Methods and apparatus for controlling flow fields

Patent metadata

Field	Value
Publication number	US-10907669-B2
Application number	US-201916676003-A
Country	US
Kind code	B2
Filing date	Nov 6, 2019
Priority date	Apr 25, 2016
Publication date	Feb 2, 2021
Grant date	Feb 2, 2021

Abstract

Methods and systems for controlling a fluid flow field near a surface are disclosed. In some embodiments, the system includes an array of oscillating bodies disposed on the surface to provide physical modification to the flow field. Fluid jets are also emitted from an outlet in the oscillating body to provide virtual modification of the flow field through momentum addition. Fluid jet sources, including synthetic jet generators such as piezoelectric drivers and sources of compressed fluids such as air or water, are positioned to be in fluid communication with the outlet at intervals during the oscillation of the oscillating body. Controlling the oscillation amplitude and frequency of the body, as well as the location of oscillating body outlets and frequency of fluid jet emission, have advantageous effects for the surface such as improved heat transfer properties and reduction in structural vibration and noise.

First claim

What is claimed is:

1. A method of manipulating a flow field over a surface comprising:
providing a body having a fluid jet outlet;
oscillating said body in said flow field; and
emitting a fluid jet from said fluid jet outlet into said flow field.

2. The method of manipulating a flow field according to claim 1 , wherein said fluid jet is generated from a compressed fluid source, a synthetic jet generator, an external flow stream, or a combination thereof.

3. The method of manipulating a flow field according to claim 1 , wherein providing a body having a fluid jet outlet further comprises:
providing an array of bodies including a first body and at least one adjacent second body; and
oscillating said first body at a first amplitude, frequency, and phase; and oscillating said adjacent second body at a second amplitude, frequency, and phase.

4. An actuator assembly for controlling a flow field over a surface comprising:
a body extending at least partially through said surface, wherein the body is configured to oscillate at least one of vertically, horizontally, and rotationally relative to said surface at a predetermined frequency in said flow field;
an oscillator, said oscillator positioned to oscillate a body; and
wherein the body includes a fluid jet outlet, and said fluid jet outlet is shaped to emit a fluid jet to said flow field at a predetermined flow path and predetermined flow velocity.

5. The actuator assembly according to claim 4 , a fluid jet source in fluid communication with said fluid jet outlet; wherein said fluid jet source is a compressed fluid, a synthetic jet generator, an external flow stream, or a combination thereof.

6. The actuator assembly according to claim 5 , further comprising:
a wall and an interior cavity defined in said body, said wall including a first opening; and
a compartment for releasably retaining said compressed fluid, said compartment having a fluid jet source opening;
wherein at first predetermined intervals during body oscillation, said compartment for releasably retaining said compressed fluid and said interior cavity are in fluid communication via said first opening in said wall and said fluid jet source opening and said compartment is in fluid communication with said fluid jet outlet.

7. The actuator assembly according to claim 6 , further comprising a second interior cavity and a second wall opening, wherein said compartment and said second interior cavity are in fluid communication via said second wall opening, and said compartment is in fluid communication with said fluid jet outlet at second predetermined intervals during body oscillation.

8. The actuator assembly according to claim 5 , further comprising an opening in said surface adjacent said body, wherein said opening is in fluid communication with said fluid jet source at least once per oscillation of said body.

9. The actuator assembly according to claim 4 , wherein said body includes a wall and an end, wherein said fluid jet outlet is positioned on said wall or said end.

10. The actuator assembly according to claim 9 , said body further comprising:
a shape that is cylindrical, prismatic, or a combination thereof;
an end having a conformation, said conformation being flat, convex, concave, angled, or a combination thereof.

11. The actuator assembly according to claim 9 , wherein one of said wall and said end are dynamically modified by said fluid jet, said dynamic modification being inflation, deflation, expansion, contraction, translation, bulging, caving, or a combination thereof.

12. The actuator assembly according to claim 5 , wherein said synthetic jet generator is a piezoelectric driver, movement of the oscillating body itself, an electromagnetic driver, a mechanically vibrated membrane, or a combination thereof.

13. The actuator assembly according to claim 4 , wherein said fluid jet outlet is circular.

14. The actuator assembly according to claim 4 , wherein said fluid jet outlet is positioned to direct said fluid jet at an oblique angle relative to at least one of said flow field and said surface.

15. The actuator assembly according to claim 9 , wherein said fluid jet outlet is positioned at a particular height on said wall, wherein said particular height is at least less than about 95 percent of a total height of said wall as measured from said surface.

16. The actuator assembly according to claim 4 , further comprising an array of bodies.

17. An actuator assembly for controlling a flow field over a surface comprising:
a surface;
an array of oscillating bodies positioned in said surface, said array of oscillating bodies configured to oscillate relative to said surface at a predetermined frequency, each of said oscillating bodies further comprising a wall and a fluid jet outlet positioned on said wall; and
a fluid jet source in fluid communication with said fluid jet outlet,
wherein said fluid jet outlet is positioned to direct a fluid jet at predetermined intervals during body oscillation at an angle between about 0 degrees to about 45 degrees relative to at least one of said flow field and said surface.

18. The actuator assembly according to claim 17 , wherein said array of oscillating bodies is arranged in a streamwise direction.

19. The actuator assembly according to claim 17 , said fluid jet source is a compressed fluid, a synthetic jet generator, an external flow stream, or a combination thereof.

20. An actuator assembly according to claim 19 , wherein a first oscillating body in said array of oscillating bodies oscillates at a first amplitude, frequency, and phase; and an adjacent second oscillating body in said array of oscillating bodies oscillates at a second amplitude, frequency, and phase.

Assignees

• Rensselaer Polytech Inst

Inventors

• Amitay Michael
• Gildersleeve Samantha

Classifications

• Y02T50/10

  Drag reduction · CPC title

• B64C2230/18

  by using small jets that make the fluid flow oscillate · CPC title

• B64C2230/04

  by actively generating fluid flow · CPC title

• F15D1/12 Primary

  by influencing the boundary layer · CPC title

• B64C2230/06

  by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure · CPC title