Patent ID: 8245587

Claim:
A deployment system for spatial appendages comprising at least one two-phase deployment articulation line, furnished with two rotation spindles ( 10 , 20 ), comprising a synchronization mechanism ( 101 , 102 , 103 , 106 , 107 ), for the two rotation spindles so that when the driving spindle ( 20 ) rotates during a first deployment phase, the driven spindle ( 10 ) does not rotate, and then, when the driving spindle rotates during the second deployment phase, the driven spindle rotates in a manner synchronized with the driving spindle, wherein: the synchronization mechanism comprises retaining means ( 101 , 102 , 103 ) making it possible during the first phase, when the driving spindle rotates from a folded-back position to an intermediate position, to hold the driven spindle and, releasing means ( 106 , 107 ) which during the second phase, when the driving spindle rotates from the intermediate position to a final position, to allow the rotation of the driven spindle in synchronism with the driving spindle so as to reach the final position; said retaining means comprising a pulley system ( 101 ) on the driven spindle ( 10 ), from which there depart two cable strands ( 102 , 103 ) attached independently of one another to the releasing means; the releasing means comprising a first winder-unwinder device ( 106 ), a second winder-unwinder device ( 107 ), these devices being eccentric, one of the cable strands comprising a point of attachment ( 104 ) onto the first winder-unwinder device while the other strand comprises a point of attachment ( 105 ) onto the second winder-unwinder device, the pulley system and the winder-unwinder devices being tied by the two cable strands so that one of the devices makes it possible to wind a cable strand from the intermediate position of the driving spindle to the final position while the other device makes it possible to unwind the other cable strand until the driven spindle reaches the final position.