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On the Microstructure and Isothermal Oxidation at 800 1200 and 1300 °C of the Al-25.5Nb-6Cr-0.5Hf (at ) Alloy

机译:Al-25.5Nb-6Cr-0.5Hf(at%)合金在800、1200和1300°C下的组织和等温氧化

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摘要

Nb-silicide-based alloys have the potential to replace Ni-based superalloys in future aero engines to enable the latter to meet environmental and performance targets. These new alloys, like the Ni-based superalloys that are currently used, will require environmental protection with a coating system that should be chemically compatible with the substrate. A challenge for alloy development is to discover αAl2O3 scale forming coating alloys and in particular to find out whether such alloys could be “compatible” with other coating alloys for environmental coating systems for the Nb-silicide-based alloys. This paper focuses on these challenges. The alloy Al-25.5Nb-6Cr-0.5Hf (at %) was studied in the cast and heat-treated (1400 °C) conditions and after isothermal oxidation for 100 h in air at 800, 1200 and 1300 °C. The microstructure consisted of the alloyed NbAl3 and C14-NbCr2 compounds, both of which were stable at least up to 1400 °C, a eutectic of the two compounds and very small volume fractions of (Cr,Al,Nb)ss and HfO2. The prior eutectic microstructure was stable at T ≤ 1200 °C and the solid solution was not stable at T < 1200 °C. At 800 °C the alloy did not pest, but exhibited external and internal oxidation, with AlNbO4, CrNbAlO4, and αAl2O3 in the former and deeper oxidation along the NbAl3/Laves phase boundaries in the latter At 1200 and 1300 °C there was only external oxidation and the scale consisted of two layers, the outer was (Al,Cr)NbO4 intermixed with αAl2O3 and the inner was continuous αAl2O3. At all three oxidation temperatures, no Nb2Al was observed below the alloy/scale interface and Hf acted as a reactive element forming HfO2 that enhanced the adhesion of the scale. The alloy exhibited good correlations with αAl2O3 scale forming silicide and silicide + aluminide intermetallic alloys in maps of the parameters δ (related to atomic size), Δχ (related to electronegativity), and VEC (number of valence electrons per atom filled into the valence band) that should assist the design of bond coats that do not pest and form αAl2O3 in their scales.
机译:基于Nb硅化物的合金有可能在未来的航空发动机中替代Ni基超级合金,从而使后者能够满足环境和性能目标。这些新合金,如目前使用的镍基高温合金,将要求环境保护,且涂层系统应与基材化学相容。合金开发的一个挑战是发现αAl2O3形成结垢的涂层合金,尤其是要发现这种合金是否可以与其他用于Nb-硅化物基合金的环境涂层系统的涂层合金“相容”。本文着重于这些挑战。在铸造和热处理(1400°C)条件下以及在800、1200和1300°C的空气中等温氧化100小时后,研究了Al-25.5Nb-6Cr-0.5Hf(at%)合金。微观结构由合金化的NbAl3和C14-NbCr2化合物组成,两者在至少1400°C的温度下都稳定,这两种化合物的共晶和(Cr,Al,Nb)ss和HfO2的体积分数非常小。先前的共晶组织在T≤1200°C时稳定,而固溶体在T <1200°C时不稳定。在800°C时,该合金无害,但表现出内部和内部氧化,前者为AlNbO4,CrNbAlO4和αAl2O3,后者沿NbAl3 / Laves相界更深的氧化。在1200和1300°C,只有外部氧化和氧化皮由两层组成,外部是(Al,Cr)NbO4与αAl2O3混合,内部是连续的αAl2O3。在所有三个氧化温度下,在合金/水垢界面下方均未观察到Nb 2 Al,Hf充当形成HfO 2 的反应元素,从而增强了水垢的附着力。在参数δ(与原子尺寸有关),Δχ(与以下有关)中,该合金与形成αAl 2 O 3 垢的硅化物和硅化物+铝化物金属间化合物显示出良好的相关性电负性)和VEC(填充到价带中的每个原子的价电子数)应有助于设计不会有害并形成αAl 2 O 3 的键合涂层在他们的规模。

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