Investigation of the benefits of plasma deposition for the additive layer manufacture of Ti-6Al-4V

被引:447
作者
Martina, F. [1 ]
Mehnen, J. [2 ]
Williams, S. W. [1 ]
Colegrove, P. [1 ]
Wang, F. [1 ]
机构
[1] Cranfield Univ, WELPC, Cranfield MK43 0AL, Beds, England
[2] Cranfield Univ, Mfg Dept, Cranfield MK43 0AL, Beds, England
关键词
Ti-6Al-4V; Additive layer manufacturing; Shaped metal deposition; Plasma welding; Plasma wire deposition; D-Optimal design; MECHANICAL-PROPERTIES; TITANIUM-ALLOYS; LASER; MICROSTRUCTURE; OPTIMIZATION; POWDER;
D O I
10.1016/j.jmatprotec.2012.02.002
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
With increasing emphasis on sustainability, additive layer manufacturing (ALM) offers significant advantages in terms of reduced buy-to-fly ratios and improved design flexibility. Plasma wire deposition is a novel ALM technique in which plasma welding and wire feeding are combined. In the present work, a working envelope for the process using Ti-6Al-4V was developed, and regression models were calculated for total wall width, effective wall width and layer height. The plasma wire deposition process is able to produce straight walls of widths up to 17.4 mm giving a maximum effective wall width after machining of 15.9 mm, which is considerably wider than competing processes. In addition. for Ti-6Al-4V the deposition efficiency averages 93% and the maximum deposition rate is 1.8 kg/h. Coarse columnar grains of beta phase grew from the base during deposition, which transformed into a Widmanstatten structure of alpha lamellae on cooling. Bands were identified in the deposits, which had a repetitive basket-weave microstructure that varied in size. The strength measured by micro-indentation hardness of 387 HV on average is as much as 12% higher than the substrate. These preliminary results indicate that plasma wire deposition is likely to be a suitable process for the ALM of large aerospace components. (C) 2012 Elsevier B.V. All rights reserved.
引用
收藏
页码:1377 / 1386
页数:10
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