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GB2276715A - Gas burner - Google Patents

Gas burner Download PDF

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Publication number
GB2276715A
GB2276715A GB9306520A GB9306520A GB2276715A GB 2276715 A GB2276715 A GB 2276715A GB 9306520 A GB9306520 A GB 9306520A GB 9306520 A GB9306520 A GB 9306520A GB 2276715 A GB2276715 A GB 2276715A
Authority
GB
United Kingdom
Prior art keywords
burner
gas
vanes
air
cooker
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
GB9306520A
Other versions
GB2276715B (en
GB9306520D0 (en
Inventor
Shui Wah Leung
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.)
YUE STOVES MANUFACTORY Ltd
Original Assignee
YUE STOVES MANUFACTORY 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
Application filed by YUE STOVES MANUFACTORY Ltd filed Critical YUE STOVES MANUFACTORY Ltd
Priority to GB9306520A priority Critical patent/GB2276715B/en
Publication of GB9306520D0 publication Critical patent/GB9306520D0/en
Priority to CA 2112920 priority patent/CA2112920A1/en
Publication of GB2276715A publication Critical patent/GB2276715A/en
Application granted granted Critical
Publication of GB2276715B publication Critical patent/GB2276715B/en
Priority to HK148496A priority patent/HK148496A/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23D14/20Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion

Landscapes

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

Abstract

A gas burner 1 comprises a burner body 3, an air supply pipe 9 and a gas supply pipe 5 arranged coaxially. The gas supply pipe 5 extends upwardly beyond the air supply pipe 9 and terminates in an outlet nozzle 7 where gas is burned. Air is guided towards and around the gas outlet nozzle 7 by an air supply fitting 11 comprising a number of vanes 15a -e arranged on a hub 16 which surrounds the periphery of the gas supply pipe 5. The vanes 15 radiate from the hub and extend along a line at an angle oblique to the radial direction. Particularly, the vanes 15a - e are twisted to form a part helical surface. Air blown into the burner through the air supply pipe 8 is guided by the vanes into a spiral path towards and around the gas outlet nozzle 7 to supply the gas with ample oxygen for combustion. <IMAGE>

Description

Gas Burner The present invention relates to a gas burner for a stove, suitable for use in Chinese cooking.
Gas burners need to have high power for successfully heating a vessel such as a wok, steam tray or the like to high enough temperatures for Chinese cooking.
Figure 1 shows a conventional burner 1 used in Chinese cooking. The burner 1 comprises a hollow burner body 3 through which a gas supply pipe 5 extends from below, the gas supply pipe 5 having a gas outlet nozzle 7 at its upper end. A large air supply pipe 9, concentric with the gas supply pipe 5,also extends up from the bottom 3a of the burner body 3. A concentric air chamber cover 11, forming an air supply fitting, covers the air supply pipe 9, whilst the gas supply pipe 5 extends through it. The air chamber cover 11 supplies air to the gas outlet nozzle 7 through small circular apertures 12 arranged around the periphery ila of the chamber cover 11 as shown in figure 2.
In use, the burner 1 has a firebrick 17 and a cover 19.
Air is blown up through the air supply pipe 9, passes through the apertures 12 and circulates around the gas outlet nozzle where the air and gas are mixed and burn.
However, such burners have the disadvantage that they generate noise levels considerably above the background noise levels. This is to a large extent due to the "whistle effect" as air is blown through the apertures in the air chamber cover.
Furthermore, conventional burners require large and powerful high static pressure blowers to force air through the apertures in the air chamber cover. Such blowers are expensive to buy and consume a lot of fuel, making the burner expensive to use.
The present invention provides a gas burner comprising a hollow burner body, a gas supply pipe extending upwardly through the burner body and having a nozzle at its upper end, an air inlet pipe for the supply of air to the burner from a blower, and an air supply fitting, arranged in the burner body between the air inlet and the nozzle, to control the flow of air towards and/or around the nozzle wherein the air supply fitting comprises a plurality of vanes which causes the air to flow in a substantially spiral path towards and around the nozzle.
Preferably the burner body, gas supply pipe and air supply fitting are arranged coaxially and more preferably the components are of circular cross section. With such a burner the vanes can be arranged between the gas supply pipe and burner body uniformly around the circumference of the gas supply pipe, each vane extending along a line at an angle oblique to the radial direction. In particular, the vanes can be twisted so that their surfaces form part of a helical surface. This arrangement of the vanes results in the air being guided towards and around the nozzle in a particularly good spiral path.
Further preferred and optional features of the invention will be apparent from the following description and the accompanying claims.
An embodiment of the present invention will now be described, by way of example, with reference to the accompanying drawings, in which: Figure 1 is an exploded view of a prior art burner; Figure 2 is a perspective view of the underside of the air supply fitting (chamber cover) of figure 1; Figure 3 is a medial longitudinal cross section of a burner forming an embodiment of the present invention; Figure 4 is a plan view of the burner of figure 3.
Figure 5 is a perspective view of the air supply fitting of the burner of figures 3 and 4, and Figure 6 is a side view of the air supply fitting of figure 5.
Figures 3 and 4 show a burner 1 having a cast iron burner body 3 with a base 3a and peripheral wall 3b. A steel gas supply pipe 5 extends vertically through and coaxially with the burner body 3. The gas supply pipe 5 passes through the centre of the base 3a of the burner body 3 and is connected, in use, to a gas supply 5a. At its upper end, the gas supply pipe 3 has a gas outlet nozzle 7 where gas is ignited and burned.
The gas outlet nozzle 7 is a steel cylinder with an annular recess 6 having gas outlet holes 6a around its periphery.
A large galvanised steel air supply pipe 9, coaxial with and surrounding the gas supply pipe 5, also extends up through the base 3a of the burner body 3. Air is blown into the air supply pipe 9 of the burner 1 by an air blower (not shown). A cast iron air supply fitting 11 covers the air supply pipe 9 whilst the gas supply pipe 5 extends through it. The air supply fitting 11 controls the direction of flow of air to and around the nozzle 7.
The air supply fitting 11 comprises five air guide vanes 15a to 15e arranged uniformly around a cylindrical hub 16 which surrounds the gas supply pipe 3. Each vane 15 overlaps almost half of the adjacent vane.
The vanes 15a-e radiate outwardly from the hub 16, each extending along a line at an angle oblique to the radial direction. The vanes 15a-e are twisted so that their surfaces each form part of a helical surface. The angle of the helical surface as about 40 degrees to the transverse plane. As can be seen in Figure 4, the thickness of each vane gradually increases outwards.
As air is blown up through the air supply pipe 9 the arrangement of vanes 15a-e causes the air to be directed towards and around the nozzle 7 in a spiral path.
The spiral circulation of the air has the advantage of increased supply of oxygen to the burner nozzle 7 and hence increased power and concentration of flame.
This new design of air supply fitting produces considerably less noise than the prior art because the vanes do not produce a "whistle effect". Furthermore the design is cheaper to manufacture and can be used with a smaller, less powerful blower,which means that the burner is less expensive to operate.
A prototype fitting in a gas burner made in accordance with the invention has been tested and gave the results set out below. The results show that the burner produces substantially less noise in comparison with the prior art while maintaining a power output high enough for heating vessels in Chinese cooking.
Example Measurements at a gas pressure of 1. 5 KPa; gas temperature of 21 0C and background sound level of 78 dB Present Prior Art Invention Burning 194.4 MJ/h 216 MJ/h Capacity Sound 88 dB 97 dB Level In use, the burner has a clay firebrick 17 which surrounds the burner nozzle 7 and a cast iron cover 19 which seats on a cast iron couple ring 21 for coupling the cover to the burner body 3.
The burner is ignited by a conventional ignition system comprising a brass or steel pilot lighter nozzle 23, a brass or steel flame failure device sensor 25 and an air supply pipe 27.
It will be appreciated that various modifications can be made to the described embodiment without departing from the scope of the accompanying claims.

Claims (12)

CLAIMS:
1. A gas burner comprising a hollow burner body, a gas supply pipe extending upwardly through the burner body and having a nozzle at its upper end, an air inlet pipe for the supply of air to the burner from a blower, and an air supply fitting, arranged in the burner body between the air inlet and the nozzle, to control the flow of air towards and/or around the nozzle, wherein the air supply fitting comprises a plurality of vanes which causes the air to flow in a substantially spiral path towards and around the nozzle.
2. A gas burner as claimed in claim 1, wherein the burner body, gas supply pipe and air supply fitting are arranged coaxially.
3. A gas burner as claimed in claim 1 or claim 2, wherein the burner body, gas supply pipe and air supply fitting are of circular cross section.
4. A gas burner as claimed in claim 3, wherein each vane radiates along a line at an angle oblique to the radial direction.
5. A gas burner as claimed in claim 1, 2, 3 or 4, wherein the vanes are twisted so that their surfaces form part of a helical surface.
6. A gas burner as claimed in claim 5, wherein each vane overlaps an adjacent vane.
7. A gas burner as claimed in claim 5 or 6, wherein the angle of the helical surface of the vanes is in the range of 30 to 60 degrees to a transverse plane.
8. A gas burner as claimed in claim 5, 6 or 7, wherein the angle of the helical surface of the vanes is in the range of 35 to 50 degrees to a transverse plane.
9. A gas burner as claimed in claim 5, 6, 7 or 8, wherein the angle of the helical surface of the vanes is 40 degrees to a transverse plane.
10. A gas burner as claimed in any preceding claim, wherein the air supply fitting includes a hub, which in use surrounds the gas supply pipe, from which the vanes radiate.
11. A gas burner as claimed in any preceding claim, wherein the thickness of each vane increases outwards.
12. A cooker comprising a gas burner substantially as described with reference to, and as shown in, Figures 3 to 6 of the accompanying drawings.
12. A gas burner substantially as described with reference to, and as shown in, Figures 3 to 6 of the accompanying drawings.
Amendments to the claims have been filed as follows CLAIMS: 1. A cooker for Chinese cooking, comprising a gas burner for heating a cooking vessel, the burner comprising a hollow burner body, a gas supply pipe extending upwardly through the burner body and having a nozzle at its upper end, the nozzle directing the gas laterally, a flame chamber surrounding the nozzle, the flame chamber having an open end, above which the cooking vessel is to be positioned, and an open lower end connected to the upper end of the burner body, an air inlet pipe for supplying an upward flow of air to the burner body from a blower, and an air supply fitting arranged in the burner body between the air inlet pipe and the nozzle, the air supply fitting having a plurality of vanes which cause air to flow through the burner in a substantially spiral path, the vanes defining between them unobstucted passageways, wherein, in use, air flows from the air inlet pipe along an unimpeded upward path through the burner body towards the nozzle.
2. A cooker as claimed in claim 1, wherein the burner body, gas supply pipe and air supply fitting are arranged coaxially.
3. A cooker as claimed in claim 1 or claim 2, wherein the burner body, gas supply pipe and air supply fitting are of circular cross section.
4. A cooker as claimed in claim 3, wherein each vane radiates along a line at an angle oblique to the radial direction.
5. A cooker as claimed in claim 1, 2, 3 or 4, wherein the vanes are twisted so that their surfaces form part of a helical surface.
6. A cooker as claimed in claim 5, wherein each vane overlaps an adjacent vane.
7. A cooker as claimed in claim 5 or 6, wherein the angle of the helical surface of the vanes is in the range of 30 to 60 degrees to a transverse plane.
8. A cooker as claimed in claim 5, 6 or 7, wherein the angle of the helical surface of the vanes is in the range of 35 to 50 degrees to a transverse plane.
9. A cooker as claimed in claim 5, 6, 7 or 8, wherein the angle of the helical surface of the vanes is 40 degrees to a transverse plane.
10. A cooker as claimed in any preceding claim, wherein the air supply fitting includes a hub, which in use surrounds the gas supply pipe, from which the vanes radiate.
11. A cooker as claimed in any preceding claim, wherein the thickness of each vane increases outwards.
GB9306520A 1993-03-29 1993-03-29 Gas burner Expired - Fee Related GB2276715B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB9306520A GB2276715B (en) 1993-03-29 1993-03-29 Gas burner
CA 2112920 CA2112920A1 (en) 1993-03-29 1994-01-06 Cooker
HK148496A HK148496A (en) 1993-03-29 1996-08-08 Gas burner

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9306520A GB2276715B (en) 1993-03-29 1993-03-29 Gas burner

Publications (3)

Publication Number Publication Date
GB9306520D0 GB9306520D0 (en) 1993-05-19
GB2276715A true GB2276715A (en) 1994-10-05
GB2276715B GB2276715B (en) 1995-10-04

Family

ID=10732948

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9306520A Expired - Fee Related GB2276715B (en) 1993-03-29 1993-03-29 Gas burner

Country Status (3)

Country Link
CA (1) CA2112920A1 (en)
GB (1) GB2276715B (en)
HK (1) HK148496A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2439097A (en) * 2006-06-15 2007-12-19 Rolls Royce Plc Fuel Injector and Associated Swirler
US9562691B2 (en) 2013-09-30 2017-02-07 Rolls-Royce Plc Airblast fuel injector

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2542346B1 (en) * 2014-02-03 2016-05-17 Bsh Electrodomesticos Espana Sa GAS BURNER, COOKING POINT, AND KITCHEN

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1356067A (en) * 1971-01-22 1974-06-12 Gen Chauffage Ind Pillard Frer Burner for liquid or gaseous fuels
GB2123946A (en) * 1982-05-24 1984-02-08 Freiberg Brennstoffinst Flat flame burner
GB2146112A (en) * 1980-06-04 1985-04-11 Foster Wheeler Energy Corp Split stream burner assembly
US4559009A (en) * 1982-08-06 1985-12-17 Hauck Manufacturing Company Aggregate dryer burner
US4673350A (en) * 1986-08-26 1987-06-16 Eclipse, Inc. Burner assembly for radiant tube heating system
US4729734A (en) * 1986-07-18 1988-03-08 Polomchak Robert W Device for improved combustion
US4813867A (en) * 1985-10-31 1989-03-21 Nihon Nensho System Kabushiki Kaisha Radiant tube burner
US4988287A (en) * 1989-06-20 1991-01-29 Phillips Petroleum Company Combustion apparatus and method

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1356067A (en) * 1971-01-22 1974-06-12 Gen Chauffage Ind Pillard Frer Burner for liquid or gaseous fuels
GB2146112A (en) * 1980-06-04 1985-04-11 Foster Wheeler Energy Corp Split stream burner assembly
GB2123946A (en) * 1982-05-24 1984-02-08 Freiberg Brennstoffinst Flat flame burner
US4559009A (en) * 1982-08-06 1985-12-17 Hauck Manufacturing Company Aggregate dryer burner
US4813867A (en) * 1985-10-31 1989-03-21 Nihon Nensho System Kabushiki Kaisha Radiant tube burner
US4729734A (en) * 1986-07-18 1988-03-08 Polomchak Robert W Device for improved combustion
US4673350A (en) * 1986-08-26 1987-06-16 Eclipse, Inc. Burner assembly for radiant tube heating system
US4988287A (en) * 1989-06-20 1991-01-29 Phillips Petroleum Company Combustion apparatus and method

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2439097A (en) * 2006-06-15 2007-12-19 Rolls Royce Plc Fuel Injector and Associated Swirler
GB2439097B (en) * 2006-06-15 2008-10-29 Rolls Royce Plc Fuel injector
US8910480B2 (en) 2006-06-15 2014-12-16 Rolls-Royce Plc Fuel injector with radially inclined vanes
US9562691B2 (en) 2013-09-30 2017-02-07 Rolls-Royce Plc Airblast fuel injector

Also Published As

Publication number Publication date
GB2276715B (en) 1995-10-04
GB9306520D0 (en) 1993-05-19
HK148496A (en) 1996-08-16
CA2112920A1 (en) 1994-09-30

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20030329