离子束增强沉积CrN膜层及其微动摩擦学性能研究

以不同氮离子辅助轰击能量制备CrN膜层．利用纳米压入仪及显微硬度计分别测试单晶Si片上膜层的硬度及断裂韧度K1C．使用XRD、XPS及EPMA分析离子轰击能量对镀层组织结构的影响。结果表明，采用能量较低的氮离子轰击得到的涂层，由于金属Cr的存在，涂层硬度虽有所降低，但断裂韧度K1C数值较高。选择较低的4keV辅助轰击能量，在M2高速钢基体上沉积CrN涂层，膜层在空气介质中表现出优异的耐磨减摩特性.但在水介质条件下，由于膜层接触区域的去钝化，再钝化使腐蚀和磨损相互加速，导致CrN膜层摩擦系数，尤其是磨损量明显高于基材。     

Comparison of tribological properties of industrial low friction coatings

MX2(M= Mo, W; X=S, Se) and DLC (a-C: H and WC/C) are the two kinds of typical low friction coatings widely used in industry. The friction and wear properties of these two kinds of coatings marked as MOVIC,MOST, MoSez/Ni, WSez, a-C: H and WC/C coatings were determined by fretting tests in ambient air of different humidity. The results show that the coefficient of friction of MXz coatings increases when the relative humidity of air increases whereas the coefficient of friction DLC coatings decreases with the increasing of relative humidity. MOVIC and WSe2 coatings have a poor friction and wear resistance because of non-basal planes (100) and ( 101 ) parallel to the surface in the MOVIC coating, or the rough and porous surface of WSe2 coatings. Among these six coatings, MoSe2/Ni and WC/C eoatinas have the highest wear resistance which seems to be unaffected by the relative humidity.     

TC4钛合金的微动疲劳行为研究

研究了TC4钛合金在柱面-平面接触条件下的微动疲劳行为.通过观察微动区的磨损特征和截面形貌,分析了微动疲劳损伤机制,探讨了磨屑的形成与演变过程及其对微动疲劳行为的影响,考察了摩擦系数随时间的变化.结果表明,TC4钛合金微动区的损伤机制以粘着磨损、磨粒磨损和接触疲劳为主,并伴有氧化磨损.磨屑是基体材料脱落、破碎、氧化形成的,磨屑中的硬质氧化物颗粒促进了合金表面的磨粒磨损,加速了疲劳失效.     

微细轴放电反拷成形方式的比较研究

阐述了放电反拷加工在微细轴、微细孔加工中的重要作用，介绍了4种常见的放电反拷加工方式。分析了不同进给方式对放电反拷加工结果的影响，给出了选择其中一种进给方式加工的微细轴实例。     

Fretting wear behavior of AZ91D magnesium alloy

The fretting behaviour of the AZ91D magnesium alloy was investigated. The influence of the number of cycles, normal load （contact pressure） and the amplitude of slip on the fretting behavior of the material were focused. Fretting tests were performed under various running conditions with regard to normal load levels and slip amplitudes. The friction coefficient between the surfaces at the fretting junction was continuously recorded. The freeing damage on the magnesium specimens was studied by SEM. The resultS show that the wear volume increases with the increase of slip amplitude, and linearly increases with the increase of normal load in the mixed and gross slip regime, but the normal load has no obvious effect on the wear volume in the partial slip regime. The predominant fretting wear mechanism of magnesium alloy in the slip regime is the oxidation wear, delaminated wear and abrasive wear.     

超临界直流锅炉冷态空气动力场研究

针对四角切圆锅炉水平烟道上普遍存在烟温偏差的情况,在河北国华定洲发电厂新建锅炉开展了冷态空气动力场试验,重点研究炉膛出口烟气流速分布情况。试验证明,通过调整分离燃尽风（SOFA）喷嘴的角度,能有效改变炉膛出口气流的分布,保证左、右烟气流速均匀,可满足锅炉正常运行的要求。     

基于Matlab的自行火炮液压管件应力分析

液压管件作为某型自行火炮液压系统的一类重要元件,其机械性能在很大程度上影响整个液压系统的工作寿命.采用建模和仿真技术研究其应力分布,提出依据广义胡克定律建立液压管件在高强度载荷作用下的力学模型的方法,利用Matlab进行仿真分析,结合仿真结果对液压管件径向及切向应力的分布规律进行了探讨,对于液压管件的疲劳分析以及力学性能研究具有一定的参考价值.     

A local tangential lifting differential method for triangular meshes

In this note we present a local tangential lifting (LTL) algorithm to compute differential quantities for triangular meshes obtained from regular surfaces. First, we introduce a new notation of the local tangential polygon and lift functions and vector fields on a triangular mesh to the local tangential polygon. Then we use the centroid weights proposed by Chen and Wu [4] to define the discrete gradient of a function on a triangular mesh. We also use our new method to define the discrete Laplacian operator acting on functions on triangular meshes. Higher order differential operators can also be computed successively. Our approach is conceptually simple and easy to compute. Indeed, our LTL method also provides a unified algorithm to estimate the shape operator and curvatures of a triangular mesh and derivatives of functions and vector fields. We also compare three different methods : our method, the least square method and Akima’s method to compute the gradients of functions.     

型材滚弯数值模拟及应力、应变分析

用通用显式动力分析软件ANSYS/LS-DYNA成功实现了对型材弯曲件滚弯及其回弹过程的数值模拟.模拟结果表明,型材滚弯成形过程中,型材腹板应力中性层和应变中性层内移,而且应力中性层内移量大于应变中性层内移量.回弹后,等效弹性应变和等效应力的峰值变小.分析了型材弹塑性弯曲卸载过程中腹板截面的切向应力变化,模拟结果与理论分析一致.