Rotating detonation engine upstream wave arrestor

Patent metadata

Field	Value
Publication number	US-10436110-B2
Application number	US-201715470783-A
Country	US
Kind code	B2
Filing date	Mar 27, 2017
Priority date	Mar 27, 2017
Publication date	Oct 8, 2019
Grant date	Oct 8, 2019

Abstract

A rotating detonation engine includes an annulus that defines a volume in which a mixture of an oxidizer and a fuel detonate in a rotating fashion, the volume defining a downstream outlet through which detonation exhaust flows. The rotating detonation engine further includes a wave arrestor positioned upstream from a location of detonation and configured to reduce a magnitude of a pressure wave traveling upstream from the location of detonation.

First claim

What is claimed is:

1. A rotating detonation engine, comprising:
an annulus that defines a volume in which a mixture of an oxidizer and a fuel detonate in a rotating fashion in which a detonation travels clockwise or counterclockwise along a circumference of the annulus, the volume defining a downstream outlet through which detonation exhaust flows; and
a wave arrestor positioned upstream from a location of detonation and configured to reduce a magnitude of a pressure wave traveling upstream from the location of detonation.

2. The rotating detonation engine of claim 1 , wherein the wave arrestor is positioned within the volume.

3. The rotating detonation engine of claim 1 , wherein the wave arrestor is positioned upstream from the volume.

4. The rotating detonation engine of claim 1 , wherein the wave arrestor includes a plurality of obstacles configured to reflect at least some of the pressure wave downstream.

5. The rotating detonation engine of claim 4 , wherein the annulus includes an inner cylinder and an outer cylinder that define the volume, and wherein the plurality of obstacles extend from the inner cylinder to the outer cylinder.

6. The rotating detonation engine of claim 4 , wherein the annulus includes an inner cylinder and an outer cylinder that define the volume, and wherein the plurality of obstacles extend partially from the inner cylinder to the outer cylinder.

7. The rotating detonation engine of claim 1 , wherein the wave arrestor includes a first main channel through which the pressure wave travels and a first channel splitter configured to split the first main channel into multiple sub-channels such that the pressure wave is split into sub-waves that each propagate through one of the multiple sub-channels.

8. The rotating detonation engine of claim 7 , wherein the wave arrestor further includes a second main channel and a second channel splitter configured to combine the multiple sub-channels into the second main channel, and wherein the multiple sub-channels each have a different length such that the sub-waves propagate through the second main channel at different times.

9. The rotating detonation engine of claim 1 , wherein the wave arrestor includes a main channel having a downstream portion and an upstream portion that has a greater cross-sectional area than the downstream portion such that the pressure wave expands in response to reaching the upstream portion, resulting in the magnitude of the pressure wave decreasing.

10. The rotating detonation engine of claim 1 , wherein the wave arrestor includes a main channel having a textured surface that reduces the magnitude of the pressure wave.

11. A rotating detonation engine, comprising:
an oxidizer outlet configured to output an oxidizer;
a fuel outlet configured to output a fuel;
an annulus that defines a volume in which a mixture of the oxidizer and the fuel detonate in a rotating fashion in which a detonation travels clockwise or counterclockwise along a circumference of the annulus, the volume defining a downstream outlet through which detonation exhaust flows; and
a wave arrestor positioned upstream from a location of detonation and configured to reduce a magnitude of a pressure wave traveling upstream from the location of detonation.

12. The rotating detonation engine of claim 11 , wherein the wave arrestor includes a plurality of obstacles configured to reflect at least some of the pressure wave downstream.

13. The rotating detonation engine of claim 12 , wherein the annulus includes an inner cylinder and an outer cylinder that define the volume, and wherein the plurality of obstacles extend from the inner cylinder to the outer cylinder.

14. The rotating detonation engine of claim 12 , wherein the annulus includes an inner cylinder and an outer cylinder that define the volume, and wherein the plurality of obstacles extend partially from the inner cylinder to the outer cylinder.

15. The rotating detonation engine of claim 11 , wherein the wave arrestor includes a first main channel through which the pressure wave travels and a first channel splitter configured to split the first main channel into multiple sub-channels such that the pressure wave is split into sub-waves that each propagate through one of the multiple sub-channels.

16. The rotating detonation engine of claim 15 , wherein the wave arrestor further includes a second main channel and a second channel splitter configured to combine the multiple sub-channels into the second main channel, and wherein the multiple sub-channels each have a different length such that the sub-waves propagate through the second main channel at different times.

17. The rotating detonation engine of claim 11 , wherein the wave arrestor includes a main channel having a downstream portion and an upstream portion that has a greater cross-sectional area than the downstream portion such that the pressure wave expands in response to reaching the upstream portion, resulting in the magnitude of the pressure wave decreasing.

18. The rotating detonation engine of claim 11 , wherein the wave arrestor includes a main channel having a textured surface that reduces the magnitude of the pressure wave.

19. A gas turbine engine, comprising:
a turbine section configured to convert detonation exhaust into torque;
a compressor section configured receive the torque from the turbine section and to utilize the torque to compress fluid; and
a rotating detonation engine configured to generate the detonation exhaust and having:
an annulus that defines a volume in which a mixture of an oxidizer and a fuel detonate in a rotating fashion in which a detonation travels clockwise or counterclockwise along a circumference of the annulus, the volume defining a downstream outlet through which the detonation exhaust flows, and
a wave arrestor positioned upstream from a location of detonation and configured to reduce a magnitude of a pressure wave traveling upstream from the location of detonation.

20. The gas turbine engine of claim 19 , wherein the wave arrestor includes a plurality of obstacles configured to reflect at least some of the pressure wave downstream.

Assignees

• United Technologies Corp

Inventors

• Holley Adam Takashi
• Cocks Peter A T
• Greene Christopher Britton

Classifications

• F23R3/16

  with devices inside the flame tube or the combustion chamber to influence the air or gas flow · CPC title

• F42B1/02

  Shaped or hollow charges (blasting cartridges with cavities in the charge F42B3/08; oil winning using shaped-charge perforators E21B43/116) · CPC title

• F02C5/12

  the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants · CPC title

• F02C5/04 Primary

  the combustion chambers being formed at least partly in the turbine rotor · CPC title

• F02C7/00 Primary

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title