Please use this identifier to cite or link to this item: https://hdl.handle.net/10316/106638
Title: Direct Energy Deposition: a complete workflow for the additive manufacturing of complex shape parts
Authors: Freire, Bernardo 
Babcinschi, Mihail 
Ferreira, Lúcia 
Señaris, Baltasar
Vidal, Felix
Neto, Pedro 
Keywords: CAD-to-part; Additive Manufacturing; Direct Energy Deposition; Complex Shape Parts
Issue Date: 2020
Publisher: Elsevier
Project: This research was partially supported by European Union's Horizon 2020 under grant agreement No 820776 (project integradde), Portugal 2020 project DM4Manufacturing POCI- 01-0145-FEDER-016418 by UE/FEDER through the program COMPETE 2020, and the Fundac¸ ˜ao para a Ciˆencia e a Tecnologia COBOTIS project (PTDC/EME-EME/32595/2017). This research is also sponsored by FEDER funds through the program COMPETE Programa Operacional Factores de Competitividade, and by national funds through FCT Fundac¸ ˜ao para a Ciˆencia e a Tecnologia under the project UIDB/00285/2020. 
Serial title, monograph or event: Procedia Manufacturing
Volume: 51
Abstract: Metal Additive Manufacturing (MAM) using Direct Energy Deposition (DED) is a fast-growing technological process that brings a positive boost to manufacturing industry. When compared with traditional manufacturing methods the advantages of DED are multiple, it is more cost-effective, reduces material waste and presents reduced manufacturing lead-times. However, the production of metallic parts with a complex shape is still challenging, demanding to avoid manufacturing support structures and the generation of non-horizontal and non-planar layers. Starting from the Computer-Aided Design (CAD) model of the part to produce, we propose an integrated CAD-to-part methodology featuring part decomposition, path planning, distortion and robot motion simulation, generation of the robot code and the production of the real part. Especially challenging is the path planning strategy that highly affects the final part quality. A real use case is proposed to the fabrication of an aircraft part using Laser Metal Deposition (LMD). Results demonstrate the effectiveness of the proposed methodology.
URI: https://hdl.handle.net/10316/106638
ISSN: 23519789
DOI: 10.1016/j.promfg.2020.10.094
Rights: openAccess
Appears in Collections:I&D CEMMPRE - Artigos em Revistas Internacionais

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