Seating unit for aircraft

1. A seating unit for an aircraft, comprising:

at least two seats,

wherein the seating unit comprises a platform for accommodating the at least two seats, the platform is configured to be mounted on at least one rail in a floor of the aircraft,

wherein each seat is pivotably mounted to an individual corresponding plate for rotary movement about a vertical axis of rotation, via a pivoting means, and each plate is mounted to the platform via a translatory movement means, disposed between the plate and the platform, for a translatory movement of the plate in relation to the platform along a substantially horizontal direction,

wherein the seating unit comprises immobilization means, disposed on the plates and the platform, for immobilizing each plate relative to the platform and for immobilizing each seat relative to its corresponding plate, and

wherein the pivoting means pivots each seat more than 90° when the seat is moved along the substantially horizontal direction.

2. The seating unit according to claim 1 , wherein each seat further comprises:

a coupling means associated with the platform and the seat for coupling of a translatory movement of the seat with the rotary movement of the seat,

wherein the translatory movement of the seat brings about a rotation of the seat or the rotation of the seat brings about a translatory movement of the seat.

3. The seating unit according to claim 1 , wherein the pivoting means comprises:

a rack disposed on the platform parallel to a direction of said translatory movement of the seat, and

at least one cogwheel associated with the seat meshing with the rack to rotate the seat.

4. The seating unit according to claim 3 , wherein

a first cogwheel meshes with the rack, and

a second cogwheel of greater diameter than the first cogwheel is centered on the vertical axis of rotation of the seat and meshes with the first cogwheel.

5. The seating unit according to claim 1 , wherein each seat further comprises:

a sitting surface, a back, and armrests, wherein

the sitting surface, the back, and the armrests form, in a view from above, a substantially circular contour.

6. The seating unit according to claim 1 , wherein each seat further comprises a storage unit arranged next to the seat and extended in a direction of translatory movement of the seat.

7. The seating unit according to claim 6 , wherein the storage unit translates with the plate of a corresponding seat.

8. The seating unit according to claim 6 , wherein

the storage unit incorporates two retractable shelves,

one of the shelves is hinged to open out on a side of the storage unit, and

an other shelf of the retractable shelves is hinged to open out on an other side of the storage unit.

9. The seating unit according to claim 1 , comprising four seats configured to translate parallel to each other.

10. The seating unit according to claim 9 , wherein

the four seats are arranged substantially in a square,

each seat is equipped with a storage unit, and

each storage unit is placed between two seats of the seating unit.

11. The seating unit according to claim 9 , wherein the four seats are rotatable so as to face each other.

12. The seating unit according to claim 9 , wherein one of the four seats is rotatable independently of the three remaining seats.

13. The seating unit according to claim 1 , wherein the translatory movement means includes guiding grooves in the platform that allow the translatory movement of the plate.

14. The seating unit according to claim 1 , wherein the immobilization means includes threaded bores in the platform to allow an immobilization of the plate in a predefined position with an aid of at least one fastening device.

15. An aircraft cabin, comprising at least one seating unit according to claim 1 .

16. An aircraft, comprising the cabin according to claim 14 .

17. The seating unit according to claim 1 , wherein one end of the translatory movement is configured to face a direction of travel of the aircraft and an other end of the translatory movement faces a direction opposite to the direction of travel.

18. The seating unit according to claim 1 , wherein the pivoting means pivots the seat 180° between one end of the translatory movement to an other end of the translatory movement.

19. The seating unit according to claim 1 , wherein the seat is configured to be locked in an intermediate position, in which the seat is rotated approximately 45° in relation to the main position of the seat.

20. The seating unit according to claim 1 , wherein the pivoting means comprises:

a rack disposed on the platform parallel to a direction of said translatory movement of the seat, and

two first cogwheels associated with the seat meshing with the rack to rotate the seat.

21. The seating unit according to claim 20 , wherein the two first cogwheels also mesh with a second cogwheel of greater diameter than the two first cogwheels, and the second cogwheel is centered on the vertical axis of rotation of the seat.

22. The seating unit according to claim 1 , wherein each seat further comprises a storage unit mounted to the plate in a fixed position and arranged next to the seat.

23. A seating unit for an aircraft, comprising:

at least two seats,

wherein the seating unit comprises a platform for accommodating the seats,

wherein each seat is pivotably mounted to an individual corresponding plate about a vertical axis of rotation, via a pivoting means, and each plate is mounted to the platform via a translatory movement means, disposed between the plate and the platform, for a translatory movement of the plate in relation to the platform along a substantially horizontal direction,

wherein the seating unit comprises immobilization means, disposed on the plates and the platform, for immobilizing each plate relative to the platform and for immobilizing each seat relative to its corresponding plate, and

wherein each seat further comprises a storage unit arranged next to the seat and extended in a direction of translatory movement of the seat,

the storage unit incorporates two retractable shelves,

one of the shelves is hinged to open out on a side of the storage unit, and

an other shelf of the retractable shelves is hinged to open out on an other side of the storage unit.

24. A seating unit for an aircraft, comprising:

at least two seats,

wherein the seating unit comprises a platform accommodating the at least two seats,

the platform is configured to be mounted on at least one rail in a floor of the aircraft,

wherein each seat is pivotably mounted to an individual corresponding plate for rotary movement about a vertical axis of rotation, via a pivoting means, and each plate is mounted to the platform via a translatory movement means, disposed between the plate and the platform, for a translatory movement of the plate in relation to the platform along a substantially horizontal direction,

wherein the seating unit comprises immobilization means, disposed on the plates and the platform, for immobilizing each plate relative to the platform and for immobilizing each seat relative to its corresponding plate, and

a coupling means associated with the platform and the seat for coupling of a translatory movement of the seat with the rotary movement of the seat, wherein

the translatory movement of the seat brings about a rotation of the seat or the rotation of the seat brings about a translatory movement of the seat, and

the pivoting means pivots the seat more than 90° when the seat is moved along the substantially horizontal direction.