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NiAl热诱发马氏体相变的分子动力学模拟

沙宪伟 , 张修睦 , 陈魁英 , 李依依

金属学报

运用NiAl合金的镶嵌原子势,进行了B2结构NiAl中热诱发马氏体相变的分子动力学模拟,从而研究马氏体形核和长大的微观机理.首先进行了0K等体积条件下NiAl的相稳定性分析,发现0K时点阵参数c与a之比约为1.31的bct结构是稳定结构,B2结构只是一种亚稳结构.在热诱发马氏体相变的模拟过程中,由于NiAl中Ni原子和Al原子的振动性质存在着差异,造成了马氏体的不均匀形核.对另两种不同初始构型的系统进行的模拟进一步证实了不均匀形核的存在,并通过计算B2结构NiAl中Ni原子和Al原子的热运动均方位移解释了其原因.模拟中,B2结构奥氏体经热诱发马氏体相变转变为fctL1_0结构的马氏体.马氏体在长大过程中内部形成了若干转变孪晶.

关键词: 马氏体相变 , molecular dynamics simulation , embedded atom method , NiAl

界面在多相金属间化合物合金形变过程中的作用

杨锐

金属学报

综述了近年来多相金属间化合物研究进展,强调界面对多相合金的形变过程及力学行为的影响,讨论范围限于TiAl基利(Ni、Fe,Co)Al基多相合金,界面位错源的启动可以提高脆性相的形变能力.采用适当的制备和加工工艺可以突出多相合金中界面的有益作用,得到比较好的综合性能

关键词: 界面 , deformation , mechanical behaviour , TiAl , NiAl

二元NiAl金属间化合物单晶的制备

张万明 , 胡壮麒 , 郑启 , 于洋 , 唐亚俊 , 管恒荣

金属学报

在小型定向凝固装置上,采用两次方向相反的定向凝固工艺,成功地制备出生长速度分别为15,30及60mm/h的Ni52Al48单晶

关键词: 金属间化合物 , NiAl , directional solidification , growth of single crystal

渗铝NiAl-20%Fe金属间合金的高温热腐蚀

曾潮流 , 吴维旻 , 郭建亭

金属学报

本文研究了在950℃空气中,表面涂Na_2SO_4盐膜的条件下,NiAl,NiAl-20%Fe及渗铝后的高温热腐蚀行为。在热腐蚀过程中,NiAl合金表面能形成Al_2O_3膜,显示出一定的耐蚀性能。但Al_2O_3膜易开裂,Al_2O_3膜的溶解及开裂会引发合金发生快速热腐蚀;20%Fe的加入则使NiAl合金的耐蚀性能显著变差,合金表面不能形成单一的Al_2O_3膜;渗铝处理可以明显提高NiAl-20%Fe合金的耐蚀性能,且渗铝涂层的耐蚀性能优于NiAl合金,这与铝化物涂层中的Al含量较高,Al_2O_3膜的开裂倾向较小有关。

关键词: 金属间化合物 , NiAl , NiAl-20%Fe , aluminide coating , Na_2SO_4 , hot corrosion

分子动力学模拟研究单个刃型位错对NiAl马氏体相变的影响

沙宪伟 , 张修睦 , 李斌 , 李依依

金属学报

利用嵌入原子类型的势函数,通过分子动力学模拟方法研究了单个刃型位错对NiAl热诱发和应力诱发马氏体相变的影响,不受外力时,单个刃型位错的应变区不能诱发马氏体形核;位错在马氏体的长大过程中被继承,并可在相变的驱动下逐渐运动拉应力作用下,3R结构的应力诱发马氏体首先在位错芯附近形核,长大过程中先形成蝶状马氏体,随后位错多余半原子面的中部也发生了马氏体形核.刃型位错降低了应力诱发马氏体形核的激活能,并在相变中起到了塑性协调作用.

关键词: 马氏体相变 , edge dislocation , molecular dynamics simulation , embedded atom type potential , NiAl

MICROSTRUCTURE AND COMPRESSIVE PROPERTIES OF NiAl-TiB_2 PARTICULATE COMPOSITES

XING Zhanping* , GUO Jianting , HU Zhuangqi , AN Geying*Institute of Metal Research , Chinese Academy of Sciences , Shenyang , China * Harbin Institute of Technology , Harbin , China

金属学报(英文版)

Ni-50at.%A1 matrix composites containing 0 to 20v.% TiB2 particles have been successfully fabricated by HPES technique. The results show that the Vickers hardness at room temperature and the compressive yield strength from room temperature to 1000℃ of the composites increase with increasing volume fraction of the strengthening phase. Especially, the yield strength of NiAl-20TiB2 was approximately twice as high as that of unreinforced NiAl. The ductility of the composites at room temperature is also superior to the monolithic NiAl.

关键词: intermetallic matrix composite , null , null , null , null

EFFECT OF Ti-ADDITION ON MECHANICAL ALLOYING OF NiAl

LIU Zhiguang+ * , GUO Jianting * , LI Gusong+ , HU Zhuangqi++State Key Lab. of RSA , Institute of Metal Research , Chinese Academy of Sciences , Shenyang , China * Institute of Metal Research , Chinese Academy of Sciences , Shenyang , China

金属学报(英文版)

Mechanical alloying (MA) of Ni50Al45Ti5 (atomic per cent) is studied by in situ thermal analyses, XRD and metallography. The results showed that the alloying process of Ni50Al45Ti5 is similar to that of Ni50Al50. The addition of 5 at.%Ti prolongs the milling time of alloy prior to the explosive reaction in the alloy. The final product is nanocrystalline β-phase NiAl(Ti) (B2 structure). The addition of 5 at.% Ti shows little effect on the lattice parameter of β-phase.

关键词: mechanical alloying , null , null , null

CREEP DEFORMATION OF INTERMETALLIC ALLOYS

Gerhard Sauthoff(Max-Planck-Institut fur Eisenforschung GmbH. , D-40074 Dusseldorf , Germany)

金属学报(英文版)

Intermetallics for structural applications at high temperatures must show a sufficient high temperature strength which is controlled by creep processes. In the first section the creep behaviour of single-phase intermetallic alloys is overviewed with respect to stress and temperature dependence and effects of composition and microstructure. It is shown in particular that creep deformation is controlled by diffusion. The second section refers to multiphase intermetallic alloys, and both particulate and non-particulate alloys are regarded. Data are presented for single-phase and multiphase alloys based on B2 phases and lesscommon phases and the consequences of diffusion control for alloy design are discussed.

关键词: :creep , null , null , null , null

HIGH TEMPERATURE COMPOSITES

M. V. Nathal (NASA Lewis Research Center Cleveland OH. USA)

金属学报(英文版)

The purpose of this paper is to review the current state of development of new composite materials for advanced aircraft engines. The advantages and disadvantages of Ti-base.NiAl-base, and MoSi_2-base composites as replacements for today's Ni-base superalloys are discussed from the standpoint of key technical issues. current status, and future directions. Results describing progress in both improved understanding of the mechanisms of deformation and fracture, and improved material performance will be covered.

关键词: : composites. Ti alloys , null , null , null , null

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