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Investigation on the oxidation behaviour of gamma titanium aluminides coated with thermal barrier coatings

机译:涂有热障涂层的γ-钛铝化物的氧化行为研究

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In the present study, the applicability of thermal barrier coatings (TBCs) on γ-TiAl alloys was investigated. Two alloys with the chemical compositions of Ti-45Al-8Nb-0.2B-0.15C and Ti-45Al-1Cr-6Nb-0.4W-0.2B-0.5C-0.2Si were used. Before TBC deposition, the specimens were pre-oxidised in laboratory air or low partial pressure oxygen atmosphere. Yttria partially stabilised zirconia top coats were then deposited using electron-beam physical vapour deposition (EB-PVD). The oxidation behaviour of the γ-TiAl specimens with TBC was studied by cyclic oxidation testing in air at 850 and 900℃. Post-oxidation analysis of the coating systems was performed using scanning electron microscopy with energy-dispersive X-ray spectroscopy (EDS). No spallation of the TBC was observed for pre-oxidised specimens of both alloys when exposed to air at 850℃ for 1100 cycles of 1 h dwell time at high temperature. SEM micrographs of the thermally grown oxide scale revealed outer mixed TiO{sub}2/Al{sub}2O{sub}3 protrusions with a columnar structure. The protrusions contained small particles of zirconia and a low amount of about 0.5 at% zirconium was measured by EDS analysis throughout this outer oxide mixture. The TBCs exhibited excellent adherence on the oxide scale. Intercolumnar gaps and pores in the root area of the TBC were filled with titania and alumina. Below the outer columnar oxide scale, a broad porous zone of predominant titania was observed. The transition region between the oxide scale and substrate consisted of a discontinuous nitride layer intermixed with alumina particles and intermetallic phases rich in niobium formed at the nitride layer/substrate interface. When thermally cycled at 900℃, the oxide scales on the alloy Ti-45Al-8Nb-0.2B-0.15C pre-oxidised in low partial pressure oxygen spalled off after 540 cycles. For the sample with TBC, spallation was observed after 810 cycles. Failure occurred in the thermally grown oxide near the oxideitride layer interface. Microstructural examinations revealed again oxide scales with columnar structure beneath the zirconia top coat and good adherence of the TBC on the thermally grown oxides formed at 900℃.
机译:在本研究中,研究了热障涂层(TBC)在γ-TiAl合金上的适用性。使用了两种化学成分为Ti-45Al-8Nb-0.2B-0.15C和Ti-45Al-1Cr-6Nb-0.4W-0.2B-0.5C-0.2Si的合金。在TBC沉积之前,将样品在实验室空气或低分压氧气气氛中进行预氧化。然后使用电子束物理气相沉积(EB-PVD)沉积氧化钇部分稳定的氧化锆面漆。通过在850和900℃的空气中循环氧化试验研究了TBC对γ-TiAl样品的氧化行为。使用带有能量色散X射线光谱仪(EDS)的扫描电子显微镜对涂层系统进行后氧化分析。两种合金的预氧化试样在850℃,暴露于高温的1100个循环(保持1小时)中均未观察到TBC散裂。热生长氧化皮的SEM显微照片显示,外部混合的TiO {sub} 2 / Al {sub} 2O {sub} 3突起具有柱状结构。突起包含氧化锆小颗粒,并且通过EDS分析在整个该外部氧化物混合物中测量到少量的约0.5原子%的锆。 TBC在氧化皮上表现出优异的附着力。 TBC根部区域的柱间间隙和孔充满了二氧化钛和氧化铝。在外部柱状氧化物垢以下,观察到主要的二氧化钛的宽多孔区域。氧化皮和基底之间的过渡区域由不连续的氮化物层和氧化铝颗粒以及形成在氮化物层/基底界面处的富含铌的金属间相混合而成。当在900℃下热循环时,在540次循环后在低分压氧气中预氧化的Ti-45Al-8Nb-0.2B-0.15C合金上的氧化皮剥落。对于具有TBC的样品,在810个循环后观察到散裂。在氧化物/氮化物层界面附近的热生长氧化物中发生失效。显微组织检查表明,氧化锆表面涂层下面的氧化物鳞片具有柱状结构,并且TBC对900℃形成的热生长氧化物具有良好的粘附性。

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