A deployable structure comprises a mast and two storage rollers each supporting a flexible solar generator, the two storage rollers being articulated on the mast. The mast comprises at least one longitudinal rod and two lateral arms, inclined angularly in two opposite directions that are symmetrical relative to the longitudinal rod, each lateral arm comprising an end provided with a hollow guide. Each storage roller has a longitudinal axis comprising a bent end forming a pivot respectively articulated inside the hollow guide of a corresponding lateral arm, the pivot of each storage roller having an axis of revolution different from the longitudinal axis of the corresponding storage roller.
STRUCTURE DEPLOYABLE COMPORTANT UN ENSEMBLE DE GENERATEURS SOLAIRES, SYSTEME DE DEPLOIEMENT D'UNE TELLE STRUCTURE DEPLOYABLE ET SATELLITE COMPORTANT UN TEL SYSTEME
DEPLOYABLE STRUCTURE COMPRISING A SET OF SOLAR GENERATORS, SYSTEM FOR DEPLOYING SUCH A DEPLOYABLE STRUCTURE AND SATELLITE COMPRISING SUCH A SYSTEM
AUSKLAPPBARE STRUKTUR, DIE EINE GESAMTHEIT VON SOLARGENERATOREN UMFASST, AUSKLAPPSYSTEM EINER SOLCHEN AUSKLAPPBAREN STRUKTUR UND SATELLIT, DER EIN SOLCHES SYSTEM UMFASST
2019-01-30
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
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