2016
DOI: 10.1007/s11666-016-0484-7
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Microstructure Effect of Intermediate Coat Layer on Corrosion Behavior of HVAF-Sprayed Bi-Layer Coatings

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Cited by 19 publications
(12 citation statements)
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“…In comparison, coatings produced by the high velocity air-fuel (HVAF) method can be characterized by a relatively denser microstructure with less amount of oxides than the above thermal spray methods [18]. Although even the HVAF coatings are not entirely free from pores either [19], [20], among the above-mentioned processes, HVAF has the lowest flame temperature and highest flame velocity (T<1800 °C, V= 700-1500 m/s) [21]. These significantly affect the microstructural features, in particular in situ oxide formation, splat morphology, and porosity that can potentially enhance the level of protection imparted by these coatings and their corrosion behaviour [22].…”
mentioning
confidence: 99%
“…In comparison, coatings produced by the high velocity air-fuel (HVAF) method can be characterized by a relatively denser microstructure with less amount of oxides than the above thermal spray methods [18]. Although even the HVAF coatings are not entirely free from pores either [19], [20], among the above-mentioned processes, HVAF has the lowest flame temperature and highest flame velocity (T<1800 °C, V= 700-1500 m/s) [21]. These significantly affect the microstructural features, in particular in situ oxide formation, splat morphology, and porosity that can potentially enhance the level of protection imparted by these coatings and their corrosion behaviour [22].…”
mentioning
confidence: 99%
“…The protective scale forming elements such as Cr or/and Al are not depleted during the HVAF spraying process and preserved for oxidation protection (see EDS point analysis in Figure a,b). This is a consequence of the negligible in situ oxide pick up or phase transformation during HVAF spraying …”
Section: Resultsmentioning
confidence: 99%
“…The as-sprayed Cr3C2-NiCr coating (Figure 3a) revealed a uniform distribution of Cr3C2 particles (dark gray) in the NiCr binder (light gray). The microstructure images and the corresponding EDS point analysis showed coatings with relatively few defects, including pores, and a negligible oxygen pick-up owing to the high velocity (700-1200 m/s) [30] and low temperature (<1800 °C) [31] of the in-flight particles in the HVAF process . No sign of splats could be seen in Figure 3a, confirming that the particles were well-splashed and plastically deformed during the HVAF process, which provided a good cohesion (particle/particle bonding).…”
Section: As-sprayed and Corroded Cr3c2-nicrmentioning
confidence: 97%