铌微合金化对1Cr21Ni5Ti屈服强度的影响

为了提高1Cr21Ni5Ti双相不锈钢的屈服强度,对其进行了铌微合金化,通过化学分析、金相观察、拉伸试验等,对微合金化前后的性能进行了对比研究。结果表明,经过Nb微合金化处理的1Cr21Ni5Ti屈服强度σ0.2显著提高,达到了技术条件的规定。     

Ti2AlNb基合金的研究进展

着重介绍了Ti2AlNb基合金的成分、显微组织及性能，综述了合金元素及热处理工艺对Ti2Al-Nb基合金组织性能的影响，介绍了Ti2AlNb基合金熔炼凝固特性，并展望Ti2AlNb基合金的未来。     

不同中间层合金对IC10合金的连接

采用B或Zr作为降熔元素分别配制不同中间层合金,并对IC10合金进行连接.分析不同状态下焊缝组织.结果表明,含B中间层合金连接IC10时,保温时间较长可以达到等温凝固,而含Zr中间层合金在本试验条件下表现为钎焊过程.     

Ti600合金板材的轧制工艺与电子束焊接性能研究

测试研究了Ti600 高温钛合金板材在不同加工及热处理状态下的室温拉伸及高温蠕变性能,分析对比了热机械处理工艺(thermomechanical process-TMP)与常规加工热处理对合金板材组织形态特征与性能的影响规律与内在机制;另外还对Ti600合金板材的焊接性能进行了研究.结果表明:采用热机械处理工艺(TMP)可获得充分生长的片层状团束组织(colony structure),这种类型的组织显著提高了合金的高温蠕变性能.而且合金经电子束焊接后仍然具有良好的综合性能.     

热模锻造对Ti-24Al-15Nb-1.5Mo/TC4双合金界面连接强度与组织的影响

研究热模锻造经真空电子束焊接的Ti-24Al-15Nb-1.5Mo与TC4双合金焊缝界面的显微硬度变化、合金元素扩散趋势、显微组织特征和拉伸性能。结果表明,焊后未经任何处理的的试样焊缝边界处Al和Nb含量有突变;经700℃保温12h,AC(空冷)的焊接件焊缝区显微硬度最高,HV0.98平均值达3780MPa;经热模锻造和热处理后,合金元素扩散充分,显微组织均匀,显微硬度均匀。焊接接头拉伸试验表明,经38%变形,1020℃锻造,700℃保温12h,AC处理的试样,高倍组织为双态组织,拉伸性能最好,室温延展率达16.5%,断面收缩率达44.5%。     

Z-A模型的修正及在预测本构关系中的应用

Zerilli-Armstrong(Z-A)模型是基于热激活位错运动理论建立的具有物理理论基础的本构模型,但是模型建立的初始假设,降低了其预测精度.为此通过引入考虑应变率和温度耦合效应的应变强化指数对Z-A模型进行修正,拓展了其适用范围,并将修正后的Z-A模型应用于描述IC10合金在不同温度和应变率条件下的塑性流变行为.与修正前Z-A模型的预测结果及试验结果比较表明:修正后Z-A模型的预测精度有较大程度的提高,最大平均相对误差值从6.41%降低到3.65%.      

离子辅助沉积Al膜层增强Ti811钛合金高温微动疲劳抗力

为提高Ti811钛合金高温微动疲劳抗力,利用离子辅助沉积技术在Ti811钛合金表面制备Al膜层。对比研究多弧离子镀(MIP)和离子辅助多弧沉积(IAD)Al膜层的膜基界面成分分布、膜基结合强度、显微硬度、摩擦学性能。探讨IAD铝膜层对Ti811合金微动疲劳抗力的影响。结果表明,利用离子辅助多弧沉积技术可以获得膜基结合强度高、硬度低、减摩润滑性能好的Al膜层,该膜层能够显著提高Ti811钛合金350℃时的微动疲劳抗力。     

The Geology of Mercury: The View Prior to the MESSENGER Mission

Mariner 10 and Earth-based observations have revealed Mercury, the innermost of the terrestrial planetary bodies, to be an exciting laboratory for the study of Solar System geological processes. Mercury is characterized by a lunar-like surface, a global magnetic field, and an interior dominated by an iron core having a radius at least three-quarters of the radius of the planet. The 45% of the surface imaged by Mariner 10 reveals some distinctive differences from the Moon, however, with major contractional fault scarps and huge expanses of moderate-albedo Cayley-like smooth plains of uncertain origin. Our current image coverage of Mercury is comparable to that of telescopic photographs of the Earth’s Moon prior to the launch of Sputnik in 1957. We have no photographic images of one-half of the surface, the resolution of the images we do have is generally poor (∼1 km), and as with many lunar telescopic photographs, much of the available surface of Mercury is distorted by foreshortening due to viewing geometry, or poorly suited for geological analysis and impact-crater counting for age determinations because of high-Sun illumination conditions. Currently available topographic information is also very limited. Nonetheless, Mercury is a geological laboratory that represents (1) a planet where the presence of a huge iron core may be due to impact stripping of the crust and upper mantle, or alternatively, where formation of a huge core may have resulted in a residual mantle and crust of potentially unusual composition and structure; (2) a planet with an internal chemical and mechanical structure that provides new insights into planetary thermal history and the relative roles of conduction and convection in planetary heat loss; (3) a one-tectonic-plate planet where constraints on major interior processes can be deduced from the geology of the global tectonic system; (4) a planet where volcanic resurfacing may not have played a significant role in planetary history and internally generated volcanic resurfacing may have ceased at ∼3.8 Ga; (5) a planet where impact craters can be used to disentangle the fundamental roles of gravity and mean impactor velocity in determining impact crater morphology and morphometry; (6) an environment where global impact crater counts can test fundamental concepts of the distribution of impactor populations in space and time; (7) an extreme environment in which highly radar-reflective polar deposits, much more extensive than those on the Moon, can be better understood; (8) an extreme environment in which the basic processes of space weathering can be further deduced; and (9) a potential end-member in terrestrial planetary body geological evolution in which the relationships of internal and surface evolution can be clearly assessed from both a tectonic and volcanic point of view. In the half-century since the launch of Sputnik, more than 30 spacecraft have been sent to the Moon, yet only now is a second spacecraft en route to Mercury. The MESSENGER mission will address key questions about the geologic evolution of Mercury; the depth and breadth of the MESSENGER data will permit the confident reconstruction of the geological history and thermal evolution of Mercury using new imaging, topography, chemistry, mineralogy, gravity, magnetic, and environmental data.     

草酸钠体系中Ti-10V-2Fe-3Al钛合金阳极氧化膜的制备与表征

对Ti-10V-2Fe-3Al钛合金在草酸钠为主盐的新型无氟环保电解液体系中的阳极氧化进行了研究,成功制备出阳极氧化膜。采用扫描电子显微镜(SEM)、能谱仪(EDS)、X射线衍射仪(XRD)等仪器研究了氧化膜的形貌、组成和相结构。采用电化学方法研究了阳极氧化后钛合金的耐腐蚀性能。结果表明:膜层具有多孔结构,孔径范围在80nm～1μm之间。膜层的主要成分是无定形的TiO2,同时有锐钛矿相及金红石相TiO2的存在。阳极氧化后钛合金的耐蚀性有显著的提高。     

Ti600合金的性能与显微组织的研究

Ｔｉ６００ 合金是一种新型近α高温钛合金,其名义成分为Ｔｉ－６Ａｌ－２．８Ｓｎ－４Ｚｒ－０．５Ｍｏ－０．４Ｓｉ－０．１Ｙ（ｗ ｔ％ ）。测试了该合金在热暴露前后拉伸性能和蠕变性能,并进行了透射电镜和光学显微镜观察。研究结果表明：合金的机械性能优异,与美国Ｔｉ１１００ 性能水平相当;在常规热处理条件下,合金组织是一种典型的针状组织,该组织具有良好的抗蠕变性能。Ｔｉ６００ 合金热暴露后,合金中存在的α２ 相（Ｔｉ３Ａｌ）和Ｓ２ 相（Ｔｉ５Ｓｉ３）使合金的室温塑性降低。讨论稀土氧化物对合金显微组织及性能的影响,表明稀土的加入对改善合金蠕变性能有较大作用。