Turbulent flow drag reduction
View Patent ↗The present invention relates to apparatus for influencing fluid flow over a surface, and more particularly, but not exclusively, to turbulent boundary layer flow drag reduction for an aircraft. The present invention provides such apparatus including a plasma generator comprising a first electrode and a signal generator, the apparatus being operable to drive the first electrode with a pulsed signal generated by the signal generator thereby to cause a change in direction of the flow of the fluid over the surface.
1. Apparatus for influencing boundary layer fluid flow over a surface, the apparatus including a plasma generator comprising:
a first electrode, said first electrode comprising first and second elongate elements; and
a signal generator for driving the first electrode with a pulsed signal and for causing said fluid to move in a direction from one of said elongate elements to the other of said elongate elements, wherein said first elongate element receives a first pulse and the second elongate element receives a second pulse after a time interval at least as long as the time taken for fluid to travel between the first and second elongate elements.
2. Apparatus according to claim 1 , wherein the pulsed signal comprises a pulse envelope containing a varying signal.
3. Apparatus according to claim 2 , wherein the pulse envelope contains a train of shorter duration pulses.
4. Apparatus according to claim 3 , wherein the pulse envelope contains 10 to 100 pulses.
5. Apparatus according to claim 2 , wherein the pulse envelope duration and the pulse envelope repetition period are independently adjustable.
6. Apparatus according to claim 1 , wherein the plasma generator is operable to cause a change in direction of the flow of the fluid over the surface primarily in a single direction.
7. Apparatus according to claim 1 , wherein the first and second elongate elements are in juxtaposed alignment.
8. Apparatus according to claim 7 , wherein the first and second elongate elements are in substantially parallel alignment.
9. Apparatus according to claim 8 , wherein the first and second elongate elements extend generally parallel to the usual direction of motion of the surface in use.
10. Apparatus according to claim 1 , wherein the apparatus is operable such that first elongate element receives a first pulse and the second elongate element receives a second pulse after a time interval at least as long as the time taken for fluid to travel between the first and second elongate elements.
11. Apparatus according to claim 10 , wherein the apparatus is operable to drive the first and second elongate elements with a common pulsed signal generated by the signal generator, the period of the pulsed signal being at least as long as the time taken for fluid to travel between the first and second elongate elements.
12. Apparatus according to claim 1 , wherein the plasma generator is operable to cause a change in direction of the flow of the fluid over the surface in alternate generally opposite directions.
13. Apparatus according to claim 12 , wherein the plasma generator further comprises a second electrode operable independently of the first electrode in response to a pulsed signal generated by the signal generator.
14. Apparatus according to claim 13 , wherein the first and second electrodes are in juxtaposed alignment.
15. Apparatus according to claim 14 , wherein the first and second electrodes are in substantially parallel alignment.
16. Apparatus according to claim 15 , wherein the first and second electrodes extend generally parallel to the usual direction of motion of the surface in use.
17. Apparatus according to claim 12 , wherein the signal generator is operable to supply pulses to the first and second electrodes alternately thereby driving the first and second electrodes alternately.
18. Apparatus according to claim 17 , wherein the apparatus is operable such that first electrode receives a first pulse and the second electrode receives a second pulse after a time interval less than the time taken for fluid to travel between the first and second electrodes.
19. Apparatus according to claim 1 , wherein the plasma generator includes a dielectric that supports the first electrode and any second electrode on a first side thereof.
20. Apparatus according to claim 19 , wherein the dielectric is in the form of a flexible sheet.
21. Apparatus according to claim 19 , wherein the dielectric comprises a second side that supports an opposed electrode of the plasma generator, the first and second sides being generally opposed.
22. Apparatus according to claim 13 , wherein each of the first and second electrodes comprise a plurality of electrically connected elongate elements.
23. Apparatus according to claim 22 , wherein the first and second electrodes are arranged such that the elongate elements are interdigitated.
24. Apparatus according to claim 23 , wherein the opposed electrode comprises a plurality of electrically connected elongate elements.
25. Apparatus according to claim 24 , wherein the elongate elements of the first, second and opposed electrodes are in a substantially parallel juxtaposed alignment when viewed facing the first side of the dielectric.
26. Apparatus according to claim 25 , wherein the elongate elements of the first, second and opposed electrodes extend substantially parallel to the usual direction of motion of the surface.
27. Apparatus according to claim 25 , wherein the elongate elements of the opposed electrode are laterally offset from the elongate elements of the first and second electrodes.
28. An aircraft aerodynamic surface including apparatus according to claim 1 , wherein the plasma generator is operable to cause a change in direction of the flow of the fluid over the surface.
29. An aircraft including apparatus according to claim 1 , wherein the plasma generator is operable to cause a change in direction of the flow of the fluid over the surface.