The quasi-zero-stiffness (QZS) vibration isolators are effective in achieving low-frequency vibration isolation for a designedpayload, but the isolation effect would be substantially reduced by payload mismatch. To ta...The quasi-zero-stiffness (QZS) vibration isolators are effective in achieving low-frequency vibration isolation for a designedpayload, but the isolation effect would be substantially reduced by payload mismatch. To tackle such a challenging problem, acompensating QZS (CQZS) vibration isolation system (VIS) is proposed to acquire QZS characteristics under arbitrarypayloads. The dynamic characteristics of the CQZS VIS are analyzed to estimate the performance decline of vibration isolationunder payload mismatch. Moreover, the compensation principle of the CQZS VIS is demonstrated, and then the CQZS VIS isfabricated by combining a passive QZS isolator and a compensation system. Finally, experiments are conducted to evaluate thecompensation capability and vibration isolation performance enhance of the CQZS VIS. It is found that the CQZS VIS is ableto compensate payload mismatch, and thus the QZS characteristic can be regained when the payload deviates from thedesigned one, which enabls the QZS VIS to achieve significant low-frequency vibration isolation under payload mismatch.展开更多
基金supported by the National Natural Science Foundation of China(Grant Nos.12302003,12272129,and 12122206)Hong Kong Scholars Program(Grant No.XJ2022012).
文摘The quasi-zero-stiffness (QZS) vibration isolators are effective in achieving low-frequency vibration isolation for a designedpayload, but the isolation effect would be substantially reduced by payload mismatch. To tackle such a challenging problem, acompensating QZS (CQZS) vibration isolation system (VIS) is proposed to acquire QZS characteristics under arbitrarypayloads. The dynamic characteristics of the CQZS VIS are analyzed to estimate the performance decline of vibration isolationunder payload mismatch. Moreover, the compensation principle of the CQZS VIS is demonstrated, and then the CQZS VIS isfabricated by combining a passive QZS isolator and a compensation system. Finally, experiments are conducted to evaluate thecompensation capability and vibration isolation performance enhance of the CQZS VIS. It is found that the CQZS VIS is ableto compensate payload mismatch, and thus the QZS characteristic can be regained when the payload deviates from thedesigned one, which enabls the QZS VIS to achieve significant low-frequency vibration isolation under payload mismatch.
