聚酰亚胺研究新进展

聚酰亚胺（PI）是一类重要的高性能聚合物,广泛应用在航空航天、微电子、汽车、石油等高科技领域。由于其结构上的可设计性,世界上越来越多的研究者投入到这类高技术材料的研究开发中。本文分别从可溶性PI的分子设计与合成、功能性PI的合成与用途、PI绿色合成方法、PI纳米复合材料的制备4个方面综述了近年来PI的研究热点和新进展,为了解聚酰亚胺的研究提供了有价值的信息。     

新型精铸热锻模具钢高温磨损性能同其显微组织的相关性

研究了经不同热处理条件下的新型精铸热锻模具钢的组织同其高温磨损性能的相关性,对比分析了新型铸钢与H13锻钢的高温磨损性能,并探讨了其磨损机理.结果表明:新型精铸热锻模具钢的高温耐磨性能明显优于锻钢H13;在马氏体、贝氏体和马贝复相3种组织中,贝氏体和马贝复相的高温耐磨性能较好,马氏体相的高温耐磨性能最差;经过400～620℃回火处理的新型精铸热锻模具钢的硬度为42～43HRC,高温耐磨性能较好;当回火温度大于650℃或小于400℃时,新型精铸热锻模具钢的磨损率明显增大,耐磨性显著降低.     

高超声速飞行器热防护材料与结构的研究进展

高超声速飞行器是航空航天的一个重要发展方向,在未来国防安全中起着重要作用．高超声速飞行器热防护材料与结构是高超声速飞行器设计与制造的关键技术之一,它关系到飞行器的安全．高超声速飞行器热防护材料与结构主要有金属TPS热防护系统、超高温陶瓷、C/C复合材料等．从材料制备、抗氧化、力学与物理性能表征等方面综述了热防护材料与结构的研究与应用现状,评述了其发展趋势．     

碳纳米管膜的高温纯化研究

为了获得纯度更高的碳纳米管膜, 保证材料发热稳定性, 需要对通过化学气相沉积法得到的碳纳米管膜进行二次纯化. 通过使用高温纯化炉, 在真空状态下, 从1700℃到3200℃分7挡温度对碳纳米管进行纯化, 并对其含碳量和方块电阻进行比较. 结果表明, 高温纯化后的碳纳米管膜含碳量从95.0%提高到99.9%, 解决了含碳量低的问题. 同时, 在高温纯化中发现碳纳米管膜方块电阻从纯化前3Ω降低到0.5Ω, 方块电阻的降低对碳纳米管膜具有十分重要的意义, 同样对碳纳米管膜后续产品的开发也有重要作用.     

The Susceptibility of the Square Lattice Ising Model: New Developments

We have made substantial advances in elucidating the properties of the susceptibility of the square lattice Ising model. We discuss its analyticity properties, certain closed form expressions for subsets of the coefficients, and give an algorithm of complexity O(N⁶) to determine its first N coefficients. As a result, we have generated and analyzed series with more than 300 terms in both the high- and low-temperature regime. We quantify the effect of irrelevant variables to the scaling-amplitude functions. In particular, we find and quantify the breakdown of simple scaling, in the absence of irrelevant scaling fields, arising first at order |T–T_c|^9/4, though high-low temperature symmetry is still preserved. At terms of order |T–T_c|^17/4 and beyond, this symmetry is no longer present. The short-distance terms are shown to have the form (T–T_c)^p (log |T–T_c|)^q with pq². Conjectured exact expressions for some correlation functions and series coefficients in terms of elliptic theta functions also foreshadow future developments.     

The studies of high-temperature and short-time annealing,phase transition process,and magnetic property for LaFe11.7Si1.3 compound

The high-temperature phase transition is analyzed according to the DSC of as-cast LaFe_11.7 Si_1.3 compound and the X-ray patterns of LaFe_11.7Si_1.3 compounds prepared by high-temperature and short-time annealing. Large amount of 1:13 phase begins to appear in LaFe_11.7Si_1.3 compound annealed near the melting point of LaFeSi phase (about 1422?K). When the annealing temperature is close to the temperature of peritectic reaction (about 1497?K), the speed of 1:13 phase formation is the fastest. The phase relation and microstructure of the LaFe_11.7Si_1.3 compounds annealed at 1523?K (5?h), 1373?K (2?h)?+?1523?K (5?h), and 1523?K (7?h) +1373?K (2?h) show that longer time annealing near peritectic reaction is helpful to decrease the impurity phases. For studying the influence of different high-temperature and short-time annealing on magnetic property, the Curie temperature, thermal, and magnetic hystereses, and the magnetocaloric effect of LaFe_11.7Si_1.3 compound annealed at three different temperatures are also investigated. Three compounds all keep the first order of magnetic transition behavior. The maximal magnetic entropy change ΔS_M (T, H) of the samples is 12.9, 16.04, and 23.8?J?kg^?1?K^?1 under a magnetic field of 0–2?T, respectively.     

SrB4 O7 : Eu磷光粉的制备及其发光性能

采用高温固相法合成了SrB₄O₇ : Eu荧光粉,并研究了不同原料、掺杂浓度、煅烧温度等因素对其发光性能的影响。发射光谱测试结果表明:SrB₄O₇ : Eu荧光粉的最佳Eu掺杂浓度为2%左右,进一步增大掺杂浓度会导致浓度猝灭。煅烧温度对基质组成影响较大,随着温度的升高,基质中BO₄四面体所占比例增大,有利于Eu³⁺离子的还原。以水合硼酸锶为原料制得样品的发光强度高于以SrCO₃和H₃BO₃为原料制得样品的发光强度。     

超高温、大热流、非线性气动热环境试验模拟及测试技术研究

超高温、大热流、非线性气动热环境试验模拟技术及相应的极端高温环境力学测试技术,是高超声速飞行器防热材料和结构安全设计中事关研制成败的关键技术。本文介绍了自行研制的可实现高至210℃/s的极快非线性升温速率、能够生成高达2MW/m2的瞬态非线性热流密度、实现高达1500℃超高温氧化热环境的石英灯红外辐射式气动热环境试验模拟系统。基于这一性能优越的超高温气动热环境试验模拟系统,发展了如下超高温热环境力学测试技术:1)提出对环境光变化不敏感的主动成像数字图像相关方法,实现了C/SiC复合材料1550℃高温变形的非接触、全场光学测量;2)发展了1400℃超高温热/力联合试验环境下SiC/SiC复合材料结构的断裂特性试验测试技术。本文还简要介绍了高速巡航导弹翼面结构900℃高温热振联合试验,950℃高温非线性热环境下的蜂窝结构隔热性试验等研究内容。本文所发展的超高温气动热环境试验模拟技术和高温热环境力学测试技术,对航天航空领域高超声速飞行器的研制具有重要的军事工程应用价值。     

Weak Interactions under Pressure: hp‐CuBi and Its Analogues

The metastable binary compound hp‐CuBi was obtained from the direct chemical reaction between copper and bismuth at a pressure of 5 GPa and a temperature of 720 K. The atomic arrangement comprises slabs of puckered Cu layers sandwiched between Bi planes. The QTAIM charges calculated for compounds of bismuth with transition metals reveal negligible charge transfer for hp‐CuBi. Analysis of the chemical bonding with position‐space techniques discloses multicenter interactions within the Bi‐Cu‐Bi slabs and lone‐pair interactions of the van der Waals type between these entities. hp‐CuBi exhibits metal‐type electrical conductivity with superconductivity below T_c=1.3 K.     

YJ-3000t型紧装式六面顶大腔体高温高压实验装置样品室的压力标定

 在温度为389~1 245 ℃和砧面压力为1.0~5.0 GPa的条件下,利用金属高压熔融标定法,采用Cu、Al、Zn和Pb四种金属,对YJ-3000t型紧装式六面顶大腔体高温高压实验装置样品室内的实际压力进行了标定。通过对由四种金属所获得的标定结果的多项式三维模拟,获得了以叶蜡石为外传压介质、氧化铝为内传压介质的情况下,由砧面压力和样品室温度估算样品室内实际压力的定量表达式。该结果可为今后该设备上类似实验组装中样品腔内实际压力的估算提供方便准确的压力标。