Phase tailoring for resonant flow devices

Patent metadata

Field	Value
Publication number	US-10605280-B2
Application number	US-201615344520-A
Country	US
Kind code	B2
Filing date	Nov 6, 2016
Priority date	Nov 6, 2016
Publication date	Mar 31, 2020
Grant date	Mar 31, 2020

Abstract

A device including a resonant array of a plurality of synthetic jet generators where neighboring jet generators are coupled, resulting in the potential for constructive and destructive interference between jets of the plurality of synthetic jet generators depending on the relative phase of a corresponding plurality of drive signals to plurality of synthetic jet generators. The device also includes a controller configured to control the relative phase of the corresponding plurality of drive signals to effect a change in a first jet emitted by a first synthetic jet generator of the plurality of synthetic jets by changing a given phase of a second jet emitted by a second synthetic jet generator of the plurality of synthetic jet generators.

First claim

What is claimed is:

1. A device comprising:
a resonant array of a plurality of synthetic jet generators where neighboring jet generators are coupled, resulting in the potential for constructive and destructive interference between jets of the plurality of synthetic jet generators depending on a relative phase of a corresponding plurality of drive signals to the plurality of synthetic jet generators; and
a controller configured to control the relative phase of the corresponding plurality of drive signals to effect a change in a first jet emitted by a first synthetic jet generator of the plurality of synthetic jet generators by changing a given phase of a second jet emitted by a second synthetic jet generator of the plurality of synthetic jet generators, wherein the given phase is different from a phase of the first jet emitted by the first synthetic jet generator of the plurality of synthetic jet generators.

2. The device of claim 1 , wherein the given phase is configured to cause a larger amplitude in each of the jets than is possible with a single jet.

3. The device of claim 1 , wherein a resulting velocity profile of the jets is shaped depending on the relative phases to each j et generator of the plurality of synthetic j et generators.

4. The device of claim 1 , wherein the second jet will only change when the first synthetic jet generator is driven.

5. The device of claim 1 further comprising:
an aircraft connected to the plurality of synthetic jet generators; and
a sensor connected to the aircraft and configured to detect local aerodynamic stall characteristics of a fluid flow on a body of the aircraft, and wherein the controller is further configured to adjust the first jet by changing a phase angle of the second jet generator to mitigate the local aerodynamic stall characteristics.

6. A device comprising:
a first synthetic j et generator configured to generate a first synthetic j et;
a second synthetic jet generator coupled to the first synthetic jet generator and configured to generate a second synthetic jet;
a controller coupled to both the first synthetic j et generator and the second synthetic jet generator, wherein the controller is configured to:
transmit a first drive signal to the first synthetic jet generator;
transmit a second drive signal to the second synthetic jet generator; and
control a combined operation of the first synthetic jet generator and the second synthetic jet generator by controlling a relative phase difference between the first drive signal and the second drive signal.

7. The device of claim 6 , wherein the controller is further configured to control operation of the first synthetic jet generator by controlling only the relative phase difference.

8. The device of claim 6 , wherein the controller is further configured to control operation of the first synthetic jet generator by transmitting only the second drive signal.

9. The device of claim 6 further comprising:
a feedback circuit coupled to the first synthetic jet generator, the second synthetic j et generator, and the controller, and wherein the controller is further configured to use a feedback signal from the feedback circuit to control the first synthetic jet generator and the second synthetic jet generator to produce a predetermined velocity profile of a combination of the first synthetic jet and the second synthetic jet.

10. The device of claim 9 further comprising:
a housing containing the first synthetic jet generator, the second synthetic jet generator, and the controller;
an aircraft connected to the housing; and
a sensor connected to the aircraft and configured to detect local aerodynamic stall characteristics of a fluid flow on a body of the aircraft, and wherein the controller is further configured to mitigate the local aerodynamic stall characteristics by producing the predetermined velocity profile.

11. The device of claim 6 , wherein the controller is further configured to drive both the first synthetic jet generator and the second synthetic jet generator at a single constant voltage amplitude.

12. The device of claim 6 , wherein the controller is further configured to increase both a first maximum velocity of the first synthetic jet and a second maximum velocity of the second synthetic jet by changing the relative phase difference.

13. The device of claim 12 , wherein the relative phase difference is about one hundred and eighty degrees.

14. A method comprising:
generating a first synthetic jet using a first synthetic jet generator;
generating a second synthetic jet using a second synthetic jet generator that is coupled to the first synthetic jet generator;
controlling, using a controller coupled to both the first synthetic jet generator and the second synthetic jet generator, the first synthetic jet and the second synthetic jet, wherein controlling includes:
transmitting a first drive signal to the first synthetic jet generator;
transmitting a second drive signal to the second synthetic jet generator; and
controlling a combined operation of the first synthetic jet and the second synthetic jet by adjusting a phase difference between the first drive signal and the second drive signal.

15. The method of claim 14 , wherein the controller is further configured to control operation of the first synthetic jet generator by controlling only the phase difference.

16. The method of claim 14 further comprising:
producing a predetermined velocity profile of a combination of the first synthetic jet and the second synthetic jet using a feedback signal from a feedback circuit, the feedback circuit coupled to the first synthetic jet generator, the second synthetic jet generator, and the controller.

17. The method of claim 16 further comprising:
detecting, using a sensor connected to an aircraft, local aerodynamic stall characteristics of a fluid flow on a body of the aircraft; and
mitigating, using a combined operation of the first synthetic jet and the second synthetic jet, the local aerodynamic stall characteristics by producing the predetermined velocity profile.

18. The method of claim 14 further comprising:
driving both the first synthetic jet generator and the second synthetic jet generator at a single constant voltage amplitude.

19. The method of claim 14 further comprising:
increasing both a first maximum velocity of the first synthetic jet and a second maximum velocity of the second synthetic jet by changing the phase difference.

20. The method of claim 19 , wherein the phase difference is about one hundred and eighty degrees.

Assignees

• Boeing Co

Inventors

• Brzozowski Daniel Paul
• Griffin Steven Fulton

Classifications

• B64C2230/18

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

• B64C23/06

  by generating vortices · CPC title

• B64C21/08

  adjustable · CPC title

• B64C21/025 Primary

  for simultaneous blowing and sucking · CPC title

• F15D1/0095 Primary

  by means of injecting jet pulses of fluid wherein the injected fluid is taken from the fluid and re-injected again, e.g. synthetic jet actuators (F15D1/008 takes precedence) · CPC title