Patent ID: 9145209
Filing Date: 2015-09-29
Classification: B64D

Abstract:
1. A cabin attendant seat comprising: a backrest element, a seat element which is fastened to the backrest element, the backrest element being rotatable about a rotation axis in order to move the cabin attendant seat between a rest position and an operating position, and a fastening device for fastening the cabin attendant seat to a side wall of an aircraft monument, the fastening device being constructed and sized in such a manner that it is capable of directing away a predetermined maximum force which can be introduced into the cabin attendant seat during operation of the cabin attendant seat via the side wall of the aircraft monument, wherein: the fastening device comprises a frame having a first, a second, a third and a fourth frame element, when the cabin attendant seat is in the operating position, the first frame element is mounted substantially perpendicular to and above an upper portion of the fourth frame element and orientated substantially parallel with and located above an upper side of a headrest of the cabin attendant seat, the second frame element is orientated substantially parallel with a rear side of the backrest element of the cabin attendant seat, the third frame element is orientated substantially parallel with a lower side of the seat element of the cabin attendant seat and the fourth frame element is orientated substantially parallel with a first side face of the backrest element of the cabin attendant seat, and when the cabin attendant seat is in the rest position, the second frame element is oriented substantially parallel to a second side face of the backrest element of the cabin attendant seat, and the fourth frame element is oriented substantially parallel to the rear side of the backrest element of the cabin attendant seat.