The present invention relates to the deployment and driving device of solar panels for satellites. More particularly, the present invention may provide a device formed in a structure in which a solar panel can be mounted in close contact with a satellite using the structure of the satellite, and which can automatically and stably deploy the solar panel using the structural shape and characteristics, and simplifies satellite operations to facilitate solar directing to improve power production since the angle of the solar panel can be adjusted using a driving device composed of a simple structure using a hinge.

    위성용 태양전지판의 전개 및 구동 장치에 관한 것으로, 위성체의 구조를 이용하여 태양전지판을 위성체에 밀착하여 장착할 수 있는 구조로 형성되되, 구조 형상 및 특성을 이용하여 태양전지판을 자동으로 안정적이게 전개할 수 있으며, 힌지를 이용한 간단한 구조로 구성된 구동 장치로 태양전지판의 각도를 조정할 수 있어 위성 운영을 간소화 하여 태양 지향을 용이하게 하여 전력 생산량을 향상시키는 장치를 제공할 수 있다.


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    Titel :

    Deployment and Driving Mechanism of Solar Panel for Satellite


    Weitere Titelangaben:

    위성용 태양전지판의 전개 및 구동 장치


    Beteiligte:
    WON YOUNG JIN (Autor:in)

    Erscheinungsdatum :

    18.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H02S GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-RED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, E.G. USING PHOTOVOLTAIC [PV] MODULES , Erzeugung elektrischer Energie durch Umwandlung von Infrarot-Strahlung, sichtbarem Licht oder ultraviolettem Licht, z.B. unter Verwendung von Photovoltaik [PV]-Modulen



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