4.6 Article

Coating deposition regularity depended on orientation difference in PS-PVD plasma jet

期刊

CHINESE JOURNAL OF AERONAUTICS
卷 33, 期 12, 页码 3460-3468

出版社

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2019.11.017

关键词

Deposition mechanism; Flow field characteristic; Numerical simulation; Orientation difference; Plasma spray - physical vapor deposition; YSZ coating

资金

  1. National Natural Science Foundation of China [51771059]
  2. R&D Program in Key Fields of Guangdong Province of China [2019B010936001]
  3. National Science and Technology Major Project of China [2017-VI-0010-0081]
  4. Science and Technology Project of Guangdong Province of China [2017A070701027, 2014B070705007]
  5. Sciences Project of Guangdong Academy of China [2019GDASYL-0104022]

向作者/读者索取更多资源

The YSZ coatings are prepared by the plasma spray-physical vapor deposition (PS-PVD) technology based on a specific experimental design. The structure, thickness and growth angle of YSZ coatings on the entire circumferential surface of the cylindrical sample are studied. The results indicated that the structure, thickness and deflection growth angle of YSZ coatings are related to the orientation of deposition location. The numerical simulation of the multiphase mixed fluid near the substrate is carried out and the deposition regularity and mechanism of YSZ coatings prepared by PS-PVD is deduced. The growth rate is related to the local characteristics of the plasma flow field, and is directly proportional to the field pressure and inversely proportional to the field velocity. The growth angle of the coating is generally affected by the flow direction of the plasma jet. Especially, the normal component of velocity vector, V-norm, mainly affects the speed at which the coating grows vertically upwards. The tangential component of velocity vector, V-tan, determines the degree that the coating growth direction deviates from the vertical direction. When V-tan not equal 0, the coating forms a fine column with a certain deflection angle and finally develops into an oblique columnar structure. (c) 2020 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

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