An aircraft check valve assembly where the fluid check valve is indexed in rotational position relative to a first duct flange and to a second opposed duct flange and to a clamping band where the check valve includes an annular check valve flange having at least one index tab extending therefrom. The index tab formed in the check valve annular flange engages a void area formed in an outer annular ridge formed in the first and second duct flanges. A clamping band holds the first duct flange to the check valve flange and to the second duct flange where the clamping band is rotationally indexed to the check valve by index fingers formed on the index tab which and extends to occupy a gap formed in a hinge point of the band clamp. The index finger is oriented relative to the operating direction of the check valve to provide for confirmation of the correct orientation of the check valve for error proofing.


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    Titel :

    AIRCRAFT FLUID CHECK VALVE ASSEMBLY WITH INDEXING


    Weitere Titelangaben:

    ENSEMBLE CLAPET DE NON-RETOUR DE FLUIDE D'AERONEF AVEC INDEXAGE


    Beteiligte:

    Erscheinungsdatum :

    21.02.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16K VALVES , Ventile / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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