Wing with extendable aerodynamic pivoted flaps
A structure with at least one flap connected to a wing, including: at least one drive device; at least one actuating device including a gear device coupled to the at least one drive device and the at least one flap; and a fairing housing swivellably mounted on the wing, at least partially surrounding the gear device, and coupled to the gear device, wherein actuation of the at least one drive device causes a combined translational and rotational movement of the at least one flap and a swivelling movement of at least a portion of the fairing housing. A method for pivoting a flap is also disclosed. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.
1. A structure with at least one flap connected to a wing, comprising:
at least one drive device;
at least one actuating device including a gear device coupled to the at least one drive device and the at least one flap; and
a fairing housing swivellably mounted on the wing, at least partially surrounding the gear device, and coupled to the gear device,
wherein actuation of the at least one drive device causes a combined translational and rotational movement of the at least one flap and a swivelling movement of at least a portion of the fairing housing,
wherein the fairing housing comprises at least two housing parts that are swivellably arranged with respect to the wing,
the at least two housing parts comprise a first housing part and a second housing part,
the first housing part is swivellably mounted to the wing, and
the second housing part is directly swivellably mounted to the first housing part.
2. The structure of claim 1 , wherein the at least one flap comprises at least one extendable aerodynamic pivotable flap.
3. The structure of claim 1 , wherein the at least one flap comprises at least one lift flap.
4. The structure of claim 1 , wherein the at least one actuating device is arranged to actuate the at least one flap.
5. The structure of claim 1 , wherein the at least one actuating device is loaded by the drive device.
6. The structure of claim 1 , wherein the gear device comprises a crank mechanism.
7. The structure of claim 1 , wherein the gear device is supported by the wing.
8. The structure of claim 1 , wherein the fairing housing comprises a plurality of housing parts.
9. The structure of claim 1 , wherein the first housing part is adjacent to the wing.
10. The structure of claim 1 , wherein the second housing part faces away from the wing.
11. The structure of claim 1 , wherein the first housing part and second housing part are coupled to the gear device.
12. A method of moving a flap connected to a gear device that is at least partially surrounded by a fairing housing, the flap being associated with a wing, comprising:
driving a leading portion of the flap;
steering the flap with the gear device for translational and rotational movement of the flap; and
pivoting at least a portion of the fairing housing with the gear devices,
wherein the pivoting comprises pivoting a first housing part and a second housing part of the fairing housing, and
the second housing part is directly swivellably mounted to the first housing part.
13. The method of claim 12 , wherein the pivoting comprises:
swivelling the first housing part relative to the wing; and
swivelling the second housing part relative to the first housing part.
14. A structure with at least one flap connected to a wing, comprising:
at least one drive device;
at least one actuating device including a gear device coupled to the at least one drive device and the at least one flap; and
a fairing housing at least partially surrounding the gear device and composed of a first fairing housing part swivellably mounted to the wing and coupled to the gear device and a second fairing housing part directly swivellably mounted to the first fairing housing part and coupled to the gear device,
wherein actuation of the at least one drive device causes a combined translational and rotational movement of the at least one flap and a swivelling movement of at least one of the first fairing housing part and the second fairing housing part.
15. The structure of claim 14 , wherein the at least one flap comprises at least one lift flap.