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| Design of Simulated Loading Test System for Aircraft Structure Health Monitoring |
| Received:July 29, 2012 Revised:December 15, 2012 |
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| DOI： |
| KeyWord:aircraft structure health monitoring simulating loading experiment system |
| Author | Institution |
| WEI Dong |
The First Air Force College of Technology，Xinyang ，China |
| HUANG Jing |
The First Air Force College of Technology，Xinyang ，China |
| HAN Fei |
The First Air Force College of Technology，Xinyang ，China |
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| Abstract: |
| The simulated loading test system for aircraft structure health monitoring was designed. The system consists of loading terrace system, large strain testing accuracy verification module, and key part simulated test module. The system can be used in studying influence of laying method of sensor on test accuracy. The purpose was to provide technique basis, theory and technique for application of fiber-optical sensor techniques in aircraft structure health monitoring. |
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