EP0145381A2 - Improvements in or relating to burner tips - Google Patents

Improvements in or relating to burner tips Download PDF

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Publication number
EP0145381A2
EP0145381A2 EP84308113A EP84308113A EP0145381A2 EP 0145381 A2 EP0145381 A2 EP 0145381A2 EP 84308113 A EP84308113 A EP 84308113A EP 84308113 A EP84308113 A EP 84308113A EP 0145381 A2 EP0145381 A2 EP 0145381A2
Authority
EP
European Patent Office
Prior art keywords
tips
gas
opening
air
gas burner
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.)
Withdrawn
Application number
EP84308113A
Other languages
German (de)
French (fr)
Other versions
EP0145381A3 (en
Inventor
John Stephen Wharmby
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.)
Doosan Babcock Ltd
Original Assignee
Babcock Power 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 Babcock Power Ltd filed Critical Babcock Power Ltd
Publication of EP0145381A2 publication Critical patent/EP0145381A2/en
Publication of EP0145381A3 publication Critical patent/EP0145381A3/en
Withdrawn legal-status Critical Current

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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
    • F23D14/46Details, e.g. noise reduction means
    • F23D14/48Nozzles
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D17/00Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel

Definitions

  • This invention relates to gas burner tips.
  • furnace burner arrangements in which combustion air is discharged in a vortex through a ring of burner tips from which combustion gas is discharged. Frequently, this vortex is unstable in that it precesses about the axis resulting in circumferential variations in air flow. A consequence is that the combination of the gas with air is not regular, resulting in combustion pulsations. If the acoustic frequency of the furnace is such that Rayleigh's criterion is satisfied, then the combustion pulsations may be sustained, leading to excessive furnace vibrations.
  • the present invention arose from a consideration of this problem and of ways in which more regular combustion might be obtained.
  • a gas burner tip in the form of a cylinder closed at one end except for an opening in an end wall that is oblique to the cylindrical surface and having an opening of smaller area lying wholly in the part of the cylindrical wall that is defined by a diametrical plane across which the end wall lies symmetrically.
  • the tip A shown in Figure 1 has a barrel 1 of which the outer diameter is about 27mm. Its length is about 70mm and at the lower end is a mounting flange 2. Centrally, at its upper end, there is a ridge 3 about 8mm wide and flat end walls 4 and 5 slope down symmetrically from the sides of the ridge 3 at about 45°.
  • a circular opening 8 of just over 20mm diameter In one of the end walls 5 is a circular opening 8 of just over 20mm diameter.
  • a circular opening 9 of smaller diameter, 15mm, is formed in the cylindrical wall of the barrel about half way between the ridge 3 and the top of the flange 2.
  • the diametrical plane of the barrel 1 that contains the centre of the opening 8 is displaced from that which contains the centre of the opening 9 by 221 ⁇ 2°.
  • the opening 9 thus lies wholly within the diametrical plane of the barrel 1 that bisects the ridge 3 and across which the end wall 5 lies symmetrically.
  • FIG 3 shows six burner tips mounted in the opening 10 in the wall of a furnace.
  • the boundary of they opening 10 tapers from a circle 11 in the inner face of the wall to a circle 12 in the outer face.
  • An oil burner 13 is arranged to discharge centrally through the opening 10, the outlet end of the burner 14 being about mid-way between the faces of the furnace wall.
  • a group of six gas burner tips A connected to a common main (not shown) lying outside the furnace, are disposed equi-spaced around a circle that is concentric with the burner 14, the leading ends of the burner tips A lying forward of the oil burner 14 but rearwardly of the inner face of the furnace wall.
  • Three of the tips, A1 are so arranged that gas discharging from the upper opening, 8, is discharged approximately towards the axis, but at a slight angle so that the gas has a swirl in the clockwise direction. Gas discharging from the lower openings 9 will be more oblique to the axis but will also swirl in the clockwise direction.
  • the other three tips, A2 are each disposed between two of the tips A1 and are arranged so that gas discharging from both the openings of each will have an anticlockwise direction of rotation and flow past, outwardly of, the tips A1.
  • An effect of the rotation of the gas will be to tend to constrain the air to flow symmetrically about the axis of the burner and so tend to decouple the zone in which gas and air is mixed and burned from the aerodynamically unstable region.
  • the combustion zone will tend better to resemble the combustion produced by an axial oil burner so that gas and oil may be burned together to give a dual firing burner i.e. a burner in which the two fuels may be burnt.
  • the flame will tend to be removed from the point of fuel injection so that the stabilising discs that are often provided on gas spuds may be dispensable. A benefit of this would be the resultant lower air velocities.
  • the opening 9 may be replaced by two or more openings in the part of the wall that is defined by a diametrical plane across which the end wall 5 lies symmetrically.
  • tips in a ring may be similarly orientated in the way that the tips A1 are orientated. Whilst gas from these tips is directed inwardly, none is directed directly to the axis, but at an angle such as to tend to induce orderly swirl.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Incineration Of Waste (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

The invention provides a gas burner tip A in the form of a cylindrical barrel (1) closed at its outer end except for an opening (8) in an end wall (5) that is oblique to the cylindrical surfaces. The cylindrical surface also contains a further opening (9), smaller than the opening (8).
In a furnace burner, a plurality of similar tips A may be arranged uniformly disposed around a ring past which swirling air is directed. The tips are similarly orientated and the discharge of gas through them is effective to restrain aberrations in the swirl of the air. These tips may be interspersed with other similar tips orientated similarly to each other but differently orientated with respect to the first.

Description

  • This invention relates to gas burner tips.
  • There are furnace burner arrangements in which combustion air is discharged in a vortex through a ring of burner tips from which combustion gas is discharged. Frequently, this vortex is unstable in that it precesses about the axis resulting in circumferential variations in air flow. A consequence is that the combination of the gas with air is not regular, resulting in combustion pulsations. If the acoustic frequency of the furnace is such that Rayleigh's criterion is satisfied, then the combustion pulsations may be sustained, leading to excessive furnace vibrations.
  • The present invention arose from a consideration of this problem and of ways in which more regular combustion might be obtained.
  • According to the present invention, there is provided a gas burner tip in the form of a cylinder closed at one end except for an opening in an end wall that is oblique to the cylindrical surface and having an opening of smaller area lying wholly in the part of the cylindrical wall that is defined by a diametrical plane across which the end wall lies symmetrically.
  • An embodiment of the invention will now be described with reference to the accompanying drawings in which
    • Figure 1 shows a gas burner tip in side view;
    • Figure 2 shown the burner tip of Figure 1 from above; and
    • Figure 3 illustrates an end view, from inside the furnace, of a burner mounted at an opening in a furnace wall.
  • The tip A shown in Figure 1 has a barrel 1 of which the outer diameter is about 27mm. Its length is about 70mm and at the lower end is a mounting flange 2. Centrally, at its upper end, there is a ridge 3 about 8mm wide and flat end walls 4 and 5 slope down symmetrically from the sides of the ridge 3 at about 45°.
  • In one of the end walls 5 is a circular opening 8 of just over 20mm diameter. A circular opening 9 of smaller diameter, 15mm, is formed in the cylindrical wall of the barrel about half way between the ridge 3 and the top of the flange 2. The diametrical plane of the barrel 1 that contains the centre of the opening 8 is displaced from that which contains the centre of the opening 9 by 22½°. The opening 9 thus lies wholly within the diametrical plane of the barrel 1 that bisects the ridge 3 and across which the end wall 5 lies symmetrically.
  • Figure 3, shows six burner tips mounted in the opening 10 in the wall of a furnace. The boundary of they opening 10 tapers from a circle 11 in the inner face of the wall to a circle 12 in the outer face. Ourwardly from the outer face of the furnace wall.there extends a duct (not shown) through which air can flow to discharge through the opening 10 with a swirl in the anticlockwise direction. An oil burner 13 is arranged to discharge centrally through the opening 10, the outlet end of the burner 14 being about mid-way between the faces of the furnace wall.
  • A group of six gas burner tips A,connected to a common main (not shown) lying outside the furnace, are disposed equi-spaced around a circle that is concentric with the burner 14, the leading ends of the burner tips A lying forward of the oil burner 14 but rearwardly of the inner face of the furnace wall. Three of the tips, A1, are so arranged that gas discharging from the upper opening, 8, is discharged approximately towards the axis, but at a slight angle so that the gas has a swirl in the clockwise direction. Gas discharging from the lower openings 9 will be more oblique to the axis but will also swirl in the clockwise direction.
  • The other three tips, A2, are each disposed between two of the tips A1 and are arranged so that gas discharging from both the openings of each will have an anticlockwise direction of rotation and flow past, outwardly of, the tips A1.
  • An effect of the rotation of the gas will be to tend to constrain the air to flow symmetrically about the axis of the burner and so tend to decouple the zone in which gas and air is mixed and burned from the aerodynamically unstable region. The combustion zone will tend better to resemble the combustion produced by an axial oil burner so that gas and oil may be burned together to give a dual firing burner i.e. a burner in which the two fuels may be burnt.
  • Since the combustion in the pure gas burner is similar to the oil flame, mixed firing - with neighbouring burners using only gas and only oil - is easily attained. Also, the detailed residual pulsation levels of the burners firing only gas and only oil are not enhanced by burner interaction and hence the residual pulsation levels are lower than for single-fuel firing. Dual firing broadens the air-fuel delay time involved in the combustion, effectively dampening any tendencies to pulsate, but the periphery of the flame is predominantly gas controlled still producing some burner interaction. The residual pulsation levels for dual firing therefore lie between the single fuel and mixed firing uses.
  • In use of the tips that have been described,the flame will tend to be removed from the point of fuel injection so that the stabilising discs that are often provided on gas spuds may be dispensable. A benefit of this would be the resultant lower air velocities.
  • In modifications of the burner tip, it is envisaged that the opening 9 may be replaced by two or more openings in the part of the wall that is defined by a diametrical plane across which the end wall 5 lies symmetrically.
  • Other arrangements of the tips are also envisaged. In particular, all tips in a ring may be similarly orientated in the way that the tips A1 are orientated. Whilst gas from these tips is directed inwardly, none is directed directly to the axis, but at an angle such as to tend to induce orderly swirl.

Claims (5)

1. A gas burner tip in the form of a cylinder closed at one end except for an opening in an end wall that is oblique to the cylindrical surface and having an opening of smaller area lying wholly in the part of the cylindrical wall that is defined by a diametrical plane across which the end wall lies symmetrically.
2. A gas burner tip as claimed in claim 1 in which the holes are both circular and the diametrical plane containing the centre diametrical plane containing the centre of the hole in the end wall is displaced from the diametrical plane containing the centre of the hole in the cylindrical wall.
3 A gas burner tip as claimed in claim 2 in which the angle between the planes is 223°.
4. A gas burner comprising a cylindrical duct and means associated with the duct by which air can be caused to flow along the duct with a swirling motion, and a plurality of gas tips as claimed in any of claims 1 to 3 disposed concentrically around the axis of the duct, uniformly spaced from each other and all similarly orientated so that the gas from both openings of each is directed counter to the direction of swirl of the air.
5. A gas burner as claimed in claim 4 in which there is interspersed with the tips specified in claim 4 another set of tips, each disposed mid-way between an adjacent pair of the tips specified in claim 4, the tips of the second set being all similarly orientated so that gas from both openings of each is directed past, outwardly of the tips specified in claim 4, and in the direction of the swirl of the air.
EP84308113A 1983-11-22 1984-11-22 Improvements in or relating to burner tips Withdrawn EP0145381A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB838331127A GB8331127D0 (en) 1983-11-22 1983-11-22 Burner tips
GB8331127 1983-11-22

Publications (2)

Publication Number Publication Date
EP0145381A2 true EP0145381A2 (en) 1985-06-19
EP0145381A3 EP0145381A3 (en) 1985-10-02

Family

ID=10552154

Family Applications (1)

Application Number Title Priority Date Filing Date
EP84308113A Withdrawn EP0145381A3 (en) 1983-11-22 1984-11-22 Improvements in or relating to burner tips

Country Status (2)

Country Link
EP (1) EP0145381A3 (en)
GB (1) GB8331127D0 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU643044B2 (en) * 1990-06-29 1993-11-04 Babcock-Hitachi Kabushiki Kaisha Combustion system
US6651645B1 (en) * 1999-06-08 2003-11-25 Nunez Suarez Rene Maurico Pressurized combustion and heat transfer process and apparatus
JP2018040562A (en) * 2017-11-08 2018-03-15 ボルカノ株式会社 Burner device for mixed combustion, and boiler
CN108758635A (en) * 2018-07-06 2018-11-06 广东科达洁能股份有限公司 A kind of kiln whirlwind sheet

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3032097A (en) * 1958-07-07 1962-05-01 Babcock & Wilcox Co Method and apparatus for burning fluent fuel
US3076496A (en) * 1960-05-20 1963-02-05 Babcock & Wilcox Co Multiple nozzle gas burner
FR1482609A (en) * 1965-06-09 1967-05-26 Babcock & Wilcox Co Fluid fuel burner
JPS5835308A (en) * 1981-08-28 1983-03-02 Babcock Hitachi Kk Combustion method preventing resonance and its apparatus
JPS5864420A (en) * 1981-10-13 1983-04-16 Babcock Hitachi Kk Gas burner unit
JPS5875613A (en) * 1981-10-29 1983-05-07 Babcock Hitachi Kk Burner with reduced resonant vibration

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3032097A (en) * 1958-07-07 1962-05-01 Babcock & Wilcox Co Method and apparatus for burning fluent fuel
US3076496A (en) * 1960-05-20 1963-02-05 Babcock & Wilcox Co Multiple nozzle gas burner
FR1482609A (en) * 1965-06-09 1967-05-26 Babcock & Wilcox Co Fluid fuel burner
JPS5835308A (en) * 1981-08-28 1983-03-02 Babcock Hitachi Kk Combustion method preventing resonance and its apparatus
JPS5864420A (en) * 1981-10-13 1983-04-16 Babcock Hitachi Kk Gas burner unit
JPS5875613A (en) * 1981-10-29 1983-05-07 Babcock Hitachi Kk Burner with reduced resonant vibration

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
PATENTS ABSTRACTS OF JAPAN, vol. 7, no. 116 (M-216)[1261], 20th May 1983; & JP - A - 58 35 308 (BABCOCK HITACHI K.K.) 02-03-1983 *
PATENTS ABSTRACTS OF JAPAN, vol. 7, no. 157 (M-227)[1302], 9th July 1983; & JP - A - 58 64 420 (BABCOCK HITACHI K.K.) 16-04-1983 *
PATENTS ABSTRACTS OF JAPAN, vol. 7, no. 169 (M-231)[1314], 26th July 1983; & JP - A - 58 75 613 (BABCOCK HITACHI K.K.) 07-05-1983 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU643044B2 (en) * 1990-06-29 1993-11-04 Babcock-Hitachi Kabushiki Kaisha Combustion system
US6651645B1 (en) * 1999-06-08 2003-11-25 Nunez Suarez Rene Maurico Pressurized combustion and heat transfer process and apparatus
JP2018040562A (en) * 2017-11-08 2018-03-15 ボルカノ株式会社 Burner device for mixed combustion, and boiler
CN108758635A (en) * 2018-07-06 2018-11-06 广东科达洁能股份有限公司 A kind of kiln whirlwind sheet
CN108758635B (en) * 2018-07-06 2024-03-12 佛山市科达机电有限公司 Kiln cyclone sheet

Also Published As

Publication number Publication date
GB8331127D0 (en) 1983-12-29
EP0145381A3 (en) 1985-10-02

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PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

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AK Designated contracting states

Designated state(s): DE FR GB IT NL

PUAL Search report despatched

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Effective date: 19860318

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Owner name: BABCOCK POWER LIMITED

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Effective date: 19861215

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18W Application withdrawn

Withdrawal date: 19880129

RIN1 Information on inventor provided before grant (corrected)

Inventor name: WHARMBY, JOHN STEPHEN