Solid-fuel burner

Patent metadata

Field	Value
Publication number	US-9599335-B2
Application number	US-201314421003-A
Country	US
Kind code	B2
Filing date	Aug 9, 2013
Priority date	Aug 14, 2012
Publication date	Mar 21, 2017
Grant date	Mar 21, 2017

Abstract

A solid-fuel burner includes: a venturi having a constricting portion where the transverse cross section of a fuel passage is reduced in a fuel nozzle for supplying a solid fuel; and a fuel concentrator for diverting the flow in the nozzle outward in the wake side of the venturi, and the nozzle is formed so that (a) the aperture in the vicinity of an opening portion of a boiler furnace wall surface has a flat shape, (b) cross-sectional shape thereof orthogonal to a nozzle center axis C on the outer peripheral wall of the nozzle is circular in a transverse cross section up to the constricting portion of the venturi, (c) a portion that has a gradually increasing degree of flatness is provided between the constricting portion and the opening portion, and (d) the flat shape in the opening portion is where the degree of flatness reaches a maximum.

First claim

What is claimed is:

1. A solid-fuel burner comprising:
a fuel nozzle that opens into an opening portion of a furnace wall, the fuel nozzle comprising:
a solid-fuel passage;
a venturi, having a constricting portion with an outlet, that reduces a transverse cross section of the solid-fuel passage in the fuel nozzle;
an upper wall and a lower wall that each extend in a straightforward direction toward the furnace wall from the outlet of the constricting portion of the venturi to the opening portion of the furnace wall; and
a fuel concentrator that diverts flow in the fuel nozzle outward on a wake side of the venturi,

a cylindrical fuel carrier piping, through which a mixed fluid of a solid fuel and a carrier gas for the solid fuel is configured to flow, is connected to the solid-fuel passage of the fuel nozzle;
at least one combustion gas nozzle is provided on an outer peripheral wall side of the fuel nozzle; and
a wind box, in which a combustion gas for the solid fuel is configured to flow, is provided on the outer peripheral wall side of the fuel nozzle and is in fluid communication with the at least one combustion gas nozzle, wherein
the fuel nozzle has a cross-sectional shape orthogonal to a nozzle center axis of an outer peripheral wall of the fuel nozzle,
the cross-sectional shape of the fuel nozzle is flattened at an opening of the fuel nozzle proximate to the opening portion in the furnace wall,
the cross-sectional shape of the fuel nozzle is circular up to the constricting portion of the venturi,
a degree of flatness of the cross-section shape of the fuel nozzle and a width of the fuel nozzle in a horizontal direction gradually increases from the constricting portion of the venturi to the opening of the fuel nozzle and reach a maximum degree of flatness and a maximum width in the horizontal direction at the opening of the fuel nozzle, and
the upper wall and the lower wall of the fuel nozzle are spaced from each other by a constant predetermined distance from the outlet of the constricting portion of the venturi to the opening portion of the furnace wall.

2. The solid-fuel burner according to claim 1 , wherein a flame stabilizer is disposed at an outer periphery of a tip of the outer peripheral wall of the fuel nozzle.

3. The solid-fuel burner according to claim 1 , wherein
the at least one combustion gas nozzle is a secondary combustion gas nozzle of a plurality of combustion gas nozzles, and
a secondary combustion gas passage is provided in the secondary combustion gas nozzle disposed on an innermost side of the plurality of combustion gas nozzles and has a cross-sectional shape orthogonal to a center axis of an outer peripheral wall of the secondary combustion gas nozzle, the cross-sectional shape of the secondary combustion gas nozzle is flattened at an outlet portion of the secondary combustion gas passage.

4. The solid-fuel burner according to claim 3 , wherein
the plurality of combustion gas nozzles includes a tertiary combustion gas nozzle, and
a tertiary combustion gas passage is provided in the tertiary combustion gas nozzle and is disposed on an outermost side in the plurality of combustion gas nozzles and has a cross-sectional shape orthogonal to a center axis of an outer peripheral wall of the tertiary combustion gas nozzle, the cross-sectional shape of the tertiary combustion gas nozzle is circular at an outlet portion of the tertiary combustion gas passage near the furnace wall.

5. The solid-fuel burner according to claim 3 , wherein the cross-sectional area of the secondary combustion gas passage is sequentially reduced from a combustion gas inflow portion of the secondary combustion gas passage toward the opening portion in the furnace wall.

6. The solid-fuel burner according to claim 5 , wherein a gas inflow direction of the combustion gas inflow portion of the secondary combustion gas passage is a direction vertical to the furnace wall, and
a flat plate having a plurality of opening portions is arranged in the combustion gas inflow portion of the secondary combustion gas passage.

7. The solid-fuel burner according to claim 6 , wherein the plurality of opening portions of the flat plate arranged in the combustion gas inflow portion of the secondary combustion gas passage are arranged in such a manner that a flow velocity of the combustion gas in the secondary combustion gas passage becomes uniform in a circumferential direction of the passage.

8. The solid-fuel burner according to claim 6 , wherein an aperture ratio of the plurality of opening portions of the flat plate relative to a cross-sectional area of the combustion gas inflow portion of the secondary combustion gas passage is 0.05 to 0.30.

9. The solid-fuel burner according to claim 5 , wherein a reduction ratio of a cross-sectional area of the secondary combustion gas passage from the combustion gas inflow portion to the outlet portion of the secondary combustion gas passage is 30% to 80%.

10. The solid-fuel burner according to claim 1 , wherein
a flame detector and a pilot torch are disposed on one of:
respective ends of an outlet of the fuel nozzle that emits the solid fuel and the solid fuel carrier gas when the outlet of the fuel nozzle is a rectangular shape,
respective focuses when the outlet of the fuel nozzle is an elliptical shape, and
on respective ends of a linear portion when the outlet of the fuel nozzle is a substantially elliptical shape having the linear portions and circular portions.

Assignees

• Mitsubishi Hitachi Power Sys

Inventors

• Mine Toshihiko
• Kiyama Kenji
• Shimogori Miki
• Tadakuma Satoshi
• Wakamatsu Hitoshi
• Ohyatsu Noriyuki
• Kuramashi Koji
• Ochi Kenichi
• Ochi Yusuke
• Okazaki Hirofumi

Classifications

• F23C7/008

  Flow control devices (F23C7/006 takes precedence) · CPC title

• F23D1/00 Primary

  Burners for combustion of pulverulent fuel · CPC title

• F23K2203/201

  using pneumatic means · CPC title

• F23D2201/20

  Fuel flow guiding devices · CPC title

• F23L9/06

  by discharging the air into the fire bed · CPC title