Deployment system for an airfoil high lift leading edge device

1. A deployment system for adjusting a leading edge high-lift device between a retracted position, in which, in use, the high-lift device is retracted with respect to an airfoil, and at least one deployed position, in which, in use, the leading edge high-lift device is deployed with respect to the airfoil, the deployment system comprising:

a leading edge high-lift device;

at least one actuation unit that is configured to actuate the leading edge high-lift device between the retracted position and the at least one deployed position, the at least one actuation unit comprising a link-and-lever mechanism of at least one link and one lever hingedly connected that are foldable in a V-shaped fashion in the retracted position of the leading edge high-lift device;

at least one guidance unit that is configured to guide the leading edge high-lift device during adjustment between the retracted position and the at least one deployed position along an adjustment path;

wherein the at least one guidance unit is independent from the at least one actuation unit;

wherein each of the at least one guidance unit comprises a track configured for fixedly mounting to the airfoil and a carriage for cooperation with the track, wherein the carriage is movable lengthwise with respect to the track and is mounted to the leading edge high-lift device; and

wherein each track of the at least one guidance unit is configured to extend through a trailing side of the leading edge high-lift device.

2. The deployment system according to claim 1 , wherein the adjustment path is solely determined by a shape of the track of the at least one guidance unit.

3. The deployment system according to claim 1 , wherein the leading edge high-lift device is a slat, wherein each carriage of the at least one guidance unit comprises at least one pair of rollers that are in contact with the track of the at least one guidance unit for movement over the track, such that the carriage can move with respect to the track to guide the slat during adjustment along the track.

4. The deployment system according to claim 1 , wherein the carriage of each of the at least one guidance unit has a shape that corresponds to the shape of the track of the at least one guidance unit.

5. The deployment system according to claim 1 , further comprising the leading edge high-lift device associated with an airfoil, wherein the track of the at least one guidance unit is configured for connection to a rib of the airfoil without penetration of a front spar of the airfoil.

6. The deployment system according to claim 1 , wherein the track of each of the at least one guidance unit is comprised of two C-shaped rails that are mounted opposite each other, an opening of the C-shape facing each other.

7. The deployment system according to claim 6 , wherein each carriage of each of the at least one guidance unit is receivable in the track of the at least one guidance unit, in a receiving space defined by the openings of the C-shaped rails.

8. The deployment system according to claim 6 , wherein each carriage comprises at least one pair of rollers, each having a rotational axis oriented mainly in a direction transverse to the carriage, wherein the rollers are receivable in the track, in a receiving space defined by the C-shape of the two rails.

9. The deployment system according to claim 8 , wherein the at least one pair of rollers is mounted to the carriage at an end of the carriage opposite of an end for connection to the leading edge high-lift device.

10. The deployment system according to claim 1 , wherein the carriage of at least the at least one guidance unit further is provided with at least one pair of side rollers, having a rotational axis oriented mainly in an upward direction.

11. The deployment system according to claim 1 , wherein each carriage of each of the at least one guidance unit is arranged for connection to the leading edge high-lift device at one end of the carriage.

12. The deployment system according to claim 1 , wherein a connection between the carriage and the leading edge high-lift device of the at least one guidance unit comprises a link for hingedly mounting to the carriage at one end and for hingedly mounting to the leading edge high-lift device at an opposite end.

13. The deployment system according to claim 1 , wherein a connection between the carriage and the leading edge high-lift device of each at least one guidance unit comprises two links for hingedly mounting to the carriage at one end and for hingedly mounting to the leading edge high-lift device at an opposite end.

14. The deployment system according to claim 1 , wherein the at least one actuation unit comprises the link-and-lever mechanism having a link arranged for mounting to the leading edge high-lift device and a lever arranged for connection to a drive rod, such that, in use, when the drive rod is driven, the actuation unit is extended or retracted to adjust the leading edge high-lift device between the at least one deployed position and the retracted position.

15. The deployment system according to claim 1 ,

wherein the at least one actuation unit is independent from the at least one guidance unit of the deployment system, and

wherein the at least one actuation unit comprises the link-and-lever mechanism configured for connection to a drive unit at one end and for connection to the leading edge high-lift device at another end.

16. The deployment system of claim 1 wherein the leading edge high-lift device comprises at an internal rib corresponding to each track and wherein an end of each track extending through the trailing side of the leading edge high-lift device is configured to connect to the corresponding rib by a connection plate attached to the rib, the connection plate being configured to receive the distal end of the track to connect the distal end of the track with the rib with the leading edge high-lift device in the retracted position.

17. A deployment system for adjusting a leading edge high-lift device between a retracted position, in which, in use, the leading edge the high-lift device is retracted with respect to an airfoil, and at least one deployed position, in which, in use, the high-lift device is deployed with respect to the airfoil, comprising:

a leading edge high-lift device;

at least one actuation unit that is configured to actuate the leading edge the high-lift device between a retracted position and at least one deployed position;

at least two guidance units that are configured to guide the leading edge the high-lift device during adjustment between the retracted position and the at least one deployed position along an adjustment path;

wherein the at least two guidance units each comprise a track configured for fixedly mounting to the airfoil and a carriage for cooperation with the track, wherein each carriage is movable with respect to the track and is mounted to the leading edge high-lift device;

wherein each track of the at least two guidance units is configured to extend through a trailing side of the leading edge high-lift device and

wherein the at least one actuation unit comprises a link-and-lever mechanism of at least one link and one lever hingedly connected that are foldable in a V-shaped fashion in the retracted position of the leading edge high-lift device.

18. The deployment system according to claim 17 , wherein the leading edge high-lift device is a slat, wherein the link-and-lever mechanism is adjustable between a folded position in a V-shaped fashion when the slat is in the retracted position and an extended position when the slat is in the deployed position.

19. The deployment system according to claim 17 , wherein the leading edge high-lift device is a slat, wherein each carriage of the at least two guidance units comprises at least one pair of rollers that are in contact with each track of the at least two guidance units for movement lengthwise of the track, such that the carriage can move with respect to the track to guide the slat during adjustment along a lengthwise path defined by the track.

20. The deployment system of claim 17 wherein the at least two guidance units are independent from the at least one actuation unit and spatially apart from the at least one actuation unit.

21. A deployment system for adjusting a leading edge high-lift device between a retracted position, in which, in use, the high-lift device is retracted with respect to an airfoil, and at least one deployed position, in which, in use, the leading edge high-lift device is deployed with respect to the airfoil, the deployment system comprising:

a leading edge high-lift device;

at least one actuation unit that is configured to actuate the leading edge high-lift device between the retracted position and the at least one deployed position, the at least one actuation unit comprising a link-and-lever mechanism of at least one link and one lever hingedly connected that are foldable in a V-shaped fashion in the retracted position of the leading edge high-lift device;

at least one guidance unit that is configured to guide the leading edge high-lift device during adjustment between the retracted position and the at least one deployed position along an adjustment path;

wherein the at least one guidance unit is independent from the at least one actuation unit;

wherein each of the at least one guidance unit comprises a track configured for fixedly mounting to the airfoil and a carriage for cooperation with the track, wherein the carriage is movable lengthwise with respect to the track and is mounted to the leading edge high-lift device;

wherein the track of each of the at least one guidance unit is comprised of two C-shaped rails that are mounted opposite each other, an opening of the C-shape facing each other; and

wherein each carriage of each of the at least one guidance unit is receivable in the track of the at least one guidance unit, in a receiving space defined by the openings of the C-shaped rails.

22. The deployment system according to claim 21 , wherein each carriage comprises at least one pair of rollers, each having a rotational axis oriented mainly in a direction transverse to the carriage, wherein the rollers are receivable in the track, in a receiving space defined by the C-shape of the two rails.