激光直接沉积NiCrSiFeB合金替代航空部件中钴的新工艺研究

J. Pereira, F. Zubiri, David Aguilar, M. C. Taboada, G. Guillonneau, J. Rocchi
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引用次数: 1

摘要

镍基NiCrSiFeB合金(Ni-Cr-Si-B自熔剂家族)是替代钴基合金用于密封圈、阀座、滑动轴承座等航空部件的优秀候选材料。在这类部件中,通常由离心铸造和传统工艺制造,高温磨损和复杂热机械应力下的刚度导致密封性不足和磨损率增加。直接激光粉末金属沉积(p-LMD)金属增材制造是这类合金复杂加工的潜在制造途径。这项研究工作涉及使用p-LMD开发新的制造路线,包括正确选择起始粉末的化学成分,LMD工艺参数的开发,以解决Ni-Cr-Si-B合金的宽凝固范围和裂纹敏感性的挑战,其监测和控制,以及实现航空部件制造所需的后处理。在本工作中,研究了不同化学成分等级和LMD工艺参数设置(慢速、正常和快速沉积速度)制造的圆柱体的孔隙率分析、原位组织、室温和高温硬度以及强化机理。
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Development of a New Manufacturing Route by Direct Laser Metal Deposition With NiCrSiFeB Alloys to Replace Cobalt in Aeronautical Components
Nickel-based NiCrSiFeB alloy (Ni-Cr-Si-B self-fluxing family) are excellent candidates for replacing Cobalt-based alloys in aeronautical components such as sealing rings, valve seats, sliding bearing seats, etc. In this type of components, commonly manufactured by centrifugal casting and conventional processes, high temperature wear and stiffness under complex thermo-mechanical stresses cause lack of sealing and an increase in the wear rate. Metal additive manufacturing by direct laser metal deposition with powder (p-LMD) is presented as a potential manufacturing route for the complex processing of this type of alloys. This research work deals with the development of a new manufacturing route using p-LMD that ranges from the proper selection of the chemical composition for the starting powders, the development of the LMD process parameters to tackle the challenges associated to the wide solidification range and crack susceptibility of Ni-Cr-Si-B alloys, its monitoring and control, as well as the post-processing required to achieve the manufacture of aeronautical components. In this work, the porosity analysis, as-built microstructure, hardness at room temperature and at high temperature, and the strengthening mechanisms have been studied in cylinders manufactured with different chemical composition grades and LMD process parameter sets (slow, normal and fast deposition speed).
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