On Health Monitor Technology Development for Damaged Aircraft Structures

Xiao Ming Liu; Yue Tao Ge; Xiao Tong Yin

doi:10.4028/www.scientific.net/AMM.482.90

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 482On Health Monitor Technology Development for...

On Health Monitor Technology Development for Damaged Aircraft Structures

Abstract:

This paper seeks to outline the concept and application of health monitoring system in aircraft structure. The focus is placed on the principles and methods of the structural health monitoring system, including SMART layers, electric potential method, Acoustic Emission, etc. The difference between the above monitoring methods is justified and clarified. Finally a perspective view on structural health monitor techniques is discussed.

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Periodical:

Applied Mechanics and Materials (Volume 482)

Pages:

90-96

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.482.90

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Online since:

December 2013

Authors:

Xiao Ming Liu*, Yue Tao Ge, Xiao Tong Yin

Keywords:

Acoustic Emission (AE), Airworthiness, Antenna Sensors, Electric Potential, SMART Layers, Structural Health Monitoring (SHM)

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* - Corresponding Author

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