Method for surface stabilized combustion (SSC) of gaseous fuel/oxidant mixtures and a burner design thereof

Patent metadata

Field	Value
Publication number	US-10488039-B2
Application number	US-201615016469-A
Country	US
Kind code	B2
Filing date	Feb 5, 2016
Priority date	Feb 9, 2015
Publication date	Nov 26, 2019
Grant date	Nov 26, 2019

Abstract

Methods of burning combustible gas mixtures on a surface of a permeable matrix providing surface stabilized combustion (SSC) with increasing amounts of radiation energy emitted by the surface of the permeable matrix and decreasing concentrations of pollutant components in the combustion products are provided. The gas mixture is fed to a burner that includes a permeable matrix material having a first thermal conductivity. The gas mixture is preheated as it travels through the permeable matrix material. The gas mixture is then combusted at or near exit pores and channels formed at a combustion surface of the permeable matrix material, the combustion surface at least in part coated with a coating material having a thermal conductivity less than the permeable matrix material thermal conductivity and a high optical transmittance in the infrared spectrum.

First claim

The invention claimed is:

1. A method of burning a combustible gas mixture on a surface of a permeable matrix base material providing surface stabilized combustion (SSC), the method comprising:
feeding the gas mixture to a burner comprising a permeable matrix base material having a first thermal conductivity;
preheating the gas mixture as it travels through the permeable matrix base material; and
combusting the gas mixture at or near exit pores and channels formed in a combustion surface of the permeable matrix base material, the combustion surface at least in part coated with a coating material, the coating material having a thermal conductivity less than the permeable matrix base material thermal conductivity and is optically transparent to IR radiation,
wherein the surface of the permeable matrix base material at least in part coated with the coating material emits an increased amount of radiation energy and a decreased concentration of pollutant components in the combustion products as compared to the permeable matrix base material without the coating material;
wherein the burner comprises a ratio of thermal conductivity of the permeable matrix base material and to the coating material is from 3 to 10; and
wherein the coating material comprises a ceramic and wherein the coating is of a thickness of 10 to 500 microns and the permeable matrix base comprises a metal material.

2. The method of claim 1 wherein the permeable matrix base material is selected from the group consisting of chromal, kanthal, heat-resistant steel, carbide of titanium, aluminum, iron, chromium, yttrium and combinations thereof.

3. The method of claim 1 wherein the ceramic is selected from the group consisting of alumina, zirconia and combinations thereof.

4. The method of claim 1 additionally comprising maintaining heat flow from the combustion products to the combustion surface to avoid flame extinction and to provide steady state SSC.

5. The method of claim 1 wherein a combustion zone of the burner is transferred and stabilized at the combustible gas mixture exit from the permeable matrix base material to the coating material.

6. The method of claim 1 wherein the method additionally comprises removing radiation from the permeable matrix base material through the material coating material.

7. The method of claim 1 wherein the burner comprises the permeable matrix base material in a thickness of from 5 millimeters to 30 millimeters.

8. The method of claim 7 wherein the coating material comprises a ceramic and wherein the coating is of a thickness of 50 to 200 microns.

9. The method of claim 1 wherein the burner provides a heat flux density per permeable matrix base material radiation surface area of from 5 w/cm 2 to 200 w/cm 2 .

10. A high-infrared radiation ultra-low pollutants emission pre-mixed gas burner comprising:
a fuel inlet for receiving a gaseous fuel; an oxidizer inlet for receiving an oxidizer gas;
a mixer for mixing gaseous fuel and oxidizer gas producing a combustible gas mixture;
a permeable matrix base material providing surface stabilized combustion at the exit of this mixture by the pores and channels of the base material which is coated by a material optically transparent to IR radiation;
wherein the coating material comprises a ceramic and wherein the coating is of a thickness of 10 to 500 microns and the permeable matrix base comprises a metal material and
wherein the burner comprises a ratio of thermal conductivity of the permeable matrix base material and to the coating material is from 3 to 10.

11. A high-infrared radiation ultra-low pollutants emission pre-mixed gas burner as recited in claim 10 wherein the thickness of the permeable matrix base material is from 5 millimeters to 30 millimeters.

12. A high-infrared radiation ultra-low pollutants emission pre-mixed gas burner as recited in claim 10 wherein the heat flux density per permeable matrix base material radiation surface area provided by the burner is from 5 w/cm 2 to 200 w/cm 2 .

13. A high-infrared radiation ultra-low pollutants emission pre-mixed gas burner assembly comprising:
a fuel inlet for receiving a gaseous fuel;
an oxidizer inlet for receiving an oxidizer gas;
a chamber to ensure that gaseous fuel and oxidizer are produced into a proper combustible gas mixture;
a burner device to which the combustible gas mixture is introduced, the burner device having a permeable matrix base material providing surface stabilized combustion at the pores and channels of the boundary exit of this mixture to a base material coat layered with a material optically transparent to IR radiation and wherein the base material has a thermal conductivity of 3 to 10 times as great as the coating layer material thermal conductivity and
wherein the coating material comprises a ceramic and wherein the coating is of a thickness of 10 to 500 microns and the permeable matrix base comprises a metal material.

14. A high-infrared radiation ultra-low pollutants emission pre-mixed gas burner as recited in claim 13 wherein the thickness of the permeable matrix base material is from 5 millimeters to 30 millimeters.

15. A high-infrared radiation ultra-low pollutants emission pre-mixed gas burner as recited in claim 13 wherein the heat flux density per permeable matrix radiation surface area provided by the burner is from 5 w/cm 2 to 200 w/cm 2 .

Assignees

• SHMELEV Vladimir
• Vasilik Nikolay
• Khinkis Mark
• Kozlov Aleksandr
• Cygan David
• KALENSKY David
• Sutherland Brian
• Gas Technology Inst

Inventors

• SHMELEV Vladimir
• Vasilik Nikolay
• Khinkis Mark
• Kozlov Aleksandr
• Cygan David
• KALENSKY David
• Sutherland Brian

Classifications

• F23D14/08

  with axial outlets at the burner head · CPC title

• F23D14/84

  Flame spreading or otherwise shaping (F23D14/70 takes precedence) · CPC title

• F23D14/16

  using permeable blocks · CPC title

• F23D14/14

  using screens or perforated plates · CPC title

• F23D14/145 Primary

  combustion being stabilised at a screen or a perforated plate · CPC title