A cushion length adjusting system for use in an ejection seat of an aircraft comprising a seat pan 406 which comprises a first cushion length adjuster 412 hingedly coupled to the seat pan 406, the first cushion length adjuster defining a pivot axis, a second cushion length adjuster 414 nested with the first cushion length adjuster and hingedly coupled to the seat pan 406, where, in response to pivoting the second cushion length adjuster, the first cushion length adjuster and the second cushion length adjuster both pivot. A cushion length adjusting system comprising a first cushion length adjuster 412 which can be slidingly or pivotally coupled to the seat pan, where the system is configured to vary a support length measured from the front side of the pan. The cushion may be slidingly extended from the slot via handle 422, 424.


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    Titel :

    Seat cushion length adjuster for ejection seat


    Beteiligte:
    GLEN SHAW (Autor:in) / TYLER FAHEY (Autor:in) / STEVE HOLSTINE (Autor:in)

    Erscheinungsdatum :

    2024-01-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet



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