Support device for an aircraft battery

摘要

The device (21) has two support frames sliding along a bar and pinching plate springs (41) by jaws of the bar for modifying a length of a portion of the springs, extending between the jaws and an end of a corresponding bar to adjust a stiffness of the springs. The springs deform in torsion under an effect of a weight of a battery (20) of an aircraft and extend parallel to an axis (Y).