于基体，平均硬度可达940HV0.2。对复合材料的显微组织分析表明：TiC增强钛基复合材料的强化机制以细晶强化和弥散强化为主。     

AZ91D镁合金在北京地区的大气腐蚀行为研究

利用室外大气暴露试验，研究了AZ91D镁合金在北京地区的平均大气腐蚀速率，并与相同条件下A3钢的大气腐蚀情况进行了对比．采用扫描电镜(SEM)、X-射线衍射(XRD)、X射线能谱(EDS)以及红外光谱(IR)等多种现代表面分析技术对腐蚀产物的形貌、组成、结构等进行分析，与A3钢相比，AZ91D镁合金具有良好的耐大气腐蚀性能，具有局部腐蚀的特征。     

Deposition of cerium contained conversion films on LC4 alloy with square wave pulse method

Cerium contained conversion films were deposited on LC4 aluminum alloy using square wave pulse (SWP) in aCeCl3 solution with KMnO4 as the oxidant. Energy dispersive spectroscopy (EDS) and scanning electron microscopy (SEM) were adopted to study the composition and the morphology of the film. It is found that the film is composed of Al, Zn, Cu,and small amount of cerium. The polarization curves of the specimens treated with SWP technique measured in 3.5% (mass fraction) NaCl solution reveal that the film thus formed inhibits both the anodic and cathodic process of the corrosion of the specimen. The immersion tests of treated specimens in 3.5% NaCl solution indicate that the corrosion resistance of the SWP treated specimen is better than that of the untreated and is equivalent to or even better than that of the traditionally electro-chemically treated specimens.     

High cycle fatigue and fracture behavior of 2124-T851 aluminum alloy

The high cycle fatigue properties and fracture behavior of 2124-T851 aluminum alloy were investigated roundly, including the fatigue crack growth rate, fracture toughness and fatigue S--N curve. Furthermore, the fatigue crack growth rate was analyzed by fitting the curves. And the microstructure of the alloy was studied using by optical microscopy, transmission electron microscopy and X-ray diffractometry, scanning electron microscop1/2 The results show that the fatigue strength and the fracture toughness of 2124-T851 thick plate are 243 MPa and 29.6 MPa.m at room temperature and R=0. 1, respectively. At high cycle fatigue condition, the characteristics of fatigue facture were observed obviously. And the higher the stress amplitude, the wider the space between the fatigue striations, the faster the rate of fatigue crack developing and going into the intermittent fracture area and the greater the ratio between the intermittent fracture area and the whole fracture area.