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An Integrated Forming Process for Manufacturing Ti6Al4V Impeller with a Functional Coating Layer Using Hot Isostatic Pressing

机译:热等静压制造具有功能涂层的Ti6Al4V叶轮的集成成型工艺

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摘要

The complex aircraft components are difficult to manufacture because of their complicated shapes and high requirements of mechanical properties. Besides, those components usually need a functional coating layer on the surface to improve the reliability, which adds an extra production cycle after manufactured. In this study, an integrated forming process was proposed to manufacture a complex-shaped impeller together with the surface coating layer using hot isostatic pressing (HIP). In this new process, an HIP mold with the graphite core pre-deposited a Ni coating layer was designed and conducted with the HIP experiment. The results show that the manufactured impeller had a dimensional precision of 0.15mm. The scanning electron microscope/X-ray diffraction (SEM/XRD) analyses show that the internal microstructure was compact with alpha+beta phases and the surface had a uniform Ti2Ni/TiNi coating layer. The mechanical experiments show that the HIPped specimens had a 70MPa higher yield strength and 95MPa higher tensile strength than the same-size forgings. Besides, a Ti2Ni/TiNi coating layer was formed on the surface of the impeller and the hardness and wear resistance had an obvious improvement. All the results show that the new process was successfully applied to near net shaping of an integrated Ti6Al4V impeller with a functional coating layer.
机译:复杂的飞机部件由于其复杂的形状和对机械性能的高要求而难以制造。此外,这些组件通常在表面上需要功能涂层以提高可靠性,这在制造后增加了额外的生产周期。在这项研究中,提出了一种集成成型工艺,以使用热等静压(HIP)来制造复杂形状的叶轮及其表面涂层。在这一新工艺中,设计并进行了带有HIP实验的HIP模具,该模具具有预先沉积了Ni涂层的石墨芯。结果表明,所制造的叶轮的尺寸精度为0.15mm。扫描电子显微镜/ X射线衍射(SEM / XRD)分析表明,内部微观结构致密,具有α+β相,并且表面具有均匀的Ti 2 Ni / TiNi涂层。力学实验表明,与相同尺寸的锻件相比,HIPped试样的屈服强度高70MPa,抗拉强度高95MPa。此外,在叶轮表面上形成了Ti2Ni / TiNi涂层,硬度和耐磨性有了明显的提高。所有结果表明,该新工艺已成功应用于带有功能涂层的集成Ti6Al4V叶轮的近净成形。

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