Fluid flow control devices

• US 5,755,408 A
• Filed: 04/03/1995
• Issued: 05/26/1998
• Est. Priority Date: 04/03/1995
• Status: Expired due to Fees

• Current Assignee: Orbital Research, Inc.
• Original Assignee: Orbital Research, Inc.
• Inventors: Shaw, Greg S., Schmidt, Robert N.
• Primary Examiner(s): Kashnikow, Andres
• Assistant Examiner(s): DINH, TIEN QUANG
• Application Number:
  US08/415,418
• Time in Patent Office: 1,149 Days
• Field of Search: 244/204, 244/130, 244/199, 244/213, 244/201, 244/207, 251/129.06
• US Class Current: 244/204
• CPC Class Codes: B64C 21/04 for blowing
• CPC Class Codes: B64C 21/08 adjustable
• CPC Class Codes: Y02T 50/10 Drag reduction

Abstract

A fluid flow control device, comprising a flow surface over which a fluid flows, a flow effect means located on the flow surface and operated by pressure such that the flow effect means improves the flow characteristics of the flow surface, pressure supply means to operate the flow effect means and at least one microelectromechanical system ("MEMS") valve means which controls the flow effect means by controlling the supply of pressure to the flow effect means from the pressure supply means.

Claims

1. A fluid flow control device, comprising:

a) a flow surface over which fluid flows;

b) a flow effect means incorporated into said flow surface and operated by pressure, such that said flow effect means improves the flow characteristics of said flow surface;

c) pressure supply means to operate said flow effect means; and

d) at least one MEMS valve means which controls said flow effect means by controlling the supply of pressure to said flow effect means from said pressure supply means.

2. The fluid flow control device of claim 1 wherein said flow effect means is a turbulence generator.

3. The fluid flow control device of claim 1 wherein said flow surface is the outer surface of an aircraft.

4. The fluid flow control device of claim 1, wherein said flow surface is the outer surface of a watercraft.

5. The fluid flow control device of claim 1, wherein said flow effect means is comprised of at least one boundary layer penetrator having a normal position capable of moving into and out of said flow surface such that the movement of said boundary layer penetrator is controlled by said MEMS valve means such that upon actuation of the MEMS valve means said boundary layer penetrator moves from a normal position.

6. The fluid flow control device of claim 5, wherein said boundary layer penetrator is cylindrical.

7. The fluid flow control device of claim 1 wherein said MEMS valve means is electrostatically actuated.

8. The fluid flow control device of claim 1 wherein said MEMS valve means is piezoelectrically actuated.

9. The fluid flow control device of claim 1 wherein said MEMS valve means is thermally actuated.

10. The fluid flow control device of claim 1 wherein said MEMS valve means is magnetically actuated.

11. The fluid flow control device of claim 1 wherein said pressure supply means comprises a micromachined fluidic channel.

12. The fluid flow control device of claim 11 wherein said micromachined fluidic channel comprises a semiconductor material.

13. The fluid flow control device of claim 1 wherein said pressure supply means utilizes a pressurized sample of fluid flowing over said flow surface flows.

14. The fluid flow control device of claim 5, further comprising reset means such that said reset means returns said boundary layer penetrator to its normal position upon deactuation of said MEMS valve means.

15. The fluid flow control device of claim 5 wherein said normal position of said boundary layer penetrator is in, and approximately flush with, said flow surface.

16. The fluid flow control device of claim 5 wherein said normal position of said boundary layer penetrator is out of said flow surface.

17. The fluid flow control device of claim 14 wherein said reset means comprises spring means and vent means.

18. The fluid flow control device of claim 14 wherein said reset means comprises a vacuum.

19. A fluid flow control device, comprising:

a) a flow surface over which fluid flows;

b) a flow effect means incorporated into said flow surface comprising at least one boundary layer penetrator having a normal position and capable of moving into and out of said flow surface such that the movement of said boundary layer penetrator improves the flow characteristics of said flow surface;

c) pressure supply means to operate said flow effect means;

d) at least one MEMS valve means which controls said flow effect means by controlling the supply of pressure to said boundary layer penetrator from said pressure supply means such that upon actuation of said MEMS valve means said boundary layer penetrator moves from a normal position; and

e) reset means such that said reset means returns said boundary layer penetrator to its normal position upon deactuation of said MEMS valve means.

20. The fluid flow control device of claim 19 wherein said flow effect means is a turbulence generator.

21. The fluid flow control device of claim 19 wherein said flow surface is the outer surface of an aircraft.

22. The fluid flow control device of claim 19 wherein said flow surface is the outer surface of a watercraft.

23. The fluid flow control device of claim 19 wherein said boundary layer penetrator is cylindrical.

24. The fluid flow control device of claim 19 wherein said MEMS valve means is electrostatically actuated.

25. The fluid flow control device of claim 19 wherein said MEMS valve means is piezoelectrically actuated.

26. The fluid flow control device of claim 19 wherein said MEMS valve means is thermally actuated.

27. The fluid flow control device of claim 19 wherein said MEMS valve means is magnetically actuated.

28. The fluid flow control device of claim 19 wherein said pressure supply means comprises a micromachined fluidic channel.

29. The fluid flow control device of claim 28 wherein said micromachined fluidic channel comprises a semiconductor material.

30. The fluid flow control device of claim 19 wherein said pressure supply means utilizes a pressurized sample of fluid flowing over said flow surface.

31. The fluid flow control device of claim 19 wherein said normal position of said boundary layer penetrator is in said flow surface.

32. The fluid flow control device of claim 19 wherein said normal position of said boundary layer penetrator is out of said flow surface.

33. The fluid flow control device of claim 19 wherein said reset means comprises spring means and vent means.

34. The fluid flow control device of claim 19 wherein said reset means comprises a vacuum.

35. A fluid flow control device, comprising:

a) a wing of an aircraft, said wing having a leading edge;

b) at least one array of flow effect means incorporated in said wing, said flow effect means being a turbulence generator comprised of at least one boundary layer penetrator having a normal position and capable of moving into and out of said wing such that the movement of said boundary layer penetrator improves the aerodynamics of said wing;

c) pressure supply means to operate said boundary layer penetrator, said pressure supply means comprised of a micromachined fluidic channel;

d) at least one MEMS valve means which controls said flow effect means by controlling the supply of pressure to said boundary layer penetrator from said pressure supply means such that upon actuation of said MEMS valve means said boundary layer penetrator moves from its normal position; and

e) reset means such that said reset means returns said boundary layer penetrator to its normal position upon deactuation of said MEMS valve means.

36. The fluid flow control device of claim 35 wherein said array is located on the leading edge of said wing.

37. The fluid flow control device of claim 35 wherein said boundary layer penetrator is cylindrical.

38. The fluid flow control device of claim 35 wherein said MEMS valve means is electrostatically actuated.

39. The fluid flow control device of claim 35 wherein said MEMS valve means is piezoelectrically actuated.

40. The fluid flow control device of claim 35 wherein said MEMS valve means is thermally actuated.

41. The fluid flow control device of claim 35 wherein said MEMS valve means is magnetically actuated.

42. The fluid flow control device of claim 35 wherein said micromachined fluidic channel comprises a semiconductor material.

43. The fluid flow control device of claim 35 wherein said pressure supply means utilizes a pressurized sample of air flowing over said wing.

44. The fluid flow control device of claim 35 wherein said normal position of said boundary layer penetrator is in said wing.

45. The fluid flow control device of claim 35 wherein said normal position of said boundary layer penetrator is out of said wing.

46. The fluid flow control device of claim 35 wherein said reset means comprises spring means and vent means.

47. The fluid flow control device of claim 35 wherein said reset means comprises a vacuum.