Surface combustion burner, composite burner, and ignition device for sintering machine

Patent metadata

Field	Value
Publication number	US-11635204-B2
Application number	US-201816489516-A
Country	US
Kind code	B2
Filing date	Mar 22, 2018
Priority date	Mar 27, 2017
Publication date	Apr 25, 2023
Grant date	Apr 25, 2023

Abstract

Provided is a surface combustion burner which solves the passage blocking in a combustion part caused by dust, and enables stable combustion for a long term. The surface combustion burner comprises: a nozzle configured to discharge fuel gas and air for combustion; and a laminate, provided on a tip of the nozzle, in which a plurality of mesh plates is laminated, wherein the laminate includes a portion having an offset arrangement between at least any adjacent ones of the mesh plates.

First claim

The invention claimed is:

1. A surface combustion burner comprising:
a nozzle; and
a laminate in which a plurality of mesh plates are laminated, wherein
the nozzle comprises:
an outer nozzle configured to discharge fuel gas and air for combustion from at least one nozzle hole on a downstream side of the outer nozzle; and
an inner nozzle, that is located in the outer nozzle, configured to discharge the air for combustion from at least one nozzle hole toward the at least one nozzle holes of the outer nozzle,

the laminate is disposed flush against the outer nozzle over an entire surface of a downstream side of the outer nozzle such that the laminate forms an outermost surface of a combustion burner and covers all the nozzle holes of the outer nozzle,
the laminate has four or more of the mesh plates,
the laminate includes a portion having an offset arrangement between at least any adjacent ones of the mesh plates,
the laminate is positioned such that flame forms on an external most surface of the laminate,
the laminate has an opening ratio of 8% or less, and
each mesh plate of the plurality of mesh plates has an opening ratio of 30%-85%.

2. The surface combustion burner according to claim 1 , wherein the laminate has a lamination interval of 2 mm or less, the lamination interval being defined as a distance between mid-thickness positions of adjacent ones of the mesh plates.

3. The surface combustion burner according to claim 1 , wherein each mesh plate of the plurality of mesh plates has mesh lines with a diameter of 0.2 mm to 2 mm.

4. The surface combustion burner according to claim 1 , wherein each mesh plate of the plurality of mesh plates has openings with an average span of 1 mm to 5 mm.

5. The surface combustion burner according to claim 1 , wherein each mesh plate of the plurality of mesh plates is a metal mesh.

6. A surface combustion burner comprising:
a nozzle;
woven metal fibers that; and
a laminate in which a plurality of mesh plates are laminated, wherein
the nozzle comprises:
an outer nozzle configured to discharge fuel gas and air for combustion from at least one nozzle hole on a downstream side of the outer nozzle; and
an inner nozzle, that is located in the outer nozzle, configured to discharge the air for combustion from at least one nozzle hole toward the at least one nozzle hole of the outer nozzle,

the woven metal fibers are disposed flush against the outer nozzle over an entire surface of a downstream side of the outer nozzle and covers all the nozzle holes of the outer nozzle,
the laminate is disposed flush against the woven metal fibers such that the laminate forms an outermost surface of the combustion burner,
the laminate has four or more of the mesh plates,
the laminate includes a portion having an offset arrangement between at least any adjacent ones of the mesh plates,
the laminate is positioned such that flame forms on an external most surface of the laminate,
the laminate has an opening ratio of 8% or less, and
each mesh plate of the plurality of mesh plates has an opening ratio of 30%-85%.

7. A surface combustion burner comprising:
a nozzle;
a heat resistant material; and
a laminate in which a plurality of mesh plates are laminated, wherein
the nozzle comprises:
an outer nozzle configured to discharge fuel gas and air for combustion from at least one nozzle hole on a downstream side of the outer nozzle; and
an inner nozzle, that is located in the outer nozzle, configured to discharge the air for combustion from at least one nozzle hole toward the at least one nozzle hole of the outer nozzle,

the heat resistant material is disposed flush against the outer nozzle over an entire surface of a downstream side of the outer nozzle and covers all the nozzle holes of the outer nozzle,
the laminate is disposed flush against the heat resistant material such that the laminate forms an outermost surface of the combustion burner,
the laminate has four or more of the mesh plates,
the laminate includes a portion having an offset arrangement between at least any adjacent ones of the mesh plates,
the laminate is positioned such that flame forms on an external most surface of the laminate,
the laminate has an opening ratio of 8% or less, and
each mesh plate of the plurality of mesh plates has an opening ratio of 30%-85%.

8. The surface combustion burner according to claim 7 , wherein the heat resistant material has a thickness of 3 mm to 20 mm.

9. The surface combustion burner according to claim 7 , wherein
the heat resistant material is a material in which particulate heat resistant materials are layered.

Assignees

• Jfe Steel Corp

Inventors

• HORIKAWA Yukimasa
• Hara Kazuaki
• Iwata Koji
• Fujiwara Hiromichi

Classifications

• F23D14/149

  with wires, threads or gauzes as radiation intensifying means · CPC title

• F23D14/145 Primary

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

• F23D14/02 Primary

  Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone · CPC title

• F23D2203/002

  Radiant burner mixing tubes · CPC title

• F23D14/58

  characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration · CPC title