Automatic wing control for sailing vessels

1. An automatic wing control mechanism for sailing vessels, comprising:

a housing assembly comprising:

a drum comprising a through hole, the drum formed mid-way along a flat wall of the housing; and

a restoring mechanism mounted to an external surface of the drum;

and;

a pivot assembly comprising:

a tube extension sized to fit the through hole, the tube extension having a through hole sized to accept and hold a mast of a sailing vessel; and

engagement means coupled to the tube extension for engaging the restoring mechanism;

wherein the restoring mechanism generates a force against the engagement means as the mast rotates around the through hole during sailing.

2. The automatic wing control mechanism of claim 1 , wherein the engagement means comprises a roller configured to contact a surface of the restoring mechanism along a length of the restoring mechanism as the mast rotates around the through hole during sailing.

3. The automatic wing control mechanism of claim 1 , wherein the restoring mechanism comprises a tension bar.

4. The automatic wing control mechanism of claim 3 , wherein the tension bar comprises a flexible, longitudinal member coupled to the drum at a midpoint of the tension bar.

5. The automatic wing control mechanism of claim 1 , wherein the restoring mechanism comprises a pair of springs.

6. The automatic wing control mechanism of claim 1 , wherein the half-circle housing assembly further comprises:

an inner, semi-circular wall surface facing the external surface of the drum; and

at least one mechanical stop protruding from the semi-circular wall surface, located at a height on the semi-circular wall surface to engage a portion of the restoring mechanism when the pivot assembly is rotated by the mast.

7. The automatic wing control mechanism of claim 1 , wherein the restoring mechanism comprises a bending stiffness characteristic, selected to cause a constant restoring force to the engagement means as the mast rotates around the through hole during sailing.

8. The automatic wing control mechanism of claim 1 , wherein the engagement means is located at a first position along the tension bar when the mast is rotated to a first position by a wing coupled to the mast, and the engagement means is located at a second, opposing position along the tension bar when the mast is rotated to a second position by the wing.

9. The automatic wing control mechanism of claim 8 , wherein the restoring force created by the restoring mechanism is equal to a rotational moment caused by the wing coupled to the mast.

10. An automatic wing control mechanism, comprising:

means for rotatably coupling a mast to an automatic wing control mechanism housing, wherein the mast causes a first rotational moment when the mast is rotated by a wing coupled to the mast, comprising:

a hollow tube for receiving and securing the mast;

an arm extending from the hollow tube; and

engagement means coupled to the arm for engaging a restoring mechanism coupled to the automatic wing control mechanism;

and

means for generating a counteracting force opposing the moment caused by the mast, wherein the counteracting force causes the wing to maintain a predetermined angle with respect to the apparent wind.

11. An automatic wing control mechanism, comprising:

means for rotatably coupling a mast to an automatic wing control mechanism housing, wherein the mast causes a first rotational moment when the mast is rotated by a wing coupled to the mast, comprising an engagement mechanism:

means for generating a counteracting force opposing the moment caused by the mast, wherein the counteracting force causes the wing to maintain a predetermined angle with respect to the apparent wind, comprising:

a drum located on an inner wall of the automatic wing control mechanism housing, the drum comprising a rounded exterior surface and a through hole for rotatably receiving the means for rotatably coupling the mast; and

a restoring mechanism mounted to the rounded exterior surface for providing the counteracting force against the engagement mechanism as the engagement mechanism contacts the restoring mechanism as the engagement mechanism is rotated by the mast.

12. The automatic wing control mechanism of claim 11 , wherein the engagement means comprises a roller configured to contact a surface of the restoring mechanism along a length of the restoring mechanism as the mast is rotated by the wing.

13. The automatic wing control mechanism of claim 11 , wherein the restoring mechanism comprises a tension bar.

14. The automatic wing control mechanism of claim 13 , wherein the tension bar comprises a flexible, longitudinal member coupled to the drum at a midpoint of the tension bar.

15. An automatic wing control mechanism, comprising:

means for rotatably coupling a mast to an automatic wing control mechanism housing, wherein the mast causes a first rotational moment when the mast is rotated by a wing coupled to the mast comprising:

a housing formed as a half circle, comprising a flat wall and a semi-circular wall coupled to the flat wall;

a drum located on an interior surface of the flat wall, the drum comprising a rounded exterior surface and a through hole for rotatably receiving the means for rotatably coupling the mast; and

at least one mechanical stop protruding from an interior surface of the semi-circular wall, located at a height on the semi-circular wall surface to engage a portion of the means for generating a counteracting force when the means for rotatably coupling the mast is rotated by the mast;

and

means for generating a counteracting force opposing the moment caused by the mast, wherein the counteracting force causes the wing to maintain a predetermined angle with respect to the apparent wind.

16. The automatic wing control mechanism of claim 11 , wherein the restoring mechanism comprises a bending stiffness characteristic, selected to cause a constant restoring force to the engagement mechanism as the mast rotates around the through hole during sailing.

17. The automatic wing control mechanism of claim 13 , wherein the engagement means is located at a first position along the tension bar when the mast is rotated to a first position by the wing, and the engagement means is located at a second, opposing position along the tension bar when the mast is rotated to a second position by the wing.

18. The automatic wing control mechanism of claim 16 , wherein the counteracting force is equal to the first rotational moment.