2009
DOI: 10.1016/j.sna.2009.02.032
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On development of a multi-channel PZT array scanning system and its evaluating application on UAV wing box

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Cited by 109 publications
(74 citation statements)
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“…The material test system MTS810 was used for applying the fatigue load. The multi-channel PZT array scanning system developed by the authors’ group [33] was employed to perform the active Lamb wave based monitoring. A 5-cycle tone-burst signal with the center frequency of 290 kHz and ±10 V amplitude was used as the excitation signal, which is expressed in Equation (38).…”
Section: Experimental Evaluation On Hole-edge Crack Specimensmentioning
confidence: 99%
“…The material test system MTS810 was used for applying the fatigue load. The multi-channel PZT array scanning system developed by the authors’ group [33] was employed to perform the active Lamb wave based monitoring. A 5-cycle tone-burst signal with the center frequency of 290 kHz and ±10 V amplitude was used as the excitation signal, which is expressed in Equation (38).…”
Section: Experimental Evaluation On Hole-edge Crack Specimensmentioning
confidence: 99%
“…The experimental object was a 2 mm thick epoxy glass fiberboard. The signal acquisition equipment was the integrated structure of health monitoring scanning system SHM4.0 developed by the National Key Laboratory of Mechanical Structural Mechanics and Control in Nanjing University of Aeronautics and Astronautics, and the sensors were ceramic piezoelectric (PZT) components [17]. During the experiment, the lead break was adopted as the stimulation force; for surface lead break, the direction of stimulating force was perpendicular to the surface of plate, while for end surface lead break, the direction of stimulating force was parallel to the surface of plate.…”
Section: The Verification Of Lamb Wave Mode Stimulated By the Internamentioning
confidence: 99%
“…28 This system is developed to control the excitation and sensing of the PZT sensor array. The dimension of the composite plate is 610 mm 3 600 mm 3 2.16 mm.…”
Section: Evaluation On a Uniform Composite Plate Structurementioning
confidence: 99%