Solid fuel burner

Patent metadata

Field	Value
Publication number	US-10731850-B2
Application number	US-201615740482-A
Country	US
Kind code	B2
Filing date	Jun 22, 2016
Priority date	Jun 30, 2015
Publication date	Aug 4, 2020
Grant date	Aug 4, 2020

Abstract

A solid fuel burner is provided with a nozzle that is provided around the central axis of the burner, that includes a straight tube section having an opening opposed to a furnace, and a curved tube section continuous with the straight tube section, and that sprays out, from the opening to the furnace, a fluid mixture which is of a solid fuel and carrier gas of the solid fuel and which is flowing in the curved tube section; a first swirler that gives the fluid mixture a swirl at the burner central axis side of the straight tube section; and a second swirler that gives, at the burner central axis side downstream of the first swirler, the fluid mixture a swirl opposite to that given by the first swirler.

First claim

The invention claimed is:

1. A solid fuel burner provided in a throat of a wall surface of a furnace, comprising:
a fuel nozzle which includes a straight tube section provided around a burner central axis and having an opening toward the furnace and a curved tube section continued to the straight tube section, wherein a mixed fluid of a solid fuel and a carrier gas thereof supplied to the curved tube section is sprayed from the opening of the straight tube section to the furnace;
a first swirler which is provided on the burner central axis in the straight tube section, includes a plurality of vanes installed in the circumferential direction to apply a swirl to the mixed fluid; and
a second swirler which is provided on the burner central axis downstream in a flow direction of the mixed fluid of the first swirler in the straight tube section, includes a plurality of vanes disposed in the circumferential direction, and is installed in a direction reverse to a direction in which vanes of the first swirler are installed,
wherein the first swirler and the second swirler are provided away from an inner wall of the fuel nozzle, and are provided apart from each other on the burner central axis, and
wherein the second swirler is separated from the opening of the straight tube section so that the swirling flow of the mixed fluid is weakened or disappears.

2. The solid fuel burner according to claim 1 , wherein a flame stabilizer is provided on the outer periphery of the opening of the straight tube section.

3. The solid fuel burner according to claim 1 , wherein respective vanes of the second swirler are installed so that an installation angle of the respective vanes of the second swirler with respect to a burner central axis direction is equal to or smaller than the installation angle of the respective vanes of the first swirler with respect to the burner central axis direction.

4. The solid fuel burner according to claim 1 , wherein a radial length of the respective vanes of the second swirler is equal to or shorter than the radial length of respective vanes of the first swirler.

5. The solid fuel burner according to claim 1 , wherein a lateral width of respective vanes of the second swirler is the same as or smaller than the lateral width of respective vanes of the first swirler.

6. The solid fuel burner according to claim 1 , wherein a disperser for solid fuel particles is provided in the curved tube section.

7. The solid fuel burner according to claim 6 , wherein the disperser is installed on a lateral face of an oil burner provided on the burner central axis on a side facing a flow of the mixed fluid.

8. The solid fuel burner according to claim 2 , wherein respective vanes of the second swirler are installed so that an installation angle of the respective vanes of the second swirler with respect to a burner central axis direction is equal to or smaller than the installation angle of the respective vanes of the first swirler with respect to the burner central axis direction.

9. The solid fuel burner according to claim 2 , wherein a radial length of the respective vanes of the second swirler is equal to or shorter than the radial length of respective vanes of the first swirler.

10. The solid fuel burner according to claim 2 , wherein a lateral width of respective vanes of the second swirler is the same as or smaller than the lateral width of respective vanes of the first swirler.

11. The solid fuel burner according to claim 2 , wherein a disperser for solid fuel particles is provided in the curved tube section.

12. The solid fuel burner according to claim 3 , wherein a disperser for solid fuel particles is provided in the curved tube section.

13. The solid fuel burner according to claim 4 , wherein a disperser for solid fuel particles is provided in the curved tube section.

14. The solid fuel burner according to claim 5 , wherein a disperser for solid fuel particles is provided in the curved tube section.

Assignees

• Mitsubishi Hitachi Power Sys

Inventors

• Taniguchi Masayuki
• Baba Akira
• Kuramashi Koji
• Ishii Shota

Classifications

• F23D2201/20

  Fuel flow guiding devices · CPC title

• F23D1/02 Primary

  Vortex burners, e.g. for cyclone-type combustion apparatus · CPC title

• F23D2900/01001

  Pulverised solid fuel burner with means for swirling the fuel-air mixture · CPC title

• F23D1/00

  Burners for combustion of pulverulent fuel · CPC title

• F23D2201/10

  Nozzle tips · CPC title