The invention relates to a method for manufacturing a panel used in an aircraft, a damping element, and the panel. The panel includes a structural substrate and the damping element including a viscoelastic material (VEM) layer coupleable to the structural substrate of the aircraft, and a constraining layer coupled to the VEM layer. The VEM layer is configured to dampen vibration of the structural substrate. The constraining layer is configured to apply a shear force to the VEM layer.


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    Titel :

    Method for manufacturing panel used in aircraft, damping element, and panel


    Beteiligte:
    LANDMANN ALAN E (Autor:in) / NEGLEY MARK A (Autor:in) / IQBAL JAFFAR S (Autor:in) / VOSS BRET A (Autor:in) / GMEREK MARK M (Autor:in) / LICCIARDI GIACOMO (Autor:in)

    Erscheinungsdatum :

    10.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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