Damage detection by piezoelectric patches in a free vibration method

被引:33
作者
Jian, XH
Tzou, HS
Lissenden, CJ
Penn, LS
机构
[1] UNIV KENTUCKY,CTR ROBOT & MFG SYST,DEPT CHEM & MAT ENGN,LEXINGTON,KY 40506
[2] UNIV KENTUCKY,CTR ROBOT & MFG SYST,DEPT ENGN MECH,LEXINGTON,KY 40506
[3] UNIV KENTUCKY,CTR ROBOT & MFG SYST,DEPT MECH ENGN,LEXINGTON,KY 40506
关键词
piezoelectric patch; damage detection; composite plates; natural vibrational frequency; frequency response; delamination; vibrational modes;
D O I
10.1177/002199839703100402
中图分类号
TB33 [复合材料];
学科分类号
摘要
An experimental program was undertaken to evaluate the feasibility of using piezoelectric patches for damage detection in composite materials. The fact that damage development can cause shifts in the natural frequencies of a structural component suggested an impulse-frequency response approach, in which free vibration was initiated by a single external mechanical pulse and was sensed by piezoelectric patches. Patches in both surface-bonded and embedded configurations were tried. The investigation was conducted on unidirectional glass fiber/epoxy laminated plates containing controlled levels of damage, present as interply delaminations. The data obtained from the piezoelectric patches showed the expected decrease in frequency of the natural vibrational modes with increase in damage. The attractiveness of this method lies in its convenience and its potential for use in the field.
引用
收藏
页码:345 / 359
页数:15
相关论文
共 26 条
[1]   BENDING AND SHEAR DAMPING IN BEAMS - FREQUENCY-DOMAIN ESTIMATION TECHNIQUES [J].
BANKS, HT ;
WANG, Y ;
INMAN, DJ .
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 1994, 116 (02) :188-197
[2]  
Blevins R.D., 1979, Formulas for natural frequency and mode shape
[3]  
CAIRNS DS, 1990, ASTM STP, V1059, P48
[4]   STRENGTH LOSS IN COMPOSITE CYLINDERS UNDER IMPACT [J].
CHRISTOFOROU, AP ;
SWANSON, SR .
JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 1988, 110 (02) :180-184
[5]  
CLEMENTS LL, 1978, UCID17874 LAWR LIV N
[6]  
GRADY JE, 1989, P AIAA ASME ASCE AHS, P2186
[7]   CORRELATION OF RESIDUAL STRENGTH WITH ACOUSTIC-EMISSION FROM IMPACT-DAMAGED COMPOSITE STRUCTURES UNDER CONSTANT BIAXIAL LOAD [J].
HAMSTAD, MA ;
WHITTAKER, JW ;
BROSEY, WD .
JOURNAL OF COMPOSITE MATERIALS, 1992, 26 (15) :2307-2328
[8]   PLY CRACKING AND PROPERTY DEGRADATIONS OF SYMMETRIC BALANCED LAMINATES UNDER GENERAL INPLANE LOADING [J].
HAN, YM ;
HAHN, HT .
COMPOSITES SCIENCE AND TECHNOLOGY, 1989, 35 (04) :377-397
[9]  
HWANG SJ, 1994, NCA18DE80, P113
[10]  
LAGACE PA, 1987, P 32 INT SAMPE S EXH, V32, P720