Thermally controlled active flow control system

Patent metadata

Field	Value
Publication number	US-10988240-B2
Application number	US-201816102179-A
Country	US
Kind code	B2
Filing date	Aug 13, 2018
Priority date	Apr 18, 2016
Publication date	Apr 27, 2021
Grant date	Apr 27, 2021

Abstract

A method and apparatus are presented. An active flow control system comprises a flow control valve, a manifold, and a temperature control system. The flow control valve is configured to control a flow of air into the manifold. The manifold is operatively connected to a number of actuators. The temperature control system is configured to heat at least a portion of the flow of air.

First claim

What is claimed is:

1. An active flow control system that comprises:
a flow control valve configured to control a flow of air into a manifold;
the manifold operatively connected to a number of actuators such that each actuator, respectively, comprises an entry that narrows to an inlet to a trifurcated chamber that converges to an outlet that comprises a diameter that increases;
a temperature control system that comprises a power source and resistive heater strips operatively connected to the power source, wherein the resistive heater strips are positioned in a portion of the manifold; and
a controller programmed to deliver a power to the resistive heater strips that, responsive to a decrease in a mass flow rate of the air flow in the manifold, raises a temperature of an air flow entering the actuator and sustains a desired momentum in a flow of air out the outlet of the actuator.

2. The active flow control system of claim 1 , wherein the temperature control system further comprises heater material within each of the number of actuators.

3. The active flow control system of claim 1 further comprising:
insulation between the manifold and surrounding structures.

4. The active flow control system of claim 1 , wherein the temperature control system comprises a heater material that lines a vertical wall in at least one actuator of the number of actuators.

5. The active flow control system of claim 4 , wherein the temperature control system further comprises a heater material that lines a bottom wall in the trifurcated chamber.

6. The active flow control system of claim 4 , wherein the temperature control system further comprises a heater material that lines a top wall in at least one actuator of the number of actuators.

7. The active flow control system of claim 6 , wherein the temperature control system further comprises a program configured to control a mass flow rate into an actuator of the number of actuators.

8. A method comprising:
controlling a flow of air into a manifold operatively connected to a number of actuators of an active flow control system; and
heating at least a portion of the flow of air using a temperature control system and forming a heated portion via controlling, responsive to a decrease in a mass flow rate of the air flow in the manifold, a power to resistive heater strips and raising a temperature of an air flow entering an inlet to an actuator in the number of actuators and sustaining a desired momentum in a flow of air out an outlet of the actuator.

9. The method of claim 8 , further comprising providing power to the resistive heater strips positioned in ductwork leading into the number of actuators.

10. The method of claim 9 , wherein directing the heated portion towards the number of actuators comprises the manifold comprising separate ductwork into each actuator in the number of actuators.

11. The method of claim 10 , wherein directing the heated portion towards the number of actuators further comprises directing the flow of the air through the manifold into the separate ductwork, and then each actuator, respectively, of the number of actuators.

12. The method of claim 8 , wherein heating the at least the portion of the flow of air using the temperature control system further comprises controlling power to a heater material lining surfaces inside the actuator.

13. The method of claim 12 , wherein heating the at least the portion of the flow of air using the temperature control system further comprises controlling power to a heater material lining surfaces of vertical walls inside the actuator.

14. The method of claim 8 , further comprising the flow of air generating from an auxiliary power unit.

15. The method of claim 8 , further comprising providing power to the resistive heater strips positioned in ductwork common to the number of actuators.

16. A method comprising:
providing active flow control having a desired momentum using an active flow control system having a number of actuators; and
decreasing a mass flow through the number of actuators while maintaining the desired momentum from the number of actuators, via heating at least a portion of a flow of air into the number of actuators via providing power to resistive heater strips positioned in a portion of a manifold of the active flow control system.

17. The method of claim 16 , wherein decreasing the mass flow comprises:
heating the at least the portion of the flow of air in the active flow control system using a temperature control system.

18. The method of claim 16 , wherein the heating of the at least the portion of the flow of air comprises locating a resistive heater strip where a ductwork enters into an actuator.

19. The method of claim 16 , wherein the heating the at least the portion of the flow of air comprises:
providing power to resistive heater strips positioned in a second portion of a manifold of the active flow control system.

20. The method of claim 16 , wherein the number of actuators exceeds two.

Assignees

• Boeing Co

Inventors

• Shmilovich Arvin
• Whalen Edward Andrew

Classifications

• B64D2033/0213

  specially adapted for auxiliary power units (APU's) · CPC title

• Y10T137/87265

  Dividing into parallel flow paths with recombining · CPC title

• F15B21/0427

  Heating · CPC title

• Y02T50/10

  Drag reduction · CPC title

• B64C2230/10

  by influencing fluid flow by heating using other means than combustion · CPC title