Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices

Patent metadata

Field	Value
Publication number	US-10794329-B2
Application number	US-201615366876-A
Country	US
Kind code	B2
Filing date	Dec 1, 2016
Priority date	Nov 27, 2013
Publication date	Oct 6, 2020
Grant date	Oct 6, 2020

Abstract

An exhaust plume cooling device for cooling an exhaust gas plume to reduce deleterious heat effects on impinged and surrounding surfaces. The device is supportable in a position downstream of an exhaust nozzle of an exhaust gas plume-producing engine and configured to periodically interrupt the flow of exhaust gases by injecting fluid into the exhaust plume zone.

First claim

What is claimed is:

1. An exhaust plume cooling device for cooling an exhaust gas plume to reduce deleterious heat effects on impinged and surrounding surfaces, the device comprising:
an injector supportable in a position adjacent an exhaust nozzle of an engine and aimed into an exhaust plume zone that is occupied by an exhaust plume when the engine is running, the injector being aimed upstream relative to the flow of the exhaust plume; and
a flow generator that is connected to and in fluid communication with the injector and generates and periodically transmits fluid flow through the injector into the exhaust plume zone at a rate and duty cycle that forms exhaust gas pulses that form vortical structures that entrain currents of ambient air.

2. An exhaust plume cooling device for cooling an exhaust gas plume to reduce deleterious heat effects on impinged and surrounding surfaces, the device comprising:
a plurality of injectors supportable in respective circumferentially-spaced positions around an exhaust nozzle of an engine and aimed into an exhaust plume zone that is occupied by an exhaust plume when the engine is running, the injectors being aimed upstream relative to the flow of the exhaust plume; and
a flow generator that is connected to and in fluid communication with each injector of the plurality of injectors and generates and transmits fluid flow through the injectors into the exhaust plume zone; and
a flow controller that is connected to and is in fluid communication with the flow generator and each injector of the plurality of injectors, and periodically and simultaneously causes fluid to be emitted through the injectors into the exhaust plume zone at a rate and at a duty cycle that forms exhaust gas pulses that form vortical structures that entrain currents of ambient air.

3. The exhaust plume cooling device as defined in claim 2 in which the injectors are aimed radially inward into the exhaust plume zone.

4. The exhaust plume cooling device as defined in claim 3 in which each of the injectors is aimed upstream at an elevation angle in the range of −45 to +45 degrees as measured upstream from a plane parallel to an exit plane of the exhaust nozzle.

5. A method for cooling an exhaust gas plume to reduce deleterious heat effects on impinged and surrounding surfaces by periodically interrupting a flow of exhaust gases by injecting fluid into an exhaust plume zone that is occupied by an exhaust plume of an engine when the engine is running, such that the injected fluid restricts the flow of exhaust gases at a rate and duty cycle that forms exhaust gas pulses that form vortical structures that entrain currents of ambient air wherein the step of injecting fluid into the exhaust plume zone includes injecting fluid in an upstream direction, relative to the flow of the exhaust plume, from circumferentially-spaced positions around the exhaust plume zone.

6. The method of claim 5 in which the step of injecting fluid into the exhaust plume zone includes injecting fluid radially inward into the exhaust plume zone from the circumferentially-spaced positions around the exhaust plume zone.

7. The method of claim 6 in which the step of injecting fluid into the exhaust plume zone includes injecting fluid upstream, relative to the flow of the exhaust plume, from the circumferentially-spaced positions at respective elevation angles in the range of −45 to +45 degrees as measured upstream from a plane parallel to an exit plane of an exhaust nozzle from which the plume is emitted.

Assignees

• Lockheed Corp

Inventors

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

Classifications

• F02C7/12

  Cooling of plants (of component parts, see the relevant subclasses, e.g. F01D; cooling of engines in general F01P) · CPC title

• B64D2041/002

  Mounting arrangements for auxiliary power units (APU's) · CPC title

• F02K1/28

  using fluid jets to influence the jet flow · CPC title

• B64D41/00

  Power installations for auxiliary purposes · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title