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EP1616128A1 - Membrane metallique pour bruleur - Google Patents

Membrane metallique pour bruleur

Info

Publication number
EP1616128A1
EP1616128A1 EP20040714333 EP04714333A EP1616128A1 EP 1616128 A1 EP1616128 A1 EP 1616128A1 EP 20040714333 EP20040714333 EP 20040714333 EP 04714333 A EP04714333 A EP 04714333A EP 1616128 A1 EP1616128 A1 EP 1616128A1
Authority
EP
European Patent Office
Prior art keywords
section
gas burner
burner
membrane
curvature
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
EP20040714333
Other languages
German (de)
English (en)
Other versions
EP1616128B1 (fr
Inventor
Dinand Lamberts
Alfred Van Goor
Geert Folkers
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.)
Bekaert NV SA
Bekaert Combustion Technology NV
Original Assignee
Bekaert NV SA
Bekaert Combustion Technology NV
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 Bekaert NV SA, Bekaert Combustion Technology NV filed Critical Bekaert NV SA
Priority to EP04714333.4A priority Critical patent/EP1616128B1/fr
Publication of EP1616128A1 publication Critical patent/EP1616128A1/fr
Application granted granted Critical
Publication of EP1616128B1 publication Critical patent/EP1616128B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/12—Radiant burners
    • F23D14/14—Radiant burners using screens or perforated plates
    • F23D14/145—Radiant burners using screens or perforated plates combustion being stabilised at a screen or a perforated plate
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2203/00—Gaseous fuel burners
    • F23D2203/10—Flame diffusing means
    • F23D2203/101—Flame diffusing means characterised by surface shape
    • F23D2203/1017—Flame diffusing means characterised by surface shape curved
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2212/00—Burner material specifications
    • F23D2212/20—Burner material specifications metallic
    • F23D2212/201—Fibres

Definitions

  • the present invention relates to a gas burner comprising a metal burner 5 membrane.
  • the first drawback of these burners is that for a given dimension, they do not allow for a large range in output power: at low power, i.e. if the gasflow is low, there is a risk for flame extinguishment, and at high powers, i.e. if the gasflow is high, there is a risk that the flame blows off.
  • a third drawback of these burners is that different parts have to be punched, formed and welded together which leads to expensive burners.
  • a gas burner according the present invention comprises a metal burner membrane. Geometrically this burner membrane comprises a base
  • the base section has a smallest radius of curvature Rb a _ ⁇ . What is meant with "smallest radius of curvature" will be
  • the base section is connected uninterruptedly to the closing section through a transition region: the transition region burner membrane comprises the same elements as the base and closing section.
  • the transition region has a smallest radius of curvature 5 reunion being larger than zero and being smaller or equal to 0 ⁇ rtransiuon ⁇ Rba ⁇ .
  • R is a plane, hence R as S is infinitely large, is not excluded. More preferred is: 0.02 x R b ase ⁇ transttion ⁇ 0.7 x Rt, asa . Even more preferred is: 0.02 R b as ⁇ r ⁇ au,,,, ⁇ 0.35 x R b as ⁇
  • the closing section is no limitation on the smallest radius of curvature of 10 .
  • curvature can be defined: each of them is associated with a particular cut according a plane containing the normal line at the point under consideration. The intersection of this plane with the burner membrane results in a trajectory.
  • the radius of curvature is the radius of the circle in the intersecting plane, which osculates to second order the trajectory at
  • the smallest radius is selected.
  • the smallest of all smallest radii of the section can be defined to be the smallest
  • the invention relates to the embodiment of this geometrical construction, which of course is subject to engineering tolerances.
  • the invention is not delimited to the abstract geometrical shape as such but to the shape of the actual burner membrane. This shape can be easily measured by means of an appropriate computerised 3-D measuring bench that allows for immediate determination of the geometrical features in general and the radii of curvature in particular.
  • the shape of the burner membrane influences the functioning of the burner in the following way: those regions of the burner membrane that have a smaller radius of curvature yield a lower gas speed outside the membrane compared to the regions with a higher radius of curvature.
  • the transition from base section to 30 closing section is realised without interruption.
  • uninterrupted is meant that the membrane forming the different sections (base, transition and closing) are not connected by any means that would lead to a seam of the membrane with a blocked gas flow at the burner surface as a result. I.e. the three sections: base, transition and closing must be gas
  • the three sections can be realised uninterruptedly in one of the following ways: 5 - by using a fabric of braided or knitted or woven stainless steel fibres.
  • Such fabric can be woven or braided or knitted in such a way that it fulfils the geometrical requirements of the invention
  • the wire mesh can also be integrated into the stainless steel fibre fabric i.e. it can be
  • the uninterrupted burner membrane ensures a flame front in every • - • :,! section of the burner and in particularin the transition region. This - •'.' improves greatly the stability of the flame.
  • FIGURE 1 illustrates the basic geometrical principles of the invention in perspective view.
  • FIGURE 2 illustrates a preferred embodiment of the invention in perspective view
  • FIGURE 3(a) shows a cut of the preferred embodiment along the line A, A' of Fig.2 along with the geometrical elements.
  • FIGURE 3(b) shows a cut of the preferred embodiment along the line 25 A, A' of Fig.2 along with the physical features.
  • FIGURE 4 (a) shows a second preferred embodiment based on a rectangular cross section of the base section.
  • FIGURES 4(b) and 4(c) show the section through planes AA' and BB' of Fig.4(a) respectively.
  • FIGURE 4(d) shows a top view cross section of the burner of Fig.
  • FIGURE 5(a) shows a third preferred embodiment in side view.
  • FIGURE 5(b) shows the third preferred embodiment from above.
  • FIGURE 5(c) shows an alternate to the third preferred embodiment in side view.
  • FIGURE 6(a) shows a fourth preferred embodiment in side view.
  • FIGURE 6(b) shows the fourth preferred embodiment from above.
  • FIGURE 6(c) shows an alternate to the fourth preferred embodiment in side view.
  • Figure 1 10 The basic geometrical features of the invention are illustrated in Figure 1 10 where a shape 100 of a burner membrane is depicted consisting out of a base section- 102, a transition section 104 and a top section 106. Take " 'a' as point under consideration, 'a' has its normal N to the surface.
  • a smallest radius of curvature 'rtransiuon' can be found for the transition region. It is essential to the invention that the smallest radius of curvature of the transition region is smaller or equal than the smallest radius of curvature of the base section.
  • Figure 2 depicts a first preferred embodiment 200 in perspective view.
  • the base section 201 is frustoconical in shape and reaches its minimum radius of curvature on the circle 204.
  • the transition region 202 is a surface section of a torus and the closing section 203 is a flat disc.
  • Figure 3 (a) shows the geometrical elements of the first preferred embodiment of Figure 2 according the line AA". Only the outer surface of the surface membrane is depicted in order to bring forward the geometrical elements.
  • the frustoconical base section 201 has its
  • the half top angle of the cone 326 was about 30° although 0° (a cylindrical base section) turned out to work just as well (embodiment not shown). Higher top angles -the maximum being 90°, a flat plane - are also not 5 excluded. All points on the circle 204 share the same minimum radius of curvature R
  • the sphere 320 with radius R ba s e defines the largest 'smallest radius of curvature' the transition region may have according the invention.
  • the transition region is part of the surface of a torus formed by a circle 324 that is rotated around the symmetry axis 340.
  • the radius of circle 324 determines the radius of the transition region 'rtran.iuon' 330/ Part of a torus surface between the plane of circle 204 and a plane parallel to the latter s taken as the transition region.
  • the' torus can.also be constructed by rotating an ellipse or an oval or any other rounded figure around the axis of symmetry 340.
  • the closing section 203 is a flat disc in this embodiment.
  • the closing section is a small inverted sphere cap thus entailing a depression at the centre of the
  • crossover from base section to transition region need not be smooth (with 'smooth' is meant continuous first order derivatives) but must be uninterrupted (zero order 25 continuity).
  • Figure 3b depicts the physical features of the first preferred embodiment along the cut according plane AA' indicated in Figure 2.
  • 201' indicates the stamped foraminated metal plate made out of a single piece of metal 30 plate.
  • the foraminated metal plate is provided with a number of holes.
  • the change in hole size at the transition region due to the deformation of the plate is not relevant to the flow speed of the gas.
  • a piece of knitted metal fibre fabric 305 is tensioned over the base
  • the fabric was attached to the foraminated plate by means of spot welding although other means of fastening are equally well possible for example - without being exhaustive - by sewing or by 5 stapling.
  • the fabric was kept on the foraminated plate by means of a clamping ring that was spot welded to the plate.
  • Knitted metal fibre fabric allows for a high elongation thus leading to a 10 continuous transition from the base section to the closing section.
  • FIG 4 a preferred embodiment is illustrated that is more suited for replacement of a rectangular type burner.
  • the cross-section of the 25 base section is essentially rectangular of which the edges are rounded.
  • Figure 4b is a cross-section along plane AA' of Figure 4a: the base section 401 smoothly goes over into the transition region 402 which approximates the upper half of an ellipse with a minor half axis indicated by 406 and a major half axis indicated by 405.407 indicates the 30 osculating circle associated with the smallest radius of curvature of the transition region.
  • Figure 4c shows a cut along the line BB'.
  • Figure 4c shows an essentially identical shape as the AA' cut, but here the half ellipse has been cut in two, and the two quarter pieces have been displaced the appropriate distance.
  • Figure 4d shows the closing view of
  • the closing section has vanished into a 5 single line 408.
  • the closing section is a
  • a knitted metal fibre fabric 512 was spot welded to the wire mesh.
  • FIG. 5(c) An alternative to the third embodiment is depicted in Figure 5(c). Like parts of the burner membrane according the third embodiment are 20 identified with primed numbers.
  • the transition region 502' is in the form of a circular ridge. The top of the ridge has a radius of curvature 506', which turns out to be the smallest radius of curvature of the transition region.
  • transition region 606 is 9 mm although values from 3 mm upward are also possible.
  • the transition region 602' is in the form of a ridge extending substantially the length of the longitudinal burner membrane.
  • the top of the ridge has a radius of curvature 606', which tums out to be the smallest radius of curvature of the transition region. Again the closing section vanishes into a line 604'.

Landscapes

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

Abstract

L'invention concerne un brûleur à gaz dont la membrane métallique comprend une partie de base (201), une partie de fermeture (203) et une zone de transition (202) entre ces deux parties. La forme de la membrane est telle que le rayon de courbure le plus faibles de la zone de transition est inférieure au rayon de courbure le plus faible de la partie de base. De plus, la membrane du brûleur s'étend en continu de la partie de base 'à la partie de fermeture via la zone de transition. Un tel brûleur à gaz offre notamment les avantages suivants : vaste plage de puissances dynamiques, front de flamme amélioré et faible coût de fabrication.
EP04714333.4A 2003-04-18 2004-02-25 Brûleur à membrane métallique Expired - Lifetime EP1616128B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP04714333.4A EP1616128B1 (fr) 2003-04-18 2004-02-25 Brûleur à membrane métallique

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP03101079 2003-04-18
PCT/EP2004/050205 WO2004092647A1 (fr) 2003-04-18 2004-02-25 Membrane metallique pour bruleur
EP04714333.4A EP1616128B1 (fr) 2003-04-18 2004-02-25 Brûleur à membrane métallique

Publications (2)

Publication Number Publication Date
EP1616128A1 true EP1616128A1 (fr) 2006-01-18
EP1616128B1 EP1616128B1 (fr) 2016-05-04

Family

ID=33185953

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04714333.4A Expired - Lifetime EP1616128B1 (fr) 2003-04-18 2004-02-25 Brûleur à membrane métallique

Country Status (5)

Country Link
US (2) US20060251998A1 (fr)
EP (1) EP1616128B1 (fr)
KR (2) KR20110104080A (fr)
CN (2) CN100557310C (fr)
WO (1) WO2004092647A1 (fr)

Cited By (3)

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WO2018215241A1 (fr) * 2017-05-24 2018-11-29 Bekaert Combustion Technology B.V. Brûleur à gaz à prémélange à allumage vers l'intérieur
WO2019011738A1 (fr) * 2017-07-13 2019-01-17 Bekaert Combustion Technology B.V. Brûleur à gaz de prémélange
WO2019011736A1 (fr) * 2017-07-13 2019-01-17 Bekaert Combustion Technology B.V. Brûleur à prémélange gazeux

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EP2079961B1 (fr) 2006-11-08 2015-12-23 Flare Industries, LLC Torche modulaire et son utilisation pour le brûlage à torche de gaz résiduaire
US8726851B2 (en) 2007-10-25 2014-05-20 Bekaert Combustion Technology B.V. Heat exchanger element with a combustion chamber for a low CO and NOx emission combustor
WO2009077505A2 (fr) 2007-12-17 2009-06-25 Bekaert Combust. Technologie. B.V. Nouveau brûleur à prémélange
US20120193452A1 (en) * 2009-12-11 2012-08-02 Nv Bekaert Sa Burner with low porosity burner deck
TWI570362B (zh) 2010-12-20 2017-02-11 索拉羅尼克斯股份有限公司 具有浮凸屏之氣體加熱輻射發射體
IT1406865B1 (it) * 2011-01-12 2014-03-14 Worgas Bruciatori Srl Bruciatore ad elevata stabilita' perimetrale
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EP2636951A1 (fr) 2012-03-07 2013-09-11 Flare Industries, LLC Appareil et procédé de brûlage à la torche de gaz résiduaire
EP2844920B1 (fr) 2012-05-03 2016-05-18 Bekaert Combustion Technology B.V. Brûleur à prémélange gazeux
JP6029857B2 (ja) * 2012-05-23 2016-11-24 株式会社パロマ 濃淡バーナ
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WO2014067744A1 (fr) 2012-10-31 2014-05-08 Bekaert Combustion Technology B.V. Brûleur à prémélange de gaz
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EP2789911B1 (fr) 2013-04-09 2016-07-20 Bekaert Combustion Technology B.V. Brûleur de gaz pré-mélangé
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EP3652484A1 (fr) * 2017-07-13 2020-05-20 Bekaert Combustion Technology B.V. Brûleur à gaz à prémélange
US10989406B2 (en) * 2018-02-23 2021-04-27 Fulton Group N.A., Inc. Compact inward-firing premix fuel combustion system, and fluid heating system and packaged burner system including the same
US11236903B2 (en) 2018-02-23 2022-02-01 Fulton Group N.A., Inc. Compact inward-firing premix fuel combustion system, and fluid heating system and packaged burner system including the same
US12338993B2 (en) 2018-02-23 2025-06-24 Fulton Group N.A., Inc. Compact flat plate premix fuel combustion system, and fluid heating system and packaged burner system including the same
WO2019165378A1 (fr) * 2018-02-23 2019-08-29 Fulton Group N.A., Inc. Système compact de combustion de surface à maille de prémélange à allumage vers l'intérieur, et système de chauffage de fluide et système de brûleur en boîtier le comprenant
WO2019207559A2 (fr) * 2018-04-13 2019-10-31 Fulton Group N.A., Inc. Système compact de combustion à deux combustibles, et système de chauffage de fluide et système de brûleur conditionné incluant celui-ci
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EP3856447A1 (fr) * 2018-10-17 2021-08-04 Beckett Thermal Solutions Ltd. Procédé de formation d'une membrane de brûleur à gaz
CN114945777A (zh) 2020-01-08 2022-08-26 贝卡尔特燃烧技术股份有限公司 气体燃烧器和加热器具
NL2024623B1 (en) 2020-01-08 2021-09-07 Bekaert Combustion Tech Bv Gas burner and heating appliance
NL2028637B1 (en) 2021-07-06 2023-01-12 Bekaert Combustion Tech Bv Premix gas burner system and method

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018215241A1 (fr) * 2017-05-24 2018-11-29 Bekaert Combustion Technology B.V. Brûleur à gaz à prémélange à allumage vers l'intérieur
US11215366B2 (en) 2017-05-24 2022-01-04 Bekaert Combustion Technology B.V. Inwardly firing premix gas burner
WO2019011738A1 (fr) * 2017-07-13 2019-01-17 Bekaert Combustion Technology B.V. Brûleur à gaz de prémélange
WO2019011736A1 (fr) * 2017-07-13 2019-01-17 Bekaert Combustion Technology B.V. Brûleur à prémélange gazeux

Also Published As

Publication number Publication date
CN101545634A (zh) 2009-09-30
US20060251998A1 (en) 2006-11-09
KR20110104080A (ko) 2011-09-21
WO2004092647A1 (fr) 2004-10-28
US20110081621A1 (en) 2011-04-07
EP1616128B1 (fr) 2016-05-04
KR20050122273A (ko) 2005-12-28
CN1777775A (zh) 2006-05-24
CN100557310C (zh) 2009-11-04
CN101545634B (zh) 2012-04-04

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