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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:
    Escriba, C. (Autor:in) / Fourniols, J. (Autor:in) / Lastapis, M. (Autor:in) / Boizard, J. (Autor:in) / Auriol, G. (Autor:in) / Andrieu, S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.02.2012


    Format / Umfang :

    6903122 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Aircraft control by propeller cyclic blades

    DeYoung, John | TIBKAT | 1979




    Aircraft propeller comprising collapsible variable pitch blades

    HERANGER CHRISTOPHE / PRAMPOLINI MARCO | Europäisches Patentamt | 2020

    Freier Zugriff