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Characterization of Multiperforated Plates Manufactured by SLM and EBM for Aeroengine Applications

机译:SLM和EBM制造的航空发动机用多孔板的特性

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Additive Manufacturing has shown growing interest in the last years compared to traditional techniques for aeronautical complex shaped parts. In this context, the development of multiperforated plates by additive techniques such as Selective Laser Melting and Electron Beam Melting with respect to conventional substractive technique by laser drilling can be promising for combustion chamber applications. Multiperforated plates have then been manufactured by SLM at ENSAM ParisTech and by EBM at SIMaP to provide efficient cooling system within the chamber. The present work has been focused on the detailed analysis of these different plates, including microstructural characterization and permeability measurements. A special attention was paid to the surface roughness since this parameter might be beneficial for an increasing heat transfer surface, but also might be deleterious for the film cooling stability because of the onset of turbulent regimes.
机译:与航空复杂形状零件的传统技术相比,增材制造在过去几年中表现出了越来越浓厚的兴趣。在这种情况下,相对于通过激光钻孔的传统的次要技术,通过诸如选择性激光熔化和电子束熔化之类的添加剂技术开发的多孔板对于燃烧室的应用是有希望的。然后,由ENSAM ParisTech的SLM和SIMaP的EBM制造了多孔板,以在腔室内提供有效的冷却系统。目前的工作集中在对这些不同板的详细分析上,包括微观结构表征和渗透率测量。特别要注意表面粗糙度,因为此参数可能有利于增加传热表面,但由于湍流状态的开始,可能对膜的冷却稳定性有害。

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