An innovative determination approach to tooth compliance for spiral bevel and hypoid gears by using double-curved shell model and Rayleigh-Ritz approach

被引:43
作者
Ding, Han [1 ,2 ]
Tang, Jinyuan [1 ,2 ]
Shao, Wen [1 ]
Peng, Shandong [1 ,2 ]
机构
[1] Cent S Univ, State Key Lab High Performance Complex Mfg, Changsha 410083, Hunan, Peoples R China
[2] Cent S Univ, Sch Mech & Elect Engn, Changsha 410083, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
Spiral bevel and hypoid gears; Tooth compliance; Double-curve shell model; Rayleigh-Ritz approach; Loaded tooth contact analysis (LTCA); MACHINE SETTINGS; STRESS-ANALYSIS; CONTACT PERFORMANCE; NATURAL FREQUENCIES; VIBRATION ANALYSIS; LOAD DISTRIBUTION; GEOMETRIC ERRORS; FGM SHELLS; IDENTIFICATION; DESIGN;
D O I
10.1016/j.mechmachtheory.2018.08.009
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In high-performance sophisticated flank design for the spiral bevel and hypoid gears, tooth compliance is always an important input for identifying the tooth mechanical properties. Distinguished with the conventional modeling, a new accurate finite element structure model is established to determine tooth compliance by using elasticity-based deformation solution. In full consideration of the flank flexural behavior characteristic, a double-curved shell model with varying thickness is established to get a more accurate representation of geometric shape for face-milling or face-hobbing gear than a beam or plate model. In determination of tooth compliance, the high order shear theory of Bhimaraddi shell is used to set the displacement assumption, and the Rayleigh-Ritz approach having algebraic polynomial trail functions is performed to obtain an expression for the transverse deflection and shear rotation by considering the geometric boundary conditions. A given numerical result for the face-milling spiral bevel and hypoid gear is provided to verify the proposed methodology by comparing with the loaded tooth contact analysis (LTCA) using well-known finite element method (FEM). (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:27 / 46
页数:20
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