Author/Authors :
Liu، نويسنده , , Kun and Tang، نويسنده , , Jianjiang and Bai، نويسنده , , Yu and Yang، نويسنده , , Qingzhen and Wang، نويسنده , , Yu and Kang، نويسنده , , Yongxia and Zhao، نويسنده , , Lei and Zhang، نويسنده , , Ping and Han، نويسنده , , Zhihai، نويسنده ,
Abstract :
This paper aims to elaborate the particle in-flight behavior during plasma spraying and its significance in determining the microstructure and mechanical properties of La2Ce2O7 (LC) coatings. One Box-Behnken Design (BBD) method was applied to analyze the effect of spray parameters on average velocity and temperature of in-flight particles during spraying. LC coatings were characterized in terms of the microstructure, hardness and fracture toughness. It was found that the argon flow rate was the most important parameter that influenced the velocity of particles, however the main factors of affecting the particles temperature was the hydrogen flow rate. The improvement of melting index of in-flight particles increased the lattice parameters of as-sprayed coatings while decreased defects (unmelted particles, pores and cracks). Decreasing defects resulted in increasing hardness and elastic modulus of the coatings. However, the fracture toughness of coatings maximized at the content of defects reached approximately 9.4%.
Keywords :
Supersonic atmospheric plasma spraying , Thermal barrier coatings , Melting index , Lanthanum-cerium oxide