Impact Force Reconstruction for Structural Health Monitoring of Composite Beam

Reconstruction of the impact force history and identification of the impact location are important tasks in structural health monitoring (SHM) applications, namely in case of composite structures. These tasks are critical especially in cases, when it is not possible to measure the impact force directly and the knowledge of the intensity and position of loading force is necessary for the damage prediction of the structure. This paper tests two methods for the reconstruction of impact force and identification of impact location. The first method uses finite element analysis (FEA) for determination of a transfer matrix of a system. The second method uses experimental results only. The methods are tested on an orthotropic prismatic wide beam with rectangular cross-section. Three piezoelectric patch transducers are bonded to the beam bottom-surface to measure deformations.

[1]  J. F. Doyle,et al.  Impact force identification from wave propagation responses , 1996 .

[2]  J. F. Doyle A wavelet deconvolution method for impact force identification , 1997 .

[3]  Robert E. Seydel Impact identification of stiffened composite panels , 2000 .

[4]  F. Chang,et al.  Impact identification of stiffened composite panels: II. Implementation studies , 2001 .

[5]  Fu-Kuo Chang,et al.  Impact identification of stiffened composite panels: I. System development , 2001 .

[6]  E. Jacquelin,et al.  Force reconstruction: analysis and regularization of a deconvolution problem , 2003 .

[7]  Jonghyun Park,et al.  System identification method for monitoring impact events , 2005, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.

[8]  F. Gunawan,et al.  Two-step B-splines regularization method for solving an ill-posed problem of impact-force reconstruction , 2006 .

[9]  Hisao Fukunaga,et al.  An efficient approach for identifying impact force using embedded piezoelectric sensors , 2007 .

[10]  Keith Worden,et al.  Impact detection in an aircraft composite panel—A neural-network approach , 2007 .

[11]  Boming Zhang,et al.  A load reconstruction model for advanced grid-stiffened composite plates , 2008 .

[12]  T. Kundu,et al.  Locating point of impact in anisotropic fiber reinforced composite plates. , 2008, Ultrasonics.

[13]  Vladislav Laš,et al.  Progressive Damage of Unidirectional Composite Panels , 2008 .

[14]  Ning Hu,et al.  Identification of Impact Force on Stiffened Composite Panels , 2009 .

[15]  Li Zhou,et al.  Impact load identification of composite structure using genetic algorithms , 2009 .

[16]  Satoshi Atobe,et al.  Identification of locations and force histories of multiple point impacts on composite isogrid-stiffened panels , 2009 .

[17]  Tomáš Kroupa,et al.  Influence of principal material directions of thin orthotropic structures on Rayleigh-edge wave velocity , 2010 .

[18]  Tomáš Kroupa,et al.  Improved nonlinear stress-strain relation for carbon-epoxy composites and identification of material parameters , 2011 .