Seat unit provided with a tubular seat-base structure
A seat unit, in particular for an aircraft cabin, includes a seat provided with seat cushion and backrest kinematics, and a seat-base structure on which the seat is mounted. The seat-base structure includes a frame with a tubular structure including a first lower tube and a second lower tube, the first lower tube and the second lower tube each carrying at least one bolt intended to be fastened to rails, and two fastening feet for fastening the seat cushion and backrest kinematics. A fastening foot is formed by a tube connected by one of its ends to the first lower tube of the frame and by its other end to the second lower tube of the frame.
1. A seat unit for an aircraft cabin, comprising:
a seat provided with a seating part and backrest kinematics, and
a lower seat structure on which the seat is mounted, wherein said lower seat structure comprises a frame with a tubular structure comprising:
a first lower tube and a second lower tube, the first lower tube and the second lower tube each carrying at least one lock to be fixed on rails, and
two fixing legs of the seating part and backrest kinematics, one fixing leg being formed by a tube connected by a first end to the first lower tube of the frame and by a second end to the second lower tube of the frame,
wherein the seat unit further comprises a privacy shell,
wherein the lower seat structure further comprises a reinforcing belt formed by a plurality of tubes, at least a part of the privacy shell being fixed to said reinforcement belt,
wherein the plurality of tubes of the reinforcement belt are mechanically connected to the first and second lower tubes.
2. The seat unit according to claim 1 , wherein the fixing legs project with respect to a plane in which the first lower tube and the second lower tube of the frame extend.
3. The seat unit according to claim 1 , wherein a fixing guide is arranged on an upper portion of one of the two fixing legs.
4. The seat unit according to claim 1 , wherein the first lower tube and the second lower tube are bent so that a gap between the first lower tube and the second lower tube is variable when moving between ends of the first and second lower tubes.
5. The seat unit according to claim 1 , wherein the reinforcement belt is surrounded by a portion of the privacy shell.
6. The seat unit according to claim 1 , wherein the reinforcement belt extends vertically over a height between 12 cm and 50 cm.
7. The seat unit according to claim 1 , wherein the privacy shell has a lower part and an upper part, wherein the lower part is dismountable from the upper part to provide access to an electrical box under the seat.
8. The seat unit according to claim 1 , wherein at least one passage trough for an electrical harnesses is fixed to the reinforcing belt.
9. The seat unit according to claim 1 , wherein the seat unit comprises three locks so as to have a three-fixation-points configuration.
10. The seat unit according to claim 1 , wherein the lock is associated with a lock support.
11. The seat unit according to claim 10 , wherein the lock support comprises a single opening for a passage of the first lower tube or the second lower tube so as to allow movement of the lock support along the first lower tube or the second lower tube before immobilization by welding said lock support in a position corresponding to a positioning of a rail.
12. The seat unit according to claim 10 , wherein the lock support comprises two openings for the passage of the first lower tube and the second lower tube respectively so as to allow movement of the lock support along the first and second lower tubes before immobilization by welding said lock support in a position corresponding to a positioning of a rail.
13. The seat unit according to claim 10 , wherein the lock support comprises two parts.
14. An aircraft comprising a plurality of seat units as defined in claim 1 .