A retention system for an aircraft seat dress cover (200) defines a cable channel (204) sewn around the periphery of a back portion. A cable (202) in the cable channel is tightened to tighten the aircraft seat dress cover around an aircraft seat back. Adjustable buckles at terminals of the cable interlock and allow the cable to be tightened. A midpoint strap (212) is disposed on opposing sides of the periphery to allow the aircraft seat dress cover to more fully conform to the structure of the aircraft seat.


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    Titel :

    DRESS COVER DRAWSTRING RETENTION SYSTEM


    Weitere Titelangaben:

    KORDELHALTESYSTEM FÜR BEZUGSABDECKUNG
    SYSTÈME DE RETENUE DE CORDON DE COUVERCLE DE PROTECTION


    Beteiligte:
    ASHBY ROBERT (Autor:in) / MEALS JOSEPH (Autor:in) / KREITZ MICHAEL (Autor:in) / POOLE DAVID (Autor:in) / MOONEY ANDREW (Autor:in) / BROWN ADAM (Autor:in) / MOORE MACK THOAS (Autor:in) / GENCO DAVID (Autor:in) / BONOMO GREGORY (Autor:in) / PETERSON ZAKARYA (Autor:in)

    Erscheinungsdatum :

    22.09.2021


    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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