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1.
用累积轧制法成功制备了平均晶粒尺寸为200--300nm的超细等轴晶Ti/A1多层复合材料.研究了Ti/A1多层复合材料的微结构变化和力学性能.  相似文献   

2.
本文利用分子动力学模拟方法, 研究了液态Ti75Al25合金在不同冷却条件下形成晶体及非晶的过程(Q1:1.0×1013 Ks-1, Q2: 1.0×1011 Ks-1). 利用平均原子体积、双体分布函数、键角分布函数、键对分析和Voronoi多面体方法研究了微观局域结构随温度的变化关系. 研究发现:在Q1冷却过程中,液态Ti75Al25合金在1000 K发生玻璃化转变,形成非晶结构; 而在Q2冷却过程中,液态Ti75Al25合金发生结晶,并最终形成hcp晶体结构。  相似文献   

3.
本文采用ICP-AES法对钛基复合材料中的合金元素Al、Mo、B的测定进行研究,着重进行了基体元素对待测元素Al、Mo、B的干扰试验及各元素在测定浓度范围内线性相关性,进行了酸度试验,测定了钛基复合材料中上述三元素的含量,得到了较好的精密度和准确度。  相似文献   

4.
用粉末冶金方法制备了6066Al合金和不同SiCp含量的6066Al/SiCp复合材料,用多功能内耗仪在200~600 K温度区间内测试了所研究材料在升温过程中的内耗变化趋势,探讨了6066 Al /SiCp复合材料在不同温度区间的内耗机制.结果表明6066Al/SiCp的内耗值比6066Al合金内耗值高,特别是在高温阶段比6066Al合金内耗值高得多;6066Al/SiCp和6066Al合金在300~470 K时的内耗主要是位错与第二相颗粒交互作用引起的位错内耗,在高温下内耗主要由Al/Al、Al/SiC的界面微滑移引起.  相似文献   

5.
用粉末冶金方法制备了6066Al合金和不同SiCp含量的6066Al/SiCp复合材料,用多功能内耗仪在200~600 K温度区间内测试了所研究材料在升温过程中的内耗变化趋势,探讨了6066 Al/SiCp复合材料在不同温度区间的内耗机制。结果表明6066Al/SiCp的内耗值比6066Al合金内耗值高,特别是在高温阶段比6066Al合金内耗值高得多;6066Al/SiCp和6066Al合金在300~470 K时的内耗主要是位错与第二相颗粒交互作用引起的位错内耗,在高温下内耗主要由Al/Al、Al/SiC的界面微滑移引起。  相似文献   

6.
用粉末冶金方法制备了6066Al合金和不同SiCp含量的6066Al/SiCp复合材料,用多功能内耗仪在200~600K温度区间内测试了所研究材料在升温过程中的内耗变化趋势,探讨了6066Al/SiCp复合材料在不同温度区间的内耗机制。结果表明6066Al/SiCp的内耗值比6066Al合金内耗值高,特别是在高温阶段比6066Al合金内耗值高得多;6066Al/SiCp和6066Al合金在300-470K时的内耗主要是位错与第二相颗粒交互作用引起的位错内耗,在高温下内耗主要由Al/Al、Al/SiC的界面微滑移引起。  相似文献   

7.
报道了Al/Ti双层薄膜超导TES的光子数分辨特性。通过设计双层薄膜的尺寸,使其满足光子数分辨所需的热导、热容需要,制备出了完好的TES。在320m K的低温下,通过测试其对1550nm光脉冲的响应,发现等效光子数分辨率可达到40个左右。这是使用超导TES实现单光子探测及进一步实现量子通讯的重要基础。  相似文献   

8.
岂云开  顾建军  刘力虎  张海峰  徐芹  孙会元 《物理学报》2011,60(5):57502-057502
采用直流磁控溅射的方法制备了Al/ZnO/Al纳米薄膜,并对薄膜分别在真空及空气中进行退火处理.利用X射线衍射仪(XRD)和物理性能测量仪(PPMS)分别对薄膜样品的结构和磁性进行了表征.XRD分析表明,不同的退火氛围对薄膜的微结构有着很大的影响.采用了一种新的修正方法对磁测量结果进行修正,计算了基底拟合误差的最大值,并对修正后样品的磁性进行了分析.结果显示,室温铁磁性可能与Al和ZnO基体之间发生的电荷转移以及在不同退火氛围下Al在ZnO晶格中的地位变化有关.关键词:Al/ZnO/Al薄膜铁磁性磁性表征  相似文献   

9.
高体分SiC_p/Al复合材料螺纹性能的测试   总被引:1,自引:0,他引:1  
从SiCp/Al复合材料性能分析着手,讨论了预置件法、焊接法和粘接法等在空间遥感器研制中常用的联接方法的优缺点,提出了在高体积分数(体分)SiCp/Al复合材料上直接加工螺纹,并加装钢丝螺套的方法来改善螺纹联接性能。对在某高体分SiCp/Al复合材料上加工的M4、M5螺纹进行了拉伸测试,结果表明:加装钢丝螺套前,复合材料螺纹有被拉脱现象;加装钢丝螺套后,M4螺纹、螺杆在3 000~4 000 N被拉断;M5螺纹、螺杆在8 000~9 000 N被拉断,测试后两种规格的螺纹状态良好,可以满足实际应用对该材料拉伸强度的要求,其已应用于工程项目中。  相似文献   

10.
从SiCp/Al复合材料性能分析着手,讨论了预置件法、焊接法和粘接法等在空间遥感器研制中常用的联接方法的优缺点,提出了在高体积分数(体分)SiCp/Al复合材料上直接加工螺纹,并加装钢丝螺套的方法来改善螺纹联接性能。对在某高体分SiCp/Al复合材料上加工的M4、M5螺纹进行了拉伸测试,结果表明:加装钢丝螺套前,复合材料螺纹有被拉脱现象;加装钢丝螺套后,M4螺纹、螺杆在3 000~4 000 N被拉断;M5螺纹、螺杆在8 000~9 000 N被拉断,测试后两种规格的螺纹状态良好,可以满足实际应用对该材料拉伸强度的要求,其已应用于工程项目中。  相似文献   

11.
《Composite Interfaces》2013,20(1):13-24
Layered composite structures can be generated in metallic sheets by roll bonding of dissimilar metals/alloys. In this investigation, heat treatable (Al(Cu)) and non-heat treatable (Al(Si)) aluminium alloys are roll bonded in sheet form. Large hardness differences between layers poses significant bonding challenges in the form of multiple necking within the hard Al(Cu) layers. For successful processing, it is vital to choose the candidate materials in a state of marginal hardness differences during rolling, but being capable of altering properties through subsequent heat treatments. Atomic diffusion takes place during heat treatment of the composite sheet and results in gradual hardness variation across sheet thickness. The Al(Cu) layers contribute to strength, whereas the Al(Si) layers provide protection from corrosion/wear-related degradation in the newly developed hybrid sheet. The overall mechanical properties of the heat-treated composite fall between the base alloys. The bonding interfaces are noted as the potential spots for initiating failure.  相似文献   

12.
    
The effect of annealing condition on the microstructure evolution, together with mechanical properties of Fe-28.5Ni steel processed by one and six cycles of accumulative roll bonding (ARB), was explored. The evolution of microstructure was studied by means of Electron Backscattered Diffraction method. The ARB-processed specimens were annealed for 30 minutes between 500°C and 600°C, and the effect of these annealing processes was elaborated. Results showed a significantly reduced martensite phase during ARB process cycles. Moreover, a refined and stabilised ultrafine structure was obtained in 6-cycle ARB-processed specimen. Results also show that by annealing the 1-cycle specimen at 550°C, no significant microstructural change and mechanical properties variation are identified. As such, no significant microstructural change and mechanical properties variation were notified for annealing of 6-cycle ARB-processed specimen at 500°C. However, annealing at 600°C in both conditions led to a complete recrystallisation of the deformed structure. Annealing at 550°C in 6-cycle ARB-processed specimen showed partial recrystallisation as well as an abnormal grain growth characteristic. The abnormal grain growth was seen by annealing of 1-cycle ARB-processed specimen at 600°C. The changing features of dislocations were discussed in these specimens in terms of changing the dynamics of low- and high-angle grain boundaries. Tensile test results also showed a significant increase in the yield/ultimate tensile strengths with the application of ARB cycles. Although ARB process led to a rapid reduction of total elongation, full restoration during high-temperature annealing returned this value back to the initial, non-deformed, condition.  相似文献   

13.
利用分子动力学方法研究了正化学比的TiAl/Ti3Al双相体系中剪切变形诱发位错形核以及相关结构转变的动态过程以及切变力场对最终结构的影响.研究发现,在TiAl/Ti3Al双相体系中剪切变形诱发黏滞-滑移式的滑移行为;界面在其中起到了传递能量、均衡协变的作用,界面两侧的异相结构保留了单相形变特征.六角密堆积(HCP)-Ti3Al部分各原子层较长时间内呈整体剪切协变,其后形变分化为应力集中诱发层错区和初始完整结构回复区;而面心立方(FCC)-TiAl部分因刚性较大仅存在微协变,其后局部受力区直接诱发相邻原子层间相对滑移,发生FCC向HCP结构转变.变形结构方面,HCP-Ti3Al部分在剪切力较大区域形成连续且稳定的FCC堆垛,近界面区FCC薄层与HCP相交替并存;而FCC-TiAl部分内禀层错和孪晶共存,当力场增大时形成亚稳HCP结构.  相似文献   

14.
采用分子动力学模拟方法,研究了Ti原子连续沉积于Al(001)表面上的薄膜生长过程,分析了入射能量为0.1、5 eV和衬底温度为300、700 K时的界面结合及微观结构.模拟结果表明,增加入射能量和衬底温度,使Ti薄膜的表面越光滑;通过径向分布函数和键对分析技术对薄膜微观结构进行分析,发现衬底温度时薄膜微观结构影响较大,温度300 K及以下时,Ti薄膜主要是FCC结构,随着温度升高,FCC结构成分减少,无序结构成分增加,而入射能量则对薄膜微观结构没有明显影响.  相似文献   

15.
    
Commercial purity aluminium sheets were severely plastic deformed by accumulative roll bonding (ARB). Changes in electrical resistivity at 77 K and microstructure during the ARB process were traced up to 12 cycles, which corresponded to an equivalent strain of 10. The resistivity at 77 K increased with increasing number of ARB cycles, then saturated after about the sixth ARB cycle with a maximum increment of resistivity from starting material of about 1.1 nΩ m. Since lattice defects affect the resistivity of metals, the internal dislocation density and the density of grain boundaries were evaluated from scanning transmission electron microscopy images using Ham's method and grain boundary maps obtained from electron back-scattering diffraction, respectively. The relationship between the change in resistivity and the lattice defects is discussed.  相似文献   

16.
The microstructure and the current transport in Ti/Al/Ni/Au ohmic contacts on AlGaN were investigated in this paper.Significant structural changes of the metal stack occurred upon annealing and ohmic contacts were obtained after thermal treatments above 700 C, with specific contact resistance values , which depend on the thickness of the Ti layer.Although the formation of a TiN interfacial layer is independent of the Ti thickness, different contact structures, i.e. the phases and grain location, were found as a function of the Ti layer, which were crucial for the nanoscale current transport through the contact stack. In particular, conductive atomic force microscopy combined with the resistivity measurement of the main phases formed upon annealing (AlNi, AlAu4, Al2Au) indicated that the low resistivity Al2Au phase provides preferential conductive paths for the nanoscopic current flow through the contact.  相似文献   

17.
    
The roll bonding technique is one of the most widely used methods to produce metal laminate sheets. Such sheets offer interesting research opportunities for both scientists and engineers. In this paper, we report on an experimental investigation of the ‘thickness effect’ during laminate rolling for the first time. Using a four-high multifunction rolling mill, Cu/Al/Cu laminate sheets were fabricated with a range of thicknesses (16, 40, 70 and 130 μm) of the Al layer. The thickness of the Cu sheets was a constant 300 μm. After rolling, TEM images show good bonding quality between the Cu and Al layers. However, there are many nanoscale pores in the Al layer. The fraction of nanoscale pores in the Al layer increases with a reduction in the Al layer thickness. The finite element method was used to simulate the Cu/Al/Cu rolling process. The simulation results reveal the effect of the Al layer thickness on the deformation characteristics of the Cu/Al/Cu laminate. Finally, we propose that the size effect of the Al layer thickness during Cu/Al/Cu laminate rolling may offer a method to fabricate ‘nanoporous’ Al sandwich laminate foils. Such foils can be used in electromagnetic shielding of electrical devices and noisy shielding of building.  相似文献   

18.
In this work, we report first-principles investigation of structural stability of all experimentally observed ordered long-period superstructures (LPSs), viz., r-Al2Ti, h-Al2Ti, Al5Ti3 along with Al5Ti3′, Al11Ti7 and Al3Ti2 LPSs, which are observed only as short-range ordered clusters at nanoscale level in Al-rich TiAl-based alloys. We adopt a procedure based on space-filling tiling arrangement of ordered Ti2Al, Ti3Al, Ti4Al motifs and their combination along with a symmetry analysis programme to determine the unit cell and the crystallographic information of Al5Ti3′, Al11Ti7 and Al3Ti2 LPSs in terms of L10 fcc unit cell. First-principles calculations are performed to further refine these crystallographic parameters (Wyckoff positions and lattice parameters) obtained from the above procedure. Moreover, it is found that the family of five LPSs have subgroup–supergroup relationships with γ-TiAl (Sp. gr. P4/mmm) and among themselves. Further, we find the inherent stability of r-Al2Ti?+?γ-TiAl and 2Al5Ti3?+?γ-TiAl phase mixtures at 0?K compared to isomolecular Al3Ti2 and Al11Ti7 LPSs at their respective concentrations. The calculations of single-crystal elastic constants of Al5Ti3, Al11Ti7, Al3Ti2 and Al5Ti3′ LPSs show all these four structures are mechanically stable. We also calculate antiphase boundary (APB) formation energies for two types of APBs, viz., type-A and type-C in ordered Al5Ti3 LPS using the supercell approach. The relaxed APB energies for type-A and type-C APBs are 15.44 and 124.16?mJ/m2, respectively.  相似文献   

19.
A low resistivity ohmic contact to Si-implanted GaN was achieved using a metal combination of Ti/Al. The effect of a protection cap during post-implantation annealing is investigated, and how it affects the specific contact resistivity (ρc). Relevant differences between the protected (PR) sample with SiO2 and unprotected (UP) sample during the post-implantation annealing were observed after metal alloying at 700 °C. The lower values of ρc have been obtained for UP sample, but with very low reproducibility. In contrast, SiO2 cap layer has demonstrated its relevance in yielding a much more uniformity of a relatively low ρc around 10−5 Ω cm2. Related mechanism for the uniformity in ρc was discussed based on the results obtained from electrical measurements, XRD (X-ray diffraction) analysis, AFM (atomic force microscopy) and SEM (scanning electron microscopy) observations.  相似文献   

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