Three-Axis Vibration Isolation of a Full-Scale Magnetorheological Seat Suspension

被引:1
|
作者
Choi, Young T. [1 ]
Wereley, Norman M. [1 ]
Hiemenz, Gregory J. [2 ]
机构
[1] Univ Maryland, Dept Aerosp Engn, College Pk, MD 20742 USA
[2] Innovital Syst Inc, Calverton, MD 20705 USA
关键词
three-axis vibration isolation; aircraft vibration; seat suspension; magnetorheological; DAMPER; PERFORMANCE;
D O I
10.3390/mi15121417
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
This study examines the three-axis vibration isolation capabilities of a full-scale magnetorheological (MR) seat suspension system utilizing experimental methods to assess performance under both single-axis and simultaneous three-axis input conditions. To achieve this, a semi-active MR seat damper was designed and manufactured to address excitations in all three axes. The damper effectiveness was tested experimentally for axial and lateral motions, focusing on dynamic stiffness and loss factor using an MTS machine. Prior to creating the full-scale MR seat suspension, a scaled-down version at one-third size was developed to verify the damper's ability to effectively reduce vibrations in response to practical excitation levels. Additionally, a narrow-band frequency-shaped semi-active control (NFSSC) algorithm was developed to optimize vibration suppression. Ultimately, a full-scale MR seat suspension was assembled and tested with a 50th percentile male dummy, and comprehensive three-axis vibration isolation tests were conducted on a hydraulic multi-axis simulation table (MAST) for both individual inputs over a frequency range up to 200 Hz and for simultaneous multi-directional inputs. The experimental results demonstrated the effectiveness of the full-scale MR seat suspension in reducing seat vibrations.
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页数:17
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