Rotating detonation combustion and heat exchanger system

Patent metadata

Field	Value
Publication number	US-11255544-B2
Application number	US-201916701521-A
Country	US
Kind code	B2
Filing date	Dec 3, 2019
Priority date	Dec 3, 2019
Publication date	Feb 22, 2022
Grant date	Feb 22, 2022

Abstract

A rotating detonation combustion (RDC) system is provided. The RDC includes a first outer wall and a second outer wall each extended around a centerline axis, and a detonation chamber formed radially inward of the second outer wall. A fuel passage extended between the first outer wall and the second outer wall, the fuel passage including a first inlet opening proximate to the aft end through which a flow of fuel is received into the fuel passage. The flow of fuel is provided through the fuel passage from the aft end to the forward end of the RDC system and to the detonation chamber.

First claim

What is claimed is:

1. A rotating detonation combustion (RDC) system, the system defining an aft end at which detonation gases exit and a forward end at which a flow of oxidizer enters, the RDC system comprising:
a first outer wall and a second outer wall each extended around a centerline axis;
a detonation chamber formed radially inward of the second outer wall;
a fuel passage extended between the first outer wall and the second outer wall, wherein the fuel passage comprises a first inlet opening proximate to the aft end through which a flow of fuel is received into the fuel passage, and wherein the flow of fuel is provided through the fuel passage from the aft end to the forward end of the RDC system;
a forward plenum positioned in serial flow arrangement between the fuel passage and a fuel injector in fluid communication with the fuel passage, the forward plenum extended at least partially circumferentially relative to the centerline axis;
a fuel bypass circuit in fluid communication with the forward plenum, wherein the fuel bypass circuit is configured to egress at least a portion of the flow of fuel from egressing the fuel injector opening into the detonation chamber; and
an egress valve positioned at the fuel bypass circuit, wherein the egress valve is configured to selectively egress the flow of fuel from the forward plenum through the fuel bypass circuit.

2. The RDC system of claim 1 , wherein the first outer wall and the second outer wall together fluidly separate the flow of fuel from the detonation chamber.

3. The RDC system of claim 1 , wherein at least a portion of a flow of fuel egresses from the fuel passage through the fuel injector into the detonation chamber.

4. The RDC system of claim 3 , wherein the fuel injector is positioned at the forward end of the system.

5. The RDC system of claim 1 , wherein the fuel passage is extended at least partially circumferentially around the centerline axis.

6. The RDC system of claim 1 , wherein the fuel passage is extended helically around the centerline axis.

7. The RDC system of claim 1 , wherein at least a portion of the fuel passage is configured to provide the flow of fuel in counter-flow arrangement relative to a flow of detonation gases in the detonation chamber.

8. The RDC system of claim 1 , comprising:
a bypass supply valve positioned at the forward end of the RDC system, wherein the bypass supply valve is configured to selectively provide a second flow of fuel to the fuel injector.

9. The RDC system of claim 1 , wherein the first outer wall and the second outer wall together define an aft plenum proximate to the aft end in fluid communication with the first inlet opening, wherein the aft plenum is extended annularly between the first outer wall and the second outer wall.

10. The RDC system of claim 9 , further comprising an internal wall extended between the first outer wall and the second outer wall, wherein the internal wall is further extended at least partially along a axial direction, and wherein the internal wall separates the fuel passage into two or more fuel passages.

11. The RDC system of claim 1 , wherein the first outer wall defines the first inlet opening therethrough in fluid communication with the fuel passage.

12. A heat engine, the heat engine comprising:
a compressor section configured to provide a flow of oxidizer to a rotating detonation combustion (RDC) system;
the RDC system defining an aft end at which detonation gases exit a detonation chamber and a forward end at which the flow of oxidizer enters the detonation chamber, the RDC system comprising a first outer wall and a second outer wall each extended around a centerline axis;
wherein the detonation chamber is formed radially inward of the second outer wall;
wherein a fuel passage is extended between the first outer wall and the second outer wall, the fuel passage comprising a first inlet opening proximate to the aft end through which a flow of fuel is received into the fuel passage, and wherein the flow of fuel is provided through the fuel passage from the aft end to the forward end of the RDC system;
a fuel injector positioned at the forward end of the RDC system in fluid communication with the fuel passage and the detonation chamber;
a bypass supply valve positioned at the forward end of the RDC system; and
a control circuit, the control circuit comprising:
a first sensor configured to receive one or more of a first parameter of a first flow of fuel; and
a second sensor configured to receive one or more of a second parameter of a second flow of fuel, wherein the control circuit provides the first parameter and the second parameter to the bypass supply valve, the bypass supply valve configured to selectively provide the second flow of fuel to the fuel injector based at least on the first parameter and the second parameter.

13. The heat engine of claim 12 , wherein the control circuit is configured to selectively open the bypass supply valve to mix the second flow of fuel with the first flow of fuel to generate a third parameter corresponding to the flow of fuel egressed from the fuel injector.

14. The heat engine of claim 12 , wherein the control circuit is configured to selectively open the bypass supply valve to mix the second flow of fuel with the first flow of fuel when the first flow of fuel is above a first threshold.

15. The heat engine of claim 12 , wherein the control circuit is configured to selectively close the bypass supply valve to only egress the first flow of fuel from the fuel injector when the first flow of fuel is below a second threshold.

Assignees

• Gen Electric

Inventors

• Dyson Thomas Earl
• Lavertu Thomas Michael
• Monahan Sarah Marie
• Singh Kapil Kumar
• Tangirala Venkat Eswarlu
• Haynes Joel Meier

Classifications

• F02C9/28

  Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title

• F02C7/224

  Heating fuel before feeding to the burner · CPC title

• F23R7/00 Primary

  Intermittent or explosive combustion chambers · CPC title

• F23R3/005

  Combined with pressure or heat exchangers · CPC title

• F02C5/02

  characterised by the arrangement of the combustion chamber in the chamber in the plant (combustion chambers per se F23R) · CPC title