Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction

E. Keller, Asok Ray

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    5 Citations (Scopus)

    Abstract

    The real-time non-destructive evaluation (NDE) of fatigue crack damage was analyzed using ultrasonic sensing. The NDE system demonstrated a approach to on-line estimation of crack damage model parameter. The ultrasonic flaw detectors were used in the aerospace and nuclear power industries to detect flaws in structures. The damage sensing system was found to be suitable for health monitoring and residual life prediction in aging and aircraft structures.

    Original languageEnglish (US)
    Title of host publicationAIAA/IEEE Digital Avionics Systems Conference - Proceedings
    Volume1
    StatePublished - 2001
    Event20th Digital Avionics Systems Conference Proceedings - Daytona Beach, FL, United States
    Duration: Oct 14 2001Oct 18 2001

    Other

    Other20th Digital Avionics Systems Conference Proceedings
    CountryUnited States
    CityDaytona Beach, FL
    Period10/14/0110/18/01

    Fingerprint

    Airframes
    Ultrasonics
    Health
    Defects
    Monitoring
    Nuclear energy
    Aging of materials
    Aircraft
    Cracks
    Detectors
    Industry
    Fatigue cracks

    All Science Journal Classification (ASJC) codes

    • Aerospace Engineering
    • Electrical and Electronic Engineering

    Cite this

    Keller, E., & Ray, A. (2001). Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction. In AIAA/IEEE Digital Avionics Systems Conference - Proceedings (Vol. 1)
    Keller, E. ; Ray, Asok. / Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction. AIAA/IEEE Digital Avionics Systems Conference - Proceedings. Vol. 1 2001.
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    abstract = "The real-time non-destructive evaluation (NDE) of fatigue crack damage was analyzed using ultrasonic sensing. The NDE system demonstrated a approach to on-line estimation of crack damage model parameter. The ultrasonic flaw detectors were used in the aerospace and nuclear power industries to detect flaws in structures. The damage sensing system was found to be suitable for health monitoring and residual life prediction in aging and aircraft structures.",
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    Keller, E & Ray, A 2001, Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction. in AIAA/IEEE Digital Avionics Systems Conference - Proceedings. vol. 1, 20th Digital Avionics Systems Conference Proceedings, Daytona Beach, FL, United States, 10/14/01.

    Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction. / Keller, E.; Ray, Asok.

    AIAA/IEEE Digital Avionics Systems Conference - Proceedings. Vol. 1 2001.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

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    AU - Ray, Asok

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    N2 - The real-time non-destructive evaluation (NDE) of fatigue crack damage was analyzed using ultrasonic sensing. The NDE system demonstrated a approach to on-line estimation of crack damage model parameter. The ultrasonic flaw detectors were used in the aerospace and nuclear power industries to detect flaws in structures. The damage sensing system was found to be suitable for health monitoring and residual life prediction in aging and aircraft structures.

    AB - The real-time non-destructive evaluation (NDE) of fatigue crack damage was analyzed using ultrasonic sensing. The NDE system demonstrated a approach to on-line estimation of crack damage model parameter. The ultrasonic flaw detectors were used in the aerospace and nuclear power industries to detect flaws in structures. The damage sensing system was found to be suitable for health monitoring and residual life prediction in aging and aircraft structures.

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    BT - AIAA/IEEE Digital Avionics Systems Conference - Proceedings

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    Keller E, Ray A. Real-time nondestructive evaluation of airframe structures for health monitoring and residual life prediction. In AIAA/IEEE Digital Avionics Systems Conference - Proceedings. Vol. 1. 2001