Design of Lu2O3-reinforced Cf/SiC-ZrB2-ZrC ultra-high temperature ceramic matrix composites: Wetting and interfacial reactivity by ZrSi2 based alloys

The wettability and infiltration of molten ZrSi₂ and ZrSi₂-Lu₂O₃ alloys into C_f/SiC and B₄C-infiltrated C_f/SiC composites were investigated to understand the interfacial interactions that occur during the development of C_f/SiC-ZrC and C_f/SiC-ZrB₂-ZrC-Lu₂O₃ materials. A significant evaporation of Si from the liquid affected the wetting behaviour of the alloy when tested in a vacuum at 1670 °C. The better wetting and spreading of the alloy over the surface was observed for the composites with lower overall porosity (12 %). On the other hand, the formation of an outer dense layer, followed up by the uniform infiltrated region up to ～ 1 mm was observed for the C_f/SiC with higher porosity (21 %). The infiltrated alloy reacted with SiC matrix to form ZrC or with B₄C-infiltrated SiC matrix to form ZrB₂-ZrC-SiC. The Lu₂O₃ particles were not wetted by the melt, and were pushed away of the reaction zone by the solidification front.     

Influence of starting powder choice on structure property relations in gadolinia stabilized zirconia 3Gd-TZP manufactured from co-milled starting powders

Two 3Gd-TZP materials were manufactured from powders produced by intense mixing and milling of unstabilized zirconia starting powders and gadolinia as stabilizer oxide by hot pressing at 1250 °C – 1400 °C. The materials show a combination of high toughness and moderate strength. In detail depending on starting powder the two TZP showed distinct differences concerning transformation characteristics, sintering temperature dependence of mechanical properties and the tendency to develop R-curve related deformation features such as non-linear stress strain curves and formation of transformation bands prior to fracture.     

注射成型立构复合聚乳酸的热变形性能分析

采用左旋聚乳酸（PLLA）和右旋聚乳酸（PDLA）为原料,采用熔融共混法制备了立构复合聚乳酸（SC?PLA）粉末,再通过注射成型制备了SC?PLA样条,并通过差示量热扫描仪（DSC）和热变形温度测定仪对SC?PLA粉末和样条的熔融、结晶情况和热变形性能进行了表征分析。结果表明,SC?PLA粉末的结晶能力与初始熔融状态直接相关;当熔融温度为220~230 ℃时,SC?PLA粉末的熔融稳定时间增加,有助于SC?PLA体系结晶,该温度适合SC?PLA的注射成型加工;SC?PLA样条中SC?PLA结晶度越高,均聚物PLA结晶度越低,越有助于样条热变形性能的提高;低注射温度和以SC?PLA粉末、PLLA、PDLA为原料成型有助于SC?PLA样条在220 ℃下加热再退火后获得较高的SC?PLA结晶度,其热变形温度最高可达到150 ℃以上;注射成型过程中,有利于保留更多SC?PLA晶体和提高SC?PLA结晶度的方式,有助于提高样条在退火后的热变形性能。     

晶须增韧EVA/PE⁃LD/ATH复合材料的阻燃性能研究

制备了晶须增韧乙烯-乙酸乙烯酯共聚物/低密度聚乙烯/氢氧化铝（EVA/PE-LD/ATH）复合材料,通过扫描电子显微镜（SEM）、热重分析仪（TG）、氧指数仪、锥形量热仪（CCT）、万能拉力机和高阻计等对添加不同晶须的EVA/PE-LD/ATH复合材料的微观结构、阻燃性能、力学性能和电学性能进行了表征。结果表明,ATH颗粒在复合材料中未出现明显团聚,复合材料中晶须呈交错分布并与基体界面结合致密;晶须对复合材料阻燃性能的提高源于晶须热解产物网络状骨架对炭层的增强作用;碱式硫酸镁晶须（MHSH）、硼酸铝晶须（ABW）和硫酸钙晶须（CSW）添加质量比为13.5∶6.75∶6.75的复合材料的800 ℃质量保留率为32.7 %,极限氧指数为26.8 %,热释放速率峰值为364.4 kW/m²,总热释放量为20.8 MJ/m²,总烟释放量为187.2 m²/m²,阻燃性能相对最优;MHSH具有降低复合材料热释放速率峰值、总烟释放量和增强复合材料拉伸强度的作用,而CSW能够延迟点燃时间,减弱出现轰燃的趋势,但增大了总烟释放量,同时,CSW还具有提高复合材料断裂伸长率的增韧作用;混合晶须对复合材料拉伸强度、邵氏硬度和电绝缘性能的影响有限。     

热膨胀法判定建窑黑瓷烧成温度的应用研究

以热膨胀仪判定建窑黑瓷烧成温度的研究为例,综合运用多种测试方法对建窑黑瓷标本进行了系统研究,探讨如何从建窑黑瓷胎体重烧热膨胀曲线中筛选有效转折点的问题及其转折点的形成原因。研究表明:(1)建窑黑瓷胎体重烧热膨胀曲线上有三个转折点,分别为收缩转折点、膨胀转折点和急剧收缩点。其中第一个收缩转折点是判定其古代烧成温度的关键点。(2)建窑黑瓷胎体重烧热膨胀曲线上膨胀转折点和急剧收缩点的形成皆与其胎体中大量Fe_2O_3在高温下发生分解反应有关。该研究不仅为热膨胀仪测定建窑黑瓷烧成温度的应用研究提供判定依据,也将为科学认识古陶瓷胎体重烧热膨胀曲线上多个转折点的形成机理提供数据支持。     

基于短时间温升试验和参数估计模型预测稳定温度

电机在稳定运行状态下的绕组温度是反映电机性能的重要参数。通常,检测机构依据GB/T1032-2012中规定的方法进行温升试验,至少需要持续3小时,甚至达到6小时。短时间内求取电机稳定温度能够提升检测机构温升检测试验的效率,节约检测机构大量的电力成本和人工成本。同时,根据预测温度能够监测绕组温度,避免绕组的绝缘漆损坏而导致电机烧毁。通过研究均匀纯铜的指数发热规律、创新实时带电测量绕组温度的装置和基于线性逼近方式建立参数估计模型的方法,搭建了在短时间高精度预估电机温度的系统。在对不同功率段电机进行现场温升实验验证中,结果表明系统能够高效准确的预测电机的稳定温度。     

颗粒强化钛基复合材料的氧化特性

研究了以ＴｉＣ颗粒增强的钛基复合材料的氧化特性。指出ＴｉＣ增强的钛基复合材料在６５０℃以上高温有着其它耐热钛合金不可比拟的高温抗氧化性能；ＴｉＣ／Ｔｉ的反应界面层有利于氧原子的扩散，使复合材料在６５０℃以下的氧化初期氧化速度较快；但在６５０℃以下经长时间保温，其氧化特性和其它耐热钛合金相似。     

ZG20CrMoV低合金耐热钢主蒸汽弯管研制

介绍了在普通铸造生产条件下一次性成功铸造出火电厂耐热高压蒸汽弯管的工艺措施，避免了因其材质独特、弯度大、管壁厚而易产生缩孔、缩松、裂纹等缺陷。     

Investigation of Creep Feed Grinding Parameters and Heat treatment Effects on the Nickel-base Superalloys

The Nickel base Superalloys are the most famous complicated and useable of Superalloys to make hot zone components of the gas turbines. The complicated dimensional tolerances, specially at the root of the blade show importance of grinding processes at the production of blades root. The prediction of the effect of machining parameters on the soundness of component surface strengthening for reaching to a suitable surface finishing and avoiding from crack formation at the work part during machining operation often is not easy and feasible so needs to more industrial investigation.This research is about frame 5 blade designed by GE and made from Superalloy IN738LC has been investigated. The formation of a plastically deformed and heat affected zone during grinding of Superalloy IN738LC with a high depth of cut but slow work speed (creep feed grinding) was investigated. Parameters such as work speed, depth of cut and radial dressing speed have been considered as variables and their effects have been studied. During experimental performed, the voltage and current of motor measured and power and special energy calculated.Some samples heat-treated (of the 1176℃ for 1 hr under neutral argon gas and cooling rate of 15℃/min up to 537℃ and then air cooling) to study grains recrystallization. Other samples have been created from the roots of blades and then coated by Nickel to measure boundary layer micro-hardness. The results show that increasing work speed leads to increasing the use power. Increasing the depth of cut, by increasing material removal rate, and the radial dressing speed, by decreasing power, lead to decreasing special energy. The temperature created by grinding lead to decreasing plastic deformation and boundary layer formation. When the radial dressing speed changes from 1 to 0.6μm/rev and other parameters are kept unchanged the roughness of surface increases and the special energy decreases. Sufficient dressing is very essential in limiting the width of the molten zone to few micrometers. As a result, it was found that local melting at contact spots to be a rather common mechanism during grinding of superalloys, lead to so-called white layers which can easily be observed on metallographic cross sections.     

Evaluation of Process Capability in Gas Carburizing Process to Achieve Quality through Limit Design Concept

NUMEROUS INDUSTRIAL APPLICATIONS requirea hard wear-resistant surface called the case,and arelatively soft,tough inside called the core.There arefive principal methods of case hardening:?Carburizing?Nitriding?Cyaniding or carbonitriding?Flame hardening?Induction hardeningThe first three methods change the chemicalcomposition,carburizing by the addition of carbon,nitriding by the addition of nitrogen and cyaniding bythe addition of both carbon and nitrogen.The last twomethods do n…