WO2002044618A1 - Bruleur a premelange presentant un capuchon d'extremite impermeable courbe - Google Patents

Bruleur a premelange presentant un capuchon d'extremite impermeable courbe Download PDF

Info

Publication number
WO2002044618A1
WO2002044618A1 PCT/EP2001/013700 EP0113700W WO0244618A1 WO 2002044618 A1 WO2002044618 A1 WO 2002044618A1 EP 0113700 W EP0113700 W EP 0113700W WO 0244618 A1 WO0244618 A1 WO 0244618A1
Authority
WO
WIPO (PCT)
Prior art keywords
end cap
impermeable end
burner body
impermeable
tubular burner
Prior art date
Application number
PCT/EP2001/013700
Other languages
English (en)
Inventor
Dirk Ten Hoeve
Original Assignee
Furigas Assen B.V.
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 Furigas Assen B.V. filed Critical Furigas Assen B.V.
Priority to AU2002220725A priority Critical patent/AU2002220725A1/en
Priority to EP01998769A priority patent/EP1337789B1/fr
Priority to DE60107597T priority patent/DE60107597T2/de
Priority to AT01998769T priority patent/ATE284005T1/de
Publication of WO2002044618A1 publication Critical patent/WO2002044618A1/fr

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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2203/00Gaseous fuel burners
    • F23D2203/10Flame diffusing means
    • F23D2203/101Flame diffusing means characterised by surface shape
    • F23D2203/1012Flame diffusing means characterised by surface shape tubular
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2211/00Thermal dilatation prevention or compensation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2213/00Burner manufacture specifications

Definitions

  • the present invention relates to a premix burner for combustion of premixed gas-air mixtures.
  • Premix burners are well known to the state of the art. Some of these premix burners comprise a tubular burner body. Such a burner is described in US5022352, where it is used to heat the water of e.g. a central heating system.
  • Such premix burner comprising a tubular burner body, preferably made out of steel plate, having along its tubular burner body at least one, but usually several matrixes of burning slots and/or holes.
  • the tubular burner body is closed at one side by a so-called end cap.
  • the premix burner as known in the art may show some defects after a certain period of use.
  • premix burners nowadays are to be able to modulate the air-gas throughput over a wider range.
  • premix burners have to be able to burn very low amounts of air-gas mixtures.
  • the combustion is situated very close to the tubular burner body. The lower the throughput, the closer the flame front is situated near the tubular burner body. A part of the combustion energy will heat the tubular burner body and the end cap, so causing thermal expansion of both tubular burner body and end cap.
  • both elements being end cap and tubular burner body, due to e.g. different temperatures of both elements, or different thermal expansion coefficients of both elements.
  • the tubular body is heated to higher temperature levels, due to a closer flame front, and is so subject of more severe thermal stresses. This difference may cause thermal cracks, especially at the welding zone of both elements.
  • tubular burner bodies which are able to resist better the severe thermal expansions at the connection between tubular burner body and impermeable end cap, both parts made out of metal, usually steel plate.
  • a premix burner comprises a tubular burner body, an impermeable end cap and possibly a diffusion system, located inside the tubular burner body.
  • the tubular burner body comprises at least one matrix of burning slots and/or holes on its surface.
  • Premix air-gas mixture is blown into the tubular burner body via an appropriate inlet, usually at the lower side of the tubular burner body. Since the tubular burner body is closed at the other side by the impermeable end cap, the air-gas mixture is forced to flow, possibly via an air-gas diffuser, through the burning slots and/or holes, where combustion takes place.
  • the risk on thermal cracks may be avoided to a large extend, by welding an impermeable end cap to the longitudinal end of the tubular burner body (to be closed by this impermeable end cap) of which the surface of the impermeable end cap is at least partially curved, whereas the bending radii of each point on the impermeable end cap surface is larger than 3 times the metal thickness of the impermeable end cap material.
  • radii larger than 4 times the metal thickness of the impermeable end cap material are used.
  • the border of the impermeable end cap and the longitudinal end of the tubular burner body has to engage closely.
  • this impermeable end cap is to be welded to the longitudinal end in such a way that the curvature of the impermeable end cap surface extends outwards of the tubular burner body.
  • extending outwards from the tubular burner body is referred to as "convex”.
  • the impermeable end cap is welded to the longitudinal end over the impermeable end cap's lower border.
  • the impermeable end cap may also be connected to the tubular burner body, having a curvature extending inwards to the tubular burner body.
  • extending outwards from the tubular burner body is referred to as "concave”.
  • the impermeable end cap may be curved over its whole surface, having bending radii larger than 3 times the metal thickness of the impermeable end cap material. However, the bending radius may differ for each point of the surface of the impermeable end cap.
  • the impermeable end cap is only bent at the outer border of the impermeable end cap, where the end cap is connected to the tubular burner body.
  • the impermeable end cap is preferably substantially flat, having a bending radii being substantially infinite, "substantially infinite” is to be understood as larger than 10 times the maximum distance between to points of the border of the impermeable end cap.
  • impermeable end cap When, according to the present invention, such impermeable end cap is welded to the longitudinal end of the tubular burner body, with a concave or convex curvature, the relatively large radius or radii will enable the impermeable end cap to compensate the difference in thermal expansion between tubular burner body and impermeable end cap, during combustion of combustible gas/air mixture at the burner slots, by slightly changing the radius or radii. This slight change prevents the occurrence of too large stresses over the welding between tubular burner body and impermeable end cap. As a result, thermal cracks may be avoided.
  • the tubular burner body and the impermeable end cap are made out of metal, e.g. metal or steel plate, preferably stainless steel. Preferably the same material is used for both elements. Metal thickness' of both tubular burner body and impermeable end cap ranging from 0.2 to 1.5 mm may be used, preferably ranging from 0.2 to 1 mm, such as 0.3mm, 0.5mm, 0.6mm, 0.8mm or 1 mm.
  • Tubular burner body may be provided by different techniques. Usually, a tubular burner body is provided by rolling a tube out of a perforated metal plate. The tube is closed by welding the plate edges in axial direction, e.g. by laser of TIG-welding.
  • the impermeable end cap is pressed out of metal plate.
  • the lower border of the impermeable end cap and the longitudinal end of the tubular burner body may be welded to each other in several different ways, depending on the dimensions of the lower border of the impermeable end cap as compared to the circumference to the longitudinal end of the tubular burner body, either when the curvature is used in a concave or convex way.
  • both impermeable end cap end tubular burner body are preferably spot welded or laser welded to each other.
  • both impermeable end cap end tubular burner body are preferably spot welded or laser welded to each other.
  • the diameter is larger than 0.5cm, preferably it ranges from 2.5 to 25 cm, most usually however it ranges between 6 to 8 cm.
  • a height of the tubular burner body preferably ranges from 10 to 50 cm, most usually in the range of 10 to 20. Even so, the tubular burner body is not to be understood as having a circular cross-section when cut longitudinally. Other cross sections may be used, such as elliptic or oval cross sections.
  • Such premix burners as subject of the invention may be used in heating devices, heating water or air, e.g. central heating systems and boilers.
  • FIGURE 1 shows schematically a premix burner as subject of the invention .
  • - FIGURE 2 is a radial cut of a tubular burner body, being part of a premix burner as subject of the invention.
  • FIGURE 3 is an impermeable end cap, being part of a premix burner as subject of the invention.
  • - FIGURE 4a is an axial cut of detail A out of FIGURE 1.
  • - FIGURE 4b is an axial cut of an alternative embodiment of the present invention.
  • FIGURES 5a, 5b, 5c and 5d show different welding possibilities to connect an impermeable end cap and a tubular burner body as subject of the invention.
  • FIGURES 6a, 6b, 6c, 6d and 6e show different impermeable end cap surfaces as subject of the invention.
  • FIGURE 1 A part of a premix burner, to which the present invention relates, is shown in FIGURE 1.
  • a tubular burner body 11 is closed at its longitudinal end 12 with an impermeable end cap 13, having a convex curvature. Both elements, being impermeable end cap 13 and tubular burner body
  • the premix air-gas mixture is forced through the burning slots and/or holes 16, which are provided in the tubular burner body 11. Leaving the burning slots and/or holes 16, the premix air-gas mixture is subjected to combustion.
  • a longitudinal cut II' at the longitudinal end 12 of the tubular burner body is shown in FIGURE 2.
  • the longitudinal end 12 has an inner circumference 21 and an outer circumference 22.
  • the material thickness of the tubular burner body is indicated by T1.
  • An impermeable end cap 13 is shown into more detain in FIGURE 3.
  • the impermeable end cap 13 comprises a lower border 31 , which has an inner side 32 and an outer side 33. According to the invention, the impermeable end cap surface 34 is curved.
  • the impermeable end cap has a material thickness as indicated by T2.
  • the thickness' T1 and T2 may be different, but an equal thickness is preferred in the range of 0.2 to 1.5mm e.g. in the range 0.4 to 1 mm, most preferably 0.6mm.
  • a preferred embodiment of a premix burner as shown in FIGURE 1 has a tubular burner body height between 10 and 14cm, e.g. 12 cm and a diameter of the tubular burner body of 7cm. Most preferably, tubular burner body and impermeable end cap are made out of stainless steel alloy.
  • FIGURE 4a An axial cut of detail A of FIGURE 1 is shown in FIGURE 4a. Again, an impermeable end cap 13 and a tubular burner body 11 are welded to each other in the welding zone 14. This welding zone has a thickness D. At least a part of the impermeable end cap surface 34 is curved, with a bending radius R. Preferably this curved part of the impermeable end cap surface is located near the welding zone 14. The curvature of the impermeable end cap surface extends outward from the tubular burner body (as indicated with flash 41 ).
  • FIGURE 4b An alternative axial cut of another embodiment of a premix burner as subject of the invention is shown in FIGURE 4b.
  • An impermeable end cap with a curvature extending inwards the tubular burner body (as indicated with flash 42) is shown.
  • a radius in the range of 2mm to 10mm is preferred, depending on the material thickness of the impermeable end cap.
  • an impermeable end cap material thickness T2 of 0.6mm a radius not smaller than 2.5mm is preferred.
  • FIGURE 5a, 5b and 5c there are different ways to weld impermeable end cap 13 and tubular burner body 11 to each other.
  • the inner side 32 of the curved impermeable end cap 13 engages the outer circumference 22 of the tubular burner body 11.
  • the impermeable end cap surface is a convex way.
  • the welding zone 14 is characterized by an overlap of both impermeable end cap and tubular burner body over a distance D.
  • D is kept smaller than 6mm. This welding may be done by spot welding, however preferably laser welding is used.
  • the outer side 33 of the curved impermeable end cap 13 engages the inner circumference 21 of the tubular burner body 11.
  • the impermeable end cap surface is a convex way.
  • the welding zone 14 is characterized by an overlap of both impermeable end cap and tubular burner body over a distance D.
  • D is kept smaller than 6mm. This welding may be done by spot welding, however preferably laser welding is used.
  • impermeable end cap and tubular burner body "face-to-face" as shown in FIGURE 5c.
  • the lower border 31 of impermeable end cap 13 and the longitudinal end 12 of tubular burner body 11 have essentially the same circumference. They are places one to the other and are welded together by TIG- welding, but preferably by laser welding.
  • An extra advantage of this connection is that at the welding zone 14, which thickness is usually less 6mm, there is no overlap of two layers of material (one from the impermeable end cap, the other from the tubular burner body).
  • laser welding techniques are used to connect impermeable end cap and tubular burner body face-to-face. Using this technique, the thickness D of the welding zone 14 is reduced to a minimum.
  • the outer side 33 of the curved impermeable end cap 13 engages the inner circumference 21 of the tubular burner body 11.
  • the impermeable end cap surface is a concave way.
  • the welding zone 14 is characterized by an overlap of both impermeable end cap and tubular burner body over a distance D.
  • D is kept smaller than 6mm. This welding may be done by spot welding, however preferably laser welding is used.
  • FIGURE 5band FIGURE 5d there is an extra additional thermal expansion difference, caused by the presence of a zone where two layers of material are present.
  • FIGURE 6a shows an impermeable end cap 13, which has an elliptic curvature. In each point of the impermeable end cap surface, a different radius may occur.
  • An alternative is shown in FIGURE
  • an impermeable end cap 13 has a substantially flat zone 61 , and a zone 62 at the border of the impermeable end cap which is curved inwards the tubular body of the premix burner as subject of the invention.
  • the bending radii in the zone 61 and 62 are larger than 3 times the thickness of the impermeable end cap material.
  • the bending radii are substantially infinite, at least larger than 10 times the diameter 63 of the circular impermeable end cap. It is clear that the tubular burner body has a diameter, which is essentially identical to the diameter 63.
  • the border of the impermeable end cap and the longitudinal end of the tubular burner body have to engage closely.
  • the bending radii are substantially infinite, at least larger than 10 times the largest distance between two points of the border of the impermeable end cap.
  • FIGURE 6c, FIGURE 6d and FIGURE 6e show an impermeable end cap 13, which has a W-like shape.
  • FIGURE 6c here, only a part 64 of the en cap 13 is curved, and this curvature is extending outwards from the tubular burner body 11.
  • FIGURE 6d a large part of the impermeable end cap 13 is concave.
  • FIGURE 6e shows an impermeable end cap which is partially convex (65) and partially concave (66)

Abstract

La présente invention concerne un brûleur à prémélange présentant un corps de brûleur tubulaire et un capuchon d'extrémité imperméable. Ce capuchon d'extrémité imperméable, qui assure la fermeture dudit corps de brûleur tubulaire, est soudé audit corps de brûleur tubulaire. Selon la présente invention, ledit capuchon d'extrémité imperméable est au moins partiellement courbe et chaque point de la surface du capuchon d'extrémité imperméable présente un rayon de courbure R et une épaisseur de matière T, chaque R étant supérieur à 3xT.
PCT/EP2001/013700 2000-12-01 2001-11-08 Bruleur a premelange presentant un capuchon d'extremite impermeable courbe WO2002044618A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AU2002220725A AU2002220725A1 (en) 2000-12-01 2001-11-08 Premix burner with curved impermeable end cap
EP01998769A EP1337789B1 (fr) 2000-12-01 2001-11-08 Bruleur a premelange presentant un capuchon d'extremite impermeable courbe
DE60107597T DE60107597T2 (de) 2000-12-01 2001-11-08 Vormischbrenner mit gekrümmter, undurchlässiger endkappe
AT01998769T ATE284005T1 (de) 2000-12-01 2001-11-08 Vormischbrenner mit gekrümmter, undurchlässiger endkappe

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP00204306.5 2000-12-01
EP00204306 2000-12-01

Publications (1)

Publication Number Publication Date
WO2002044618A1 true WO2002044618A1 (fr) 2002-06-06

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Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2001/013700 WO2002044618A1 (fr) 2000-12-01 2001-11-08 Bruleur a premelange presentant un capuchon d'extremite impermeable courbe

Country Status (5)

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EP (1) EP1337789B1 (fr)
AT (1) ATE284005T1 (fr)
AU (1) AU2002220725A1 (fr)
DE (1) DE60107597T2 (fr)
WO (1) WO2002044618A1 (fr)

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WO2004092647A1 (fr) 2003-04-18 2004-10-28 N.V. Bekaert S.A. Membrane metallique pour bruleur
JP2013513774A (ja) * 2009-12-11 2013-04-22 ベーカート・コンバスチョン・テクノロジー・ベスローテン・フェンノートシャップ 低多孔率バーナデッキを有するバーナ
EP2037175B1 (fr) * 2007-09-12 2016-11-23 Polidoro S.p.A. Brûleur à prémélange
WO2021078949A1 (fr) 2019-10-25 2021-04-29 Bekaert Combustion Technology B.V. Brûleur à prémélange gazeux entièrement prémélangé stabilisé en surface pour brûler de l'hydrogène gazeux, et procédé de démarrage d'un tel brûleur
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FR2676269A3 (en) * 1991-03-13 1992-11-13 Hans Viessmann Perforated-surface gas burner
US5211552A (en) * 1990-08-15 1993-05-18 Alzeta Corporation Adiabatic surface combustion with excess air
US5743727A (en) * 1997-01-21 1998-04-28 Burner Systems International, Inc. Premixed gas burner
EP0905446A2 (fr) * 1997-09-24 1999-03-31 Robert Bosch Gmbh Brûleur atmosphérique à gaz refroidi par eau

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US1874346A (en) * 1929-05-27 1932-08-30 Frederick A Paschke Fuel burner
GB1258784A (fr) * 1968-01-18 1971-12-30
GB1423829A (en) * 1972-11-22 1976-02-04 Greaves D V Noise reduction in gas burners
US5050385A (en) * 1982-10-06 1991-09-24 Hitachi, Ltd. Inner cylinder for a gas turbine combustor reinforced by built up welding
EP0245084A1 (fr) * 1986-05-08 1987-11-11 Aos Holding Company Elément de combustion pour un brûleur à rayonnement
WO1992019920A1 (fr) * 1989-11-06 1992-11-12 Bruno Coussement Chaudiere de chauffage central et/ou de production d'eau chaude sanitaire, bruleur pour combustible gazeux, et installation de chauffage central et de production d'eau chaude sanitaire utilisant ladite chaudiere
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2004092647A1 (fr) 2003-04-18 2004-10-28 N.V. Bekaert S.A. Membrane metallique pour bruleur
EP2037175B1 (fr) * 2007-09-12 2016-11-23 Polidoro S.p.A. Brûleur à prémélange
JP2013513774A (ja) * 2009-12-11 2013-04-22 ベーカート・コンバスチョン・テクノロジー・ベスローテン・フェンノートシャップ 低多孔率バーナデッキを有するバーナ
US11378273B2 (en) 2017-01-11 2022-07-05 A. O. Smith Corporation Reduced resonance burner
WO2021078949A1 (fr) 2019-10-25 2021-04-29 Bekaert Combustion Technology B.V. Brûleur à prémélange gazeux entièrement prémélangé stabilisé en surface pour brûler de l'hydrogène gazeux, et procédé de démarrage d'un tel brûleur
NL2024101B1 (en) 2019-10-25 2021-07-19 Bekaert Combustion Tech Bv Surface stabilized fully premixed gas premix burner for burning hydrogen gas, and method for starting such burner

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Publication number Publication date
EP1337789A1 (fr) 2003-08-27
ATE284005T1 (de) 2004-12-15
DE60107597D1 (de) 2005-01-05
EP1337789B1 (fr) 2004-12-01
AU2002220725A1 (en) 2002-06-11
DE60107597T2 (de) 2005-12-08

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