CA1207653A - Burner for gaseous fuels - Google Patents
Burner for gaseous fuelsInfo
- Publication number
- CA1207653A CA1207653A CA000432435A CA432435A CA1207653A CA 1207653 A CA1207653 A CA 1207653A CA 000432435 A CA000432435 A CA 000432435A CA 432435 A CA432435 A CA 432435A CA 1207653 A CA1207653 A CA 1207653A
- Authority
- CA
- Canada
- Prior art keywords
- burner
- elements
- combustion zone
- wall
- brackets
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Landscapes
- Gas Burners (AREA)
Abstract
ABSTRACT OF DISCLOSURE
A burner for gaseous fuels has a combustion zone of elongate cross section which is defined between divergent flame-confining walls. Each wall comprises a plurality of wall elements which are arranged edge to edge, the adjacent edges being relatively movable and mounted so as to prevent significant gas flow therebetween, the wall elements being rigidly secured to the remainder of the burner only at locations which are upstream of the combustion zone.
A burner for gaseous fuels has a combustion zone of elongate cross section which is defined between divergent flame-confining walls. Each wall comprises a plurality of wall elements which are arranged edge to edge, the adjacent edges being relatively movable and mounted so as to prevent significant gas flow therebetween, the wall elements being rigidly secured to the remainder of the burner only at locations which are upstream of the combustion zone.
Description
This invention rela-tes to burners Eor fuel yas, and in particular to E~lel~heating gas burners.
It is known, for example from British Patent 9~3,733 to provicle a gas burner which comprises a plurali-ty oE elongate burner bodies which are secured end--to-end, and which are provided with flame confining wall elements which are rigidly secured end-to-end, to define an elongate combus-tion zone downstream of ports through which fuel gas emerges from the burner bodies. The flame-confining walls, being adjacent the combustion zone, are subjected to high temperatures and thus undergo considerable thermal expansion. The burner bodies, being upstream of the combustion zone and surrounded by an air flow to the combus-tion zone, experience much less thermal expansion, wi-th the result that the flame-confining walls tend to buckle in use.
The present invention provides a gas burner oE the type indicated above in which the flame-confining walls are less subject to buckling.
According to the invention, a burner for gaseous fuel comprises a burner for gaseous fuels, comprising a burner body for delivering a fuel gas to a combustion zone which is, in part, defined between two flame-confining walls on respective oppOsite sides of said zone, the cross-section of said combustion zone, transversely of the direction of gas flow there-through, being elongate, each said wall being divided in the elongate direction -thereof in-to a plurality of separate wall elements whose adjacent edges are free to move relatively so as to permit thermal expansion of said elements in said elongate direction, and a plurali-ty of brackets supporting said elements, each said bracket being secured to said body and extending ., ~ .. . . .
,:
;~ot~3 the:refrom in said direc-tion of gas flow, each said bracke-t including a pair of slo-ts on respective opposite sides thereof, said adjacent edges of said elements being slidably received in the respective slots so as to prevent a signiEicant gas flow between said adjacent edges, said wall elements being rigidly secured to said burner body only at locations on said elements which are upstream of said combustion zone.
,~
In a preferred embodiment, said wall elements are rigidly secured to said burner body only at locations on said elements which are upstream of said combustion zone.
An embodiment of the invention will now be d~scribed by way of example only and with reference to ~he accompanying drawings in which:-Figure 1 is a diagrammatic and pictorial YieW of a partof a burner according to the invention;
Figure 2 is a section on the plane 2-2 in Figure 1, and Figure 3 is a view on arrow 3 in Figure 2 of a support bracket.
As shown ir. Figure 1, a plurality of burner body sections 10 are secured side-by-side. Each of the sections 10 includes a cast iron gas supply manifold ll (Figure 2~ which terminates in a gas outlet p2ssage 12 and gas ports 13. The body sections 10 also include a casing 14 which surrounds the manifold ll and defines an air supply passage 15. The casing 14 bas a front wall 16 through which the gas outlet passage 12 projects, so as to define air outlet por~s 17 on either side of the passage 12. As shown in Figure 2, the gas outlet passage 12 projects substantially downstream of the front wall 16.
Secured to the front walls 16 of the bodies 10 are a plurality of brackets 18 which support flame conining wall elements 19. The wall elements 19 diverge in a direction downstream of the end o~ the gas supply passage 12 and define a combustion zone 20 for a mixture of the gas and air issuing from the respective .. . . . . . . ..
i6S3 ports 13, 17.
The brackets 18 are provided by two bracket elements 21, 22 which are of opposite hand and are arranged back-to-back. Each bracket element 21, 22 is provided with a slot in which an edge of a wall element 19 is slidable, the overlap between the edges of the wall elements 19 and ~e opposite sides of tbe bracket slots being such as effectively to prevent passage of gas between the combustion æone 20 between adjacent edges of tbe elements 19. The dimensions of the wall elements 19 between the brackets 18 are such as to permit thermal expansion of the elements 19, transversely of the direction of gas flow through the zone 20, without distortion. Additionally, end cover plates, one of which is indicated at 35 in Figure 1 are provided with flanges which can be engaged in outwardly facing slots in brackets 18 at outer ends of the burn~r. The covar plates 35 are secured to the burner body 10 only at locations which are upstream of the combustion 20ne 20, and are free to move in the slots of the brackets 18 in response to thermal expansion, and are therefore less subject to buckling.
As shown in Figure 2, flanges 23 extend downstream from ~he front walls 16, on either side of the air outlet ports 17. The inner ends of the wall elements 19 are rigidly fixed to the flanges 23 by screws 24. These fixings are adjacent the airstream from the ports 17 and are upstream of the gas outlet ports 13. The fixings provided by the screws ~4 are thus not subjected to the temperature rise encountered by the parts of the wall elements 19 adjaeent the combustion zone 20.
~IL2~i3 Even if a large number of burner bodies lO and wall elemer~ts 19 are connected side-by-side; in the manner shown in Figure l, to provide a combustion zone of greatly elongated cross section, the freedom for expansion of the separate wall elements 19 will prevent buckling of the flame conining walls.
The arrangement shown in Figure 2 is for a nozzle mixing burner, in which fuel gas and air are mixed adjacent the gas outlets -13. In alternative arrangements a fuel gas may be supplied to the manifold 11 and primary combustion air supplied through smaller air outlets adjacent the gas passage 12. In such an embodiment cover plates, as indicated at 30 are secured across the outer faces of the brackets 13 to define chambers 31 to which secondary combustion air is admitted through openings in the walls 16. This secondary combustion air flow to the combustion zone 20 through apertures indicated at 32 in Figure 1.
In further alternative arrangements a gas and air mixture is supplied througb the manifold 11. In such arrangements additional air may be supplied through the ports 17 and the apertures 32. In yet other embodiments these last air supplies may be dispensed with.
It is known, for example from British Patent 9~3,733 to provicle a gas burner which comprises a plurali-ty oE elongate burner bodies which are secured end--to-end, and which are provided with flame confining wall elements which are rigidly secured end-to-end, to define an elongate combus-tion zone downstream of ports through which fuel gas emerges from the burner bodies. The flame-confining walls, being adjacent the combustion zone, are subjected to high temperatures and thus undergo considerable thermal expansion. The burner bodies, being upstream of the combustion zone and surrounded by an air flow to the combus-tion zone, experience much less thermal expansion, wi-th the result that the flame-confining walls tend to buckle in use.
The present invention provides a gas burner oE the type indicated above in which the flame-confining walls are less subject to buckling.
According to the invention, a burner for gaseous fuel comprises a burner for gaseous fuels, comprising a burner body for delivering a fuel gas to a combustion zone which is, in part, defined between two flame-confining walls on respective oppOsite sides of said zone, the cross-section of said combustion zone, transversely of the direction of gas flow there-through, being elongate, each said wall being divided in the elongate direction -thereof in-to a plurality of separate wall elements whose adjacent edges are free to move relatively so as to permit thermal expansion of said elements in said elongate direction, and a plurali-ty of brackets supporting said elements, each said bracket being secured to said body and extending ., ~ .. . . .
,:
;~ot~3 the:refrom in said direc-tion of gas flow, each said bracke-t including a pair of slo-ts on respective opposite sides thereof, said adjacent edges of said elements being slidably received in the respective slots so as to prevent a signiEicant gas flow between said adjacent edges, said wall elements being rigidly secured to said burner body only at locations on said elements which are upstream of said combustion zone.
,~
In a preferred embodiment, said wall elements are rigidly secured to said burner body only at locations on said elements which are upstream of said combustion zone.
An embodiment of the invention will now be d~scribed by way of example only and with reference to ~he accompanying drawings in which:-Figure 1 is a diagrammatic and pictorial YieW of a partof a burner according to the invention;
Figure 2 is a section on the plane 2-2 in Figure 1, and Figure 3 is a view on arrow 3 in Figure 2 of a support bracket.
As shown ir. Figure 1, a plurality of burner body sections 10 are secured side-by-side. Each of the sections 10 includes a cast iron gas supply manifold ll (Figure 2~ which terminates in a gas outlet p2ssage 12 and gas ports 13. The body sections 10 also include a casing 14 which surrounds the manifold ll and defines an air supply passage 15. The casing 14 bas a front wall 16 through which the gas outlet passage 12 projects, so as to define air outlet por~s 17 on either side of the passage 12. As shown in Figure 2, the gas outlet passage 12 projects substantially downstream of the front wall 16.
Secured to the front walls 16 of the bodies 10 are a plurality of brackets 18 which support flame conining wall elements 19. The wall elements 19 diverge in a direction downstream of the end o~ the gas supply passage 12 and define a combustion zone 20 for a mixture of the gas and air issuing from the respective .. . . . . . . ..
i6S3 ports 13, 17.
The brackets 18 are provided by two bracket elements 21, 22 which are of opposite hand and are arranged back-to-back. Each bracket element 21, 22 is provided with a slot in which an edge of a wall element 19 is slidable, the overlap between the edges of the wall elements 19 and ~e opposite sides of tbe bracket slots being such as effectively to prevent passage of gas between the combustion æone 20 between adjacent edges of tbe elements 19. The dimensions of the wall elements 19 between the brackets 18 are such as to permit thermal expansion of the elements 19, transversely of the direction of gas flow through the zone 20, without distortion. Additionally, end cover plates, one of which is indicated at 35 in Figure 1 are provided with flanges which can be engaged in outwardly facing slots in brackets 18 at outer ends of the burn~r. The covar plates 35 are secured to the burner body 10 only at locations which are upstream of the combustion 20ne 20, and are free to move in the slots of the brackets 18 in response to thermal expansion, and are therefore less subject to buckling.
As shown in Figure 2, flanges 23 extend downstream from ~he front walls 16, on either side of the air outlet ports 17. The inner ends of the wall elements 19 are rigidly fixed to the flanges 23 by screws 24. These fixings are adjacent the airstream from the ports 17 and are upstream of the gas outlet ports 13. The fixings provided by the screws ~4 are thus not subjected to the temperature rise encountered by the parts of the wall elements 19 adjaeent the combustion zone 20.
~IL2~i3 Even if a large number of burner bodies lO and wall elemer~ts 19 are connected side-by-side; in the manner shown in Figure l, to provide a combustion zone of greatly elongated cross section, the freedom for expansion of the separate wall elements 19 will prevent buckling of the flame conining walls.
The arrangement shown in Figure 2 is for a nozzle mixing burner, in which fuel gas and air are mixed adjacent the gas outlets -13. In alternative arrangements a fuel gas may be supplied to the manifold 11 and primary combustion air supplied through smaller air outlets adjacent the gas passage 12. In such an embodiment cover plates, as indicated at 30 are secured across the outer faces of the brackets 13 to define chambers 31 to which secondary combustion air is admitted through openings in the walls 16. This secondary combustion air flow to the combustion zone 20 through apertures indicated at 32 in Figure 1.
In further alternative arrangements a gas and air mixture is supplied througb the manifold 11. In such arrangements additional air may be supplied through the ports 17 and the apertures 32. In yet other embodiments these last air supplies may be dispensed with.
Claims (3)
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A burner for gaseous fuels, comprising a burner body for delivering a fuel gas to a combustion zone which is, in part, defined between two flame-confining walls on respective opposite sides of said zone, the cross-section of said combustion zone, transversely of the direction of gas flow therethrough, being elongate, each said wall being divided in the elongate direction thereof into a plurality of separate wall elements whose adjacent edges are free to move relatively so as to permit thermal expansion of said elements in said elongate direction, and a plurality of brackets supporting said elements, each said bracket being secured to said body and extending therefrom in said direction of gas flow, each said bracket including a pair of slots on respective opposite sides thereof, said adjacent edges of said elements being slidably received in the respective slots so as to prevent a significant gas flow between said adjacent edges, said wall elements being rigidly secured to said burner body only at locations on said elements which are upstream of said combustion zone.
2. A burner as claimed in claim 1 in which said burner body comprises a plurality of body sections connected end to end in said elongate direction.
3. A burner as claimed in claim 1 which includes cover members which extend between said brackets and define, in conjunction with said brackets and a wall of said burner body, air chambers on opposite sides of said combustion zone, means for supplying air to said chambers, and apertures in said flame-confining walls, through which apertures air can flow from said chambers to said combustion zone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000432435A CA1207653A (en) | 1983-07-14 | 1983-07-14 | Burner for gaseous fuels |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA000432435A CA1207653A (en) | 1983-07-14 | 1983-07-14 | Burner for gaseous fuels |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1207653A true CA1207653A (en) | 1986-07-15 |
Family
ID=4125664
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000432435A Expired CA1207653A (en) | 1983-07-14 | 1983-07-14 | Burner for gaseous fuels |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA1207653A (en) |
-
1983
- 1983-07-14 CA CA000432435A patent/CA1207653A/en not_active Expired
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0695911B1 (en) | A gas burner with an improved diffuser | |
| EP1144916B1 (en) | Burner and process for operating gas turbines | |
| US4601655A (en) | Heating apparatus | |
| US3800527A (en) | Piloted flameholder construction | |
| EP0026594A1 (en) | Low emissions prevaporization type combustor assembly | |
| US4523905A (en) | Burner for gaseous fuels | |
| PL191766B1 (en) | Burner for combustion of powdered fuel | |
| US3574507A (en) | Air/fuel mixing and flame-stabilizing device for fluid fuel burners | |
| GB2043868A (en) | Gas turbine | |
| US4610135A (en) | Combustion equipment for a gas turbine engine | |
| US5551869A (en) | Gas staged burner | |
| US4643670A (en) | Burner | |
| JPS5837414A (en) | Mixing type gas burner | |
| US7481650B2 (en) | Direct gas-fired burner assembly with two-stage combustion | |
| US3630499A (en) | Burner | |
| US2588895A (en) | Gas burner with flame retaining ports | |
| CA1207653A (en) | Burner for gaseous fuels | |
| US5001898A (en) | Fuel distributor/flameholder for a duct burner | |
| JPS58150704A (en) | Gas fuel burner device | |
| US5057008A (en) | Line burner | |
| US20050181321A1 (en) | Air/gas burner system | |
| GB2117506A (en) | Burner for gaseous fuels | |
| JP2705022B2 (en) | Fuel burner | |
| US5662467A (en) | Nozzle mixing line burner | |
| US3361367A (en) | Gas burner |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MKEX | Expiry |