Experimental validation of a magnetorheological energy absorber design analysis

被引:42
作者
Mao, Min [1 ]
Hu, Wei [1 ]
Choi, Young T. [1 ]
Wereley, N. M. [1 ]
Browne, Alan L. [2 ]
Ulicny, John [2 ]
机构
[1] Univ Maryland, Dept Aerosp Engn, Smart Struct Lab, College Pk, MD 20742 USA
[2] Gen Motors, Ctr Res & Dev, Warren, MI USA
关键词
Magnetorheological; impact; energy absorber; Bingham plastic; minor losses; drop tests; SEMIACTIVE SUSPENSION SYSTEMS; FLIGHT DROP TOWER; ELECTRORHEOLOGICAL DAMPERS; NONDIMENSIONAL ANALYSIS; MITIGATION; SHOCK;
D O I
10.1177/1045389X13494934
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A key challenge when designing linear stroke magnetorheological energy absorbers for high-speed impact is that high piston speeds in linear stroke magnetorheological energy absorbers induce high Reynolds number flows in the magnetic valve of the magnetorheological energy absorber, so that achieving high controllable dynamic range can be a design challenge. So far, the research on magnetorheological energy absorbers has typically assumed that the off-state force increases linearly with piston velocity. But at the higher piston velocities occurring in impact events, the off-state damping exhibits nonlinear velocity squared damping effects. This problem was recognized in our prior work, where it was shown that minor losses are important contributing factors to off-state damping. In this study, a nonlinear analytical magnetorheological energy absorber model is developed based on a Bingham-plastic nonlinear flow model combined with velocity squared dependent minor loss factors. This refined model is denoted as the Bingham-plastic nonlinear flow model with minor losses. From this Bingham-plastic nonlinear flow model with minor losses, an effective design strategy is presented for conventional magnetorheological energy absorbers. The Bingham-plastic nonlinear flow model with minor losses is validated via computational fluid dynamics simulation, so that magnetorheological energy absorber performance can be analytically verified before being manufactured. The magnetorheological energy absorber is fabricated and tested up to an effective piston velocity of 5 m/s by using the high-speed drop tower facility at the GM R&D Center. Comparison of our analysis with measured data is conducted, and the effective design of the magnetorheological energy absorber using the Bingham-plastic nonlinear flow model with minor losses is validated.
引用
收藏
页码:352 / 363
页数:12
相关论文
共 27 条
[1]   Rheological controllability of double-ended MR dampers subjected to impact loading [J].
Ahmadian, M ;
Norris, JA .
SMART STRUCTURES AND MATERIALS 2004: DAMPING AND ISOLATION, 2004, 5386 :185-194
[2]   Dynamic crush tests using a "Free-Flight" drop tower: Theory [J].
Browne, AL ;
Johnson, NL .
EXPERIMENTAL TECHNIQUES, 2002, 26 (05) :43-46
[3]   Impact Performance of Magnetorheological Fluids [J].
Browne, Alan L. ;
Mccleary, Joseph D. ;
Namuduri, Chandra S. ;
Webb, Scott R. .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2009, 20 (06) :723-728
[4]   Shock isolation systems using magnetorheological dampers [J].
Choi, Young-Tai ;
Wereley, Norman M. .
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 2008, 130 (02)
[5]  
Dixon J.C., 1999, The Shock Absorber Handbook
[6]   A new magneto-rheological fluid damper for high-mobility multi-purpose wheeled vehicle (HMMWV) [J].
Dogruer, Umit ;
Gordaninejad, Faramarz ;
Evrensel, Cahit A. .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2008, 19 (06) :641-650
[7]   Modeling and control of magnetorheological dampers for seismic response reduction [J].
Dyke, SJ ;
Spencer, BF ;
Sain, MK ;
Carlson, JD .
SMART MATERIALS & STRUCTURES, 1996, 5 (05) :565-575
[8]  
Franzini J.B., 1997, Fluid Mechanics with Engineering Applications
[9]   Electrorheological dampers .1. Analysis and design [J].
Gavin, HP ;
Hanson, RD ;
Filisko, FE .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1996, 63 (03) :669-675
[10]   Semi-active control of vertical stroking helicopter crew seat for enhanced crashworthiness [J].
Hiemenz, Gregory J. ;
Choi, Young-Tai ;
Wereley, Norman M. .
JOURNAL OF AIRCRAFT, 2007, 44 (03) :1031-1034