| Citation: | Shi Lei, Lu Zhiqiang, Peng Hongbo, et al. Study on influence of particle kinematics on fan blade erosion[J]. Journal of Aerospace Power, 2026, 41（8）：20250025 doi: 10.13224/j.cnki.jasp.20250025
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The fan boost stage components of high bypass ratio turbofan engines were taken as the research object to conduct a simulation study on the particle erosion phenomenon that occurs during aircraft takeoff and landing in the northwest and southeast coastal regions of China. The Lagrangian particle tracking theory was employed to precisely capture the positional parameters and kinematic characteristics of particle-wall collision dynamics. The results showed that the erosion rate on the pressure side of the blade in the northwest region was much higher than that in the coastal region. As the rotational speed decreased, the erosion area expanded and extended towards the trailing edge, the number of particles entering the core passage increased, the number of particles entering the bypass passage and the number of particles impacting the fan blade decreased. The increase or decrease in the number of larger particles was more significant. When the full speed condition was reduced to 80% speed condition, the blade wear rate in the northwest region decreased by approximately 49.4%, the maximum erosion rate at the 95% blade height section decreased by approximately 54.1%, and the particle impact velocity on the pressure side decreased by approximately 7.5% to 24.6%. In the coastal region, the blade wear rate decreased by approximately 45.8%, the maximum erosion rate at the 95% blade height section decreased by approximately 60.6%, and the particle impact velocity on the pressure side decreased by approximately 12.5% to 22.9%.
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