A flight attendant seat comprising a frame that can be mounted on a carrier fixture or integrated into the carrier fixture, and at least one seat arrangement integrated into the frame. The frame comprises a lower section, an upper section and a central section taking up the at least one seat arrangement, at least partially. The lower section is formed bent at least in a region adjoining the central section. A method is provided for fitting a flight attendant seat.

Seat mounting assemblies and vehicle seat systems which include the same are provided whereby a pivot bracket is operatively connected to a mounting bracket for reciprocal vertical movements while a tubular support member is operatively be associated with the pivot bracket so as to be pivotally movable about a substantially vertical central axis of the pivot bracket. A cantilevered support base arm is fixed to and extends outwardly from the tubular support member. An arm member is telescopically connected to the cantilevered support base arm to allow reciprocal rectilinear movements relative to the support base arm along a substantially horizontal axis thereof between retracted and extended positions thereof and carries a swivel plate at a distal end thereof to thereby allow swivel movements of a vehicle seat about a substantially vertical seat axis parallel to the substantially vertical central axis of the pivot bracket.

An aircraft seat may include a seat back coupled to a shell of one or more passenger compartment shell sections of a passenger compartment installed within an aircraft cabin. The aircraft seat may include a seat pan coupled to a floor of the aircraft cabin proximate to an ottoman installed within the passenger compartment. The seat back may be in contact with a surface of the seat pan when the aircraft seat is in a first position. The seat back may be separated from the surface of the seat pan when the aircraft seat is in a second position. The seat back may be configured to move independently of the seat pan when the aircraft seat transitions between the first position and the second position.

An aircraft seat system is disclosed, in accordance with one or more embodiments of the present disclosure. In one embodiment, the aircraft seat system includes a seat casement; a headrest portion; a seat back portion; a seat pan; and one or more armrests pivotably coupled to one or more portions of the seat casement. In another embodiment, the one or more armrests include an armrest body; a rotator link system; and a pivot link system. In another embodiment, the pivot link system may be configured to pivotably extend the armrest cap and pivotably retract the armrest cap.

An apparatus for use with a wall and by a person leaning against the wall and including: a receiver mounted in use to the wall; a support having an operative position whereat the support generally follows the curvature of the buttocks of the person; and a mechanism adapted to suspend the support from the receiver at the operative position.

An apparatus for use with a wall and by a person leaning against the wall and including: a receiver mounted in use to the wall; a support having an operative position whereat the support generally follows the curvature of the buttocks of the person; and a mechanism adapted to suspend the support from the receiver at the operative position.

A folding seat, having a supporting structure, to be fixed to a wall, for a sitting surface which can be tilted from a vertical inactive position to a horizontal active position by way of a tilting mechanism. The seat includes a group of elements used for adjusting a tilting force.

A stowable cabin attendant seat assembly includes a frame assembly mountable within a wall recess, a backrest mounted for reciprocating vertical translation within the frame assembly, a seat pan mounted for pivoting motion relative to the frame assembly, and at least one link connecting the seat pan to the backrest. The at least one link coordinates the seat pan and backrest motions such that upward lifting motion on the seat pan pushes the backrest vertically up for compact stowing and downward pivoting motion on the seat pan pulls the backrest vertically down.

A flight attendant seat comprising a frame that can be mounted on a carrier fixture or integrated into the carrier fixture, and at least one seat arrangement integrated into the frame. The frame comprises a lower section, an upper section and a central section taking up the at least one seat arrangement, at least partially. The lower section is formed bent at least in a region adjoining the central section. A method is provided for fitting a flight attendant seat.

An example seat pan for an aircraft includes a first portion having a first end and a second portion that is adjacent to the first portion and is adjustable to be in a first position in which the second portion forms a seating surface together with the first portion, the seating surface having a width that is wider than a width of the first end of the first portion. The second portion is adjustable to alternatively be in a second position in which the first end of the first portion extends beyond the second portion to be insertable into a footwell.