2013
DOI: 10.1016/j.surfcoat.2013.08.002
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Pulsed electrospark deposition of MAX phase Cr2AlC based coatings on titanium alloy

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Cited by 32 publications
(20 citation statements)
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“…Comparison of all coatings shows that preferential (103) planes grew during the deposition process instead of (110) or (100/101). A dominant (103) diffraction peak has been reported by Zamulaeva et al [45,46] for the Cr 2 AlC coatings deposited on Ti substrates, as well as by Field [47]. In contrast, Li et al [48] discussed preferential coating growth at (110) planes taking place during deposition on the M38G super alloy.…”
Section: Coating Microstructurementioning
confidence: 92%
“…Comparison of all coatings shows that preferential (103) planes grew during the deposition process instead of (110) or (100/101). A dominant (103) diffraction peak has been reported by Zamulaeva et al [45,46] for the Cr 2 AlC coatings deposited on Ti substrates, as well as by Field [47]. In contrast, Li et al [48] discussed preferential coating growth at (110) planes taking place during deposition on the M38G super alloy.…”
Section: Coating Microstructurementioning
confidence: 92%
“…Nowadays, the ternary carbide Cr 2 AlC has a great potential for industrial application due to excellent high-temperature oxidation resistance and hot corrosion resistance due to the formation of a protective Al 2 O 3 layer [ 16 , 17 , 18 , 19 ]. Cr 2 AlC film has been successfully deposited onto silicon wafers [ 20 ], single crystalline oxide [ 21 , 22 ], steel [ 23 ], Ni-based superalloy [ 17 , 24 ], and Ti alloy [ 25 ]. Cr 2 AlC has been produced using magnetron sputtering, either by sputtering from elemental targets [ 26 ] or compound targets [ 23 ].…”
Section: Introductionmentioning
confidence: 99%
“…Теоретически оценить характер взаимодейст-вия между электродом и подложкой, предсказать состав покрытия можно, рассчитав критерий Па-латника (τ а /τ к ) [32]. Соотношение, использующее только физические константы материалов элект-родов (теплоемкость С, теплопроводность λ, плот-ность ρ), описывает процессы переноса (или оп-ределяет преобладающее направление процесса массопереноса) и имеет следующий вид: (3) где τ а и τ к -характерные времена эрозии (обра-зования очагов плавления в зоне разряда) анода и катода соответственно; С а,к -теплоемкость, Дж/(кг·К); ρ а,к -плотность, кг/м 3 ; λ а,к -тепло-проводность, Вт/(м·К); Т а,к -температура плавле-ния, К; Т 0 -температура окружающей среды, К.…”
Section: исследование эрозионной способности электродных материалов иunclassified