Monitoring the health of engine components in-situ and in real-time is critical for reducing life cycle costs of military aircraft, such as F-35. As aircraft complexity and performance requirements increase, inspection-based maintenance at pre-defined intervals becomes costly and insufficient. A more efficient approach is to integrate sensor systems, capable of withstanding harsh operating environments, to provide real-time diagnostics and support condition-based maintenance and failure prognostics.


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    Title :

    High temperature telemetry systems for in situ monitoring of gas turbine engine components


    Contributors:


    Publication date :

    2009-03-01


    Size :

    1735346 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English