Load-Carrying Ability and Erosion Resistance of Carbon Composites in a Convective Heat Flow

This paper presents results of studying the regularities in the variation of the load-carrying ability and erosion resistance of carbon/carbon composites with both pure carbon and borosiliconized matrices under conditions of unilateral heating with a flow of air plasma. A comparative assessment of the characteristics under study for several types of carbon composites is given. The degree of influence of borosiliconizing carbon/carbon composites on their performance in operation in convective flows has been determined.     

纯镍渗硼硅处理工艺及组织性能研究

采用粒状渗剂分别在渗硼硅温度为850、900、950℃,保温时间为2、8 h的工艺参数下对纯镍表面进行固体渗硼硅处理。用光学显微镜(OM)对渗层横断面进行了显微组织观察,用显微硬度计测试渗层的硬度分布,用M200型磨损试验机研究未渗硼硅和渗硼硅纯镍的耐磨性,采用循环氧化试验研究未渗硼硅和渗硼硅纯镍的抗高温氧化性。结果表明,纯镍渗硼硅后,渗层为硅化物层和硼化物层,且硅化物和硼化物的显微硬度都大于基体硬度,渗层厚度随着渗硼硅时间和温度的增加而增加,其范围约为36~237?m,用X射线衍射仪(XRD)分析出渗层为硼化物层(Ni2B)和硅化物层(Ni3Si、Ni5Si2和Ni2Si)。磨损试验结果表明渗硼硅后试样的耐磨性得到提高。抗高温氧化试验结果显示未渗硼硅纯镍试样抗高温氧化性优于渗硼硅后纯镍试样。     

氧乙炔喷焊NiCrBSi-WC涂层激光改性组织及性能影响

采用氧-乙炔火焰喷焊在Q235钢上制备NiCrBSi-WC涂层,使用激光对喷焊层表面改性处理后在电炉中进行固体硼硅共渗。通过SEM、XRD、EDS及显微硬度计等对处理前后涂层组织的微观形貌、物相和显微硬度进行分析,使用摩擦磨损实验机研究对比处理前后各涂层的耐磨性能。结果表明喷焊层表面微孔及夹杂在激光扫描处理后变得平整、致密,涂层主相Ni2.9Cr0.7Fe0.36、FeNi3成分未变,但主相在晶面排列上具有择优取向性且结晶度提高。WC部分分解为W2C、W及C,C被固溶进Ni基中使Cr3C2等碳化物相增多,淬硬层深度达0.25mm,显微硬度提高到909HV,耐磨性能得到提高。在涂层激光重熔的基础上硼硅共渗能够增加Ni3B、Ni2B、NiSi等硼化物及硅化物硬质相,平均摩擦系数由0.583降低为0.428,耐磨性较激光处理后提高近一倍。