1. 中国民航大学 机构 航空工程学院,天津,300300
2. 中国民航航空地面特种设备研究基地,天津,300300
3. 民航智慧机场理论与系统重点实验室,天津,300300
[ "祝恒佳,副教授,博士," ]
[ "张威,教授,博士生导师,博士," ]
纸质出版:2025
移动端阅览
祝恒佳, 沈云, 田思远, 等. 馈能式悬架耦合振动系统相似建模方法[J]. 机械科学与技术, 2025,44(5):768-776.
祝恒佳, 沈云, 田思远, et al. Similarity Modeling Method for Coupling Vibration System with Energy-regenerative Suspension[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(5): 768-776.
祝恒佳, 沈云, 田思远, 等. 馈能式悬架耦合振动系统相似建模方法[J]. 机械科学与技术, 2025,44(5):768-776. DOI: 10.13433/j.cnki.1003-8728.20230225.
祝恒佳, 沈云, 田思远, et al. Similarity Modeling Method for Coupling Vibration System with Energy-regenerative Suspension[J]. Mechanical Science and Technology for Aerospace Engineering, 2025, 44(5): 768-776. DOI: 10.13433/j.cnki.1003-8728.20230225.
馈能式悬架通过将车辆振动能量转换为电能为微功耗装置供电,其电磁耦合作用会影响系统的动力学性能。考虑电磁耦合作用力对馈能式悬架系统动力学特性的影响,推导馈能式悬架1/4车振动系统微分方程。基于相似原理,建立车辆机械振动系统电路模型,通过Maxwell和MATLAB/Simulink建立机械-电磁耦合振动系统的有限元联合仿真模型并进行模型验证。进一步对比研究机械-电磁耦合振动系统与仅考虑车辆机械振动系统在正弦、脉冲和随机路面位移激励工况下车身加速度、悬架动挠度特性。结果表明:该文有限元联合仿真相似模型与数值计算结果基本一致,而机械振动模型与机械-电磁耦合振动模型动态响应结果差异为12.12% ~ 16.67%。
The energy-regenerative suspension can convert the vehicle vibration energy to the electrical energy for the micro-power devices
but the electromagnetic coupling effect maybe affect the vehicle dynamic performances. Considering the influence of electromagnetic coupling on the energy-regenerative suspension's dynamic characteristics
the differential equations of a quarter car vibration system with the energy-regenerative suspension are derived. Based on the similar principle
the circuit model of the vehicle mechanical vibration system is established
and the finite element co-simulation model of the mechanical-electromagnetic coupling vibration system is established by Maxwell and MATLAB/Simulink
and the model verification is carried out. Furthermore
the vehicle body acceleration and suspension dynamic deflection characteristics under harmonic
bump and random road displacement excitations
are simulated and compared respectively with those of the vehicle mechanical vibration system. It shows that the results of the proposed model are basically consistent with those obtained through the numerical method
while the dynamic response differences between the proposed model and the mechanical model without considering the coupling effects are in the range 12.12% - 16.67%.
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