A chute-deployment-seat-release system (120) for an ejection seat (106) may be configured to deploy a parachute (112) from the ejection seat (106) and release an occupant restraint (114) of the ejection seat (106). The chute-deployment-seat-release system (120) may comprise an auto-deployment assembly (140), including a first power supply (146), and a manual deployment assembly (150), including a second power supply (158) and a handle (152). The first power supply (146) may be configured to activate in response to expulsion of the ejection seat (106) from an aircraft (102). The second power supply (158) may be configured to activate in response to an actuation of the handle (152).


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    Titel :

    EMERGENCY MANUAL PARACHUTE OPERATION SYSTEM


    Weitere Titelangaben:

    MANUELLES FALLSCHIRMBETÄTIGUNGSSYSTEM FÜR DEN NOTFALL
    SYSTÈME DE FONCTIONNEMENT DE PARACHUTE MANUEL D'URGENCE


    Beteiligte:

    Erscheinungsdatum :

    06.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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