Swirl burner with fuel injection upstream and downstream of the swirler

Patent metadata

Field	Value
Publication number	US-10741855-B2
Application number	US-201515537351-A
Country	US
Kind code	B2
Filing date	Dec 2, 2015
Priority date	Dec 19, 2014
Publication date	Aug 11, 2020
Grant date	Aug 11, 2020

Abstract

The present invention is concerned with improved swirl burners, particularly, but not limited to, swirl burners used in fuel cell systems.

First claim

The invention claimed is:

1. A swirl burner assembly comprising:
(i) a hollow longitudinally elongate body extending along a central axis and having a hollow longitudinally elongate body first end and a hollow longitudinally elongate body second end,
(ii) an end wall at said hollow longitudinally elongate body first end,
(iii) a burner wall located between said hollow longitudinally elongate body first end and said hollow longitudinally elongate body second end, and defining a first volume from said hollow longitudinally elongate body first end to said burner wall, and a second volume from said burner wall to said hollow longitudinally elongate body second end,
(iv) an oxidant inlet into said first volume,
(v) at least one hollow longitudinally elongate burner unit having a burner unit first end extending outwardly of an opening in said body from said first volume, the burner unit extending through an opening in said burner wall from said first volume to said second volume to a burner unit second end, and defining a burner unit inner volume, and comprising:
(a) an axial-swirl swirl mixer positioned inward of the burner unit and located between said burner unit first end and said burner unit second end, said swirl mixer comprising a plurality of vanes having an inner diameter and an outer diameter, a first side which is positioned towards and opening into said first volume, and a second side positioned towards and opening into said second volume,
(b) a first fuel inlet into said first volume, said first fuel inlet positioned between said oxidant inlet and said swirl mixer and radially inward of said outer diameter of said plurality of vanes, said first fuel inlet having a first fuel inlet flow area, and
(c) a second fuel inlet into said second volume proximal said burner unit second end and radially inward of said outer diameter of said plurality of vanes,

where each at least one burner unit:
(A) defines a first point which is the point along said central axis closest to said hollow longitudinally elongate body first end where a plane perpendicular to said central axis intersects said plurality of vanes of said swirl mixer;
(B) defines a second point which is the point along said central axis furthest from said hollow longitudinally elongate body first end where a plane perpendicular to said central axis intersects said plurality of vanes of said swirl mixer; and
(C) defines a geometric mid-point along said central axis equidistant from said first point and said second point,

wherein:
each first fuel inlet is located at a point between said oxidant inlet and said swirl mixer which intersects with a plane perpendicular to said central axis, and which plane intersects with a point along said central axis between 1 and 2 equivalent circular diameters of said first fuel inlet flow area from said first point, and
each second fuel inlet is located at a point between said first fuel inlet and said hollow longitudinally elongate body second end which intersects with a plane perpendicular to said central axis, and which plane intersects with a point along said central axis equal to or less than said inner diameter of said plurality of vanes from said geometric mid-point.

2. The swirl burner assembly according to claim 1 , at least one burner unit further comprising:
i) an outer collar extending through said opening in said burner wall from said first volume toward said second volume, said outer collar having an outer collar outer diameter, an outer collar inner diameter, an outer collar first end and an outer collar second end; and
ii) comprises an inner collar extending through said opening in said burner wall from said first volume toward said second volume, said inner collar having an inner collar outer diameter, an inner collar inner diameter, an inner collar first end and an inner collar second end.

3. The swirl burner assembly according to claim 2 , wherein said inner collar is located radially internal to said outer collar.

4. The swirl burner assembly according to claim 2 , wherein said plurality of vanes extend radially between said outer collar and said inner collar, and said outer collar inner diameter is equal to said outer diameter of the plurality of vanes and said inner collar outer diameter is equal to said inner diameter of the plurality of vanes.

5. The swirl burner assembly according to claim 1 , wherein said first and second fuel inlets are each located at points radially inward of the inner diameter of the plurality of vanes.

6. The swirl burner assembly according to claim 1 , said body being multi-walled, said multiple walls extending from said burner wall to said hollow longitudinally elongate body second end, and comprising:
an inner wall having an inner surface, said second volume being defined between said burner wall, said hollow longitudinally elongate body second end and said inner wall inner surface; and
(ii) an outer wall located outwards of said inner wall, a third volume being defined between said burner wall, said inner wall, said outer wall and said hollow longitudinally elongate body second end,

said burner wall additionally comprising at least one bypass opening between said first volume and said third volume and defining a fluid flow path, wherein said bypass opening is a channel in fluid flow communication from said first volume to said third volume.

7. The swirl burner assembly according to claim 6 , wherein said at least one bypass opening comprises a plurality of bypass openings radially concentric with reference to said outer diameter of said plurality of vanes.

8. A method of operating a swirl burner assembly according to claim 1 , the method comprising the steps of:
supplying an oxidant to said oxidant inlet;
(ii) supplying a fuel comprising at least one of an HCV fuel to said first fuel inlet and an LCV fuel to said second fuel inlet; and
(iii) combusting said fuel in said second volume.

9. The method according to claim 8 , wherein when HCV fuel is supplied to said HCV fuel inlet, said oxidant and said HCV fuel flow converge in said first volume between said first fuel inlet and said swirl mixer, and when LCV fuel is supplied to said LCV fuel inlet, said oxidant and said LCV fuel flow converge in said second volume between said swirl mixer and said hollow longitudinally elongate body second end.

10. The method according to claim 8 , wherein said HCV fuel and/or said LCV fuel is ignited or combusted in said second volume by an igniter.

11. The method according to claim 8 , wherein the velocity of said HCV fuel through said first fuel inlet of said at least one burner unit is between 3 and 6 m/2 and/or the velocity of said LCV fuel through said second fuel inlet of said at least one burner unit is between 10 and 35 m/s.

12. A swirl burner assembly comprising:
(i) a hollow longitudinally elongate body extending along a central axis and having a hollow longitudinally elongate body first end and a hollow longitudinally elongate body second end,
(ii) an end wall at said hollow longitudinally elongate body first end,
(iii) a burner wall located between said hollow longitudinally elongate body first end and said hollow longitudinally elongate body second end, and defining a first volume from said hollow longitudinally elongate body first end to said burner wall, and a second volume from said burner wall to said hollow longitudinally elongate body second end,
(iv) an oxidant inlet into said first volume,
(v) at least one hollow longitudinally elongate burner unit having a burner unit first end extending outwardly of an opening in said body from said first volume, the burner unit extending through an open

Assignees

• Ceres Ip Co Ltd

Inventors

• Schmidt Martin
• Barnard Paul
• Toher Tony

Classifications

• F23D14/02 Primary

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

• Y02E60/50

  Fuel cells · CPC title

• F23D2900/14021

  Premixing burners with swirling or vortices creating means for fuel or air · CPC title

• F23D2900/14701

  Swirling means inside the mixing tube or chamber to improve premixing · CPC title

• F23C7/004 Primary

  using vanes · CPC title