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发动机用GH4169合金NiAl涂层离子镀制备及其高温氧化分析

High Temperature Oxidation-Resistance of GH4169 Alloy Surface Modified with NiAl Ion-Plated Coatings

  • 摘要: 采用离子镀方法在发动机用GH4169合金表面制备NiAl涂层,并通过实验测试的方式对其组织结构以及抗1100℃高温氧化能力进行分析。研究结果表明:热处理后基体表面形成了约15μm的NiAl涂层,涂层和基体间形成了致密的界面。经过真空热处理后,在涂层内只剩下β相。在涂层表面产生了连续分布的多边形氧化物,在涂层表面也没有观察到明显的孔隙结构,涂层内形成了以α-Al2O3相与γ-Ni3Al相为主的成分。随着氧化时间的增加,在涂层内产生了许多尖晶石结构,已观察不到β相的衍射峰,导致氧化皮受到破坏,从而减弱了涂层防护能力。NiAl涂层试样发了抗氧化能力的明显增强,具备比基底更强抗氧化能力。当氧化初期涂层发生了氧化速率下降,此时在涂层表面产生了致密氧化铝膜,可以有效保护涂层,降低Al消耗量。

     

    Abstract: The surfaces of GH4169 alloy,an important aero-engine material,were modified with NiAl coatings deposited by ion plating.Oxidized at 1100℃,the surface microstructures,phase structures and oxidation behavior of the NiAl-coating were characterized with X-ray diffraction,energy dispersive spectroscopy and scanning electron microscopy.The results show that the NiAl coating significantly increased the high temperature oxidation resistance.After annealing and ageing,β-phase grains dominated the compact 15 μm thick NiAl coatings with strong interfacial adhesion.In oxidation at 1100℃,a dense and compact Al2O3,top-layer formed in the initial stage,effectively prevented further oxidation and consumption of Al;later on,α-phased Al2O3 and γ-phased Ni3Al coexisted in the NiAl coating;as the oxidation time increased,the spinel structured grains formed,possibly resulting in vanishing of β-phased NiAl diffraction peak and weakening of the Al2O3-layer protection.

     

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