2016
DOI: 10.1016/j.phpro.2016.08.078
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Laser Metal Deposition as Repair Technology for a Gas Turbine Burner Made of Inconel 718

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Cited by 90 publications
(29 citation statements)
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“…The applications of LMD in industry have been growing in recent years [1][2][3][4]. For its development, research nowadays involves all kinds of areas, such as process optimization [5][6][7][8][9], modelling/simulation [10][11][12][13][14], and material microstructure and mechanical properties [15][16][17][18][19].…”
Section: Introductionmentioning
confidence: 99%
“…The applications of LMD in industry have been growing in recent years [1][2][3][4]. For its development, research nowadays involves all kinds of areas, such as process optimization [5][6][7][8][9], modelling/simulation [10][11][12][13][14], and material microstructure and mechanical properties [15][16][17][18][19].…”
Section: Introductionmentioning
confidence: 99%
“…Similarly, defects in end-of-life marine components such as the crankpin journal surface consist of ridges, cuts, and grooves that are restored through grinding on a stationary machine [27]. Likewise, in the aerospace or aircraft industry, remanufacturing involves the repair of landing gear parts and flight surface actuators as well as rebuilding chipped parts of gas turbines [20,28].…”
Section: Producers Output Value (In Usd)mentioning
confidence: 99%
“…The progress in AM application today is depicted in Figure 2. in the aerospace or aircraft industry, remanufacturing involves the repair of landing gear parts and flight surface actuators as well as rebuilding chipped parts of gas turbines [20,28]. With the advancement of technologies, it is foreseen that the manual reparation processes of remanufacturable products can be possibly replaced by digital restoration such as additive manufacturing (AM) as the primary option [29][30][31].…”
Section: Producers Output Value (In Usd)mentioning
confidence: 99%
“…Powder bed fusion (PBF) and directed-energy-deposition (DED) are the two most widely-employed techniques for printing functional metal components. (A) Pure-Copper component manufactured via EBM with internal core structure [127] (B) Porous Nickel-Titanium shape-memory structure enabled via SLM [128] (C) LMD (or DED) repair of SLM-based Inconel 718 fuel burner [39] (D) Porous Ti6Al4V components enabled via SLM technique [129] (E) Structurally-optimized titanium-alloy component enabled via SLM [122] (F) Titanium hip stems manufactured via EBM [130]. …”
Section: Figurementioning
confidence: 99%