The invention discloses a control valve of an aircraft carrier ejector, wherein a contoured plug moves in the axial direction to communicate, short out and open and close various relative gas ports according to demands, thereby achieving graded compression of controlled air cylinders. The control valve of the aircraft carrier ejector is pushed or indirectly electromagnetically controlled through an outer side surface of a thin steel strip rope by being acted by utilizing multiple self-control acceleration strips in an aircraft carrier ejector which application number is 201410098405.3 on a given position, and enables various impact amounts to be as small as possible during the ejection process, thereby achieving the purpose of automatic control.


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    Titel :

    Control valve of aircraft carrier ejector


    Beteiligte:
    XU YANMING (Autor:in)

    Erscheinungsdatum :

    2016-02-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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