Optimization design of spiral bevel gear's dynamic characteristics based on genetic algorithm
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Optimization design of spiral bevel gear's dynamic characteristics based on genetic algorithm
Vol. 25, Issue 10, (2010)
作者机构:
西北工业大学 机电学院,西安,710072
作者简介:
基金信息:
DOI:
CLC:
Published:2010
稿件说明:
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ZHAO Ning, KANG Shi-peng, GUO Hui, et al. Optimization design of spiral bevel gear's dynamic characteristics based on genetic algorithm[J]. 2010, 25(10).
DOI:
ZHAO Ning, KANG Shi-peng, GUO Hui, et al. Optimization design of spiral bevel gear's dynamic characteristics based on genetic algorithm[J]. 2010, 25(10).DOI:
Optimization design of spiral bevel gear's dynamic characteristics based on genetic algorithm
The three-dimensional eight-degree non-linear dynamical model of the spiral bevel gear was established based on the lumped mass method.Time-varying mesh stiffness
non-linear geometric transmission error
gear clearance and non-linear bearing stiffness were considered in this model.The dynamic response for the transmission system was solved by using Runge-Kutta method.Then
by taking meshing cycle root mean square vibration acceleration as an optimizing object
GA(genetic algorithm) was used to optimize these two local control parameters in the local synthesis
meanwhile optimized machining parameters of the gear pair were also obtained.By the way of tooth surface modification
the purpose of reducing gear's vibration and noise was realized.
Synthetical optimization design of rotor airfoil by genetic algorithm
Optimization design of shroud configuration of transporter based on surrogate model
Aerodynamic optimization method for duct design
Thermeset coupling analysis and optimization design of turbine cooling blade
Identification of flexible nozzle torque properties based on wavelet neural network optimized by genetic algorithm
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ZHAO Qi-jun
MA Yang
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YANG Tao
FENG Zhi-wei
ZHANG Qing-bin
YE Kun
Related Institution
National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics
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