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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2018, Vol. 39 ›› Issue (6): 221721-221721.doi: 10.7527/S1000-6893.2018.21721

• Solid Mechanics and Vehicle Conceptual Design • Previous Articles     Next Articles

Design and parameter optimization of a new tunable dynamic vibration absorber

LI Qiang, DONG Guangxu, ZHANG Xinong, LUO Yajun, ZHANG Yahong, XIE Shilin   

  1. State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace, Xi'an Jiaotong University, Xi'an 710049, China
  • Received:2017-09-06 Revised:2018-03-20 Online:2018-06-15 Published:2018-03-19

Abstract: To effectively suppress the low-frequency or ultra-low-frequency vibration induced by the disturbances in aerospace equipment, a New tunable Dynamic Vibration Absorber (NDVA) with tuning stiffness is proposed in this paper. The implementation of the NDVA is mainly carried out by connecting a Spiral Flexure Spring (SFS) and a Magnetic Negative Stiffness Spring (MNSS). As the proposed NDVA is applied to suppression of resonance, the steady-state frequency response equations and the stability criterion under harmonic force are derived with the averaging method. Based on stability analysis, a new optimization method is offered to attain the optimal parameters with simple iteration. Robustness of the NDVA is analyzed. The results show that besides attenuating vibration in a large low-frequency range, the proposed NDVA can achieve better vibration reduction effect than the linear absorber due to its advantage of robustness in practical application.

Key words: dynamic absorber, negative stiffness, nonlinearity, saddle-node bifurcation, robustness

CLC Number: