压力容器环缝焊接自动跟踪系统的研究

作者研制了一种新型摆动式电弧传感器及其焊缝自动跟踪系统。采用计算机控制，成功地应用于压力容器的环缝脉冲ＭＡＧ焊工艺。实践证明采用这种系统跟踪精度高并获得了优质焊缝。     

大型薄壁铝铸件表面沟槽缺陷的产生及消除

针对大型薄壁铝铸件内腔表面出现的沟槽缺陷,从差压铸造、树脂砂、铸件结构等工艺条件方面探讨了产生的机理,并通过试验和对比研究,确定排气不畅是该缺陷的首要引发因素,找到了消除该缺陷的工艺方法,提出了相关预防措施,避免了因此产生的废品损失.     

节能降碳的蓄热式加热炉烟气反吹关键技术

摘要：蓄热式加热工艺是大型钢铁企业轧钢工序普遍采用的加热技术,但该工艺高频率换向蓄热燃烧导致公共管道内的燃气交替排入大气造成环境污染和能源浪费,使其成为钢铁生产流程中少有未进行污染物治理的生产工序。基于消除蓄热式加热炉热工制度缺陷,系统介绍了蓄热式加热炉烟气反吹扫技术及与之匹配的加热炉烟气反吹安全联锁与防爆技术、烟气反吹工艺设计与时序调控技术。该成果应用于某钢铁企业蓄热式加热炉（160t/h）建设国内首套换向残留燃气反吹技术示范线,该加热炉燃气放散体积分数由9.0%降低至0.208%,CO放散减排率达92%以上,轧钢燃气耗量节约4.38%。其后承建多家钢铁企业19条蓄热式轧钢加热炉烟气反吹改造工程,均取得较好效果,节能、环保及社会效益显著,同时减少碳氧化物的排放量,助力国家实现双碳目标。     

Microstructures and mechanical properties of welded Fe-12Cr-20Mn austenitic stainless steel

The effects of welding on the tensile and fatigue properties of fully annealed and cold-worked Fe-12Cr-20Mn austenitic stainless steel were evaluated. Room temperature and 500 °C tensile tests and room temperature cantilever beam fatigue tests were accomplished on specimens that contained autogenous bead-on-plate welds. The tensile and fatigue properties of the fully annealed material were not significantly influenced by welding. The tensile properties of the welded cold-worked material were also not significantly affected by the presence of a weldment. However, welding caused a large reduction of the fatigue life of the cold-worked material. Fatigue cracks preferentially initiated at large Mn-Si inclusions that formed in the fusion zones of the weldments.     

晶化机制与激活能的晶化速率参比法确定

本文根据修正的Kissinger公式提出一种确定非晶材料晶化机制与激活能的最大晶化速率参比法。以Ar_(70)Cu_(30)非晶合金为例,研究了晶化机制与激活能及其与压力的关系。     

应变速率对闭孔泡沫铝力学性能和能量吸收性能的影响

采用分离式霍普金森压杆 (SHPB)技术 ,研究了应变速率 (1× 10 - 3s- 1 ～ 2 5 0 0s- 1 )对泡沫铝力学性能和能量吸收性能的影响。结果表明 :泡沫铝有较高的应变速率敏感性 ,随应变速率的增加 ,泡沫铝的屈服强度和吸能能力增加 ,泡沫铝的应变速率敏感性随应变、应变速率变化幅度的增加而增加。     

Fe3Al氢脆机理的研究

用余氏理论计算了氢对Ｆｅ３Ａｌ金属间化合物键结构、键能和电子分布的影响，分析发现，Ｆｅ３Ａｌ的氢脆是由于氢原子溶入扣引起Ｆｅ，Ａｌ原子状态变化。使晶体内晶格电子数大大减少，导致晶体局域金属性减弱，并构成具有严重各向异性的键络的结果。同时得出，氢在Ｆｅ３Ａｌ中占据间隙位置。     

Effects of sintering pressure and temperature on microstructure and tribological characteristic of Cu-based aircraft brake material

A novel Cu-based P/M aircraft brake material was prepared and the effects of sintering pressure and temperature on microstructure and tribological characteristic were investigated. For the constant sintering temperature, when the sintering pressure increases from 0.5 MPa to 1.5 MPa, the porosity, wear loss and friction coefficient decrease remarkably. When the sintering pressure increases from 1.5 MPa to 2.5 MPa, the porosity further decreases but in a little degree and wear behaviors are improved slightly. However, once the sintering pressure is larger than 2.5 MPa, it has no obvious effect on microstructure and tribological characteristic. For the constant sintering pressure, when the sintering temperature increases from 900 ℃ to 930 ℃, the sintered density remarkably-increases, and wear behaviors are obviously improved. For further increasing sintering temperature to l 000 ℃, the density keeps on increasing, but wear behaviors change slightly.     

Structure and electronic properties of SiC thin-films deposited by RF magnetron sputtering

SiC thin-films were prepared by RF-magnetron sputtering technique(RMS) with the target of single crystalline SiC and then annealed. The surface morphology of thin-films was characterized by AFM. The result shows that the surface of the thin-films is smooth and compact; XRD analysis reveals that the thin-films are amorphous. The thickness, square-resistance and curves of resistance—temperature were measured. The results show that the curves of lnR versus 1/kT both before and after annealing satisfy the expression of lnR∝△W/kT, where ?W is electron excitation energy in the range of 0.014 2-0.018 5 eV, and it has a trend of increasing when the temperature is increased. After synthetical analysis we get the conclusion that the electronic mechanism of the thin-films is short distance transition between the localized states in the temperature range of 25-250 ℃. The resistivity is in the range of 2.4×10-3-4.4×10-3 Ω·cm and it has the same trend as electron excitation energy when annealing temperature is increased, which further confirms the electronic mechanism of thin-films and the trend of electron excitation energy versus annealing temperature.     

空间高能质子对飞行器材料的损伤分析

针对高能粒子在空间环境中的辐射,本文简要介绍了空间高能质子在空间环境中的分布情况及在物质中的传输问题,评述了国外有关高能质子的非电离能损失及线性能量转移研究,并在此基础上重点分析和研究了高能质子对航空、航天材料的辐射损伤.从空间高能质子对材料的辐射损伤的角度,分析讨论了材料厚度与屏蔽效果的关系并提出了一些相关性的结论和展望;能量为10MeV～80MeV的质子最可能发生辐射损伤效应,质子拟合公式适合于入射质子能量较小的情况.