Wireless sensor networks for aerospace applications- thermal monitoring for a gas turbine engine

D. Goldsmith, E. Gaura, J. Brusey, J. Shuttleworth, R. Hazelden, M. Langley

    Research output: Contribution to conferencePaper

    8 Citations (Scopus)
    25 Downloads (Pure)

    Abstract

    The paper here reports on the development of a prototype wireless sensor network for thermal monitoring of aircraft gas turbine engines. The prototype acts as a concept demonstrator for the application at hand. Building upon the state of the art in the domain, the authors pursued a rapid prototyping approach, supported by a base prototyping framework - FieldMAP. As a key property, the framework enables the conceptual shift from data to user relevant information. Consequently, an information extraction and visualisation component is put forward as an addition to traditional “sense and send” WSN systems. The component offers an intuitive approach to user understanding of the global evolution of the observed phenomena. Integrated within the prototype, this component makes use of the processing power available within the WSN coupled with interpolation algorithms borrowed from the geosciences domain. Reconstruction of field representations of the phenomena from the sparse sensed data allows identification of abnormalities and inference of their likely cause.
    Original languageEnglish
    Pages507-512
    Publication statusPublished - 2009

    Fingerprint

    Aerospace applications
    Rapid prototyping
    Gas turbines
    Wireless sensor networks
    Interpolation
    Turbines
    Visualization
    Aircraft
    Monitoring
    Processing
    Hot Temperature

    Bibliographical note

    Paper presented at the Nanotech International Conference and Trade Show, held 03-07 May, 2009 in Texas, USA.
    © 2009 NSTI http://nsti.org. Reprinted, with permission, from Nanotechnology 2009, p509-512, 2009, Texas, USA.

    Keywords

    • Aircraft gas turbine engines
    • Concept demonstrators
    • Engine monitoring
    • Field representations
    • Gas turbine engine
    • Geosciences
    • Information Extraction
    • Interpolation algorithms
    • Processing power
    • Prototyping
    • State of the art
    • Thermal monitoring
    • Visualisation, Aerospace applications
    • Aircraft
    • Aircraft engines
    • Concurrent engineering
    • Gas turbines
    • Job analysis
    • MEMS
    • Microelectromechanical devices
    • Nanotechnology
    • Rapid prototyping
    • Routing protocols
    • Sensor networks
    • Turbomachinery
    • Wireless telecommunication systems, Wireless sensor networks

    Cite this

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    title = "Wireless sensor networks for aerospace applications- thermal monitoring for a gas turbine engine",
    abstract = "The paper here reports on the development of a prototype wireless sensor network for thermal monitoring of aircraft gas turbine engines. The prototype acts as a concept demonstrator for the application at hand. Building upon the state of the art in the domain, the authors pursued a rapid prototyping approach, supported by a base prototyping framework - FieldMAP. As a key property, the framework enables the conceptual shift from data to user relevant information. Consequently, an information extraction and visualisation component is put forward as an addition to traditional “sense and send” WSN systems. The component offers an intuitive approach to user understanding of the global evolution of the observed phenomena. Integrated within the prototype, this component makes use of the processing power available within the WSN coupled with interpolation algorithms borrowed from the geosciences domain. Reconstruction of field representations of the phenomena from the sparse sensed data allows identification of abnormalities and inference of their likely cause.",
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    AU - Goldsmith, D.

    AU - Gaura, E.

    AU - Brusey, J.

    AU - Shuttleworth, J.

    AU - Hazelden, R.

    AU - Langley, M.

    N1 - Paper presented at the Nanotech International Conference and Trade Show, held 03-07 May, 2009 in Texas, USA. © 2009 NSTI http://nsti.org. Reprinted, with permission, from Nanotechnology 2009, p509-512, 2009, Texas, USA.

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    AB - The paper here reports on the development of a prototype wireless sensor network for thermal monitoring of aircraft gas turbine engines. The prototype acts as a concept demonstrator for the application at hand. Building upon the state of the art in the domain, the authors pursued a rapid prototyping approach, supported by a base prototyping framework - FieldMAP. As a key property, the framework enables the conceptual shift from data to user relevant information. Consequently, an information extraction and visualisation component is put forward as an addition to traditional “sense and send” WSN systems. The component offers an intuitive approach to user understanding of the global evolution of the observed phenomena. Integrated within the prototype, this component makes use of the processing power available within the WSN coupled with interpolation algorithms borrowed from the geosciences domain. Reconstruction of field representations of the phenomena from the sparse sensed data allows identification of abnormalities and inference of their likely cause.

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