Provided is a shock reducing tape spring hinge including fixing members fixed to at least two objects, respectively, a thin shell type tape spring having both end portions that are fastened to the fixing members, respectively, and a shell-shaped damping plate aligned with the tape spring, the damping plate having both end portions that are fastened to the fixing members, respectively. The damping plate and the tape spring may be configured to connect the at least two objects being spaced through the fixing members, and the damping plate may be configured to reduce a deployment shock occurring when the tape spring is deployed.


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    Titel :

    SHOCK REDUCING TAPE SPRING HINGE


    Beteiligte:
    LEE CHANG HO (Autor:in) / KIM KYUNG WON (Autor:in) / JEONG JU WON (Autor:in) / KIM YOUNG JIN (Autor:in) / LEE JUNG JU (Autor:in)

    Erscheinungsdatum :

    2018-05-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16C SHAFTS , Wellen / B64G Raumfahrt , COSMONAUTICS / F16F SPRINGS , Federn



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