TY - JOUR
T1 - Identification of bolted joints through laser vibrometry
AU - Ma, X.
AU - Bergman, L.
AU - Vakakis, A.
PY - 2001/9/20
Y1 - 2001/9/20
N2 - We present a new technique for identifying the dynamics of bolted joints. The technique relies on the comparison of the overall dynamics of the bolted structure to that of a similar but unbolted one. The difference in the dynamics of the two systems can be attributed solely to the joint; modelling this difference in the dynamics enables us to construct a non-parametric model for the joint dynamics. Non-contacting, laser vibrometry is utilized to experimentally measure the structural responses with increased accuracy and to perform scans of the structural modes at fixed frequency. A numerical algorithm is then developed to post-process the experimental data and identify the joint force. Theoretical calculations are first used to validate the technique, which is then utilized to identify a practical joint. Experimental force-displacement plots at the joint reveal clear hysteresis loops which, in turn, can be used to estimate the damping dissipation at the joint. Moreover, experimental frequency responses and scans of the mode shapes of the bolted structure reveal non-proportional damping and non-linear effects due to microimpacts of the connected beams at the bolted joint.
AB - We present a new technique for identifying the dynamics of bolted joints. The technique relies on the comparison of the overall dynamics of the bolted structure to that of a similar but unbolted one. The difference in the dynamics of the two systems can be attributed solely to the joint; modelling this difference in the dynamics enables us to construct a non-parametric model for the joint dynamics. Non-contacting, laser vibrometry is utilized to experimentally measure the structural responses with increased accuracy and to perform scans of the structural modes at fixed frequency. A numerical algorithm is then developed to post-process the experimental data and identify the joint force. Theoretical calculations are first used to validate the technique, which is then utilized to identify a practical joint. Experimental force-displacement plots at the joint reveal clear hysteresis loops which, in turn, can be used to estimate the damping dissipation at the joint. Moreover, experimental frequency responses and scans of the mode shapes of the bolted structure reveal non-proportional damping and non-linear effects due to microimpacts of the connected beams at the bolted joint.
UR - http://www.scopus.com/inward/record.url?scp=0035921919&partnerID=8YFLogxK
UR - https://www.sciencedirect.com/science/article/abs/pii/S0022460X01935734?via%3Dihub
U2 - 10.1006/jsvi.2001.3573
DO - 10.1006/jsvi.2001.3573
M3 - Article
AN - SCOPUS:0035921919
SN - 0022-460X
VL - 246
SP - 441
EP - 460
JO - Journal of Sound and Vibration
JF - Journal of Sound and Vibration
IS - 3
ER -