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
2018-01-05
Patent
Electronic Resource
French
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 |
European Patent Office | 2019
|STRUCTURE PLIABLE/DÉPLOYABLE COMPORTANT UN MÂT DÉPLOYABLE
European Patent Office | 2022
|MAT DEPLOYABLE A DEPLOIEMENT SPONTANE AUTONOME ET SATELLITE COMPORTANT AU MOINS UN TEL MAT
European Patent Office | 2017
|MAT DEPLOYABLE A DEPLOIEMENT SPONTANE AUTONOME ET SATELLITE COMPORTANT AU MOINS UN TEL MAT
European Patent Office | 2017
|MAT DEPLOYABLE A DEPLOIEMENT SPONTANE AUTONOME ET SATELLITE COMPORTANT AU MOINS UN TEL MAT
European Patent Office | 2017
|