DARK RADIATOR
20240310038 ยท 2024-09-19
Assignee
Inventors
- Edgar KREIS (Freigericht, DE)
- Alexander GENZEL (Bonn, DE)
- Torsten STOHLER (Mettmann, DE)
- Thomas RENNER (Wesseling, DE)
Cpc classification
F24D5/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C6/047
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24H3/006
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C3/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2201/301
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2202/50
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2202/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2900/9901
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C2900/03009
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23D14/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F23D14/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23C6/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A dark radiator includes a first burner, a fan and a radiant tube. The first burner is connected to a fuel gas supply, the fan is designed to supply the first burner with combustion air and the first burner is designed to output a flame into the radiant tube. The fuel gas supply is connected to a hydrogen source as a fuel gas source and a secondary burner is connected downstream in the radiant tube spaced apart from the first burner functioning as the primary burner in the flame direction. The fuel gas supply thereof is connected to a hydrogen source as a fuel gas source and the exhaust gas flow of the upstream primary burner is supplied to the secondary burner as combustion air.
Claims
1. A dark radiator having a first burner, a fan (2), and a radiant tube (3), wherein the first burner is connected to a fuel gas supply, wherein the fan (2) is set up for supplying combustion air to the first burner, wherein the first burner is set up for outputting a flame into the radiant tube (3), wherein the fuel gas supply is connected to a hydrogen source as the fuel gas source, and wherein a secondary burner (4) follows the first burner that serves as the primary burner (1), in the radiant tube (3), at a distance from the first in the flame direction, the fuel gas feed of which secondary burner is connected to a hydrogen source as the fuel gas source, wherein the exhaust gas stream of the upstream primary burner (1) is supplied to the secondary burner (4) as combustion air.
2. The dark radiator according to claim 1, wherein the fan (2) is connected to an ejector having a suction connector connected to the hydrogen supply, wherein the combustion air drawn in by the fan (2) serves as a driving medium, so that a hydrogen/combustion air mixture is supplied to the burner (1) by the fan (2).
3. The dark radiator according to claim 1, wherein an equalization element (31) is arranged between the primary burner (1) and the secondary burner (4), to equalize thermally related length changes within the radiant tube (3).
4. The dark radiator according to claim 1, wherein the primary burner (1) comprises a gas jet, wherein the fan (2) is set up for flushing the gas jet (11) with combustion air, and whereby no fuel gas mixing chamber is provided for pre-mixing fuel gas and combustion air, and the gas jet is supplied exclusively with fuel gas.
5. The dark radiator according to claim 1, wherein the primary burner (1) comprises a gas jet (11) and a mixing tube (14), which is supplied with hydrogen by the gas jet (11), wherein the mixing tube (14) is flushed with combustion air by the fan (2), wherein the gas jet (11) forms an ejector with the mixing tube (14), wherein the driving medium of the ejector is hydrogen introduced by the gas jet (11) and the medium drawn into the mixing tube (14) is combustion air situated in the radiant tube (3), and wherein an ignition apparatus (13) for igniting the hydrogen/combustion air mixture follows at a distance from the mixing tube (14), in the flame direction.
6. The dark radiator according to claim 1, wherein a combustion air mixing chamber is arranged to precede the primary burner (1) in the flame direction, which chamber is connected to a combustion air source and to the exhaust gas discharge line.
7. The dark radiator according to claim 6, wherein the fan (2) is arranged to precede the burner (1) in the flame direction, and the combustion air mixing chamber is arranged within the fan (2).
8. The dark radiator according to claim 6, wherein the connection between the exhaust gas discharge line and the combustion air mixing chamber comprises a branching-off device (5) by means of which the ratio of the branched-off exhaust gas volume stream and the combustion air volume stream is determined.
9. The dark radiator according to claim 8, wherein the branching-off device (5) comprises an adjustment device by means of which the ratio of the exhaust gas volume stream and the combustion air volume stream can be set.
Description
[0013] Other further developments and embodiments of the invention are indicated in the remaining dependent claims. Exemplary embodiments of the invention are shown in the drawings and will be described in detail below. The figures show:
[0014]
[0015]
[0016]
[0017] The dark radiator according to
[0018] The primary burner 1 comprises a gas jet 11 that serves as a gas/air mixture jet and is provided, in the exemplary embodiment, with a flashback barrier, and is connected to a hydrogen supply 12. At a distance from the gas jet 11, an ignition electrode 13 is arranged in the primary burner 1. The fan 2 is connected to a combustion air supply 21 on the suction side, and set toward the primary burner 1 in such a manner that it flushes the gas jet 11 with combustion air. The hydrogen gas that exits from the gas jet 11 is ignited by the ignition electrode 13 after it is mixed with the combustion air that is supplied by way of the fan 2, and thereby a flame that extends through the radiant tube 3 is generated.
[0019] Alternatively the gas jet can also be connected to the fan 2, wherein the fan 2 is connected, on its suction side, to an ejector, the drive connector of which is connected to a combustion air supply and the suction connector of which is connected to a hydrogen supply. The combustion air drawn in by the fan 2 serves as a driving medium here, by means of which intake of the hydrogen is brought about. On the pressure side, the gas jet 11 has a hydrogen/combustion air mixture supplied to it by the fan 2 as a result, in this case; after this mixture exits through the gas jet 11, it is ignited by the ignition electrode 12.
[0020] The primary burner 1 is followed, in the flame direction, by a radiant tube 3 configured in U shape, which tube is connected to a secondary burner 4 by way of an equalization element 31. In the exemplary embodiment, the equalization element is configured as an axial compensator that absorbs the movements of the tube line along the axis. Once again, a second part of the radiant tube 3 follows the secondary burner 4, which part is once again configured in U shape in the exemplary embodiment.
[0021] The secondary burner once again comprises a gas jet 4 connected to a hydrogen supply 42, wherein an ignition electrode 43 is positioned at a distance from the gas jet 41.
[0022] The gas jet 11 of the primary burner 1 is flushed with combustion air by the fan 2. The hydrogen/combustion air mixture that forms in front of the gas jet 11 is ignited by the ignition electrode 13, and thereby a first flame forms at a distance in front of the hydrogen jet 11. The exhaust gas stream of this first flame flows through the equalization element 31 and flushes the gas jet 41 of the secondary burner 4. The exhaust gas/hydrogen mixture that forms in front of the gas jet 41 has a sufficiently high oxygen content so that it can be ignited by the ignition electrode 43, and thereby a second flame is formed, which extends along the second part of the radiant tube 3. The exhaust gas stream 32 of this second flame is derived from the second part of the radiant tube 3. The equalization element 31, which is positioned in the section of the radiant tube 3 that is exposed to a high temperature, by means of the secondary burner 4, serves for equalization of thermally caused length changes within the radiant tube.
[0023] In this exemplary embodiment, combustion air is supplied to the primary burner 1 by way of the fan 2, which air flushes the gas jet 11 of the primary burner 1. In a modified embodiment, the fan 2 that precedes the primary burner 1 can also be connected to an ejector, wherein the combustion air that is drawn in serves as a driving medium, by way of which an exhaust gas stream is drawn in from the second part of the radiant tube 3. In this way, the flame temperature of the first flame of the primary burner 1 can be adjusted. Furthermore, in this way a further reduction in the nitrogen oxide content of the exhaust gas that is conducted away is made possible.
[0024] In the exemplary embodiment according to
[0025] The fan 2 is oriented in such a manner that it flushes the gas jet 11 and the mixing tube 14 with combustion air. By means of the hydrogen stream introduced into the mixing tube 14 by way of the gas jet 11, combustion air is drawn in by way of the suction gap 15, which air mixes with the hydrogen. The hydrogen/combustion air mixture exiting from the mixing tube 14 is ignited by means of the ignition electrode 13 arranged at a distance from the mixing tube 14, and thereby a flame is formed, which extends into the radiant tube 3 over its length. A part of the combustion air 5 blown into the primary burner 1 by the fan flows through the flushing openings of the separating frame 16 and flushes the flame that extends into the radiant tube 3, which flame is thereby cooled. The ejector formed by the gas jet 11 and the mixing tube 14 is configured in such a manner that combustion air having an air number of 2.5 is supplied to the hydrogen in the mixing tube 14, and thereby a temperature of about 900? C. is achieved.
[0026] In the exemplary embodiment according to
[0027] The ejector tube 5 comprises a main tube piece 51, by way of which the radiant tube 3 is connected to the suction tube 22. An exhaust gas off-take tube 52 branches off from the main tube piece 51, and, at a distance from it, a combustion air supply tube 53 branches off. A recirculation shutter 54 is arranged in the main tube piece 51, between the exhaust gas supply tube 52 and the combustion air supply tube 53. The combustion air stream 531 drawn in by way of the suction tube 22, by means of the fan 2, serves as a drive medium of the ejector tube 5, by way of which a part of the exhaust gas stream 521 is drawn in by means of the recirculation shutter 54. The exhaust gas/combustion air mixture produced in this way is introduced into the primary burner 1 by means of the fan 2 and flushes the gas jet 11 there. By means of the recirculation shutter 54, the proportion of the exhaust gas stream in the combustion air stream can be adjusted, and thereby, once again, the oxygen content of the exhaust gas/combustion air mixture that flushes the hydrogen jet 11 is determined. The main exhaust gas stream is carried away by way of the exhaust gas off-take tube 52.
[0028] The primary burner 1, the parts of the radiant tube 3, the secondary burner 4, the ejector tube 5, and the fan 2 connected to the suction tube 22 are connected to one another, in each instance, by way of flange connections.