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New real-time structural health monitoring microsystem for aircraft propeller blades

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6 Author(s)
Escriba, C. ; LAAS, Univ. de Toulouse, Toulouse, France ; Fourniols, J. ; Lastapis, M. ; Boizard, J.
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This presents work done on the project “Blade Parameters Recording Microsystem” funded by the French research program FUI. It resulted in a fully operational recorder that can be embedded on a plane. This system allows blade monitoring to be conducted using computing algorithms. Using a top-down modelling method, this recorder can be adapted to any kind of blade. Herein, recorder was devised for a Transall plane blade. This device was used to record data in order to subsequently compute a real-time blade monitoring algorithm. The algorithm takes several blade parameters into account. The top-down modelling easily allows the algorithm parameters to be adapted to various blades.

Published in:

Aerospace and Electronic Systems Magazine, IEEE  (Volume:27 ,  Issue: 2 )