2011
DOI: 10.1016/j.surfcoat.2011.07.095
|View full text |Cite
|
Sign up to set email alerts
|

Deposition of Ti–6Al–4V using laser and wire, part I: Microstructural properties of single beads

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
2

Citation Types

7
48
0

Year Published

2012
2012
2022
2022

Publication Types

Select...
3
3
2

Relationship

0
8

Authors

Journals

citations
Cited by 166 publications
(55 citation statements)
references
References 20 publications
7
48
0
Order By: Relevance
“…Further away from the weld centre line, Zone 5 in Figure 11, is the unaffected base material microstructure. Similar variations in the microstructure as for welding are induced by metal deposition with wire (Brandl et al 2011a). Figure 12 shows an exemple of such microstructure.…”
Section: Microstructure Due To Weld Thermal Cyclementioning
confidence: 66%
See 1 more Smart Citation
“…Further away from the weld centre line, Zone 5 in Figure 11, is the unaffected base material microstructure. Similar variations in the microstructure as for welding are induced by metal deposition with wire (Brandl et al 2011a). Figure 12 shows an exemple of such microstructure.…”
Section: Microstructure Due To Weld Thermal Cyclementioning
confidence: 66%
“…The welding metallurgy for the studied alloy is detailed in the following. The schematic drawings in Figure 11 are proposed based on the physical metallurgy of welding by Easterling (1993), a general fusion weld analysis of titanium in Lütjering and Williams (2003), the microstructure investigation in Brandl et al (2011a), and own microstructure analysis and modelling. The Fusion Zone (FZ), or solidified weld, is situated in the centre of the joint, Zone 1 in Figure 11.…”
Section: Microstructure Due To Weld Thermal Cyclementioning
confidence: 99%
“…When it comes to metal AM, aerospace appears to be leading the way, seeing opportunities to produce light-weight components, reduce manufacturing lead-times, and improve the buy-to-fly ratios [1][2][3][4][5]. While much development is focused on powder-based processes for fine detail in small parts, commercially available equipment is limited in terms of part build envelope and build rate, especially in aerospace applications [6].…”
Section: Introductionmentioning
confidence: 99%
“…Laser metal deposition process is a contactless manufacturing process that is used for difficult to process materials such as Ti6Al4V [3]. Aerospace industry is in dear need of technology such as LMD process to reduce buy to fly ratio and for repair of high valued components that were not repairable in the past [4,5]. The flexibility offered by the LMD process makes it possible to fabricate parts made of composite and functionally graded materials [6][7][8][9][10].…”
Section: Introductionmentioning
confidence: 99%
“…A number of studies have been carried out in the literature to understand the influence of processing parameters on the economy and properties of laser metal deposited materials [11][12][13][14][15][16]. In this study, the influence of powder flow rate on the microstructure and microhardness of laser metal deposited Ti6Al4V.…”
Section: Introductionmentioning
confidence: 99%