TY - JOUR
T1 - Erosion wear patterns of turboshaft engine compressor under different radial inlet distortion conditions
AU - Yang, Pingping
AU - Li, Chao
AU - Bin, Guangfu
AU - Miao, Haiyan
AU - Gu, Fengshou
N1 - Funding Information:
This work is supported by the National Natural Science Foundation of China [Grant No. 52175091 and 52075165]; The National Funded Local Science and Technology Development Projects [Grant No. 2022ZYT025]; The Key Research and Development Program of Hunan Province [Grant No. 2022GK2023]; The National Natural Science Foundation of Hunan Province [Grant No. 2023JJ30247, 2024JJ5156 and 2024JJ6216].
Publisher Copyright:
© 2024
PY - 2024/10/1
Y1 - 2024/10/1
N2 - Particle velocimetry setup was used to accurately measure the velocity of SiO2 particles. Subsequently, a titanium alloy erosion wear setup enabled the acquisition of data on erosion rate and erosion angle. Leveraging this data, the Tabakoff erosion wear model for compressors was established. Particle motion characteristics, blade erosion wear areas, and erosion rates were meticulously analyzed under no, tip, and hub distortions. The findings reveal that tip distortion has the most severe impact on compressor erosion wear, followed by no distortion, while hub distortion leads to the least erosion wear. In the rotor and stator blades, the maximum erosion rate increased by 51.6 % and 37.3 % under tip distortion and by 46.2 % and 28.6 % under hub distortion compared to no distortion.
AB - Particle velocimetry setup was used to accurately measure the velocity of SiO2 particles. Subsequently, a titanium alloy erosion wear setup enabled the acquisition of data on erosion rate and erosion angle. Leveraging this data, the Tabakoff erosion wear model for compressors was established. Particle motion characteristics, blade erosion wear areas, and erosion rates were meticulously analyzed under no, tip, and hub distortions. The findings reveal that tip distortion has the most severe impact on compressor erosion wear, followed by no distortion, while hub distortion leads to the least erosion wear. In the rotor and stator blades, the maximum erosion rate increased by 51.6 % and 37.3 % under tip distortion and by 46.2 % and 28.6 % under hub distortion compared to no distortion.
KW - Compressor
KW - Erosion wear
KW - Radial inlet distortion
KW - Turboshaft
UR - http://www.scopus.com/inward/record.url?scp=85196793666&partnerID=8YFLogxK
U2 - 10.1016/j.triboint.2024.109907
DO - 10.1016/j.triboint.2024.109907
M3 - Article
AN - SCOPUS:85196793666
VL - 198
JO - Tribology International
JF - Tribology International
SN - 0301-679X
M1 - 109907
ER -
