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Laser metal deposition and microstructural evaluation of Ti-5553, Ti-811 and Mar-M247 as a repair and manufacturing approach for aerospace applications

机译:Ti-5553,Ti-811和Mar-M247的激光金属沉积和显微组织评估,作为航空航天应用的维修和制造方法

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1. Both titanium alloys deposited acceptably, producing test blocks that were fully dense and free from cracks and fusion flaws. 2. Laser deposition performed at powers greater than 1,250 W resulted in excessive heat build-up within the anaerobic chamber, which resulted in damage to gas, water and powder delivery pipework. A large amount of fine par-ticulate material was also ejected from the melt pool during deposition, which caused contamination of the chamber and optical elements, contributing to heat build-up and premature failure. 3. The as-deposited microstructure of Ti-5553 consisted of large columnar and equiaxed prior p grains, with what appear to be concentrations of a forming elements at grain boundaries. This is likely due to chemical segregation during solidification.
机译:1.两种钛合金均可接受地沉积,产生的试块完全致密且无裂纹和熔合缺陷。 2.功率大于1,250 W的激光沉积导致厌氧室内过多的热量积聚,从而损坏了气体,水和粉末输送管道。在沉积过程中,大量细小颗粒材料也从熔池中喷出,这导致腔室和光学元件受到污染,从而导致热量积聚和过早损坏。 3. Ti-5553的沉积显微组织由大的柱状和等轴的先有p晶粒组成,似乎是晶界上形成元素的浓度。这可能是由于固化过程中的化学偏析。

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