首页> 外文会议>Diffusion in materials. >ON THE INFLUENCE OF A HEAT TREATMENT FOR AN ALUMINIZING PROCESS BASED ON Al MICROPARTICLES SLURRY FOR MODEL Ni AND Ni20Cr. EXPERIMENTAL AND THEORETICAL APPROACHES.
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ON THE INFLUENCE OF A HEAT TREATMENT FOR AN ALUMINIZING PROCESS BASED ON Al MICROPARTICLES SLURRY FOR MODEL Ni AND Ni20Cr. EXPERIMENTAL AND THEORETICAL APPROACHES.

机译:Ni微粒和Ni20Cr微粒对铝微粉浆的热处理工艺对铝化工艺的影响实验和理论方法。

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The use of thermal barrier coating systems allows superalloys to withstand higher operating temperatures in aeroengine turbines. Aiming at providing oxidation protection to such substrates, an aluminum-rich layer is deposited to form the (X-AI2O3 scale over which a ceramic layer (i.e. YSZ layer) is applied to provide thermal insulation. A new approach is now being investigated within the FP7 European project « PARTICOAT », in which a single step process is employed by applying micro-sized aluminum particles. The particles are mixed in a binder and deposited by brushing or spraying on the substrate surface. During a heat treatment, the particles sinter and oxidize to form a top coat composed of hollow con-joint alumina spheres and simultaneously, an Al-rich diffusion zone is formed in the substrate. For a better understanding of the diffusion / growth processes, preliminary tests were carried out on pure nickel and Ni20Cr model alloys prior to further application on commercial superalloys. The effect of the heat treatment on the coating characteristics (number of layers, thickness, composition, homogeneity, etc.) was particularly investigated to emphasize the mechanisms of diffusion governing the growth of the coatings. The establishment of the diffused layers occurred very readily even at intermediate temperatures (650 and 700℃). However, the layers formed did not match perfectly with the thermodynamic modeling because of the quick incorporation of Ni into molten Al at intermediate temperatures (650℃). In contrast, at higher temperatures (700 and 1100℃) the phases predicted by Thermocalc are in good agreement with the observed thickness of the diffused layers. The incorporation of Cr as an alloying element restrained Al ingress by segregation of Cr even at very low temperatures aluminizing temperatures (625℃).
机译:隔热涂层系统的使用使超级合金能够承受航空发动机涡轮机中更高的工作温度。为了向此类基板提供氧化保护,沉积了一层富含铝的层以形成(X-Al2O3氧化皮),在其上应用陶瓷层(即YSZ层)以提供隔热效果。 FP7欧洲项目“ PARTICOAT”,其中通过应用微细的铝颗粒进行单步处理,将颗粒与粘合剂混合,然后通过刷涂或喷涂将其沉积在基材表面上。氧化形成中空的氧化铝球面涂层,同时在基材中形成富铝扩散区,为更好地理解扩散/生长过程,对纯镍和Ni20Cr进行了初步测试模型合金在进一步应用于商业高温合金之前,热处理对涂层特性(层数,厚度,组成,均匀性等)的影响进行了专门研究,以强调控制涂层生长的扩散机理。即使在中间温度(650和700℃)下,扩散层的建立也很容易发生。然而,由于Ni在中等温度(650℃)下迅速掺入熔融的Al中,因此形成的层与热力学模型并不完全匹配。相反,在较高温度(700和1100℃)下,Thermocalc预测的相与观察到的扩散层厚度高度吻合。即使在非常低的渗铝温度(625℃)下,Cr作为合金元素的掺入也会通过Cr的偏析来抑制Al的进入。

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