A New Technology of Aircraft Structural Health Monitoring

Xiao Hua Lu; Hong Fu Zuo

doi:10.4028/www.scientific.net/AMR.764.71

Paper Titles

Microstructure and Properties of Laser Cladding Co-Based Alloy Layer
p.47

Study on Friction and Wear of Several Metal Materials under Oil Lubrication
p.55

The Evaluation of Tool Wears in Machining of SiCp/Al Composites
p.61

Tribological Properties of Ceramics Tool Materials in Contact with Wood-Based Materials
p.65

A New Technology of Aircraft Structural Health Monitoring
p.71

Crowned Profile Design of Roller Bearings Used in Rolling Mill Based on Three Dimension FEA
p.75

Preliminary Study on the Effect of Mass-Induced Damping on Machining Delicate Workpiece Geometry
p.83

Research and Development on the Query Systems of NC Machining Process
p.91

Research on the Process of Numerical Control Electrochemical Turning Based on Finite Element Method
p.95

HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 764A New Technology of Aircraft Structural Health...

A New Technology of Aircraft Structural Health Monitoring

Abstract:

A new technique of aircraft structural health monitoring so-called Comparative Vacuum Monitoring (CVM) is introduced in this paper. Compared with the traditional and some novel Non-Destructive Testing (NDT) techniques, it is capable of real-time crack initiation and growth detection reliably and accurately, and especially suitable to monitor the interior locations with hard accessibility. With the advantages of this technique, the aircraft manufacturers (such as Boeing, Airbus, Bombardier, Embraer, ect.) are much interested in applying it into aircraft structural health monitoring and have carried out verification tests on aircrafts or technology ready for the future usage. Through the use of CVM technique, it is possible to quickly, routinely and remotely monitor the integrity of a structure in service.

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Periodical:

Advanced Materials Research (Volume 764)

Pages:

71-74

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.764.71

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Online since:

September 2013

Authors:

Xiao Hua Lu, Hong Fu Zuo

Keywords:

Aircraft, CVM Technique, Structural Health Monitoring (SHM)

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