![]() |
customer@davidpublishing.com |
![]() |
3275638434 |
![]() |
![]() |
| Paper Publishing WeChat |
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License
DONG Yun1, LIU Chun-yang1, LIN Xiao-ping1, WANG Tie-bao1, ZHANG Li-juan1, WANG Zhi-ping2
Full-Text PDF
XML 73 Views
DOI:10.17265/2161-6213/2009.03.008
1. School of Material Science and Engineering, Hebei University of Technology, Tianjin 300130, China;
2. College of Science, Civil Aviation University of China, Tianjin 300300, China
Thermal barrier coating (TBC) obtained on GH99 high-temperature alloy by APS, NiCoCrAlY bond coat was treated by supersonic fine particles bombarding. The microstructure and oxidation behavior of TBC were characterized by transmission electron microscope, scanning electron microscope equipped with energy dispersive spectroscopy (EDS). As shown in the results: After disposed on bond coat by supersonic fine particles bombarding, plastic deformation and large quantities of dislocation obtained on the top of bond coat. The dislocations accelerate the diffusion of atoms to the BC/TC interface. A continuous Al2O3 layer forms on the interface quickly. High temperature oxidation resistance of TBC could be improved.
thermal barrier coating; supersonic fine particles bombarding; high temperature oxidation resistance




