0 INTRODUCTION The Andean orogenic belt,a globally significant active continental margin(Lamb et al.,1997),extends in a north-south direction along the western coast of South America.The Colombian Andes,located in the...0 INTRODUCTION The Andean orogenic belt,a globally significant active continental margin(Lamb et al.,1997),extends in a north-south direction along the western coast of South America.The Colombian Andes,located in the northern segment of this orogen,constitute a vital component and host abundant Au-Cu resources.Three principal Au-Cu metallogenic belts(Chocó,Middle Cauca,and Antioquia)are developed from west to east across Colombia(Lesage et al.,2013;Sillitoe,2008;Figure 1a).展开更多
The active Lamb wave and piezoelectric transducer(PZT)-based structural health monitoring(SHM)technology is a kind of efficient approach to estimate the health state of aircraft structure.In practical applications,PZT...The active Lamb wave and piezoelectric transducer(PZT)-based structural health monitoring(SHM)technology is a kind of efficient approach to estimate the health state of aircraft structure.In practical applications,PZT networks are needed to monitor large scale structures.Scanning many of the different PZT actuator-sensor channels within these PZT networks to achieve on-line SHM task is important.Based on a peripheral component interconnect extensions for instrumentation(PXI)platform,an active Lamb wave and PZT network-based integrated multi-channel scanning system(PXI-ISS)is developed for the purpose of practical applications of SHM,which is compact and portable,and can scan large numbers of actuator-sensor channels and perform damage assessing automatically.A PXI-based 4 channels gain-programmable charge amplifier,an external scanning module with 276 actuator-sensor channels and integrated SHM software are proposed and discussed in detail.The experimental research on a carbon fiber composite wing box of an unmanned aerial vehicle(UAV)for verifying the functions of the PXI-ISS is mainly discussed,including the design of PZTs layer,the method of excitation frequency selection,functional test of damage imaging,stability test of the PXI-ISS,and the loading effect on signals.The experimental results have verified the stability and damage functions of this system.展开更多
基金supported by the National Natural Science Foundation of China(No.42572076)the Continental Gold Ltd.,Colombian Branch(No.CG-EXP-041-23).
文摘0 INTRODUCTION The Andean orogenic belt,a globally significant active continental margin(Lamb et al.,1997),extends in a north-south direction along the western coast of South America.The Colombian Andes,located in the northern segment of this orogen,constitute a vital component and host abundant Au-Cu resources.Three principal Au-Cu metallogenic belts(Chocó,Middle Cauca,and Antioquia)are developed from west to east across Colombia(Lesage et al.,2013;Sillitoe,2008;Figure 1a).
基金National High-tech Research and Development Program of China(2007AA03Z117)National Natural Science Foundation of China(50830201)Graduate Education Innovation Project of Nanjing University of Aeronautics and Astronautics of China(BCXJ09-01).
文摘The active Lamb wave and piezoelectric transducer(PZT)-based structural health monitoring(SHM)technology is a kind of efficient approach to estimate the health state of aircraft structure.In practical applications,PZT networks are needed to monitor large scale structures.Scanning many of the different PZT actuator-sensor channels within these PZT networks to achieve on-line SHM task is important.Based on a peripheral component interconnect extensions for instrumentation(PXI)platform,an active Lamb wave and PZT network-based integrated multi-channel scanning system(PXI-ISS)is developed for the purpose of practical applications of SHM,which is compact and portable,and can scan large numbers of actuator-sensor channels and perform damage assessing automatically.A PXI-based 4 channels gain-programmable charge amplifier,an external scanning module with 276 actuator-sensor channels and integrated SHM software are proposed and discussed in detail.The experimental research on a carbon fiber composite wing box of an unmanned aerial vehicle(UAV)for verifying the functions of the PXI-ISS is mainly discussed,including the design of PZTs layer,the method of excitation frequency selection,functional test of damage imaging,stability test of the PXI-ISS,and the loading effect on signals.The experimental results have verified the stability and damage functions of this system.
