A canopy fragilization system for use in an aircraft ejection system may comprise: a sharp breaker disposed on a first side of an ejection seat, the sharp breaker configured to act as a primary breaker of a canopy of an aircraft; a blunt breaker disposed on a second side of the ejection seat, the blunt breaker configured to act as a secondary breaker of the canopy of the aircraft; and a deployable overhead protection assembly comprising a first tertiary breaker and a second tertiary breaker.


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    Titel :

    Deployable overhead protection assembly and methods of use for canopy fragilization system


    Beteiligte:
    HOLSTINE STEVEN A (Autor:in) / EISCHEID NATHAN (Autor:in) / MASTROLIA BRADLEY (Autor:in) / HAMPTON JOHN (Autor:in) / CROSS NEIL (Autor:in) / CARSON KASSIDY L (Autor:in) / HAAS IAN WALTER (Autor:in) / HYDE PATRICK EMMETT (Autor:in) / KEENE AARON H (Autor:in) / TEAL CYLE (Autor:in)

    Erscheinungsdatum :

    2022-05-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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