FR2800844A1 - Arrangement, for improving combustion of air pulse fuel burner used for heater, comprises sleeve having thin wall and frontal orifice of dimension slightly greater to that of nose of burner - Google Patents
Arrangement, for improving combustion of air pulse fuel burner used for heater, comprises sleeve having thin wall and frontal orifice of dimension slightly greater to that of nose of burner Download PDFInfo
- Publication number
- FR2800844A1 FR2800844A1 FR9914391A FR9914391A FR2800844A1 FR 2800844 A1 FR2800844 A1 FR 2800844A1 FR 9914391 A FR9914391 A FR 9914391A FR 9914391 A FR9914391 A FR 9914391A FR 2800844 A1 FR2800844 A1 FR 2800844A1
- Authority
- FR
- France
- Prior art keywords
- ring
- burner
- nose
- upstream
- orifice
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C9/00—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber
- F23C9/006—Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber the recirculation taking place in the combustion chamber
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/40—Mixing tubes or chambers; Burner heads
- F23D11/402—Mixing chambers downstream of the nozzle
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
Description
<B>DISPOSITIF</B> POUR AMELIORER <B>LA COMBUSTION D'UN</B> BRULEUR <B>A</B> FIOUL <B>A</B> AIR<B>PULSE</B> La présente invention a trait aux brûleurs<B>à</B> fioul <B>à</B> air pulsé et vise plus particulièrement<B>à</B> améliorer la combustion en favorisant une combustion plus complète et moins émettrice d'oxydes d'azote et de carbone. <B> DEVICE </ B> TO IMPROVE <B> THE COMBUSTION OF A </ B> BURNER <B> A </ B> FIOUL <B> A </ B> AIR <B> PULSE </ B> The present invention relates to burners <B> to </ B> fuel <B> to </ b> pulsed air and more particularly aims <B> to </ B> improve combustion by promoting a more complete combustion and less emitting oxides of nitrogen and carbon.
<B>A</B> cet effet, l'invention a pour objet un dispositif pour améliorer la combustion d'un brûleur<B>à</B> fioul <B>à</B> air pulsé, caractérisé en ce qu'il est constitué d'une bague de recirculation des gaz brûlés, de forme tubulaire, coaxiale au brûleur et disposée devant le nez de ce dernier, ladite bague présentant une paroi mince et un orifice amont de dimensions sensiblement supérieures<B>à</B> celles du nez du brûleur, la distance entre ledit orifice amont et le nez du brûleur, ainsi que la longueur et le diamètre amont de ladite bague étant déterminés en fonction de la forme et du volume de la chambre de combustion, de la puissance du brûleur et de l'angle de pulvérisation, du gicleur de fioul. For this purpose, the invention relates to a device for improving the combustion of a burner <B> to </ B> oil <B> to </ B> pulsed air, characterized in that it consists of a recirculating ring burnt gases, tubular, coaxial with the burner and disposed in front of the nose of the latter, said ring having a thin wall and an upstream orifice of substantially larger dimensions <B> to < / B> those of the nose of the burner, the distance between said upstream orifice and the nose of the burner, as well as the length and the upstream diameter of said ring being determined according to the shape and the volume of the combustion chamber, the burner power and spray angle, oil nozzle.
Sur la figure<B>1</B> des dessins annexés, on a illustré le principe de réalisation du dispositif de l'invention. In Figure <B> 1 </ B> of the accompanying drawings, the principle of embodiment of the device of the invention is illustrated.
En<B>1</B> est schématisée la chambre de combustion d'un générateur de chaleur<B>à</B> fioul <B>à</B> brûleur<B>à</B> air puisé dont le nez du brûleur est schématisé en 2. La chambre<B>1</B> ainsi que le nez 2 sont cylindriques et coaxiaux. In <B> 1 </ B> is shown schematically the combustion chamber of a heat generator <B> to </ B> fuel <B> to </ b> burner <B> to </ B> air drawn from which the nose of the burner is schematized in 2. The chamber <B> 1 </ B> as well as the nose 2 are cylindrical and coaxial.
Conformément<B>à</B> l'invention, il est prévu légèrement en avant du nez de brûleur 2 et coaxialement <B>à</B> celui-ci une bague de recirculation <B>3</B> de forme générale cylindrique et<B>à</B> paroi mince, réalisée en tous matériaux appropriés tels que matériaux réfractaires, métalliques ou céramiques. Le diamètre de la bague<B>3</B> est sensiblement supérieur<B>à</B> celui du nez 2 en sorte que les gaz brûlés puissent être (flèches 4) réintroduits en partie en amont de la bague<B>3 à</B> l'intérieur de celle-ci, dans le pied de flamme<B>5,</B> ces gaz brûlés étant mélangés<B>à</B> l'air neuf pénétrant dans la bague. According to the invention, it is provided slightly in front of the burner nose 2 and coaxially <B> to it a recirculation ring <B> 3 </ B> of cylindrical general shape and <B> to </ B> thin wall, made of any suitable materials such as refractory materials, metallic or ceramic. The diameter of the ring <B> 3 </ B> is substantially greater <B> than </ B> that of the nose 2 so that the burned gases can be (arrows 4) reintroduced partly upstream of the ring <B > 3 to </ B> the inside of it, in the foot of flame <B> 5, </ B> these burned gases being mixed <B> to </ B> the fresh air penetrating the ring .
Avantageusement et comme illustré par la figure 2 montrant en coupe la bague de recirculation <B>3,</B> cette dernière présente un bord amont en forme de bourrelet annulaire<B>6 à</B> section aérodynamique sensiblement en goutte d'eau, le diamètre intérieur de l'extrémité amont de la bague<B>3</B> n'étant pas réduit mais au contraire légèrement évasé pour supprimer les turbulences<B>à</B> l'entrée et permettre,<B>à</B> section équivalente d'améliorer sensiblement le débit de recyclage (flèches 4) arrivant en pied de flamme<B>5.</B> Advantageously and as illustrated in FIG. 2, showing in section the recirculation ring <B> 3, the latter has an upstream edge in the form of an annular bead <B> 6 with an aerodynamic section substantially in droplet. water, the inner diameter of the upstream end of the ring <B> 3 </ B> not being reduced but on the contrary slightly flared to remove the turbulence <B> to </ B> the inlet and allow, <B> to </ B> equivalent section significantly improve the recycling flow (arrows 4) arriving at the bottom of the flame <B> 5. </ B>
La bague<B>3</B> est également munie d'une série d'orifices<B>7</B> de réintroduction partielle des gaz brûlés (flèches<B>8) à</B> l'intérieur de la bague pour accélérer le refroidissement de la flamme schématisée par les flèches<B>9,</B> entourée par la bague<B>3.</B> Cette accélération du refroidissement de la flamme vise<B>à</B> réduire la formation d'oxydes d'azote tout en complétant la combustion par l'oxygène résiduel qu'ils contiennent. The ring <B> 3 </ B> is also equipped with a series of orifices <B> 7 </ B> of partial reintroduction of flue gases (arrows <B> 8) to </ B> inside the the ring to accelerate the cooling of the flame schematized by the arrows <B> 9, </ B> surrounded by the ring <B> 3. </ B> This acceleration of the cooling of the flame aims <B> to </ B > reduce the formation of nitrogen oxides while completing the combustion with the residual oxygen they contain.
La figure<B>3</B> illustre diverses formes et implantations des orifices<B>7</B> qui sont répartis<B>à</B> intervalles réguliers dans un plan perpendiculaire<B>à</B> l'axe de la bague<B>3</B> de préférence dans la demi-partie aval de cette dernière. Figure <B> 3 </ B> illustrates various shapes and locations of <B> 7 </ B> holes that are spread <B> to </ B> regular intervals in a perpendicular plane <B> to </ B> the axis of the ring <B> 3 </ B> preferably in the downstream half-part of the latter.
Les orifices<B>7</B> peuvent être circulaires (repère<B>10),</B> elliptiques ou ovales (repère<B>11)</B> ou rectangulaires (repère<B>1</B>2). Ils peuvent être réalisés par emboutissage en direction du centre de la bague (repère<B>13)</B> le plan des orifices étant parallèle<B>à</B> la paroi de la bague<B>3,</B> ou encore réalisés de façon<B>à</B> former un canal 14 d'introduction en sifflet (flèche<B>15) à</B> l'intérieur de la bague<B>3.</B> Holes <B> 7 </ B> may be circular (<B> 10), elliptical or oval (<B> 11) </ B>, or rectangular (<B> 1 </ B) > 2). They can be made by stamping towards the center of the ring (mark <B> 13) </ B> the plane of the orifices being parallel <B> to </ B> the wall of the ring <B> 3, </ B> or even made <B> to </ B> form a whistle introduction channel 14 (arrow <B> 15) to </ B> inside the ring <B> 3. </ B >
Les dimensions de la bague de reciréulation <B>3</B> ainsi que sa distance ou éloignement<B>d</B> par rapport au nez du brûleur 2 sont, comme illustré par la figure 4, déterminées,<B>à</B> savoir le diamètre<B>D,</B> la longueur L, ledit éloignement<B>d</B> ainsi que la distance<B>1</B> entre le bord aval de la bague<B>3</B> et l'alignement des orifices<B>7,</B> en fonction de la forme et du volume de la chambre de combustion <B>1,</B> de la puissance du brûleur et de l'angle de pulvérisation du gicleur de fioul. Avantageusement, la bague<B>3</B> peut comporter comme illustré par la figure<B>5</B> un bord aval sinusoïdal<B>16,</B> la période de la sinusoïde correspondant<B>à</B> l'écartement entre deux orifices<B>7</B> consécutifs et les pointes arrondies<B>17</B> dudit bord aval se trouvant en regard d'un intervalle entre deux orifices<B>7.</B> The dimensions of the recirculation ring <B> 3 </ B> as well as its distance or distance <B> d </ B> from the nose of the burner 2 are, as illustrated in FIG. 4, determined, <B> to know the diameter <B> D, </ B> the length L, said distance <B> d </ B> as well as the distance <B> 1 </ B> between the downstream edge of the ring <B> 3 </ B> and the alignment of holes <B> 7, </ B> depending on the shape and volume of the burner <B> 1, </ B> burner capacity and the spray angle of the fuel nozzle. Advantageously, the ring <B> 3 </ B> can comprise as illustrated by the figure <B> 5 </ B> a sinusoidal downstream edge <B> 16, </ B> the period of the corresponding sinusoid <B> to </ B> the distance between two consecutive <B> 7 </ B> holes and the rounded ends <B> 17 </ B> of the said downstream edge lying opposite an interval between two orifices <B> 7. </ B>
Ces pointes arrondies<B>17</B> créent des points chauds uniformément répartis<B>à</B> l'extrémité aval de la bague et qui contribuent<B>à</B> réduire le taux d'oxyde de carbone. La forme sinusoïdale ainsi que sa disposition par rapport aux orifices<B>7</B> sont déterminées pour que lesdits points chauds<B>(17)</B> ne soient pas influencés par l'effet refroidissant des orifices<B>7.</B> These rounded tips <B> 17 </ B> create uniformly distributed hot spots <B> at the downstream end of the ring and help <B> to </ B> reduce the carbon. The sinusoidal shape and its arrangement with respect to the <B> 7 </ B> holes are determined so that the said hot spots <B> (17) </ B> are not influenced by the cooling effect of the orifices <B> 7. </ B>
Suivant encore une autre caractéristique du dispositif de l'invention, illustré par la<B>f</B>igure<B>6,</B> la zone annulaire<B>18</B> de la bague<B>3</B> munie des orifices<B>7</B> est avantageusement légèrement rétreinte, un tel étranglement de la bague favorisant l'aspiration des gaz brûlés (flèches 4). According to yet another characteristic of the device of the invention, illustrated by the <B> f </ B> igure <B> 6, </ B> the annular zone <B> 18 </ B> of the ring <B> 3 </ B> with holes <B> 7 </ B> is advantageously slightly shrunken, such a throttling of the ring favoring the aspiration of flue gas (arrows 4).
La bague<B>3</B> peut par ailleurs avoir une forme ondulée en section comme illustré par la figure<B>7,</B> ou avoir une forme de révolution avec un diamètre en s'élargissant de l'amont vers l'aval, comme illustré par la figure<B>8.</B> The ring <B> 3 </ B> can also have a wavy shape in section as illustrated by the figure <B> 7, </ B> or have a shape of revolution with a widening diameter upstream downstream, as shown in Figure <B> 8. </ B>
La bague<B>3</B> peut aussi, quelle que soit sa forme, comporter intérieurement des nervures radiales<B>19</B> comme illustré par la figure<B>9,</B> de préférence régulièrement distribuées.The ring <B> 3 </ B> can also, whatever its shape, have internally radial ribs <B> 19 </ B> as illustrated by the figure <B> 9, </ B> preferably regularly distributed .
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9914391A FR2800844B1 (en) | 1999-11-08 | 1999-11-08 | DEVICE FOR IMPROVING THE COMBUSTION OF A PULSE AIR FUEL BURNER |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9914391A FR2800844B1 (en) | 1999-11-08 | 1999-11-08 | DEVICE FOR IMPROVING THE COMBUSTION OF A PULSE AIR FUEL BURNER |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2800844A1 true FR2800844A1 (en) | 2001-05-11 |
FR2800844B1 FR2800844B1 (en) | 2002-04-19 |
Family
ID=9552169
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9914391A Expired - Lifetime FR2800844B1 (en) | 1999-11-08 | 1999-11-08 | DEVICE FOR IMPROVING THE COMBUSTION OF A PULSE AIR FUEL BURNER |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2800844B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11353211B2 (en) * | 2018-04-09 | 2022-06-07 | Gas Technology Institute | High turndown ratio gaseous fuel burner nozzle and control |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2734216A1 (en) * | 1977-07-29 | 1979-02-08 | Broetje Fa August | High pressure oil atomising burner head - has double walled flame section with flared and inwards turned ends |
US4318688A (en) * | 1979-05-08 | 1982-03-09 | Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. | Oil burner |
US4364725A (en) * | 1977-01-08 | 1982-12-21 | Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. | Blue-flame oil burner |
JPS58127007A (en) * | 1982-01-22 | 1983-07-28 | Nissei Oobaru Kk | Combustion device for liquid fuel |
DE3241731A1 (en) * | 1982-11-11 | 1984-05-17 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn | Gasification oil burner |
EP0386732A2 (en) * | 1989-03-10 | 1990-09-12 | Oertli Wärmetechnik Ag | Combustion apparatus for dual fuel burner |
DE3919797A1 (en) * | 1989-06-16 | 1991-01-03 | Bernhard W Braukmann | Oil burner for boiler - has oil atomising nozzle mounted on end of oil supply pipe inside air supply duct |
-
1999
- 1999-11-08 FR FR9914391A patent/FR2800844B1/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4364725A (en) * | 1977-01-08 | 1982-12-21 | Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. | Blue-flame oil burner |
DE2734216A1 (en) * | 1977-07-29 | 1979-02-08 | Broetje Fa August | High pressure oil atomising burner head - has double walled flame section with flared and inwards turned ends |
US4318688A (en) * | 1979-05-08 | 1982-03-09 | Deutsche Forschungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. | Oil burner |
JPS58127007A (en) * | 1982-01-22 | 1983-07-28 | Nissei Oobaru Kk | Combustion device for liquid fuel |
DE3241731A1 (en) * | 1982-11-11 | 1984-05-17 | Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5300 Bonn | Gasification oil burner |
EP0386732A2 (en) * | 1989-03-10 | 1990-09-12 | Oertli Wärmetechnik Ag | Combustion apparatus for dual fuel burner |
DE3919797A1 (en) * | 1989-06-16 | 1991-01-03 | Bernhard W Braukmann | Oil burner for boiler - has oil atomising nozzle mounted on end of oil supply pipe inside air supply duct |
Non-Patent Citations (1)
Title |
---|
PATENT ABSTRACTS OF JAPAN vol. 007, no. 240 (M - 251) 25 October 1983 (1983-10-25) * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11353211B2 (en) * | 2018-04-09 | 2022-06-07 | Gas Technology Institute | High turndown ratio gaseous fuel burner nozzle and control |
Also Published As
Publication number | Publication date |
---|---|
FR2800844B1 (en) | 2002-04-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CH631800A5 (en) | COMBUSTION CHAMBER FOR GAS TURBINE. | |
EP1431658B1 (en) | Compact gas burner with internal flame | |
EP2870410B1 (en) | Surface-combustion gas burner | |
CA2033366C (en) | Industrial oil burner with low nitrogen oxides emission generating multiple elementary flames and use thereof | |
EP0291372A1 (en) | Gas burner of the cold nozzle type | |
EP0270424A1 (en) | Ignition device for a high-speed burner with a cold nozzle, and burner using this device | |
CN109323258B (en) | Burner structure based on multiple types of nozzles | |
FR2800844A1 (en) | Arrangement, for improving combustion of air pulse fuel burner used for heater, comprises sleeve having thin wall and frontal orifice of dimension slightly greater to that of nose of burner | |
US5433601A (en) | Deposit-free burner | |
EP0884528A2 (en) | Combustion head for gas burners | |
KR200249581Y1 (en) | Tip for Torch | |
RU2113656C1 (en) | Device for eddy dispersion of air for combustion in turbulent injector | |
US20120037053A1 (en) | Burner for a Thermal Post-Combustion Device | |
EP0679838B1 (en) | Improvements to gas burners | |
FR2465158A3 (en) | SPRAY FUEL OIL BURNER, PARTICULARLY FOR LOW POWER APPLIANCES | |
JP2563009B2 (en) | Two-stage combustion vaporization combustion burner | |
FR2624255A1 (en) | Air-gas burner with a very-stable inner-core flame, constituting the functional part of a torch nozzle | |
JP2004077012A (en) | Radiant tube type heating device | |
RU2200904C1 (en) | Burner device | |
JP3058152U (en) | Burner | |
JP3469704B2 (en) | Pressure spray type combustion device | |
FR2728329A1 (en) | Burner for industrial furnace, e.g. rotary furnace | |
JP2569979Y2 (en) | Low NOx burner | |
CH306495A (en) | Combustion apparatus. | |
JPH0120505Y2 (en) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 17 |
|
PLFP | Fee payment |
Year of fee payment: 18 |
|
PLFP | Fee payment |
Year of fee payment: 19 |
|
PLFP | Fee payment |
Year of fee payment: 20 |