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.


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    Title :

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


    Contributors:
    Escriba, C. (author) / Fourniols, J. (author) / Lastapis, M. (author) / Boizard, J. (author) / Auriol, G. (author) / Andrieu, S. (author)


    Publication date :

    2012-02-01


    Size :

    6903122 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English