A rotary damper (100) comprising a fixed structure (130), a rotor (110) configured to rotate about an axis (R-R), and two opposing bellows (140a, 140b). The bellows (140a, 140b) each extend between the rotor (110) and the fixed structure (130) and are attached thereto. The bellows (140a, 140b) each define a chamber for holding hydraulic fluid and are configured to expand and contract as the rotor (110) rotates. The damper (100) further comprises a damping orifice (118) extending through the rotor (110) or the fixed structure (130). The bellows (140a, 140b) are sealingly engaged around the damping orifice (118) and the damping orifice (118) permits fluid communication between the chambers (140a, 140b) defined by the bellows (140a, 140b).


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    Titel :

    ROTARY DAMPER, ACTUATOR AND METHOD OF DAMPING ROTARY MOTION


    Weitere Titelangaben:

    DREHDÄMPFER, AKTUATOR UND VERFAHREN ZUR DREHSCHWINGUNGSDÄMPFUNG
    AMORTISSEUR ROTATIF, ACTUATEUR ET MÉTHODE D'AMORTISSEMENT DE MOUVEMENT ROTATIF


    Beteiligte:
    BREWER PAUL (Autor:in) / RAVAL REG (Autor:in) / BEKIRCAN SUAT (Autor:in)

    Erscheinungsdatum :

    05.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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