The invention belongs to the technical field of ejection escape of fighters, and in particular relates to an ejection escape early-warning system. The system is characterized in that a data acquiring circuit is used for acquiring flight parameters from a fighter inertial navigation platform and an atmospheric data machine and continuously inputs into an early-warning computer; the early-warning computer is used for processing the acquired data and calculating the rest time that the ejection is to be carried out under the current distance and the rest time variation rate; a display system is used for directly displaying the rest time to a pilot; a warning system warns when the rest time is close to a warning value and alarms when the rest time variation rate is close to the warning value. With the adoption of the ejection escape early-warning system, the rest time for ejection is reminded to the pilot when the fighter is to suffer from an accident, and the pilot is warned when the rest time and the rest time variation rate are close to the warning value, so that the pilot can quickly determine and handle with the time limit, and as a result, the delay of ejection due to human factors can be avoided, and the ejection escape success rate can be increased.


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    Titel :

    Ejection escape early-warning system


    Beteiligte:
    GUAN YUEMING (Autor:in) / LI GUODONG (Autor:in)

    Erscheinungsdatum :

    2015-05-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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