The paper outlines the requirements for the Master Warning System aboard Concorde. It is shown that the system must be a high integrity one, and must have no single point failure which would constrain the operation of the remainder. The effects of electrical noise and the new aspects of the Concorde MWS circuitry are discussed, in particular, the digital filtering system. The operational experience obtained with the device is mentioned, and so far no spurious signals have been recorded, no occasional electrical noise surges have triggered the MWS and all displays on the Display Panel have reflected the true state of the aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft master warning systems


    Weitere Titelangaben:

    Ein Hauptwarnsystem fuer Flugzeuge


    Beteiligte:
    Daniels, S.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1975


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    The Philosophy of Aircraft Warning Systems

    Newman, T P | SAGE Publications | 1993


    The philosophy of aircraft warning systems

    Newman, T.P. | Online Contents | 1993


    The philosophy of aircraft warning systems

    Newman, T. P. / IMechE; Aerospace Industries Division / Royal Aeronautical Society | British Library Conference Proceedings | 1992


    AIRCRAFT WARNING SPHERE

    Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT COLLISION WARNING

    SHENFELD URI / ROSENFELD SAMUEL | Europäisches Patentamt | 2016

    Freier Zugriff