IP Library › Granted Patent US 10,086,927
Granted Patent B2
US 10,086,927 · App. 15/131,393 · Granted Oct 2, 2018

Thermally controlled active flow control system

Inventors: Arvin Shmilovich (Huntington Beach, CA); Edward Andrew Whalen (St. Louis, MO)
Assignee: The Boeing Company
B64C21/04F15B21/12F15C1/00B64C2230/04B64C2230/06B64C2230/10B64C2230/18B64D2033/0213B64D2033/0226Y02T50/166Y10T137/87265
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Quick Facts
Patent No.
US 10,086,927
App. No.
15/131,393
Granted
Oct 2, 2018
Kind
B2
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.

Claims (46)

1. An active flow control system comprising:

a flow control valve configured to control a flow of air into a manifold;

the manifold operatively connected to a number of actuators;

a temperature control system configured to heat at least a portion of the flow of air; and

ductwork connected to a heater and running from the heater into a portion of the manifold, the ductwork extending inside the manifold to each of the number of actuators.

2. The active flow control system of claim 1 , wherein the temperature control system comprises:

a heater configured to heat at least the portion of the flow of air to form a heated portion.

3. The active flow control system of claim 2 , wherein the temperature control system further comprises:

a proportioning valve to direct the at least the portion of the flow of air towards the heater.

4. The active flow control system of claim 2 , wherein the temperature control system further comprises:

ductwork extending through a portion of the manifold, wherein the ductwork directs the heated portion towards the number of actuators.

5. The active flow control system of claim 4 , wherein the temperature control system further comprises:

a space between the ductwork and the manifold configured to insulate surrounding structures.

6. The active flow control system of claim 1 , further comprising:

an auxiliary power unit configured to provide the flow of air to the manifold.

7. The active flow control system of claim 1 , further comprising:

a flow proportioning valve configured to direct a portion of the flow of air to the heater.

8. The active flow control system of claim 7 , wherein the heater is configured to heat the portion of the flow of air received from the flow proportioning valve portion.

9. A method comprising:

controlling a flow of air into a manifold operatively connected to a number of actuators of an active flow control system;

heating at least a portion of the flow of air using a temperature control system to form a heated portion; and

directing the heated portion towards the number of actuators;

wherein ductwork connected to a heater runs from the heater into a portion of the manifold, the ductwork extending inside the manifold to each of the number of actuators.

10. The method of claim 9 , wherein heating the at least the portion of the flow of air using the temperature control system comprises:

routing the at least the portion of the flow of air towards a heater of the temperature control system using a proportioning valve of the temperature control system.

11. The method of claim 10 , wherein directing the heated portion towards the number of actuators comprises:

routing the heated portion using ductwork of the temperature control system, wherein the ductwork extends through a portion of the manifold, and wherein the ductwork directs the heated portion towards the number of actuators.

12. The method of claim 11 , wherein directing the heated portion towards the number of actuators further comprises:

directing a remainder of the flow of air through the manifold around the ductwork.

13. The method of claim 9 , wherein heating the at least the portion of the flow of air using the temperature control system to form the heated portion decreases a mass flow through the number of actuators.

14. The method of claim 9 , further comprising:

configuring an auxiliary power unit to provide the flow of air to the manifold.

15. The method of claim 9 , further comprising:

configuring a flow proportioning valve to direct a portion of the flow of air to the heater.

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;

wherein ductwork connected to a heater runs from the heater into a portion of a manifold, the ductwork extending inside the manifold to each of the number of actuators.

17. The method of claim 16 , wherein decreasing the mass flow comprises:

heating at least a portion of a flow of air in the active flow control system using a temperature control system.

18. The method of claim 17 , wherein the heating of the at least the portion of the flow of air comprises:

routing the at least the portion of the flow of air towards a heater of the temperature control system using a proportioning valve of the temperature control system.

19. The method of claim 16 , further comprising:

configuring an auxiliary power unit to provide a flow of air to the manifold.

20. The method of claim 19 , further comprising:

configuring a flow proportioning valve to direct a portion of the flow of air to the heater.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 18, 2016
From: SHMILOVICH, ARVIN; WHALEN, EDWARD ANDREW
To: THE BOEING COMPANY
Reel/Frame 038307/0390 →
Continuity (1)
Related Publication 20170297680A1 · Oct 19, 2017
Cited By (1)
US 12,663,028