Following the first flight of the A310 Airbus (of international manufacture) one of its original features is presented, namely, the engine vibration measurement system, operative in flight, which is based on systems used in large turbine testing equipment. The purpose of the measurements is examined and the system comprising piezo-electric detectors, temperature and noise compensation is described and the location and mounting of the detectors is indicated. Some account is given of the analysis and presentation of the signals.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Measurement in flight of vibrations in the A310 Airbus


    Weitere Titelangaben:

    Messung der Vibration im A310 Airbus waehrend des Flugs
    Titel franzoesisch


    Erschienen in:

    Erscheinungsdatum :

    1982


    Format / Umfang :

    5 Seiten


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Französisch




    Airbus Industrie A310 Update

    Emerald Group Publishing | 1982


    Airbus looks at A310 Lite

    Online Contents | 1996




    Simulation of flight instrument system (EFIS) of aircraft airbus A310

    Kroupa, Stepan / Pachner, Daniel / Pech, Zdislav | Tema Archiv | 2003