Paper
20 July 1999 Microsensors and MEMS for health monitoring of composite and aircraft structures in flight
Author Affiliations +
Abstract
Microsensors and Microelectromechanical Systems (MEMS) are currently being applied to the structural health monitoring of critical aircraft components. The approach integrates acoustic emission, strain gauges, MEMS accelerometers and vibration monitoring devices with signal processing electronics to provide real-time indicators of incipient failure of aircraft components with a known history of catastrophic failure due to fracture.
© (1999) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Vijay K. Varadan and Vasundara V. Varadan "Microsensors and MEMS for health monitoring of composite and aircraft structures in flight", Proc. SPIE 3673, Smart Structures and Materials 1999: Smart Electronics and MEMS, (20 July 1999); https://doi.org/10.1117/12.354290
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CITATIONS
Cited by 7 scholarly publications.
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KEYWORDS
Sensors

Microelectromechanical systems

Microsensors

Nondestructive evaluation

Electronics

Aircraft structures

Composites

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