There exists a need to have a reliable comprehensive software/hardware to monitor the condition of airframe structures and aircraft components. Failure of any structural parts of aircraft are often prohibitively costly and could even lead to loss of life. The existing technologies deal with the use of some of the characteristics of structural vibration and thus resulting in false detections. The use of complete vibration signature measured by an array of embedded (or attached) fiber-optic sensors, which are loaded with multiple laser beams generated by a single optical source, is the focus of this project. The hardware will be light weight, low cost, and effective for monitoring discontinuities, damage, and delamination in both composite and metal airframes.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Smart aircraft by continuous condition monitoring of aircraft structures and components


    Beteiligte:

    Kongress:

    Second European Conference on Smart Structures and Materials ; 1994 ; Glasgow,United Kingdom


    Erschienen in:

    Erscheinungsdatum :

    13.09.1994





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Smart Monitoring System for Aircraft Structures

    Foucher, Bruno / Rouet, Vincent | SAE Technical Papers | 2011


    Smart Aircraft Structures

    Crowe, C. R. / Sater, J. M. / Advisory Group for Aerospace Research and Development | British Library Conference Proceedings | 1997


    AIRCRAFT CONDITION MONITORING SYSTEM

    HAUKOM MICHAEL JAMES | Europäisches Patentamt | 2023

    Freier Zugriff


    Smart Patches for Monitoring Crack Growth in Aircraft Structures

    Ihn, Jeong-Beom / Chang, Fu-Kuo | AIAA | 2002