A vibration isolation system for attenuating vibration energy between two aircraft structures, such as between the aircraft's fuselage and interior cabin. The vibration isolation system includes a first isolator attached to the first structure, a second isolator attached to the second structure, and an intermediate mass attached between the first and second isolators. The intermediate mass may be electrical cables, wiring bundles, a cable holder, or other component disposed between the two structures. Cable holder intermediate masses can be fabricated from an electrically conductive material to provide electromagnetic interference shielding for cables disposed therein. Multiple vibration isolation systems can be disposed between the fuselage and interior cabin to provide a less noisy cabin. Additional noise and vibration suppressors, such as skin damping material and acoustic blankets, also can be disposed between the fuselage and interior cabin to further reduce noise in the interior cabin.


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    Titel :

    VIBRATION ISOLATION SYSTEM


    Weitere Titelangaben:

    SCHWINGUNGSISOLATIONSSYSTEM
    SYSTÈME D'ISOLATION DES VIBRATIONS


    Beteiligte:
    WANG TONGAN (Autor:in) / HORNICK DAVID C (Autor:in) / MAXON JR JOHN W (Autor:in) / FOOSE ANDREW S (Autor:in) / FILA JOSEF A (Autor:in)

    Erscheinungsdatum :

    2020-02-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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