Nozzle wall for an air-breathing engine of a vehicle and method therefor

Patent metadata

Field	Value
Publication number	US-11060484-B2
Application number	US-201816023411-A
Country	US
Kind code	B2
Filing date	Jun 29, 2018
Priority date	Jun 29, 2018
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

A nozzle wall for an air-breathing engine, the nozzle wall including a first wall surface subject to engine exhaust flow, a nozzle cooling system including at least one heat exchange fluid passage disposed adjacent the first wall surface so as to increase a temperature of a cooling fluid flowing from a fluid reservoir to at least a power extraction device, and the cooling fluid is ejected from the nozzle cooling system downstream from the power extraction device.

First claim

What is claimed is:

1. A method for operating a vehicle, the method comprising:
transferring, with a coolant pump, a cooling fluid from a fluid reservoir to a first cooling subsystem of a nozzle cooling system;
transferring heat to the cooling fluid from a nozzle of an air-breathing engine of the vehicle using the first cooling subsystem of the nozzle cooling system coupled to the nozzle, where the cooling fluid flows from the fluid reservoir through the first cooling subsystem to at least a power extraction device, and where the power extraction device is separate and distinct from the coolant pump and engine thrust exhaust flow exits the air-breathing engine through the nozzle; and
ejecting the cooling fluid from the nozzle cooling system downstream from the power extraction device, wherein the cooling fluid is physically separated from and distinct from fluid flow through the air-breathing engine until after the cooling fluid is ejected from the nozzle cooling system, wherein the cooling fluid is one of: (a) ejected, during operation of the air-breathing engine, from an exhaust collector of the power extraction device to an external environment without combusting the cooling fluid in the engine exhaust flow or (b) ejected through the nozzle to effect film cooling of the nozzle.

2. The method of claim 1 , further comprising: receiving the cooling fluid from the first cooling subsystem in a second cooling subsystem, of the nozzle cooling system, coupled to both the nozzle and the first cooling subsystem; and ejecting the cooling fluid, from the second cooling subsystem, through the nozzle effecting film cooling of a first wall surface of the nozzle subject to engine thrust exhaust flow.

3. The method of claim 2 , further comprising: sensing, with at least one sensor, one or more of a temperature, a pressure, and a vapor quality of the cooling fluid within one or more of the first cooling subsystem and the second cooling subsystem; and controlling, with a controller coupled to the coolant pump and the at least one sensor, the coolant pump based on signals received from the at least one sensor.

4. The method of claim 3 , further comprising: effecting, with the controller and an expansion valve, conversion of the cooling fluid from a liquid phase to a gas phase based on the signals received from the at least one sensor, where the expansion valve is coupled to the controller and is disposed between, so as to be in fluid communication with, the first cooling subsystem and the second cooling subsystem.

5. A nozzle wall cooling system for an air-breathing engine, the nozzle wall cooling system comprising:
a first wall surface of a nozzle wall, the first wall surface being subject to engine exhaust flow;
a fluid reservoir containing a cooling fluid;
at least one heat exchange fluid passage disposed adjacent the first wall surface;
a coolant pump coupled between the fluid reservoir and the at least one heat exchange fluid passage; and
wherein:
the at least one heat exchange fluid passage is configured to increase a temperature of the cooling fluid flowing from the fluid reservoir to at least a power extraction device, the power extraction device being separate and distinct from the coolant pump; and
the nozzle wall cooling system is configured such that the cooling fluid is physically separated from and distinct from fluid flow through the air-breathing engine until after the cooling fluid is ejected from the nozzle wall cooling system downstream from the power extraction device, through the first wall surface of the nozzle wall to effect film cooling of the first wall surface.

6. The nozzle wall cooling system of claim 5 , wherein the nozzle wall cooling system further includes a plurality of film cooling apertures defined by and extending through at least the first wall surface so that the plurality of film cooling apertures eject the cooling fluid as power extraction device exhaust gas at the first wall surface to effect film cooling of the first wall surface.

7. The nozzle wall cooling system of claim 6 , further comprising a second wall surface wherein the plurality of film cooling apertures are defined by and extend through the first wall surface and the second wall surface.

8. The nozzle wall cooling system of claim 6 , wherein one or more of the at least one heat exchange fluid passage is disposed upstream of one or more of the plurality of film cooling apertures relative to a flow direction of the engine exhaust flow.

9. The nozzle wall cooling system of claim 6 , wherein one or more of the at least one heat exchange fluid passage is disposed downstream of one or more of the plurality of film cooling apertures relative to a flow direction of the engine exhaust flow.

10. The nozzle wall cooling system of claim 6 , wherein the at least one heat exchange fluid passage and the plurality of film cooling apertures are alternately arranged relative to each other in a direction substantially parallel with a flow direction of the engine exhaust flow.

11. The nozzle wall cooling system of claim 5 , wherein the nozzle wall further comprises: an upstream end, relative to a flow direction of the engine exhaust flow, defined at least by the first wall surface; and a downstream end defined at least by the first wall surface and disposed downstream from the upstream end.

12. The nozzle cooling system wall of claim 11 , wherein the at least one heat exchange fluid passage comprises a first heat exchange fluid passage and a second heat exchange fluid passage, wherein the first heat exchange fluid passage is configured to increase the temperature of the cooling fluid flowing through the first heat exchange fluid passage in liquid phase, and the second heat exchange fluid passage is coupled to the first heat exchange fluid passage and is configured to increase another temperature of the cooling fluid flowing through the second heat exchange fluid passage in gas phase.

13. A vehicle comprising:
an air-breathing engine having a nozzle wherein engine thrust exhaust flow exits the air-breathing engine through the nozzle;
a nozzle cooling system including:
a fluid reservoir configured to contain a cooling fluid,
a power extraction device,
a first cooling subsystem coupled to the nozzle so as to transfer heat from the nozzle to the cooling fluid flowing from the fluid reservoir to at least the power extraction device, and
a coolant pump coupled between the fluid reservoir and the first cooling subsystem where the coolant pump is separate and distinct from the power extraction device and configured to transfer the cooling fluid from the fluid reservoir to the first cooling subsystem along a flow path that is physically separated and distinct from a flow path of fluid through the air-breathing engine; and
wherein the cooling fluid is physically separated from and distinct from fluid flow through the air-breathing engine until after the cooling fluid is ejected from the nozzle cooling system downstream from the power extraction device, through the nozzle to effect film cooling of the nozzle.

14. The vehicle of claim 13 , wherein: the nozzle includes a first wall surface; and the first cooling subsystem includes at least one heat exchange fluid passage disposed adjacent the first wall surface so as to increase a temperature of the cooling fluid flowing from the fluid reservoir to the power extraction device.

15. The vehicle of claim 13 , wherein the nozzle cooling system further includes a second cooling subsystem coupled to both the nozzle and the first cooling subsystem, wherein the second cooling subsystem is configured to receive the

Assignees

• Boeing Co

Inventors

• Silkey Joseph S
• Franklin Timothy H
• Dyer Richard S

Classifications

• B64D33/04

  of exhaust outlets or jet pipes · CPC title

• F05D2260/202

  by film cooling · CPC title

• B64D2033/026

  for supersonic or hypersonic aircraft · CPC title

• B64D41/00

  Power installations for auxiliary purposes · CPC title

• Y02T50/60

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