System for driving a flap arrangement between a retracted position and an extended position

1. A flap system for driving a leading-edge flap between a retracted position and an extended position, the system comprising:

a leading-edge flap having a first flap joint and a second flap joint,

a first scissor link,

a second scissor link,

a first connecting link, and

an actuator,

wherein the actuator is coupled with either the first scissor link or the first connecting link,

wherein the first scissor link comprises a first support joint for rotatably supporting the first scissor link on a first structurally fixed point, wherein an end of the first scissor link opposed to the first support joint is coupled with the first flap joint,

wherein the first connecting link comprises a second support joint for rotatably supporting the first connecting link on a second structurally fixed point and wherein an end of the first connecting link opposed to the second support joint is rotatably coupled with an end of the second scissor link,

wherein an end of the second scissor link opposed to the end coupled with the first connecting link is coupled with the second flap joint,

wherein additionally the first scissor link and the second scissor link are rotatably coupled to each other to form a scissor arrangement,

wherein the actuator, the first scissor link, the second scissor link and the first connecting link are arranged to actively place the leading-edge flap from a retracted position into an extended position

wherein the first scissor link is coupled to the flap through a second connecting link, which is rotatably supported to the first scissor link and rotatably supported to the first flap joint, and

wherein the second connecting link has a length less than a third of the length of the first connecting link.

2. The system of claim 1 , wherein the second connecting link has a shorter length than the first connecting link.

3. The system of claim 1 ,

wherein one of the first scissor link and the second scissor link comprises a recess along a main extension direction through which the other one of the first scissor link and the second scissor link passes, and

wherein the first scissor link and the second scissor link are rotatably coupled in a region of the recess.

4. The system of claim 1 ,

wherein the first scissor link and the second scissor link comprise a rotary scissor joint for coupling the first scissor link and the second scissor link,

wherein the scissor joint is placed in a central region of each scissor link.

5. The system of claim 1 , wherein the second scissor link is directly coupled with the flap.

6. The system of claim 1 , wherein only a single actuator is used.

7. The system of claim, 1 wherein the actuator, the first scissor link, the second scissor link and the first connecting link are arranged to actively place the leading-edge flap from a retracted position into an intermediate position, in which a chord axis of the flap is adjusted to a desired angle, and to provide a translational motion afterwards along the chord axis of the flap.

8. A wing having a leading-edge region and a trailing edge region, as well as at least one system according to claim 1 installed inside the wing.

9. The wing according to claim 8 , wherein the system is arranged in the leading-edge region.

10. The wing according to claim 8 , wherein the system is configured to move the flap below a wing leading edge point up to an angle of 117° between a local flap chord and a local wing chord.

11. The wing according to claim 8 , wherein the flap system is further designed to limit a gap between a trailing edge of the flap and a leading-edge point of the wing to 2% of a local wing chord.

12. An aircraft having at least one wing according to claim 8 .