To provide desired engine restart capability and limit ignition operating time to a minimum, it was considered desirable to develop a flameout sensor. The compressor discharge pressure (CDP) was used as the most desirable sensing parameter to obtain positive indication of flameout.Diagrams of the sensor and a brief description of its operation are given in this paper. Flight testing of the flameout sensor has proved its reliability.


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    Titel :

    Bendix Flameout Sensor for Turbine Engine Aircraft


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Welch, H. C. (Autor:in)

    Kongress:

    SAE World Congress & Exhibition ; 1964



    Erscheinungsdatum :

    01.01.1964




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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