TY - JOUR
T1 - Meshing position shift induced by eccentricity errors
T2 - Mechanisms and influences on stiffness, wear, and load sharing in planetary gears
AU - Dong, Xingjian
AU - Ouyang, Weiping
AU - Hu, Shengyang
AU - Fang, Zongde
AU - Peng, Zhike
AU - Gao, Shuai
AU - Pu, Huayan
AU - Luo, Jun
N1 - Publisher Copyright:
© 2026 Elsevier B.V.
PY - 2026/7/1
Y1 - 2026/7/1
N2 - Planetary gear systems inherently contain eccentricity errors that degrade dynamic performance and load sharing, causing distinct tooth wear patterns. To address this issue, an improved Loaded Tooth Contact Analysis (LTCA) model is developed to determine actual meshing positions through nonlinear iteration and predict the modulation effect of eccentricity on Time-Varying Mesh Stiffness (TVMS). A tooth wear prediction model accounting for micro-cycles of contact stress is also established. These components are integrated into a planetary gear dynamics model, forming a comprehensive “TVMS-dynamics-wear” framework for simulating full-lifecycle dynamic wear evolution. For healthy gears, early meshing increases average mesh stiffness by approximately 12% for external mesh pair and 15% for internal mesh pair, whereas delayed meshing reduces it by 9% and 3%, respectively. Throughout all wear stages, eccentricity errors continue exerting significant modulation on TVMS, leading to clearly differentiated wear patterns across tooth surfaces. Notably, under identical input shaft revolutions, the wear-induced TVMS fluctuation amplitude for internal mesh pairs is merely 3%–6% of that for external mesh pairs, indicating substantially less wear accumulation on internal meshing surfaces. Furthermore, as wear progresses, intensified force fluctuations cause progressive degradation of load sharing performance. Validated by experimental data, the integrated framework provides an effective numerical tool for investigating dynamic behavior and wear evolution in planetary gear systems with eccentricity errors, demonstrating good application potential for life cycle fault prognosis based on digital twins.
AB - Planetary gear systems inherently contain eccentricity errors that degrade dynamic performance and load sharing, causing distinct tooth wear patterns. To address this issue, an improved Loaded Tooth Contact Analysis (LTCA) model is developed to determine actual meshing positions through nonlinear iteration and predict the modulation effect of eccentricity on Time-Varying Mesh Stiffness (TVMS). A tooth wear prediction model accounting for micro-cycles of contact stress is also established. These components are integrated into a planetary gear dynamics model, forming a comprehensive “TVMS-dynamics-wear” framework for simulating full-lifecycle dynamic wear evolution. For healthy gears, early meshing increases average mesh stiffness by approximately 12% for external mesh pair and 15% for internal mesh pair, whereas delayed meshing reduces it by 9% and 3%, respectively. Throughout all wear stages, eccentricity errors continue exerting significant modulation on TVMS, leading to clearly differentiated wear patterns across tooth surfaces. Notably, under identical input shaft revolutions, the wear-induced TVMS fluctuation amplitude for internal mesh pairs is merely 3%–6% of that for external mesh pairs, indicating substantially less wear accumulation on internal meshing surfaces. Furthermore, as wear progresses, intensified force fluctuations cause progressive degradation of load sharing performance. Validated by experimental data, the integrated framework provides an effective numerical tool for investigating dynamic behavior and wear evolution in planetary gear systems with eccentricity errors, demonstrating good application potential for life cycle fault prognosis based on digital twins.
KW - Dynamic characteristics
KW - Eccentricity error
KW - Load sharing
KW - Mesh stiffness
KW - Planetary gear system
KW - Wear
UR - https://www.scopus.com/pages/publications/105035150526
U2 - 10.1016/j.wear.2026.206685
DO - 10.1016/j.wear.2026.206685
M3 - 文章
AN - SCOPUS:105035150526
SN - 0043-1648
VL - 596
JO - Wear
JF - Wear
M1 - 206685
ER -