Systems, apparatuses and methods for improved rotating detonation engines

Patent metadata

Field	Value
Publication number	US-11592183-B2
Application number	US-202017022616-A
Country	US
Kind code	B2
Filing date	Sep 16, 2020
Priority date	Sep 22, 2016
Publication date	Feb 28, 2023
Grant date	Feb 28, 2023

Abstract

Rotating detonation engines are provided with various improvements pertaining to performance and reliability. Improvements pertain to, for example, a fluidic valve/premixing chamber, injection/swirl, flow control and turning, ignition, and cooling. A rotating detonation engine can include a cylindrical inner shell within an outer housing, a cylindrical outer shell positioned between the inner shell and the outer housing, an annular gap between the outer shell and the outer housing functioning as a detonation chamber.

First claim

The invention claimed is:

1. A rotating detonation engine, comprising:
a cylindrical outer housing including a front end, a rear end, and a central longitudinal axis that extends between the front and rear ends;
a head mount mounted to the front end of the cylindrical outer housing, the head mount including injection ports configured to deliver fuel and oxidizer to the rotating detonation engine, coolant inflow holes configured to deliver coolant to the rotating detonation engine, and a coolant outflow hole configured to deliver coolant from the rotating detonation engine;
a cylindrical inner shell contained within the cylindrical outer housing, the inner shell including a central coolant return channel that extends along the central longitudinal axis of the housing that is in fluid communication with the coolant outflow hole of the head mount;
a cylindrical outer shell positioned between the inner shell and the cylindrical outer housing;
a first annular gap formed between the outer shell and the cylindrical outer housing, the first annular gap functioning as a detonation chamber configured to facilitate continuous detonation of a mixture of fuel and oxidizer; and
a second annular gap formed between the inner shell and the outer shell radially inward of the detonation chamber, the second annular gap functioning as a coolant supply channel, the second annular gap being in fluid communication with the coolant inflow holes of the head mount and the central coolant return channel of the inner shell,
wherein, during operation of the rotating detonation engine, coolant can circulate through the coolant inflow holes of the head mount and the front end of the cylindrical outer housing, through the second annular gap formed between the inner and outer shells toward the rear end of the housing radially inward of the detonation chamber, through the central coolant return channel of the inner shell also radially inward of the detonation chamber back toward the front end of the housing, and through the coolant outflow hole of the head mount to provide cooling to a center region of the rotating detonation engine.

2. The rotating detonation engine of claim 1 , wherein the injection ports of the head mount are axial injection ports extending at an angle greater than 0° and less than 90° relative to the central longitudinal axis of the cylindrical outer housing.

3. The rotating detonation engine of claim 2 , wherein each injection port is (1) straight, (2) contoured converging-diverging, or (3) conical converging-diverging.

4. The rotating detonation engine of claim 1 , wherein the cylindrical outer housing further includes a coolant inlet hole and a coolant outlet hole formed through a side of the housing and auxiliary coolant channels formed within the housing that are in fluid communication with the inlet and outlet holes, wherein the auxiliary coolant channels provide additional cooling to the rotating detonation engine.

5. The rotating detonation engine of claim 1 , wherein the head mount further includes a mixing chamber in fluid communication with the injection ports.

6. The rotating detonation engine of claim 5 , wherein the mixing chamber is configured as an annular recess formed in an inner side of the head mount.

7. The rotating detonation engine of claim 6 , further comprising an injection plate positioned between the mixing changer and the second annular gap, the injection plate including a plurality of injection holes through which the fuel and oxidizer can pass to reach the first annular gap.

8. The rotating detonation engine of claim 1 , further comprising an end cap mounted to ends of the inner and outer shells.

9. The rotating detonation engine of claim 8 , wherein the inner shell further includes mounting legs to which the end cap is mounted.

10. The rotating detonation engine of claim 9 , wherein gaps between the legs of the inner shell form coolant recirculation ports that provide flow paths between the second annular gap and the central coolant return channel.

11. The rotating detonation engine of claim 1 , further comprising an igniter connected to the cylindrical outer housing and configured to ignite a mixture of the fuel and oxidizer within the first annular gap.

12. The rotating detonation engine of claim 11 , wherein the igniter is a pulse detonation engine.

Assignees

• Univ Texas

Inventors

• Mizener Andrew R
• Lu Frank K

Classifications

• F23R7/00 Primary

  Intermittent or explosive combustion chambers · CPC title

• F02K1/002

  with means to modify the direction of thrust vector (F02K1/54 takes precedence; thrust vectoring of rockets F02K9/80) · CPC title

• F02C3/165

  the combustion chamber contributes to the driving force by creating reactive thrust · CPC title

• F02K7/04

  with resonant combustion chambers · CPC title

• F02K9/66 Primary

  of the rotary type · CPC title