High bandwidth micro-actuators for active flow control

• US 20100282858A1
• Filed: 05/07/2010
• Published: 11/11/2010
• Est. Priority Date: 05/07/2009
• Status: Active Grant

• Current Assignee: Florida State University (State University System of Florida)
• Original Assignee: Florida State University (State University System of Florida)
• Inventors: Kumar, Rajan, Solomon, John T., Alvi, Farrukh S.
• Granted Patent: US 8,286,895 B2
• Time in Patent Office: Days
• US Class Current: 239/8
• CPC Class Codes: F15D 1/12 by influencing the boundary layer use of materials, e.g. to reduce surface friction C09K3/00

Abstract

A high bandwidth multi-stage microjet actuator. The actuator can produce relatively large amplitude flow disturbances over a broad range of frequencies. The disturbance frequency can be varied by altering the geometry of the device, altering the pressure ratio(s) within the device, and combinations of the two. The actuator has many potential applications, including noise abatement for jet aircraft, and flow control over a moving airfoil.

Claims

1. A method for creating a microjet having a desired frequency of pressure oscillation, comprising:

a. providing a primary nozzle, said primary nozzle directing a primary jet of compressible fluid with said primary jet exiting said primary nozzle at a primary nozzle exit plane, said primary jet having a diameter “

d”

;

b. providing a source of pressurized gas through said primary nozzle to create said primary jet, said pressurized gas flowing through said nozzle creating a nozzle pressure ratio;

c. providing an impingement block including a cavity commencing at a cavity entrance plane parallel to said primary nozzle exit plane and separated therefrom by a distance “

h”

;

d. said cavity including a cavity floor separated from said cavity entrance plane by a distance “

L”

;

e. said cavity including at least one micronozzle extending through said cavity floor; and

f. adjusting the ratio L/d to produce a pressure oscillation in said microjet which is approximately equal to said desired frequency of pressure oscillation.

2. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 1, further comprising adjusting said nozzle pressure ratio in order to alter said frequency of pressure oscillation to more nearly match said desired frequency of pressure oscillation.

3. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 1, further comprising adjusting the ratio h/d in order to alter said frequency of pressure oscillation to more nearly match said desired frequency of pressure oscillation.

4. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 2, further comprising adjusting the ratio h/d in order to alter said frequency of pressure oscillation to more nearly match said desired frequency of pressure oscillation.

5. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 3, further comprising moving either said primary nozzle or said impingement block in order to adjust said ratio h/d.

6. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 1, wherein said step of adjusting said L/d ratio comprises:

a. providing a movable insert in said impingement block, said movable insert including said cavity floor and said at least one micronozzle; and

b. moving said movable insert with respect to said cavity entrance plane in order to vary L and thereby adjust said L/d ratio.

7. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 6, further comprising moving either said primary nozzle or said impingement block in order to adjust said ratio h/d.

10. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 1, further comprising adjusting the ratio h/d in order to alter said frequency of pressure oscillation to more nearly match said desired frequency of pressure oscillation.

12. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 10, further comprising moving either said primary nozzle or said impingement block in order to adjust said ratio h/d.

8. A method for creating a microjet having a desired frequency of pressure oscillation, comprising:

a. providing an impingement block, said impingement block opening into a cavity at a cavity entrance plane;

b. providing a primary nozzle directing a primary jet having a diameter “

d”

into said cavity, said primary nozzle being separated from said cavity entrance plane by a distance “

h”

;

c. said cavity having a cavity floor separated from said cavity entrance plane by a distance “

L”

;

d. said cavity floor having at least one micronozzle extending therefrom, said micronozzle being parallel to said primary jet; and

e. adjusting the ratio L/d to produce a frequency of pressure oscillation in said microjet which closely approximates said desired frequency of pressure oscillation.

9. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 8, further comprising adjusting said nozzle pressure ratio in order to alter said frequency of pressure oscillation to more nearly match said desired frequency of pressure oscillation.

11. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 9, further comprising adjusting the ratio h/d in order to alter said frequency of pressure oscillation to more nearly match said desired frequency of pressure oscillation.

13. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 8, wherein said step of adjusting said L/d ratio comprises:

a. providing a movable insert in said impingement block, said movable insert including said cavity floor and said at least one micronozzle; and

b. moving said movable insert with respect to said cavity entrance plane in order to vary L and thereby adjust said L/d ratio.

14. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 13, further comprising moving either said primary nozzle or said impingement block in order to adjust said ratio h/d.

15. A method for creating a microjet having a significant pressure oscillation, comprising:

a. providing a cylindrical cavity commencing at a cavity entrance plane;

b. providing a primary nozzle directing a primary jet having a diameter “

d”

into said cavity, said primary nozzle being separated from said cavity entrance plane by a distance “

h”

;

c. said cavity ending in a floor separated from said cavity entrance plane by a distance “

L”

;

d. providing at least one micronozzle extending from said cavity floor; and

e. adjusting the ratio L/d to produce a desired range of frequencies of pressure oscillation in said microjet.

16. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 15, further comprising adjusting said nozzle pressure ratio in order to alter said frequency of pressure oscillation to a desired frequency within said range of frequencies.

17. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 15, further comprising adjusting the ratio h/d in order to alter said frequency of pressure oscillation to a desired frequency within said range of frequencies.

18. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 16, further comprising adjusting the ratio h/d in order to alter said frequency of pressure oscillation to a desired frequency within said range of frequencies.

19. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 17, further comprising moving either said primary nozzle or said impingement block in order to adjust said ratio h/d.

20. A method for creating a microjet having a desired frequency of pressure oscillation as recited in claim 15, wherein said step of adjusting said L/d ratio comprises:

a. providing an impingement block to house said cylindrical cavity, said impingement block including a movable insert, said movable insert including said cavity floor and said at least one micronozzle; and

b. moving said movable insert with respect to said cavity entrance plane in order to vary L and thereby adjust said L/d ratio.