[Problem] To improve the degree of freedom in the start timing of panel deployment without complicating a hinge structure.[Solution] A panel deployment apparatus includes a guide (101) provided on a first hinge axis of a main hinge (Hm1); a guide (102) provided on a second hinge axis of a side hinge (Hs11); and a deployment stop arm (200, 201, 202) that stops deployment of a second side panel (Ps2) by sequential engagement with the guide (101) and the guide (102), the deployment stop arm being fixed to the second side panel (Ps2), wherein the second main panel is deployed in a state of the deployment stop arm being engaged with the guide (101) and, when the deployment stop arm is disengaged from the guide (101) and then engaged with the guide (102), the first side panel is deployed in a state of the deployment stop arm being engaged with the guide (102) and, when the deployment stop arm is disengaged from the guide (102), the second side panel is deployed.


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    Titel :

    PANEL DEPLOYMENT DEVICE AND PANEL DEPLOYMENT METHOD


    Weitere Titelangaben:

    VORRICHTUNG ZUM ENTFALTEN EINER PLATTE UND VERFAHREN ZUM ENTFALTEN EINER PLATTE
    DISPOSITIF ET PROCÉDÉ DE DÉPLOIEMENT DE PANNEAU


    Beteiligte:
    HIROSE TAICHI (Autor:in) / KANEKO NAOYUKI (Autor:in)

    Erscheinungsdatum :

    2023-03-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16C SHAFTS , Wellen



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