CPC B64D 11/0601 (2014.12) [B64D 11/0604 (2014.12); B64D 11/0641 (2014.12)] | 16 Claims |
1. A seat assembly of individual seats to be installed in an aircraft cabin having a longitudinal axis, said seat assembly comprising:
a first seat and a second seat facing one another, each seat having an axis,
a central console arranged between the first seat and the second seat, said central console comprising a first foot zone and a second foot zone,
wherein the first foot zone is associated with the first seat, the first seat facing an opening of the first foot zone,
wherein the second foot zone is associated with the second seat, the second seat facing an opening of the second foot zone,
wherein the first seat faces inwardly towards the longitudinal axis of the aircraft cabin and the second seat faces outwardly away from the longitudinal axis of the aircraft cabin, so that the axis of the first seat forms a first non-zero angle with respect to a reference straight line parallel to the longitudinal axis of the aircraft cabin and the axis of the second seat forms a second non-zero angle with respect to the reference straight line,
at least part of the first seat and the first foot zone define at least part of a first bed surface facing outwardly and away from the longitudinal axis of the aircraft cabin, so that an axis of the first bed surface forms a third non-zero angle with respect to the reference straight line,
at least part of the second seat and the second foot zone define at least part of a second bed surface facing inwardly and towards the longitudinal axis of the aircraft cabin, so that an axis of the second bed surface forms a fourth non-zero angle with respect to the reference straight line.
|