A vibration damper (210, 210A, 210B, 210C) including a frame (300) having at least a first cavity (310), a frame first end (300E1) and a frame second end (300E2) spaced from the frame first end (300E1); a shaft (330) slidably coupled to and extending into the frame (300) where the shaft (330) extends through the first cavity (310); a first vibration isolator (340) disposed within the first cavity (310) where the shaft (330) extends through the first vibration isolator (340) so as to capture the first vibration isolator (340) within the first cavity (310) where the first vibration isolator (340) interfaces with the frame second end (300E2); and a second vibration isolator (350) disposed on the shaft (330), where the shaft (330) extends through the second vibration isolator (350) so as to capture the second vibration isolator (350) on the shaft (330) where the second vibration isolator (350) interfaces with the frame second end (300E2) opposite the first vibration isolator (340), where the first vibration isolator (340) and the second vibration isolator (350) act only in compression.


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    Titel :

    VIBRATION DAMPING LINK AND METHOD THEREFOR


    Weitere Titelangaben:

    SCHWINGUNGSDÄMPFUNGSELEMENT UND VERFAHREN DAFÜR
    LIAISON D'AMORTISSEMENT DE VIBRATIONS ET PROCÉDÉ ASSOCIÉ


    Beteiligte:

    Erscheinungsdatum :

    12.05.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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