Fiber optic sensors are being developed for health monitoring of future aircraft. Aircraft health monitoring involves the use of strain, temperature, vibration and chemical sensors. These sensors will measure load and vibration signatures that will be used to infer structural integrity. Since the aircraft morphing program assumes that future aircraft will be aerodynamically reconfigurable there is also a requirement for pressure, flow and shape sensors. In some cases a single fiber may be used for measuring several different parameters.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Fiber optic sensors for health monitoring of morphing aircraft



    Conference:

    Smart Structures and Materials 1999: Industrial and Commercial Applications of Smart Structures Technologies ; 1999 ; Newport Beach,CA,USA


    Published in:

    Publication date :

    1999-07-09





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Fiber Optic Sensors in Structural Health Monitoring

    Lopez-Higuera, J.M. / Rodriguez, L. / Quintela, A. et al. | British Library Online Contents | 2011



    Aircraft health monitoring using optical fiber sensors

    Borinski, J.W. / Meller, S.A. / Pulliam, W.J. et al. | IEEE | 2000


    Application of Fiber-Optic Sensors for the Aircraft Structure Monitoring

    Zakirov, Ruslan / Giyasova, Feruza | Springer Verlag | 2021