EP2863121B1 - Buse pour un brûleur à gaz - Google Patents

Buse pour un brûleur à gaz Download PDF

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Publication number
EP2863121B1
EP2863121B1 EP14185135.2A EP14185135A EP2863121B1 EP 2863121 B1 EP2863121 B1 EP 2863121B1 EP 14185135 A EP14185135 A EP 14185135A EP 2863121 B1 EP2863121 B1 EP 2863121B1
Authority
EP
European Patent Office
Prior art keywords
outlet opening
nozzle
diameter
channel
pin
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.)
Active
Application number
EP14185135.2A
Other languages
German (de)
English (en)
Other versions
EP2863121A3 (fr
EP2863121A2 (fr
Inventor
Ricardo Ferreira
Vasco Zeferina
Alexandre Afonso
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch GmbH
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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP2863121A2 publication Critical patent/EP2863121A2/fr
Publication of EP2863121A3 publication Critical patent/EP2863121A3/fr
Application granted granted Critical
Publication of EP2863121B1 publication Critical patent/EP2863121B1/fr
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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
    • F23D14/58Nozzles characterised by the shape or arrangement of the outlet or outlets from the nozzle, e.g. of annular configuration
    • 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
    • F23D14/26Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
    • 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
    • F23D14/70Baffles or like flow-disturbing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/11001Impinging-jet injectors or jet impinging on a surface
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/11401Flame intercepting baffles forming part of burner head

Definitions

  • the invention relates to a nozzle for a gas burner according to claim 1.
  • a nozzle for a burner wherein the nozzle has a channel, wherein in the channel a pin is provided with a guide surface for guiding a fuel.
  • a burner for fossil fuels wherein the burner has a nozzle which emits fuel into a channel, wherein a flow-shaping element is arranged in the channel. After the flow-shaping element, the outlet opening of the channel is provided.
  • a nozzle for a gas burner according to the preamble of the first claim wherein the nozzle has a channel with an outlet opening, wherein a flow element is arranged outside the outlet opening, wherein the flow element is fastened via a sleeve in the channel.
  • a nozzle for a gas burner wherein a channel is provided, wherein the channel has an outlet opening, wherein outside of the outlet opening a flow element is provided, wherein the flow element has a gyro plate and a spaced apart in the flow direction mushroom head as another flow element.
  • the object of the invention is to provide an improved nozzle for a gas burner.
  • An advantage of the described nozzle is that the fuel is efficiently fluidized with air by the nozzle with little pressure loss. This is achieved in that the nozzle has a channel in which the fuel is conveyed, wherein a flow element is provided, which is arranged outside the outlet opening of the nozzle.
  • the flow element is designed in such a way that an optimal turbulence of the fuel with air, which is conveyed outside the nozzle along the nozzle, takes place.
  • due to the shape of the flow element a small pressure drop is achieved.
  • the flow element is arranged outside the outlet opening, and that the cross section of the flow element increases with increasing distance to the outlet opening.
  • a guide surface is provided, which leads away the fuel from a center axis of the nozzle and thus efficiently mixed with an air flow, which flows along an outer surface of the nozzle at the outlet opening.
  • the nozzle has a flow element in which the second portion is tapered to a tip. In this way, the turbulence of the fuel is improved with the air flow at low pressure drop.
  • the flow element in the first section has a first radius of curvature.
  • a symmetrical and targeted guidance of the fuel is achieved. Due to the first radius of curvature, the fuel is deflected radially outward with a relatively small pressure drop from its longitudinal flow parallel to the longitudinal axis of the channel of the nozzle. However, the deflection occurs in such a way that a small pressure drop occurs.
  • a transition region between the first and the second section of the end piece has a second radius of curvature. In this way, a defined, but in the flow direction continuously extending tear zone for the fuel flow. This feature also prevents the occurrence of a large pressure drop.
  • the second diameter has an order of magnitude which is in the range between 0.8 and 1.1 times the diameter of the outlet opening.
  • the second diameter is in the range between 0.9 and 0.98 times the diameter of the outlet opening.
  • the second diameter is at a distance from the plane of the exit opening ranging between 0.2 and 1.2 times the diameter of the outlet opening is located.
  • the distance of the second diameter from the plane of the outlet opening is in the range between 0.33 and 0.9 times the diameter of the outlet opening.
  • a flow molding has a pin, at the end of which the flow element is formed, the pin having a constant cylindrical cross section in the channel at least in one end region in front of the outlet opening.
  • the pin has a constant cylindrical cross section substantially in the channel.
  • the pin is fastened to the nozzle via a fastening part.
  • the pin may be formed as a separate component and be positively or non-positively attached to the nozzle. In this way it is possible to retrofit existing nozzles with the pen.
  • the pin is connected to one or two struts with an annular or partially annular fastening part. Due to the design of the struts only a small area of the channel is blocked by the struts, so that only a slight turbulence or a small pressure drop occurs in the region of the fastening part.
  • the nozzle has a surface which is rotationally symmetrical to the center axis of the nozzle in the region of the outlet opening and tapers in the direction of the outlet opening of the channel. In this way, an efficient guidance of the air flow is achieved.
  • the nozzle in the region of the outlet opening has a wall thickness which lies in the region of the diameter of the channel in the region of the outlet opening.
  • FIG. 1 shows a schematic partial sectional view of a cross section through a nozzle 1, which has a housing 3, which surrounds an inner space 2.
  • fuel is introduced, which is discharged via a channel 4 via an outlet opening 6.
  • the channel 4 opens via an inlet opening 5 in the interior 2.
  • the channel 4 is rotationally symmetrical to a central axis 7 is formed.
  • the cylindrical section 8 merges into a tapered section 9.
  • the conically tapering section 9 merges into a cylindrical further section 10.
  • the channel 4 tapers into a cylindrical outlet channel 11.
  • the outlet channel 11 merges into the outlet opening 6, which is arranged perpendicular to the center axis 7 at the tip of the nozzle 1.
  • a flow shaping part 12 is arranged, which has a cylindrical pin 13, wherein the pin 13 is fastened via a fastening part 14 on the cylindrical portion 8 of the channel 4 on the housing 3.
  • the fastening part is formed, for example, part-ring-shaped.
  • the fastening part 14 is formed in the form of a ring.
  • the fastening part 14 may be positively or non-positively connected to the housing 3.
  • the fastening part 14 is formed for example as a ring which is rectangular in cross-section.
  • the fastening part 14 may be fixed to the housing 3 by means of an interference fit.
  • the pin 13 is connected via struts 15 with the fastening part 14.
  • the struts 15 are preferably arranged in a plane perpendicular to the center axis 7.
  • the pin 13 is arranged with its center axis in the center axis 7 of the channel 4 and extends beyond the outlet opening 6 addition.
  • the channel 4 has a flow element 16 as an end piece.
  • the flow element 16 is rotationally symmetrical to the center axis 7 and formed to the center axis of the pin 13.
  • the housing 3 has, in the region of the channel 4, a rotationally symmetrical outer surface 33 with respect to the center axis 7. In the direction of the outlet opening 12, the surface 33 of the housing 3 is tapered.
  • the nozzle 1 in the region of the outlet opening 12 preferably has a wall thickness which lies in the region of the diameter of the outlet opening 12.
  • the housing of the nozzle may also have other shapes and / or dimensions.
  • the flow element 16 may also be connected directly to the nozzle 1 via at least one strut. It can be dispensed with the pin 13 and the fastening part 14.
  • FIG. 2 shows in a schematic representation of the flow element 16.
  • the pin 13 preferably has a cylindrical cross section with a first diameter.
  • the diameter of the flow element 16 expands continuously in a first section 18, starting from the diameter of the pin 13 to a second diameter.
  • the first section 18 is followed by a second section 19, along which the diameter of the flow element 16 tapers again.
  • the flow element 16 in the second section 19 tapers conically up to a tip 20.
  • the end of the flow element 16 may also have a third diameter that is smaller than the first diameter.
  • the flow element 16 is like the pin 13 rotationally symmetrical to the center axis 7 formed.
  • the diameter of the flow element 16 in the region of the first section 18 may widen conically or with a first radius of curvature.
  • the surface of the flow element 16 preferably merges with the second section 19 from the first section over a second radius of curvature.
  • the first portion 18 preferably presents a concave surface in cross-section.
  • the transition region between the first and second portions 18, 19 is a convex surface in cross-section.
  • the second portion 19 may also be used instead of the conical Form having a convex or concave surface in cross-section.
  • the flow element 16 in the first section may be formed in cross-section also in the form of a convex surface.
  • the diameter of the flow element reaches a maximum diameter h.
  • the transition region 21 is spaced a fixed distance d from the plane of the outlet opening 6.
  • the maximum diameter h is preferably in the range between 0.8 and 1.1 times the diameter of the outlet opening.
  • the maximum diameter h of the flow element 16 is in the range between 0.9 and 0.98 times the diameter of the outlet opening.
  • the distance d between the plane of the outlet opening and the plane of the maximum diameter is in the range between 0.2 and 1.1 times the diameter of the outlet opening.
  • the distance d is between 0.33 and 0.9 times the diameter of the outlet opening.
  • the conical surface 33 of the housing 3 has, for example, an angle 17 with respect to the center axis 7, which lies in the range between 5 and 30 °.
  • FIG. 3 shows in a perspective view of the flow molding part 12.
  • the attachment member 14 has two openings 22, 23 through which fuel flows into the channel 4.
  • the fastening part 14 may also be formed only partially annular and it may be provided only a single strut 15 to connect the pin 13 with the fastening part 14.
  • FIG. 4 shows in a front view of the flow molding part 12. The symmetrical arrangement of the struts 15 and the symmetrical arrangement of the openings 22, 23 are clearly visible.
  • the openings 22, 23 have a rounded cross-sectional shape.
  • the struts 15 are arranged on an axis.
  • the struts 15 are also arranged mirror-symmetrically to the plane through the center axis 7.
  • the openings 22, 23 are formed mirror-symmetrically to a plane in the center axis 7. In this way, the lowest possible turbulence or pressure change of the fuel flow is achieved when entering from the interior 2 into the channel 4.
  • FIG. 5 shows a cross section AA through the flow molding part 12 along the center axis 7 of FIG. 4 ,
  • FIG. 6 shows the arrangement of the nozzle 1 in a flow tube 24.
  • the nozzle 1 along a center axis of the flow tube 24 is arranged.
  • the flow tube 24 is traversed by an air flow 25 in the illustrated arrow direction.
  • the air flow 25 flows along the surface 33 of the nozzle 1 in the direction of the outlet opening 6.
  • the air flow 25 swirls with the fuel 26, which is discharged from the nozzle 1.
  • turbulences 27 are generated in the flow tube 24, which are shown schematically in the form of curved arrows. Due to the described embodiments of the nozzle 1 with the flow molding 12, an efficient turbulence of the fuel 26 is achieved with the air flow 25, wherein the lowest possible pressure drop is generated.
  • the air flow 25 is generated for example by means of a blower.
  • the described nozzle 1 can be used for example in gas heating systems, in particular in gas-water heaters.
  • the nozzle described can be used to produce a low NO x emissions, for example less than 40 ppm on combustion.
  • a low NO x emissions for example less than 40 ppm on combustion.
  • the nozzle described achieves rapid vertical mixing of the fuel with the air flow. In addition, a rapid distribution of the fuel and a molecular mixing of the fuel with the air flow possible. Furthermore, due to the proposed nozzle, only a small pressure drop of the fuel stream when leaving the nozzle is caused.
  • the nozzle can be used to mix methane as fuel with air. Experiments have shown that the proposed nozzle can increase the uniform mixing of methane with air by 25%.
  • the flow tube 24 may have further surfaces for swirling and guiding the air flow.

Landscapes

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

Claims (12)

  1. Buse (1) pour un brûleur à gaz, dans laquelle la buse (1) présente un canal (4), qui est prévu pour évacuer du gaz, dans laquelle le canal(4) aboutit à une ouverture de sortie (6), dans laquelle un élément d'écoulement (16) est disposé à l'extérieur de l'ouverture de sortie (6), dans laquelle l'élément d'écoulement (16) présente une première portion (18), qui augmente à partir d'un premier diamètre dans la direction s'éloignant de l'ouverture de sortie (6) jusqu'à un deuxième diamètre, dans laquelle l'élément d'écoulement (16) diminue à nouveau jusqu'à un troisième diamètre à partir du deuxième diamètre dans une deuxième portion avec un espacement croissant de l'ouverture de sortie dans le diamètre, dans laquelle l'élément d'écoulement (16) est conçu et disposé de manière symétrique en rotation par rapport à un axe médian (7) du canal (4), caractérisée en ce que l'élément d'écoulement (16) est relié avec une goupille (13), dans laquelle la goupille (13) est disposée dans le canal (4), dans laquelle la goupille est guidée à travers l'ouverture de sortie (6), dans laquelle la goupille (13) est disposée de manière symétrique en rotation par rapport à l'axe médian (7) du canal (4), dans laquelle l'élément d'écoulement (16) est réalisé sur une extrémité de la goupille (13), dans laquelle la goupille (13) est reliée sur une deuxième extrémité avec une partie de fixation (14), dans laquelle la partie de fixation (14) est fixée sur la buse, notamment sur une paroi intérieure du canal (4).
  2. Buse selon la revendication 1, dans laquelle la deuxième portion (19) est taillée en cône dans la direction d'une pointe (20).
  3. Buse selon une des revendications précédentes, dans laquelle dans la première portion (18) une surface de l'élément d'écoulement (16) présente un premier rayon de courbure.
  4. Buse selon une des revendications précédentes, dans laquelle dans une zone de transition (21) entre la première et la deuxième portion (18,19) la surface de l'élément d'écoulement (16) présente un deuxième rayon de courbure.
  5. Buse selon une des revendications précédentes, dans laquelle le deuxième diamètre est situé dans la plage comprise entre 0,8 et 1,1 fois le diamètre de l'ouverture de sortie (6), notamment dans la plage entre 0,9 et 0,98 fois le diamètre de l'ouverture de sortie (6).
  6. Buse selon une des revendications précédentes, dans laquelle le deuxième diamètre présente un espacement par rapport au plan de l'ouverture de sortie (6), qui est situé dans la plage entre 0,2 et 1, 1 fois le diamètre de l'ouverture de sortie, dans laquelle de préférence le deuxième diamètre présente un espacement par rapport au plan de l'ouverture de sortie (6), qui est situé dans la plage entre 0,33 et 0,9 fois le diamètre de l'ouverture de sortie (6).
  7. Buse selon une des revendications précédentes, dans laquelle la goupille (13) dans le canal (4) présente au moins dans une zone précédant l'ouverture de sortie (6) une section transversale cylindrique constante.
  8. Buse selon la revendication 1, dans laquelle la goupille (13) est conçue comme un composant séparé avec la partie de fixation (14) et l'élément façonné d'écoulement (16), qui est fixé par conjonction de force ou de forme à la buse.
  9. Buse selon une des revendications 1 à 8, dans laquelle la partie de fixation (14) présente au moins une bague partielle, dans laquelle la bague partielle est fixée sur la buse (1) et entoure au moins partiellement le canal (4), et dans laquelle la goupille (13) est reliée par l'intermédiaire d'au moins une entretoise (15) avec la bague partielle.
  10. Buse selon la revendication 9, dans laquelle la partie de fixation présente une bague, dans laquelle la bague est reliée par l'intermédiaire de deux entretoises (15) avec la goupille (13), dans laquelle les entretoises (15) sont disposées de préférence dans un plan.
  11. Buse selon la revendication 10, dans laquelle les entretoises (15) sont disposées sur un axe, qui est disposé dans un plan de la bague (14), dans laquelle les entretoises (15) délimitent deux ouvertures (22,23) arrondies dans la section transversale du plan de la bague.
  12. Buse selon une des revendications précédentes, dans laquelle la buse (1) présente une surface (33), qui est conçue de manière symétrique en rotation par rapport à l'axe médian (7) de la buse (1) et est taillée en cône dans la direction de l'ouverture de sortie (6) du canal (4) et/ou dans laquelle la buse présente dans la région de l'ouverture de sortie (6) une épaisseur de paroi, qui est de l'ordre du diamètre de l'ouverture de sortie (6).
EP14185135.2A 2013-10-16 2014-09-17 Buse pour un brûleur à gaz Active EP2863121B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE201310220980 DE102013220980A1 (de) 2013-10-16 2013-10-16 Düse für einen Gasbrenner

Publications (3)

Publication Number Publication Date
EP2863121A2 EP2863121A2 (fr) 2015-04-22
EP2863121A3 EP2863121A3 (fr) 2015-07-15
EP2863121B1 true EP2863121B1 (fr) 2016-11-09

Family

ID=51570311

Family Applications (1)

Application Number Title Priority Date Filing Date
EP14185135.2A Active EP2863121B1 (fr) 2013-10-16 2014-09-17 Buse pour un brûleur à gaz

Country Status (3)

Country Link
EP (1) EP2863121B1 (fr)
DE (1) DE102013220980A1 (fr)
PT (1) PT2863121T (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2671507A (en) * 1950-06-03 1954-03-09 Selas Corp Of America Radiant gas burner
US4168950A (en) * 1975-07-17 1979-09-25 Selas Corporation Of America Furnace wall construction
US4342426A (en) 1980-09-24 1982-08-03 Feecon Corporation Nozzle
SE454460B (sv) * 1983-06-14 1988-05-02 Sandstroem Christer Brennare for olja, gas, kolpulversuspension m fl brenslen
CA1201649A (fr) * 1985-03-28 1986-03-11 Loudenco Ltd. Tete de retention pour bruleurs

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
PT2863121T (pt) 2016-12-27
EP2863121A3 (fr) 2015-07-15
DE102013220980A1 (de) 2015-04-16
EP2863121A2 (fr) 2015-04-22

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