Flight passenger seat with an integrated spring element

1. A flight passenger seat for an airplane comprising:

a pivotable back element;

a seat element; and

at least one first reset element, one end of the at least one first reset element mounted inside the back element in a fixed manner relative to the back element and an end opposite to the fixedly mounted end of the at least one first reset element mounted to a first intermediate lever in a rotatable manner;

wherein the at least one first reset element acts on the pivotable back element to cause pivoting.

2. The flight passenger seat of claim 1 ,

wherein a locking mechanism is provided to lock the back element in a pivoted position.

3. The flight passenger seat of claim 1 , further comprising

an arm rest element;

wherein the arm rest element is pivotable;

wherein at least one second reset element acts on the arm rest element.

4. The flight passenger seat of claim 1 ,

wherein the back element comprises at least one rocker element;

wherein the at least one first reset element acts on the rocker element such that on pivoting the back element, a force is applied on the back element by means of the at least one first reset element which acts against a pivoting movement.

5. The flight passenger seat of claim 1 ,

wherein the at least one first reset element is disposed in a generally vertical arrangement.

6. The flight passenger seat of claim 1 , further comprising a submerged rod having an end, a connecting link and a linear guide and

wherein the end of the submerged rod is guided in the connecting link with the linear guide;

wherein the linear guide defines an elongated hole;

wherein the elongated hole has a first end and a second end;

wherein the first end defines a first distance to a pivoting axis of the back element;

wherein the second end of the elongated hole defines a second distance to the pivoting axis of the back element;

wherein the elongated hole is adapted in such a way that the first distance is larger than the second distance;

wherein, on moving in a pivoting direction, the end of the submerged rod performs a circular movement about the pivoting axis, such that by guiding the end of the submerged rod in the elongated hole, the reset element is compressed in such a manner that a force counteracting the pivoting movement is generated which, on releasing the first reset element, forces the back element into an upright position.

7. The flight passenger seat of claim 1 ,

wherein the at least one first reset element is mounted at a first distance to the at least one rotating axis of the back element such that on pivoting the back element, a torque is applied, which urges the back element into an upright position;

wherein at least one second reset element is arranged in the seat element;

wherein the seat element is rotatably supported by at least one other rotating axis;

wherein the at least one second reset element is mounted at a second distance to the at least one other rotating axis in such a way that a torque is applied, which, on pivoting in a horizontal position, urges the seat element into a vertical position.

8. The flight passenger seat of claim 7 ,

wherein the at least one first reset element and the at least one second reset element are mounted onto a shared bolt.

9. The flight passenger seat of claim 7 ,

wherein the at least one second reset element is mounted to a second intermediate lever in a rotatable manner; and

wherein the first and second intermediate levers are mounted to a shared axis in a rotatable manner.

10. The flight passenger seat of claim 1 ,

wherein the at least one first reset element is arranged as an element with a linear expansion or spring.

11. Flight passenger seat group, comprising at least two flight passenger seats according to claim 1 .

12. Airplane with at least one flight passenger seat according to claim 1 or one flight passenger seat group, according to claim 11 .

13. A flight passenger seat for an airplane, comprising:

a back element;

a pivotable seat element; and

at least one first reset element, one end of the at least one first reset element mounted inside the seat element in a fixed manner relative to the seat element and an end opposite to the fixedly mounted end of the at least one first reset element mounted to a first intermediate lever in a rotatable manner;

wherein the at least one first reset element acts on the pivotable seat element.

14. The flight passenger seat of claim 13 , further comprising:

a pivotable arm rest element;

at least one second reset element, the at least one second reset element acting on the arm rest element.

15. The flight passenger seat of claim 13 , wherein the seat element comprises at least one rocker element;

wherein the at least one first reset element acts on the rocker element such that on pivoting the seat element, a force is applied on the seat element by means of the at least one first reset element which acts against a pivoting movement.

16. The flight passenger seat of claim 13 , further comprising a submerged rod having an end, a connecting link and a linear guide and

wherein the end of the submerged rod is guided in the connecting link with the linear guide;

wherein the linear guide defines an elongated hole;

wherein the elongated hole has a first end and a second end;

wherein the first end defines a first distance to a pivoting axis of the back element;

wherein the second end of the elongated hole defines a second distance to the pivoting axis of the back element;

wherein the elongated hole is adapted in such a way that the first distance is larger than the second distance;

wherein, on moving in a pivoting direction, the end of the submerged rod performs a circular movement about the pivoting axis, such that by guiding the end of the submerged rod in the elongated hole, the reset element is compressed in such a manner that a force counteracting the pivoting movement is generated which, on releasing the first reset element, forces the seat element into a horizontal position.