Exhaust impingement cooling

Patent metadata

Field	Value
Publication number	US-9995181-B2
Application number	US-201113307741-A
Country	US
Kind code	B2
Filing date	Nov 30, 2011
Priority date	Nov 30, 2011
Publication date	Jun 12, 2018
Grant date	Jun 12, 2018

Abstract

An exhaust impingement cooling device for reducing heating effects of an exhaust plume on an impinged surface. An exhaust nozzle exit screen is positioned across an exhaust plume flow path, and includes a plurality of flowpath diverging apertures that spread at least a portion of an exhaust plume that is being emitted along the exhaust plume flow path from an exhaust plume source. Flow control jets are arrayed within the exhaust plume flow path in respective positions where their operation will augment the flow of exhaust plume gases through the screen, thereby increasing the momentum and mixing of the exhaust plume with cooler ambient air.

First claim

What is claimed is:

1. An exhaust impingement cooling device for reducing heating effects of an exhaust plume on an impinged surface, the device comprising:
an exhaust nozzle exit screen positioned across an exhaust plume flow path, and including a plurality of flowpath diverging apertures configured to spread at least a portion of an exhaust plume that is being emitted along the exhaust plume flow path from an exhaust plume source; and
a plurality of flow control jets arrayed within the exhaust plume flow path in respective positions where their operation will entrain a flow of exhaust plume gases through the exhaust nozzle exit screen, thereby increasing the momentum and mixing of the exhaust plume with cooler ambient air.

2. An exhaust impingement cooling device as defined in claim 1 in which the exhaust nozzle exit screen is configured to spread the exhaust plume radially outward relative to a central plume axis.

3. An exhaust impingement cooling device as defined in claim 1 in which the exhaust nozzle exit screen is configured to spread the exhaust plume away from one or more imaginary planes parallel to and intersecting the plume axis.

4. An exhaust impingement cooling device as defined in claim 1 in which the exhaust nozzle exit screen is configured to spread the exhaust plume in one or more preferred directions.

5. An exhaust impingement cooling device as defined in claim 1 in which the flow control jets are distributed across the exhaust plume flow path upstream of the exhaust nozzle exit screen.

6. An exhaust impingement cooling device as defined in claim 5 in which the flow control jets are mounted at an optimum distance upstream from the exhaust nozzle exit screen to minimize the amount of impedance the jets introduce when they are not actively augmenting mass flow.

7. An exhaust impingement cooling device as defined in claim 5 in which the control jets comprise zero-net-mass-flux (ZNMF) actuators.

8. An exhaust impingement cooling device as defined in claim 5 in which the device includes a flow control actuator configured to selectively actuate the control jets to force air through the exhaust nozzle exit screen when necessary or desirable to overcome flow impedance, and to shut off the control jets when jet actuation is not necessary or desirable to overcome flow impedance.

9. An exhaust impingement cooling device as defined in claim 5 in which the control jets are configured to provide pulsed flow injections.

10. An exhaust impingement cooling device as defined in claim 8 in which the flow control actuator is a pulsing actuator connected to the control jets and configured to selectively pulse the control jets.

11. An exhaust impingement cooling device as defined in claim 10 in which the flow control actuator is configured to sequence the control jets.

12. An exhaust impingement cooling device as defined in claim 10 in which the flow control actuator is configured to pulse the control jets in unison.

13. An exhaust impingement cooling device as defined in claim 1 in which at least one of the flow control jets is spaced from any wall or walls defining the exhaust plume flow path.

Assignees

• Miller Daniel N
• Domel Neal D
• Baruzzini Dan J
• Lockheed Corp

Inventors

• Miller Daniel N
• Domel Neal D
• Baruzzini Dan J

Classifications

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F01D25/305 Primary

  with fluid, e.g. liquid injection · CPC title

• F02K1/40

  Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet · CPC title

• F02K1/822

  Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors · CPC title

• Y02T50/672

  Cross-Sectional Technologies · mapped topic