초록 ▼

An oscillatory vorticity generator device for controlling the flow on an aero- or hydrodynamic surface of an element, the oscillatory vorticity generator device comprising: two main walls, positioned opposite to each other, forming a first pair of walls and two other walls, the four walls each havin

An oscillatory vorticity generator device for controlling the flow on an aero- or hydrodynamic surface of an element, the oscillatory vorticity generator device comprising: two main walls, positioned opposite to each other, forming a first pair of walls and two other walls, the four walls each having proximal and distal ends, the distal ends connected to an aero- or hydrodynamic surface;a connection connecting the walls at their proximal ends; andan opening in the aero- or hydrodynamic surface, the opening being substantially contiguous with the two main walls and the two other walls.

대표청구항 ▼

1. An element comprising: at least one aerodynamic or hydrodynamic surface; andat least one oscillatory vorticity generator,wherein the at least one vorticity generator comprises: four side walls, having proximal and distal ends;a connector connecting the side walls at their proximal ends;wherein th

1. An element comprising: at least one aerodynamic or hydrodynamic surface; andat least one oscillatory vorticity generator,wherein the at least one vorticity generator comprises: four side walls, having proximal and distal ends;a connector connecting the side walls at their proximal ends;wherein the walls and connector form a cavity within the element,wherein the distal ends of the walls are connected to an opening within the aerodynamic or hydrodynamic surface, andwherein two of the four walls are main walls, positioned opposite to each other; andat least one actuator mounted on at least one of the two main walls, such that when activated, the at least one actuator in conjunction with the at least one main wall produces oscillatory pressures within the cavity;wherein the opening in the aerodynamic or hydrodynamic surface is contiguous with the distal ends of the four walls. 2. The element according to claim 1, wherein said at least one actuator is a piezo-electric actuator. 3. The element according to claim 1 wherein a piezo-electric actuator is mounted on each of the two main walls. 4. The element according to claim 1, wherein the distance between the main walls is between 0.1 mm and 10 mm. 5. The element according to claim 1, wherein the distance between the main walls is between 0.5 mm and 1.5 mm. 6. The element according to claim 1, wherein the distance between the main walls is about 1 mm. 7. The element according to claim 1, wherein the two main walls are substantially parallel to each other. 8. The element according to claim 1, wherein the two main walls are substantially non-parallel to each other. 9. The element according to claim 1, wherein the aerodynamic or hydrodynamic surface is an airfoil. 10. An element comprising: at least one aerodynamic or hydrodynamic surface; andat least one wedge-shaped oscillatory vorticity generator; wherein the at least one wedge-shaped vorticity generator comprises: four side walls having proximal and distal ends;a connector connecting the walls at their proximal ends;wherein the walls and connector form a cavity within the element,wherein the distal ends of the walls are connected to an opening within the aerodynamic or hydrodynamic surface, andwherein two of the four walls are main walls which are positioned opposite to and non-parallel to each other forming a wedge shape, andwherein the distal end of the walls of the wedge shape are spaced apart further than the proximal ends; andat least one piezo-electric actuator mounted on at least one of the main walls, such that when activated, the at least one actuator in conjunction with the at least one main wall produces oscillatory pressures within the cavity. 11. The element according to claim 10, wherein the connector comprises a proximal wall. 12. The element according to claim 10, wherein the connector is a bonding element. 13. The element according to claim 12, wherein the bonding element comprises glue. 14. A retrofit device for an element having an aerodynamic or hydrodynamic surface, the retrofit device comprising: an outer surface and an inner surface;wherein the inner surface is adapted to conform to the aerodynamic or hydrodynamic surface and the outer surface comprises a new aerodynamic or hydrodynamic surface for the element;at least one oscillatory vorticity generator associated with the outer surface;wherein the at least one oscillatory vorticity generator comprises: four side walls, having proximal and distal ends;a connector connecting the side walls at their proximal ends;wherein the walls and connector form a cavity within the element,wherein the distal ends of the walls are connected to an opening within the aerodynamic or hydrodynamic surface, andwherein two of the four walls are main walls, positioned opposite to each other; andat least one actuator mounted on at least one of the two main walls, such that when activated, the at least one actuator in conjunction with the at least one main wall produces oscillatory pressures within the cavity;wherein the opening in the aerodynamic or hydrodynamic surface is contiguous with the distal ends of the four walls;at least one fastener adapted to attach the retrofit device to the element. 15. The retrofit device according to claim 14, wherein said at least one fastener comprises a sleeve adapted to cover the aerodynamic or hydrodynamic surface. 16. The retrofit device according to claim 14, wherein said at least one fastener comprises screws, glue, magnets or silicon. 17. A retrofit device for an element having an aerodynamic or hydrodynamic surface, the retrofit device comprising: an outer surface and an inner surface;wherein the inner surface is adapted to fit over the aerodynamic or hydrodynamic surface and the outer surface comprises a new aerodynamic or hydrodynamic surface for the element; andone or more wedge-shaped oscillatory vorticity generators; wherein the at least one wedge-shaped oscillatory vorticity generator comprises: four side walls having proximal and distal ends;a connector connecting the walls at their proximal ends;wherein the walls and connector form a cavity within the retrofit device,wherein the distal ends of the walls are connected to an opening within the new aerodynamic or hydrodynamic surface, andwherein two of the four walls are main walls which are positioned opposite to and non-parallel to each other forming a wedge shape, andwherein the distal end of the walls of the wedge shape are spaced apart further than the proximal ends; andat least one piezo-electric actuator mounted on at least one of the main walls, such that when activated, the at least one actuator in conjunction with the at least one main wall produces oscillatory pressures within the cavity. 18. The retrofit device according to claim 14, further comprising one or more sensors for sensing the flow over the new aerodynamic or hydrodynamic surface. 19. The retrofit device according to claim 14, further comprising one or more controllers for controlling the at least one oscillatory voracity generator. 20. The retrofit device according to claim 14, further comprising conduits located between the inner and outer surfaces, wherein the conduits are configured to connect the oscillatory vorticity generators to power. 21. The element according to claim 1, wherein the element is a turbine blade. 22. A wind turbine comprising at least one wind turbine blade according to claim 21. 23. An aircraft having an aerodynamic surface comprising the element according to claim 1. 24. The retrofit device according to claim 14, wherein a longitudinal axis of the at least one oscillatory vorticity generator is perpendicular to the new aerodynamic or hydrodynamic surface. 25. The retrofit device according to claim 14, wherein an angle between a longitudinal axis of the at least one oscillatory vorticity generator and the new aerodynamic or hydrodynamic surface is between 10° to 170°. 26. The element according to claim 1, wherein the connector comprises a proximal wall. 27. The element according to claim 1, wherein a longitudinal axis of the at least one oscillatory vorticity generator is perpendicular to the aerodynamic or hydrodynamic. 28. The element according to claim 1, wherein an angle between a longitudinal axis of the at least one oscillatory vorticity generator and the aerodynamic or hydrodynamic surface is between 10° to 170°.