Tm2CrFe14.5Si1.5化合物的反常热膨胀性质研究

通过X射线衍射手段研究了Tm2CrFe14.5 Si1.5化合物的热膨胀性质及本征磁致伸缩性质.研究结果表明,Tm2CrFe14.5Si1.5化合物在303～623 K范围内,具有单相的Th2Ni17型结构;Tm2CrFe14.5Si1.5化合物的居里温度约为453 K,比其母合金Tm2 Fe17高约163 K;沿a轴方向上,Tm2CrFe 14.5 Si1.5化合物在423～448 K温度范围内出现负热膨胀现象,其热膨胀系数(α)a为-0.716×10-5/K;沿c轴方向上,在303～398 K温度范围内也出现负热膨胀现象,其热膨胀系数(α)c为-0.547×10-5/K.两者综合的结果使得在423～448 K温度范围内,Tm2CrFe14.5Si1.5化合物的体热膨胀系数(α)为-0.794 × 10-5/K.对本征磁致伸缩的研究结果表明,Tm2CrFe14.5 Si1.5化合物中存在着较强的各向异性的本征磁致伸缩.     

环氧树脂在碳纤维表面的浸润行为

利用场发射环境扫描电境(FESEM)测定了室温下环氧树脂在单纤维表面的接触角,观测并计算了环氧树脂液滴在单根碳纤维表面的接触角随温度的变化,结果表明接触角随温度升高明显降低,说明升高温度有利于改善环氧树脂对碳纤维的浸润性能.用液滴形状分析仪(DSA)在垂直和平行于纤维排列方向上观测了不同温度下单向排列碳纤维集束表面环氧树脂的铺展过程,发现在不同方向上观测到的接触角差别较大,其中垂直于纤维排列方向上观测到的接触角随温度的变化与环氧树脂在单根碳纤维表面的接触角变化基本一致,说明环氧树脂在平行于纤维束方向的接触角真正代表其浸润性能.     

超微Ni(OH)_2纳米粒子的合成及其对Li~+的超高吸附性能（英文）

在葡萄糖水溶液中合成得到平均粒径为5 nm的α-Ni(OH)_2超微纳米粒子。研究结果发现,在水溶液中葡萄糖浓度能够控制α-Ni(OH)_2纳米粒子粒径的大小,我们对其中的原理进行了剖析。当没有葡萄糖存在时,合成得到的Ni(OH)_2晶型为β型,且颗粒粒径尺寸分布为微米级别。另外,研究发现α-Ni(OH)_2超微纳米粒子室温下对中性水溶液中Li~+具有较强的吸附性能,且这种吸附性能随粒径的减小而剧烈增大;粒径为5 nm的α-Ni(OH)_2粒子对Li~+的最大吸附量为214 mg·g~(-1)(远大于文献报道的有关吸附剂对Li~+的吸附容量),而粒径为1μm的β-Ni(OH)_2在相同条件下对Li~+的最大吸附量低于30 mg·g~(-1)。计算分析表明,Li~+在α-Ni(OH)_2纳米粒子表面吸附满足Freundlich方程,符合层层吸附模型。     

热场效应下聚酰亚胺纤维力学性质有限元分析

利用COMSOL Multiphysics 5.3软件构建了聚酰亚胺纤维三维有限元模型。 该模型实现了固体传热和表面对表面辐射传热产生的温度场中聚酰亚胺纤维固体力学的计算,重点分析了孔洞的大小、位置和热膨胀系数的差异对聚酰亚胺纤维力学性能的影响。 结果表明,聚酰亚胺(PI)纤维在两端固定约束的条件下,在固体传热和表面对表面辐射传热产生的温度场中呈现相似的应力变化趋势,即聚酰亚胺纤维出现孔洞,使纤维的力学性能降低,孔洞越大,应力分布越不均衡,越不利于纤维性质的稳定;温度越高,应力越大;但随着负轴向热膨胀系数的增加,应力逐渐减小。     

苯基聚倍半硅氧烷改性大豆油基聚氨酯的合成及其性能研究

以环氧大豆油为起始原料经开环反应合成出大豆油多元醇,并与聚乙二醇(PEG-600)互混作为多元醇原料制备出植物油基聚氨酯.在预聚体合成过程中,加入不同含量的七苯基三环庚硅氧烷三硅醇,通过醇羟基与异氰酸酯基的反应,将聚倍半硅氧烷(POSS)引入到植物油聚氨酯基体中,制备出聚氨酯(PU/POSS)纳米复合材料,并探讨纳米粒子—聚倍半硅氧烷对聚氨酯材料热稳定性,表面疏水性及力学性能的影响.热重分析(TGA)结果表明,在O2条件下,复合材料的初始降解温度Td5和最终稳定温度Tf都会提高,特别是当POSS含量达到9.27 wt%后,聚氨酯在450~500℃之间较强的失重现象消失;DSC结果表明玻璃化温度Tg随粒子含量的增加呈现先增大后减小的趋势;静态接触角测试结果表明随POSS含量的增加,材料表面的疏水、疏油性随之增大.拉伸测试结果表明POSS的引入能在一定程度上提高材料的拉伸强度.     

硅灰石纤维增强聚甲醛复合材料的制备与性能研究

采用经硅烷偶联剂处理的无机矿物硅灰石纤维(WF)填充改性聚甲醛(POM),通过熔融共混制备POM/WF复合材料,并讨论了纤维含量对复合材料的力学性能及热稳定性的影响.研究结果表明:当硅灰石纤维的添加量为1%(质量分数)时,复合材料的断裂伸长率、缺口冲击强度、洛氏硬度最大,分别为44.8%、6.5kJ/m~2、86.1,较纯POM基体分别提升19.5%、7.1%和4.1%.此外,硅灰石的加入能够有效提高复合材料的热稳定性.当硅灰石纤维含量为10%(质量分数)时,复合材料的起始分解温度较纯POM提高了11℃.     

超高分子量聚乙烯纤维表面改性的研究进展

超高分子量聚乙烯(UHMWPE)纤维具有诸多优异性能,因此被广泛应用于纤维增强复合材料(FRP)。但是由于UHMWPE纤维表面光滑且无极性基团,与树脂基体粘接性差,可通过纤维表面改性有效提高FRP的界面强度,进而提升材料性能。本文总结了近几年基于化学处理、等离子体处理、电晕放电和辐射引发表面接枝等方法对UHMWPE纤维表面改性的研究进展,并对改性方法的发展进行了展望。     

离子液体四氟硼酸-1-戊基-3-甲基咪唑的物理化学性质的估算

根据标准加入法原理配制一系列含有已知微量水的离子液体四氟硼酸-1-戊基-3-甲基咪唑([C5mim][BF4])样品,在278.15～338.15 K温度范围内,样品的密度与其含水量呈很好线性关系. 利用外推方法确定了含水量为零时[C5mim][BF4]的密度ρ,得到了密度随温度变化的经验方程:ln ρ=0.120 11-5.79×10-4(T-298.15)和离子液体的热膨胀系数α=5.79×10-4K-1. 根据Glasser理论估算了[C5mim][BF4]的标准熵、表面能和晶格能,晶格能较小使离子液体在室温下能以液态形式存在. 利用空隙模型计算得到了[C5mim][BF4] 热膨胀系数α(计算),与实验测定值在数量级上一致,说明空隙模型有一定的合理性.     

α'-(BEDT-TTF)_2C_6H_4(SO_3)_2的合成、结构与导电性

用恒电流电化学结晶法合成了一种新的基于BEDT-TIF的电荷转移盐α'-(BEDT- TIF)_2C_6H_4(SO_3)_2 [BEDT-TIF = 双亚乙基二硫四硫富瓦烯,C_6H_4(SO_3) _2~(2-) = 对苯二磺酸根]。通过四圆X射线衍射方法测定了α'-(BEDT-TTF) _2C_6H_4-(SO_3)_2的结构。晶体属于单斜晶系,P2/n空间群;晶胞参数：a = 0. 77937(17)nm, b = 0.66989(11) nm, c = 3.4422 (7) nm, β = 91.135(12) °, V = 1.7968(6) nm~3。该晶体中BEDT-TTF~+自由基沿a轴方向形成具有二聚体结构 的交错排列型柱状堆积,沿b轴方向由户并户强分子间相互作用形成一维分子链。 电荷补偿阴离子C_6H_4(SO_3)_2~(2-)则在a方向存在较强的作用。沿c轴方向, BEDT-TTF~+自由基层和阴离子层交替排列形成夹心式结构。α'-(BEDT-TTF) _2C_6H_4-(SO_3)_2在ab面的某方向的室温电导率为0.5913 Ω~(-1)·m~(-1),电 阻率-温度测定曲线表明它具有半导体导电行为。在150K附近,晶体发生了某种相 变。     

HCl溶液中1,2-二(苯并咪唑-2-硫基)乙烷对碳钢的缓蚀行为研究

合成了缓蚀剂1,2-二(苯并咪唑-2-硫基)乙烷((bit)_2E),用元素分析、红外光谱、核磁共振谱和液质联用技术确证了缓蚀剂的分子结构。用静态失重法、动电位极化曲线法和扫描电子显微镜评价了(bit)_2E在HCl溶液中对碳钢的缓蚀性能。结果表明(bit)_2E是一种混合型缓蚀剂,缓蚀率随缓蚀剂浓度增加而增大,随HCl浓度增大而减小,受腐蚀体系温度和放置时间影响较小。在30℃的1.0 mol·L~(-1)HCl溶液中,(bit)_2E浓度为1.0×10~(-3)mol·L~(-1)时的缓蚀率为95.68%。(bit)_2E作为新型缓蚀剂在碳钢表面上的吸附符合Langmuir吸附等温方程式,属于自发进行的物理和化学吸附。     

A mesoscale study of thermal expansion behaviors of epoxy resin and carbon fiber/epoxy unidirectional composites based on periodic temperature and displacement boundary conditions

The thermal expansion behaviors of neat epoxy resin and carbon fiber/epoxy unidirectional (UD) composites were experimentally and numerically studied in this paper. The dynamic mechanical analysis (DMA), thermogravimetric analysis (TG), differential scanning calorimetry (DSC) and thermal conductivity measurement were used to measure the thermo-mechanical properties of epoxy resin at different temperatures. The dilatometer was used to measure the thermal strains and linear CTEs of neat epoxy resin and UD composites. In addition, a mesoscale finite element model based on the periodic temperature and displacement boundary conditions was presented to analyze the thermal expansion behaviors of UD composites. The resin-voids representative volume element (RVE) was used to calculate the thermo-mechanical properties of several kinds of resin-voids mixed matrix. From the results it can be found that the glass transition temperature of epoxy resin, porosity and fiber orientation angle have significant effects on the thermal expansion behaviors of UD composites. The mesoscale finite element analyses (FEA) have obvious advantages than various existing analysis models by comparing their predictive results. The distributions of thermal displacement, thermal stress and thermal strain were extracted between the carbon fiber, resin-voids mixed matrix and their interface, and also between the front and back surfaces of the loading direction, to further investigate thermal expansion structure effects of UD composites. This paper revealed that the mesoscale FEA based on periodic temperature and displacement boundary conditions can be also used for thermal expansion researches of other complex structure composites.     

The dynamic mechanical behavior of random-in-plane short fiber-reinforced epoxy resin composites

In the present paper, the dynamic mechanical properties of random-in-plane short fiber-reinforced epoxy resin composites were studied by using a rheometrics solids analyzer. The three-point bend testing of the four composites (glass fiber/913 epoxy resin, glass fiber/924 epoxy resin, carbon fiber/913 epoxy resin and carbon fiber/924 epoxy resin) was carried out over temperatures from −100°C to 200°C at a frequency of 10 Hz and strain 0.05%. The composites based on 924 epoxy resin, which has been designed specially for high temperature applications, have less energy loss than the 913 epoxy resinbased composites. For the same resin, the carbon fiber-reinforced composites have less energy loss than the glass fiber-reinforced composites. All the composites have less energy loss than their corresponding matrices; the greater the fiber content, the lower the energy loss. The beta transition of 913 epoxy resin has been shifted to a higher temperature after being reinforced. It was shifted from −50°C to −30°C after being reinforced with glass fiber and made a diffuse shoulder-like peak commencing at −30°C after being reinforced with carbon fiber. The 924 epoxy resin has undergone the same change in beta transition as the 913 resin, though to a smaller extent. The phenomenon suggested that interactions between the macromolecules of the epoxy resins and the molecules along the fiber's surface.     

Thermal and mechanical properties of particulate fillers filled epoxy composites for electronic packaging application

Epoxy composites containing particulate fillers‐fused silica, glass powder, and mineral silica were investigated to be used as substrate materials in electronic packaging application. The content of fillers were varied between 0 and 40 vol%. The effects of the fillers on the thermal properties—thermal stability, thermal expansion and dynamic mechanical properties of the epoxy composites were studied, and it was found that fused silica, glass powder, and mineral silica increase the thermal stability and dynamic thermal mechanical properties and reduce the coefficient of thermal expansion (CTE). The lowest CTE value was observed at a fused silica content of 40 vol% for the epoxy composites, which was traced to the effect of its nature of low intrinsic CTE value of the fillers. The mechanical properties of the epoxy composites were determined in both flexural and single‐edge notch (SEN‐T) fracture toughness properties. Highest flexural strength, stiffness, and toughness values were observed at fillers content of 40 vol% for all the filled epoxy composites. Scanning electron microscopy (SEM) micrograph showed poor filler–matrix interaction in glass powder filled epoxy composites at 40 vol%. Copyright © 2007 John Wiley & Sons, Ltd.     

Effect of carbon fiber surface functionality on the moisture absorption behavior of carbon fiber/epoxy resin composites

Polyacrylonitrile (PAN)‐based carbon fibers were electrochemically oxidized in aqueous ammonium bicarbonate with increasing current density. The electrochemical treatment led to significant changes of surface physical properties and chemical structures. The oxidized fibers showed much cleaner surfaces and increased levels of oxygen functionalities. However, it was found that there was no correlation between surface roughness and the fiber/resin bond strength, i.e. mechanical interlocking did not play a major role in fiber/resin adhesion. Increases in surface chemical functionality resulted in improved fiber/resin bonding and increased interlaminar shear strength (ILSS) of carbon fiber reinforced epoxy composites. The relationship between fiber surface functionality and the hydrothermal aging behavior of carbon fiber/epoxy composites was investigated. The existence of free volume resulted from poor wetting of carbon fibers by the epoxy matrix and the interfacial chemical structure were the governing factors in the moisture absorption process of carbon fiber/epoxy composites. Copyright © 2016 John Wiley & Sons, Ltd.     

Viscoelastic properties and residual stresses in polyhedral oligomeric silsesquioxane-reinforced epoxy matrices

Fiber-filled thermosetting polymer composites are extensively used in aerospace industries. One disadvantage of these materials is cure induced or thermally induced residual stresses in the matrix, which may result in deteriorated performance and premature failure. This article explores the use of epoxy/multifunctional polyhedral oligomeric silsesquioxane (POSS) nanocomposites as resins with reduced thermal stress coefficients that result in mitigated residual stresses. The effect of POSS loading on the thermal stress coefficient of the epoxy/POSS nanocomposite resins was investigated from below the β-relaxation to the α-relaxation, or glass transition temperature, (i.e., from −100 to 180 °C) by measuring the shear modulus and linear thermal expansion coefficient. The thermal stress coefficient of the epoxy/POSS nanocomposites is found to be a strong function of temperature, decreasing rapidly with decreasing temperature through the α-relaxation region, increasing in the vicinity of the β-relaxation, and then decreasing below the temperature associated with the peak in the β-relaxation. With increasing POSS content, the thermal stress coefficient is reduced compared with the neat resin in the vicinity of the α-relaxation; however, the thermal stress coefficient increases with increasing POSS content below the temperature of the β-relaxation peak. © 2008 Wiley Periodicals, Inc. J Polym Sci Part B: Polym Phys 46: 2719–2732, 2008     

偶联剂对玻璃纤维/环氧树脂基复合材料介电性能的影响

偶联剂对玻璃纤维／环氧树脂基复合材料介电性能的影响陈平刘胜平张明艳（哈尔滨理工大学电工材料系哈尔滨１５００４０）关键词环氧树脂基复合材料，介电性能，偶联剂，浸润性玻璃纤维／环氧树脂基复合材料（ＧＦＲＰ）具有优异的电气和力学性能．然而孔隙的存在强烈地...     

Determination of Water Diffusion Coefficients and Dynamics in Adhesive/ Carbon Fiber Reinforced Epoxy Resin Composite Joints

To determinate the water diffusion coefficients and dynamics in adhesive/carbon fiber reinforced epoxy resin composite joints,energy dispersive X-ray spectroscopy analysis(EDX)is used to establish the content change of oxygen in the adhesive in adhesive/carbon fiber reinforced epoxy resin composite joints.As water is made up of oxygen and hydrogen,the water diffusion coefficients and dynamics in adhesive/carbon fiber reinforced epoxy resin composite joints can be obtained from the change in the content of oxygen in the adhesive during humidity aging,via EDX analysis.The authors have calculated the water diffusion coefficients and dynamics in the adhesive/carbon fiber reinforced epoxy resin composite joints with the aid of both energy dispersive X-ray spectroscopy and elemental analysis.The determined results with EDX analysis are almost the same as those determined with elemental analysis and the results also show that the durability of the adhesive/carbon fiber reinforced epoxy resin composite joints subjected to silane coupling agent treatment is better than those subjected to sand paper burnishing treatment and chemical oxidation treatment.     

芳纶纤维/SMPU-SiO2复合材料的界面性能研究

选用形状记忆聚氨酯(SMPU)和正硅酸乙酯(TEOS)为前驱体,固体酸对甲基苯磺酸(PTSA)为催化剂,利用空气中的水分为水解水源,通过溶胶-凝胶法原位制备了形状记忆聚氨酯与二氧化硅( SMPU-SiO2)杂化材料,并将杂化材料应用于芳纶纤维增强的柔性复合材料中,以期改善芳纶纤维与基体的界面性能.同时,针对芳纶纤维表面...     

In situ thermoset molecular composites

The polymerization of rigid rod polymer precursors in a reactive matrix precursor, which is later cured in the mold, constitutes the in situ process. A poly-azomethine (PAM) was used as the rigid rod molecule. The resin used was an epoxy. We discuss the prediction of mechanical properties using micromechanics equations for chopped fiber composites. The chemistry used to synthesize the rigid rod polymer PAM in the epoxy precursor is reviewed. Approaches to better control the cure of these epoxy systems through cure kinetics and cure rheology studies completes the thermoset in situ molecular composite process. There was a 71% increase in tensile modulus in comparison to that of the neat epoxy resin. Molecular modeling simulations and continuum mechanics are used to help understand these findings. PAM/epoxy systems were used as a matrix material in the fabrication of unidirectional glass fiber/(PAM/epoxy) structural composites. © 1994 John Wiley & Sons, Inc.     

Effects of surface synergy for the dispersion of short carbon fibers sized by adipic acid modified epoxy resin potassium

The carbon fiber (CF) surface plays a critical role in the performance of CF composite materials. Adipic acid modified epoxy resin potassium (AAEK) prepared with epoxy resin and adipic acid, and KOH was employed as the CF sizing agent. Then, series of surface properties of AAEK‐treated carbon fiber (CF‐AAEK) including surface charge, morphology, and groups were characterized by using Faraday cup, friction coefficient gauge, atomic force microscopy, X‐ray photoelectron spectroscopy, and thermogravimetry. The results indicated that the dispersion coefficient of CF‐AAEK was increased by 1.72 times and there were synergistic effects for the dispersion of short CFs during the sizing treatment process with AAEK. In addition, the flexural strength of treated short CF composite proved to increase by 168%, which evaluated that the better CF dispersion in the matrix was a critical factor for the mechanical property improvement of short CF‐AAEK/epoxy resin composites.