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Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration Control

机译:基于传动系启动扭转振动控制的双质量飞轮参数调查

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摘要

This paper is aimed to investigate the influence of dual-mass flywheel (DMF) kinetic parameters on driveline torsional vibration in engine start-up process, which prescribes the design requirements under start-up condition for DMF matching. On the basis of driveline excitation analysis during engine start-up, the analytical model of DMF driveline torsional vibration system is built and simulated. The vehicle start-up test is conducted and compared with the simulation results. On account of the partial nonstationary characteristic of driveline during start-up, the start-up process is separated into 3 phases for discussing the influence of DMF rotary inertia ratio, hysteresis torque, and nonlinear torsional stiffness on attenuation effect. The test and simulation results show that the DMF undergoes severe oscillation when driveline passes through resonance zone, and the research model is verified to be valid. The DMF design requirements under start-up condition are obtained: the appropriate rotary inertia ratio (the 1st flywheel rotary inertia-to-the 2nd flywheel rotary inertia ratio) is 0.7∼1.1; the interval of DMF small torsion angle should be designed as being with small damping, while large damping is demanded in the interval of large torsion angle; DMF should be equipped with low torsional stiffness when working in start-up process.
机译:本文旨在探讨双质量飞轮(DMF)动力学参数对发动机启动过程中动脉扭转振动的影响,规定了DMF匹配的启动条件下的设计要求。在发动机启动期间的传动系励磁分析的基础上,建立和模拟了DMF传动系扭转振动系统的分析模型。与仿真结果进行比较并将车辆启动测试进行比较。由于启动期间驱动线的部分非间断特征,启动过程分离为3个阶段,以讨论DMF旋转惯性比,滞后扭矩和非线性扭转刚度对衰减效果的影响。测试和仿真结果表明,当传动系统通过共振区时,DMF经历严重振荡,并验证研究模型有效。获得了启动条件下的DMF设计要求:适当的旋转惯性比(第一飞轮旋转惯性至第二飞轮旋转惯量比)为0.7~1.1; DMF小扭转角度的间隔应设计为小阻尼,而大量扭转角度要求大阻尼;在启动过程中工作时,DMF应配备低扭转刚度。

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