首页> 外文期刊>Coatings >Comparison of the Microstructure Evolution and Wear Resistance of Ti6Al4V Composite Coatings Reinforced by Hard Pure or Ni-plated Cubic Boron Nitride Particles Prepared with Laser Cladding on a Ti6Al4V Substrate
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Comparison of the Microstructure Evolution and Wear Resistance of Ti6Al4V Composite Coatings Reinforced by Hard Pure or Ni-plated Cubic Boron Nitride Particles Prepared with Laser Cladding on a Ti6Al4V Substrate

机译:用激光覆层在Ti6Al4V基板上制备的硬纯或镍立方硼氮化物颗粒增强Ti6Al4V复合涂层的微观结构演化和耐磨性

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Titanium alloy is a major structural material with excellent high specific strength in aerospace applications. Cubic boron nitride (cBN) is a synthetic wear-resistant material with high hardness, similar to that of diamond, that is used in mechanical cutting and grinding. In addition, the thermal stability of cubic boron nitride particles is much better than that of diamond. In order to further enhance the wear resistance of the Ti6Al4V alloy, the laser cladding (LC) technology characteristics of metallurgical bonding were used to prepare cubic boron nitride/Ti6Al4V and Ni-plated cubic boron nitride/Ti6Al4V composite coatings on Ti6Al4V substrates in this paper. However, in the laser molten pool, it is difficult to retain the raw properties of cubic boron nitride particles under laser radiation. Both composite coatings were analyzed using scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), X-ray diffraction (XRD), and X-ray photoelectron spectroscopy (XPS). The microstructures and interface bonding between cubic boron nitride particles and the Ti6Al4V matrix were examined using SEM, and the wear resistance and the worn track morphology of the composite coatings were evaluated using the ball-on-disc wear test and step profiler (WTM-2E). The results indicated that the Ni-plated cubic boron nitride/Ti6Al4V composite coating showed fewer thermal defects in comparison with the cubic boron nitride/Ti6Al4V coating. The Ni plating on the surface of cubic boron nitride particles was able to avoid the generation of thermal cracking of the cubic boron nitride particles in the composite coating. The TiN reaction layer was formed between the cubic boron nitride particles and Ti6Al4V matrix, which effectively prevented the further decomposition of the cubic boron nitride particles. The XRD and XPS results confirmed that the TiN reaction layer formed between the cubic boron nitride particles and Ti6Al4V. The Ni plating on the surface of the cubic boron nitride particles was also beneficial for increasing the wear resistance of the composite coating.
机译:钛合金是主要结构材料,在航空航天应用中具有优异的高度强度。立方氮化硼(CBN)是一种具有高硬度的合成耐磨材料,类似于机械切割和研磨的金刚石。此外,立方硼氮化物颗粒的热稳定性远优于金刚石的热稳定性。为了进一步提高Ti6Al4V合金的耐磨性,使用冶金键合的激光熔覆(LC)技术特性在本文中,在Ti6Al4V底板上制备立方硼氮化物/ Ti6A1V和Ni镀立方氮化硼/ Ti6Al4V复合涂层。然而,在激光熔池中,难以在激光辐射下保留立方硼氮化物颗粒的原始性质。使用扫描电子显微镜(SEM),能量分散光谱(EDS),X射线衍射(XRD)和X射线光电子谱(XPS)分析两种复合涂层。使用SEM检查立方氮化硼颗粒与Ti6Al4V基质之间的微观结构和界面,以及使用球形盘磨损试验和步进分布器评估复合涂层的耐磨性和磨损轨道形态(WTM-2E )。结果表明,与立方氮化硼/ Ti6Al4V涂层相比,Ni镀立方氮化硼/ Ti6Al4V复合涂层显示出较少的热缺陷。立方氮化硼颗粒表面上的Ni电镀能够避免在复合涂层中产生立方氮化物颗粒的热裂纹。在立方氮化硼颗粒和Ti6Al4V基质之间形成锡反应层,有效地防止了立方氮化硼颗粒的进一步分解。 XRD和XPS结果证实,在立方氮化硼颗粒和Ti6Al4V之间形成的锡反应层。立方氮化硼颗粒表面上的Ni电镀也有利于增加复合涂层的耐磨性。

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