GB2134642A - Atmospheric gas burner - Google Patents

Atmospheric gas burner Download PDF

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Publication number
GB2134642A
GB2134642A GB08402083A GB8402083A GB2134642A GB 2134642 A GB2134642 A GB 2134642A GB 08402083 A GB08402083 A GB 08402083A GB 8402083 A GB8402083 A GB 8402083A GB 2134642 A GB2134642 A GB 2134642A
Authority
GB
United Kingdom
Prior art keywords
slot
atmospheric gas
gas burner
intermediate member
burner according
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.)
Granted
Application number
GB08402083A
Other versions
GB8402083D0 (en
GB2134642B (en
Inventor
Colin Walter Norton
James Edward Addison
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Furigas UK Ltd
Original Assignee
Furigas UK Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from GB838302977A external-priority patent/GB8302977D0/en
Application filed by Furigas UK Ltd filed Critical Furigas UK Ltd
Priority to GB08402083A priority Critical patent/GB2134642B/en
Publication of GB8402083D0 publication Critical patent/GB8402083D0/en
Publication of GB2134642A publication Critical patent/GB2134642A/en
Application granted granted Critical
Publication of GB2134642B publication Critical patent/GB2134642B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D14/00Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F23D14/04Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner
    • F23D14/045Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone induction type, e.g. Bunsen burner with a plurality of burner bars assembled together, e.g. in a grid-like arrangement

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

The burner comprises a body 10 for receiving gas and a plurality of parallel spaced apart burner elements 12 fixed to the body in a substantially gas-tight manner. The elements 12 locate in slots 18 in the body, with a slotted intermediate member 13 arranged between the body and the element. Each of the elements has marginal portions 27 which project through associated slots in the body and intermediate member. The portions 27 are deformed so as to interconnect the body and the burner. <IMAGE>

Description

SPECIFICATION An atmospheric gas burner The invention relates to an atmospheric gas burner.
Hitherto it has been known to construct an atmospheric gas burner by welding e.g. spot welding, brazing or soldering burner elements to a gas receiver. Whilst such a manner of interconnecting the elements and receiver produces strong joints, it is generally labour intensive and therefore relatively costly. Also spot welding is particularly tedious and results in a burner which is unattractive from a sales aspect.
An object of the present invention is to provide a gas burner which dispenses with the need to weld, braze or solder a burner element to a body.
According to the invention there is provided an atmospheric burner comprising a body for receiving gas and a burner element fixed to the body in a substantially gas-tight manner characterised in that the element is fixed to the body by deforming a portion of the element and/or the body.
Such an arrangement provides a simple mechanical interconnection between the body and the element which does not involve welding, brazing or soldering as required hitherto to provide a substantially gas-tight fixing.
Preferably an intermediate member engages parts of the body and the element in a substantially gas-tight manner. In such a case the intermediate member may be formed with a slot having ends which engage the element in a substantially gas-tight manner. Preferably the substantially gas-tight engagement of the ends of the slot and the element is effected by cold flow of the material of the element and/or the intermediate member during assembly of the burner. The use of the intermediate member greatly enhances sealing between the body and the element in a particularly simple manner.
The element may locate in a slot in the body and portions of the element may be deformed so as to overlie portions of the body adjacent the slot to fix the element to the body. In such a case the body may be formed with a part cylindrical surface formed with said slot and the element may define marginal sections which are deformed by bending so as to engage in a substantially gas-tight manner portions of the body adjacent the slot. The use of such marginal portions on the element provides a low cost and simple way of interconnecting the burner and body without the need for welding etc.
The intermediate member may simply comprise a part cylindrical plate or sheet formed by bending thin metal. Preferably the intermediate member and the part cylindrical portion of the body are of complementary shape.
Preferably the slot in the body terminates at ends short of the ends of the slot in the intermediate member so that the slot in the intermediate member extends alongside an unslotted portion of the body. The element may be formed with shoulders which engage the ends of the slot in the body in a substantially gas tight manner. The element may also be formed with edges which engage said unslotted portion of the body in a substantially gas-tight manner.
An atmospheric gas burner in accordance with the invention will now be described by way of example with reference to the accompanying drawings in which: Fig. 1 is a perspective view of a burner in accordance with the invention, Fig. 2 is an inverted exploded view of part of the burner of Fig. 1 showing one burner element only, Fig. 2A is an enlarged view of part of the body of the burner in Fig. 2, Fig. 3 is a transverse cross section through part of the inverted burner shown partially assembled, Fig. 4 is a view in the direction of arrow IV in Fig. 3 with the body removed, Fig. 5 is a view of part of the burner of Fig. 1 in an assembled condition, and Fig. 6 is a view similar to Fig. 3 illustrating part of the fully assembled burner and indicating areas providing a substantially gas-tight seal.
In Fig. 1 a burner comprises a gas receiving body 10 (hereinafter called "a receiver") which carries a plurality of burner elements 1 2 and an intermediate member 1 3. The usual gas feed venturi or mixing tube 2 extends into the body from an end wall 3 and is supplied with gas from a gas feed unit 4. The unit is carried by a bracket 5 on the receiver 10. The receiver has side walls 14, inturned flanges 1 5 and an inverted U-shaped cross-section portion 1 6 having a cylindrical surface 1 7. As shown clearly in Fig. 2, the portion 1 6 is formed with a plurality of circumferential slots 1 8 having ends 11 and radiussed corners 1 8a (see Fig. 2A).
As shown in Fig. 2 each burner element 12 comprises a generally rectangular cross section tube having welded edge seams 19 and a generally U-shaped recess 20. The ends of the recess terminate at four shoulders 22 (three of which are shown in Fig. 2) which lie adjacent inner edges 22a of the element. The seams 1 9 are stepped at 23. The burner element is formed with gas outlets 9 in known manner.
The intermediate member 1 3 comprises a sheet of metal formed so that its internal surface is substantially of complementary shape to the external surface of the portion 1 6 of the receiver 10. The intermediate member is formed with slots 24 equal in number and spacing to the slots 1 8 in the receiver. The ends 21 of each slot 24 are formed with shallow recesses 25 and are radiussed at 24a in a manner similar to slots 1 8.
To assemble the burner, the elements 12 are placed side by side in a carrier (not shown) with the recesses 20 facing upwardly as in Fig. 2 so as to align with the slots 24 in the intermediate member 13. The intermediate member 13 arranged as shown in Fig. 2 is then placed on the elements 1 2 so that marginal portions 27 of the elements project through the slots 24. The width of each slot 24 is such that the edges of the slots grip the sides of the burner elements. The receiver 10 is then placed in the intermediate member so that the marginal portions 27 of the elements project through the slots 1 8. The distance d between opposite inner surfaces of portion 1 6 is such that those surfaces grip the adjacent outer surfaces of the intermediate member 13.The complete assembly of the body 10, burners 12 and intermediate member 1 3 thus holds together frictionally. The arrangement of the assembled elements, receiver and intermediate member is shown in Fig. 3, the stepped portions 23 of each burner element 12 locating in the recesses 25 (see Fig. 4) with the shoulders 22 spaced from the ends 11 of the slot 1 8. A tool (not shown) is then applied to the receiver and a force F (Fig. 2) is applied to the tool with the burner elements 12 supported by a reaction member to provide a reaction R so that the portion 1 6 is urged firmly against the intermediate member and the ends 21 of the slots 24 are urged against the elements 12.
The force F causes the material of each element 12 2 and/or the intermediate member 1 3 to "cold flow" in the area adjacent the ends 21 of each slot so that a substantially gas tight seal is achieved both between the stepped portions 23 and the recesses 25, and between the adjacent surfaces of the element 12 and the ends 21 and radiussed corners 24a of the slot 24. The application of force F also urges the shoulders 22 firmly against the radiussed section 1 8a of slots 1 8. The loading of the elements normally causes a smali amount of distortion of the elements in the vicinity of the ends 21 of the slots 24 to effect the cold flow of material.The tool also deforms the marginal portion 27 of each element by urging them slightly outwardly over the interior surface of the portion 1 6 alongside the slots 1 8 to lock the assembled components together. The tool is then removed and a further tool is applied to urge the marginal portions 27 firmly against the interior surface of the portion 1 6 as shown clearly in Figs. 5 and 6.
Such a method of assembly effects a substantially gas tight seal between the portion 1 6 of the receiver 10 and the intermediate member 13, and between each element 12 and the portion 1 6 adjacent the associated slot 1 8. The method of assembly also causes the adjacent inner edges 22a of the element 1 2 and the unslotted adjacent outer surface of portion 1 6 to be urged into firm engagement with each other thereby forming a further substantially gas-tight seal. For that purpose the ends 21 of the slots 24 lie closer to the flanges 1 5 than the ends 11 of slots 18. A substantially gas-tight fit is also achieved between the shoulders 22 and the radiussed sections 1 8a of slots 18.
Substantially gas-tight sealing is therefore effected at the areas marked S in Fig. 4 by means of simple mechanical operations which are reliable, less costly and less iabour intensive than fixing the elements by welding, soldering or brazing.
The burner is completed by adding a base 29 (Fig. 1) and end walls 3 (one only of which is shown in Fig. 1).
The receiver 10 may be made from stainless steel and the intermediate member 1 3 may be made from a similar material or an alternative material such as aluminium. The elements 12 will normally be made from stainless steel.
It is envisaged that the portion 1 6 of the receiver may be formed to provide sections which can be bent to secure the burner elements on to the receiver instead of or in addition to bending a portion of the burner elements.
In order to provide a lead-in for each burner element 12 during assembly, the seams 19 may be cut away as indicated by broken lines 8 in Figs.
3 s 6 adjacent the steps 23.
As shown in Fig. 1 , cross lighting holes 30 may be provided in the body portion 16 between the slots 1 8. In such a case the intermediate member 1 3 is formed with clearance apertures 31 which reveal the cross lighting holes.

Claims (12)

1. An atmospheric gas burner comprising a body for receiving gas and a burner element fixed to the body in a substantially gas-tight manner by deforming a portion of the element and/or the body.
2. An atmospheric gas burner according to claim 1 in which an intermediate member engages parts of the body and the element in a substantially gas-tight manner.
3. An atmospheric gas burner according to claim 2 in which the intermediate member is formed with a slot having ends which engage the element in a substantially gas-tight manner.
4. An atmospheric gas burner according to claim 3 in which the substantially gas-tight engagement of the ends of the slots and the element is effected by cold flow of the material of the element and/or the intermediate member during assembly of the burner.
5. An atmospheric gas burner according to any preceding claim in which the element locates in a slot in the body.
6. An atmospheric gas burner according to claim 5 in which portions of the elements are deformed so as to overlie portions of the body adjacent the slot to fix the element to the body.
7. An atmospheric gas burner according to claim 5 or 6 in which the body is formed with a part cylindrical portion formed with the slot and the element defines marginal sections which are deformed by bending so as to engage in a substantially gas-tight manner portions of the body adjacent the slot.
8. An atmospheric gas burner according to claim 7 when appendant to claim 3 or 4 in which the intermediate member comprising a part cylindrical plate or sheet which is complementary to the part cylindrical portion of the body.
9. An atmospheric gas burner according to claim 8 in which the slot in the body terminates at ends short of the ends of the slot in the intermediate member so that the slot in the intermediate member extends alongside an unslotted portion of the body.
10. An atmospheric gas burner according to claim 9 in which the element is formed with shoulders which engage the ends of the slot in the body in a substantially gas-tight manner.
11. An atmospheric gas burner according to claim 9 or 10 in which the element is formed with edges which engage said unslotted portion of the body in a substantially gas-tight manner.
12. An atmospheric gas burner constructed and arranged substantially as described herein with reference to the accompanying drawings.
GB08402083A 1983-02-03 1984-01-26 Atmospheric gas burner Expired GB2134642B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08402083A GB2134642B (en) 1983-02-03 1984-01-26 Atmospheric gas burner

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB838302977A GB8302977D0 (en) 1983-02-03 1983-02-03 Atmospheric gas burner
GB08402083A GB2134642B (en) 1983-02-03 1984-01-26 Atmospheric gas burner

Publications (3)

Publication Number Publication Date
GB8402083D0 GB8402083D0 (en) 1984-02-29
GB2134642A true GB2134642A (en) 1984-08-15
GB2134642B GB2134642B (en) 1986-05-14

Family

ID=26285124

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08402083A Expired GB2134642B (en) 1983-02-03 1984-01-26 Atmospheric gas burner

Country Status (1)

Country Link
GB (1) GB2134642B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0371715A1 (en) * 1988-11-28 1990-06-06 Caradon Ideal Limited Modular gas burner assembly
EP0452108A1 (en) * 1990-04-10 1991-10-16 Caradon Ideal Limited Gas burner assembly

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1123648A (en) * 1966-11-02 1968-08-14 Saunier Duval Universal gas burner
GB1148943A (en) * 1966-06-14 1969-04-16 Geo Bray & Company Ltd Improvements in or relating to gas burners
GB1191993A (en) * 1967-05-12 1970-05-13 Vulcan Australia Improvements in or relating to Gas Burners
GB1224443A (en) * 1968-07-10 1971-03-10 Vaillant Joh Kg Bunsen burner for gas-fired heating apparatus
GB1261797A (en) * 1968-03-26 1972-01-26 Ferroli Gas S N C Gas burner
GB1318306A (en) * 1969-08-19 1973-05-31 Nederlandse Gasunie Nv Atmospheric gas burner

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1148943A (en) * 1966-06-14 1969-04-16 Geo Bray & Company Ltd Improvements in or relating to gas burners
GB1123648A (en) * 1966-11-02 1968-08-14 Saunier Duval Universal gas burner
GB1191993A (en) * 1967-05-12 1970-05-13 Vulcan Australia Improvements in or relating to Gas Burners
GB1261797A (en) * 1968-03-26 1972-01-26 Ferroli Gas S N C Gas burner
GB1224443A (en) * 1968-07-10 1971-03-10 Vaillant Joh Kg Bunsen burner for gas-fired heating apparatus
GB1318306A (en) * 1969-08-19 1973-05-31 Nederlandse Gasunie Nv Atmospheric gas burner

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0371715A1 (en) * 1988-11-28 1990-06-06 Caradon Ideal Limited Modular gas burner assembly
EP0452108A1 (en) * 1990-04-10 1991-10-16 Caradon Ideal Limited Gas burner assembly

Also Published As

Publication number Publication date
GB8402083D0 (en) 1984-02-29
GB2134642B (en) 1986-05-14

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Legal Events

Date Code Title Description
7732 Case decided by the comptroller ** patent revoked (sect. 73(2)/1977)