Combustor having a nonmetallic body with external electrodes

Patent metadata

Field	Value
Publication number	US-10161625-B2
Application number	US-201615012842-A
Country	US
Kind code	B2
Filing date	Feb 1, 2016
Priority date	Jul 30, 2013
Publication date	Dec 25, 2018
Grant date	Dec 25, 2018

Abstract

A combustor may include a nonmetallic combustor body configured to hold a combustion reaction. The combustor may include and one or more electrodes disposed outside the nonmetallic combustor body and configured to apply electrical energy to the combustion reaction. The combustor may include a power supply operatively coupled to the one or more electrodes.

First claim

What is claimed is:

1. A combustor, comprising:
a nonmetallic combustor body having an inner surface and an outer surface defining at least a portion of a combustion volume aligned to carry a combustion reaction with flow in a longitudinal direction, the nonmetallic combustor body inner surface defining a lateral periphery of the combustion volume between an input end configured to receive combustion air and an output end configured to output combustion products, the nonmetallic combustor body being configured to prevent passage of gas from inside the combustion volume to outside the combustion volume between the input end and the output end of the nonmetallic combustor body;
at least one electrode disposed outside the combustion volume with the nonmetallic combustor body lying at least partially between the at least one electrode and the combustion volume; and
a power supply operatively coupled to the at least one electrode;
an electrically conductive shield disposed between a portion of the outer surface of the nonmetallic combustor body and the at least one electrode; and
at least one port formed in the nonmetallic combustor body;
wherein the at least one port is configured to allow passage of a flow of air or flue gas from a volume proximate to the at least one electrode and outside the combustion body and the electrically conductive shield into the combustion volume;
wherein the at least one electrode includes a corona electrode configured to eject ions into the flow of air or flue gas;
wherein the at least one port is configured to allow the passage of the ions from the volume proximate the at least one electrode into the combustion volume; and
wherein the at least one electrode is configured to apply electrical energy to the combustion volume.

2. The combustor of claim 1 , wherein the power supply is configured to at least intermittently apply one or more voltages to the at least one electrode.

3. The combustor of claim 1 , wherein the combustor is configured to provide a flow of cooling air along the outer surface of the nonmetallic combustor body.

4. The combustor of claim 1 , wherein the nonmetallic combustor body is configured to protect the at least one electrode from heat evolved from the combustion reaction.

5. The combustor of claim 1 , wherein the nonmetallic combustor body comprises:
a dielectric material.

6. The combustor of claim 5 , wherein the nonmetallic combustor body comprises:
a material having a dielectric constant less than 20.

7. The combustor of claim 6 , wherein the nonmetallic combustor body comprises:
a material having a dielectric constant less than 12.

8. The combustor of claim 1 , wherein the nonmetallic combustor body is formed from a material that is semiconducting at room temperature and/or semiconducting at an operating temperature of the nonmetallic combustor body.

9. The combustor of claim 1 , wherein the nonmetallic combustor body is formed at least partly from a ceramic.

10. The combustor of claim 9 , wherein the ceramic includes silicon carbide.

11. The combustor of claim 1 , wherein the nonmetallic combustor body is formed at least partly from at least one selected from the group consisting of alumina, silica, an aerogel, fused quartz glass, sapphire, hafnium diboride (HfB2), zirconium diboride (ZrB2), hafnium nitride (HfN), zirconium nitride (ZrN), titanium carbide (TiC), titanium nitride (TiN), thorium dioxide (ThO2), and tantalum carbide (TaC).

12. The combustor of claim 1 , further comprising:
a power supply controller configured to cause the power supply to apply a DC voltage to the at least one electrode.

13. The combustor of claim 1 , further comprising:
a power supply controller configured to cause the power supply to apply a time-varying voltage to the at least one electrode.

14. The combustor of claim 1 , wherein applying electrical energy to the combustion volume includes applying an electric field to the combustion volume.

15. The combustor of claim 1 , wherein applying electrical energy to the combustion volume includes providing charged particles to the combustion volume.

16. The combustor of claim 1 , wherein the combustion reaction is configured to at least intermittently carry particles having a charge, and wherein the at least one electrode is configured to carry a voltage configured to impart, on the charged particles, an electric field selected to move the charged particles at a velocity component at an angle off-axis to the longitudinal direction defined by the nonmetallic combustor body.

17. The combustor of claim 1 , wherein electrical energy is selected to increase a rate of the combustion reaction.

18. The combustor of claim 1 , wherein electrical energy is selected to decrease an amount of oxides of nitrogen (NOx) evolved from the combustion reaction.

19. The combustor of claim 1 , wherein electrical energy is selected to decrease an amount of carbon monoxide (CO) evolved from the combustion reaction.

20. The combustor of claim 1 , wherein the at least one electrode includes a corona electrode configured to eject ions into the flow of air or flue gas.

21. A gas turbine apparatus, comprising:
a compressor configured to compress air;
a combustor configured to receive compressed air from the compressor and support a combustion reaction using oxygen from the compressed air;
a turbine configured to receive a heated combustion gas from the combustor and convert a portion of heat energy of the heated combustion gas into rotational kinetic energy;
a turbine shaft operatively coupled to the turbine and the compressor and configured to transmit at least a portion of the rotational kinetic energy from the turbine to the compressor;
wherein the combustor further comprises:
a nonmetallic combustor body having an inner surface and an outer surface defining at least a portion of a combustion volume aligned to carry the combustion reaction with flow in a longitudinal direction, the nonmetallic combustor body inner surface defining a lateral periphery of the combustion volume between an input end configured to receive combustion air and an output end configured to output combustion products, the nonmetallic combustor body being configured to prevent passage of gas from inside the combustion volume to outside the combustion volume between the input end and the output end of the nonmetallic combustor body;
at least one electrode disposed outside the combustion volume with the nonmetallic combustor body lying at least partially between the at least one electrode and the combustion volume; and
a power supply operatively coupled to the at least one electrode;

wherein the at least one electrode is configured to apply electrical energy to the combustion volume;
an electrically conductive shield disposed between a portion of the outer surface of the nonmetallic combustor body and the at least one electrode; and
at least one port formed in the nonmetallic combustor body;
wherein the at least one port is configured to allow passage of a flow of air or flue gas from a volume proximate to the at least one electrode and outside the combustion body and the electrically conductive shield into the combustion volume;
wherein the at least one electrode includes a corona electrode configured to eject ions into the flow of air or flue gas; and
wherein the at least one port is configured to allow the passage of the ions from the volume proximate the at least one electrode into the combustion volume.

22. The g

Assignees

• Clearsign Comb Corp

Inventors

• Krichtafovitch Igor A
• Colannino Joseph
• Breidenthal Robert E
• Goodson David B
• Wiklof Christopher A

Classifications

• F23R3/16

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

• F23M2900/05004

  Special materials for walls or lining · CPC title

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title

• F23C99/001 Primary

  Applying electric means or magnetism to combustion (for combustion engines F02B51/04, F02M27/04) · CPC title

• F23M20/00

  Details of combustion chambers, not otherwise provided for {, e.g. means for storing heat from flames} · CPC title