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

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...

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Main Authors: Liupeng He, Changgao Xia, Sida Chen, Jiwei Guo, Yi Liu
Format: Article
Language:English
Published: Wiley 2019-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2019/3171698
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author Liupeng He
Changgao Xia
Sida Chen
Jiwei Guo
Yi Liu
author_facet Liupeng He
Changgao Xia
Sida Chen
Jiwei Guo
Yi Liu
author_sort Liupeng He
collection DOAJ
description 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.
format Article
id doaj-art-bb9ee7a5829745429c9548fd4a117331
institution Kabale University
issn 1070-9622
1875-9203
language English
publishDate 2019-01-01
publisher Wiley
record_format Article
series Shock and Vibration
spelling doaj-art-bb9ee7a5829745429c9548fd4a1173312025-02-03T01:32:42ZengWileyShock and Vibration1070-96221875-92032019-01-01201910.1155/2019/31716983171698Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration ControlLiupeng He0Changgao Xia1Sida Chen2Jiwei Guo3Yi Liu4School of Automotive and Traffic Engineering, Jiangsu University, Zhenjiang 212013, ChinaSchool of Automotive and Traffic Engineering, Jiangsu University, Zhenjiang 212013, ChinaSchool of Automotive and Traffic Engineering, Jiangsu University, Zhenjiang 212013, ChinaShanghai Sachs Powertrain Components Systems Co. Ltd., Shanghai 201799, ChinaShanghai Sachs Powertrain Components Systems Co. Ltd., Shanghai 201799, ChinaThis 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.http://dx.doi.org/10.1155/2019/3171698
spellingShingle Liupeng He
Changgao Xia
Sida Chen
Jiwei Guo
Yi Liu
Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration Control
Shock and Vibration
title Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration Control
title_full Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration Control
title_fullStr Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration Control
title_full_unstemmed Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration Control
title_short Parametric Investigation of Dual-Mass Flywheel Based on Driveline Start-Up Torsional Vibration Control
title_sort parametric investigation of dual mass flywheel based on driveline start up torsional vibration control
url http://dx.doi.org/10.1155/2019/3171698
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AT changgaoxia parametricinvestigationofdualmassflywheelbasedondrivelinestartuptorsionalvibrationcontrol
AT sidachen parametricinvestigationofdualmassflywheelbasedondrivelinestartuptorsionalvibrationcontrol
AT jiweiguo parametricinvestigationofdualmassflywheelbasedondrivelinestartuptorsionalvibrationcontrol
AT yiliu parametricinvestigationofdualmassflywheelbasedondrivelinestartuptorsionalvibrationcontrol