High lift system for an aircraft and aircraft having such a high lift system

A high lift system for an aircraft, comprising a wing structure and a leading edge slat movably supported relative to a leading edge of the wing structure, the leading edge slat comprising:

• a leading edge and a trailing edge, wherein the trailing edge is configured to take different positions to form a gap between the leading edge slat and the wing structure,
• a skin enclosing an interior space of the leading edge slat, the skin having a flexible leading skin section facing away from the wing structure, and a flexible trailing skin section facing towards the wing structure, and
• at least one actuation arrangement arranged inside the interior space for selectively introducing a normal force onto at least one of the leading skin section and the trailing skin section,
• wherein said normal force changes the profile of the skin in such a way that the trailing edge changes its position relative to the wing structure to selectively close or open the gap between the leading edge slat and the wing structure,
• wherein the at least one actuation arrangement comprises a rotary actuator, which is coupled with a first lever pivotably attached to a first joint on the inside of at least one of the trailing skin section and the leading skin section, and which is coupled with a second lever pivotably attached to a second joint on the inside of at least one of the trailing skin section and the leading skin section, wherein the rotary actuator, the levers, and the joints being arranged inside the interior space, and
• wherein the rotary actuator comprises a single transmission shaft coupled to a first pair of bevel gears and to a second pair of bevel gears, the first pair of bevel gears couplable with a first spindle screw, which engages with a first screw nut coupled to the at least one of the trailing skin section and the leading skin section by a first coupling element, and the second pair of bevel gears couplable with a second spindle screw, which engages with a second screw nut coupled to the at least one of the trailing skin section and the leading skin section by a second coupling element, wherein the single transmission shaft, the pairs of bevel gears, the spindle screws, the screw nuts, and the coupling elements are arranged inside the interior space.

A high lift system for an aircraft, comprising a wing structure and a leading edge slat movably supported relative to a leading edge of the wing structure, the leading edge slat comprising:

• a leading edge and a trailing edge, wherein the trailing edge is configured to take different positions to form a gap between the leading edge slat and the wing structure,
• a skin enclosing an interior space of the leading edge slat, the skin having a flexible leading skin section facing away from the wing structure, and a flexible trailing skin section facing towards the wing structure, and
• at least one actuation arrangement arranged inside the interior space for selectively introducing normal forces onto the leading skin section and the trailing skin section,
• wherein said normal forces change the profile of the skin in such a way that the trailing edge changes its position relative to the wing structure to selectively close or open the gap between the leading edge slat and the wing structure,
• wherein the at least one actuation arrangement comprises a rotary actuator, which is coupled with at least one lever, pivotably attached to a joint on the inside of the trailing skin section and to a joint on the inside of the leading skin section, wherein the rotary actuator, the at least one lever, and the joints are arranged inside the interior space, and
• wherein the rotary actuator comprises a single transmission shaft coupled to a first pair of bevel gears and to a second pair of bevel gears, the first pair of bevel gears couplable with a first spindle screw, which engages with a first screw nut coupled to the trailing skin section by a first coupling element, and the second pair of bevel gears couplable with a second spindle screw, which engages with a second screw nut coupled to the leading skin section by a second coupling element, wherein the single transmission shaft, the pairs of bevel gears, the spindle screws, the screw nuts, and the coupling elements are arranged inside the interior space.