DYNAMIC ELECTRO-MECHANICAL OTTOMAN

A dynamic electro-mechanical ottoman for an aircraft, comprising a rail assembly (230) comprising one or more rails (232); and one or more actuatable tracks (242) coupled to the one or more rails (232); and a cushion assembly (200) translatable via the one or more actuatable tracks (242) between a first translation position and a second translation position, the cushion assembly comprising one or more cross plates (208) coupled to the one or more actuatable tracks; a pivot shaft (214) coupled to the one or more cross plates; and a cushion sub-assembly (212) comprising one or more support plates (204) coupled to the pivot shaft; and a cushion (202) coupled to the one or more support plates, the cushion sub-assembly rotatable about an axis through the pivot shaft between a first rotation position and a second rotation position to actuate a front edge in a downward direction and a rear edge in an upward direction, a top surface of the cushion at least partially facing an aircraft seat (104) when the cushion sub-assembly is in the second rotation position.