US20060286498A1 - Porous burner having a flame barrier - Google Patents
Porous burner having a flame barrier Download PDFInfo
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- US20060286498A1 US20060286498A1 US11/447,726 US44772606A US2006286498A1 US 20060286498 A1 US20060286498 A1 US 20060286498A1 US 44772606 A US44772606 A US 44772606A US 2006286498 A1 US2006286498 A1 US 2006286498A1
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- porous
- recited
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- porous burner
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- 230000004888 barrier function Effects 0.000 title claims abstract description 39
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 31
- 239000001257 hydrogen Substances 0.000 claims abstract description 31
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 28
- 238000002485 combustion reaction Methods 0.000 claims abstract description 28
- 239000000463 material Substances 0.000 claims abstract description 27
- 239000011148 porous material Substances 0.000 claims abstract description 21
- 238000002156 mixing Methods 0.000 claims abstract description 18
- 239000007789 gas Substances 0.000 claims abstract description 15
- 239000003638 chemical reducing agent Substances 0.000 claims abstract description 8
- 239000007800 oxidant agent Substances 0.000 claims abstract description 7
- 239000000446 fuel Substances 0.000 claims description 23
- 239000000203 mixture Substances 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 7
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 4
- 239000000470 constituent Substances 0.000 claims description 4
- 229910052593 corundum Inorganic materials 0.000 claims description 4
- 229910001845 yogo sapphire Inorganic materials 0.000 claims description 4
- 229910052681 coesite Inorganic materials 0.000 claims description 3
- 229910052906 cristobalite Inorganic materials 0.000 claims description 3
- 239000000377 silicon dioxide Substances 0.000 claims description 3
- 229910052682 stishovite Inorganic materials 0.000 claims description 3
- 229910052905 tridymite Inorganic materials 0.000 claims description 3
- 239000003570 air Substances 0.000 claims 1
- 206010016754 Flashback Diseases 0.000 description 10
- 230000008901 benefit Effects 0.000 description 7
- 239000000835 fiber Substances 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 4
- 239000004215 Carbon black (E152) Substances 0.000 description 3
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 3
- 239000003344 environmental pollutant Substances 0.000 description 3
- 229930195733 hydrocarbon Natural products 0.000 description 3
- 150000002430 hydrocarbons Chemical class 0.000 description 3
- 150000002431 hydrogen Chemical class 0.000 description 3
- 231100000719 pollutant Toxicity 0.000 description 3
- 230000003197 catalytic effect Effects 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- 206010053615 Thermal burn Diseases 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 239000003792 electrolyte Substances 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 229920005597 polymer membrane Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 238000002407 reforming Methods 0.000 description 1
- 238000007569 slipcasting Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 230000002123 temporal effect Effects 0.000 description 1
Images
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
- F23C99/00—Subject-matter not provided for in other groups of this subclass
- F23C99/006—Flameless combustion stabilised within a bed of porous heat-resistant material
-
- 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
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/9901—Combustion process using hydrogen, hydrogen peroxide water or brown gas as fuel
Definitions
- the present invention relates to a porous burner having a mixing space for mixing reducing agent and oxidizing agent, and an adjoining combustion space, which is filled with a porous material, a flame barrier with holes being arranged between the mixing space and the combustion space. Furthermore, the present invention relates to the use of a porous burner of this type.
- WO 95/01532 A1 has disclosed a burner which includes a combustion space filled with a porous material and a mixing space. This burner also has a flame barrier or flame trap between the mixing space and the burner space.
- Premix combustion techniques such as porous burner technology
- the conventional flame barriers used in porous burners are optimized for use with hydrocarbon-based fuels, such as natural gas or gasoline. They typically comprise generally ceramic fiber plates with parallel holes. The thickness of these fibers is generally approximately 3.0-3.5 ⁇ m, while their length is approximately 2-3 mm, and the fibers comprise 95-97% Al 2 O 3 .
- the plates which are formed have a high material porosity and, as a result, a low thermal conductivity and a high strength under the high spatial and temporal temperature gradients which occur.
- These perforated flame barriers allow operation with a high power modulation (1:25) over a wide range of air/fuel ratios using hydrocarbon-containing fuels.
- the typical material porosity of flame barriers of this type is approx. 90%.
- the material porosity is in each case determined from the quotient ( ⁇ F ⁇ T / ⁇ F , where ⁇ F stands for the density of the nonporous solid, ⁇ T stands for the density of the porous material of the same composition under the same external conditions, e.g. standard conditions. In the context in which it is used here, therefore, the material porosity indicates the proportion of “empty” volume in the material.
- An object of the invention is to provide a porous burner as a premix burner which allows flashback-free use with hydrogen or hydrogen-rich gas.
- the present invention provides a porous burner having a mixing space for mixing reducing agent and oxidizing agent, and an adjoining combustion space, which is filled with a porous material, a flame barrier with holes being arranged between the mixing space and the combustion space, characterized in that the flame barrier includes a porous material with a material porosity of less than 60%, this material having a density of greater than 1300 kg/m 3 .
- the flame barrier includes a porous material with a material porosity of less than 60%, this material having a density of greater than 1300 kg/m 3 .
- the novel design may allow a power modulation of 1:10.
- the widening of the operating range using the flame barrier according to the present invention opens up the possibility of new application areas and increases the versatility for existing application areas.
- FIGURE shows a diagrammatic cross section through a porous burner.
- porous burner 1 having a flame barrier 2 according to the present invention, as well as the resulting options with regard to flexibility and widening the operating range, by way of example, on the basis of an afterburner or heating burner for a hydrogen-operated fuel cell system, for example based on a polymer membrane as electrolyte (PEM), for mobile applications.
- PEM polymer membrane as electrolyte
- the porous burner 1 is not restricted to an application of this nature.
- purging i.e. the blow-off of hydrogen-containing gases from the fuel cell or from an anode hydrogen circuit thereof, when shutting down or from time to time during operation
- One way of avoiding emission of these exhaust gases into the atmosphere is afterburning.
- the chemical energy contained in this exhaust gas is well below the thermal power required when starting. The use of a single burner both as a starting burner and for the afterburning is therefore only possible if this burner can be reliably operated with a sufficient load spread.
- FIG. 1 shows a diagrammatic cross section through the porous burner 1 having the perforated flame barrier 2 .
- the flame barrier 2 is located between a mixing space 3 , in which air as oxidizing agent and hydrogen or hydrogen-rich gas as reducing agent/fuel are premixed, and a combustion space 4 .
- the combustion space 4 is filled with a porous material, in which the actual combustion takes place.
- This porous material could, for example, be an SiC foam with 10 ppi (pores per inch).
- all other conceivable configurations of the combustion space 4 which have already been used in previous porous burners are also possible.
- the porous burner 1 illustrated here differs from known porous burners only by virtue of the flame barrier 2 or the material from which the latter is formed.
- the material used for the flame barrier 2 is typically ceramic produced by a slip casting. To minimize the shrinkage during the production process, this material, in addition to the powder fraction, may contain less than 30%, preferably less than 15%, e.g. approx. 10%, by mass of fibrous constituents. These fibrous constituents have the additional advantage of increasing the stability of the material. To keep the material porosity at a sufficiently low level, however, it would also be possible to dispense with adding fibers altogether.
- the flame barrier 2 should have a density of at least 1300 kg/m 3 and a material porosity, as defined above, of less than 60%.
- a typical material-based upper limit for the density can be specified as 2000 kg/m 3
- the typical manufacturing-related lower limit for the material porosity can be specified as 40%.
- a perforated flame barrier 2 made from material of this type was used in tests.
- the sum of the cross sections of the holes in the flame barrier 2 should not exceed 5% of the total area of the flame barrier 2 . Particularly good results can be achieved between 1% and 4%.
- the sum of the cross sections of the holes within the tests undertaken were, for example, approx. 1.4% of the total area of the flame barrier 2 . This effectively avoided a flashback on the part of the flame front.
- the porous burner 1 or the flame barrier 2 should be optimized on the basis of the pressure losses which are just still tolerable within the context given above.
- the sum of the cross sections of the holes in the flame barrier 2 should be selected from 1% to 2% for ultrahigh security against flashbacks. If, on the other hand, the air and/or hydrogen is delivered at only a low excess pressure, for example by means of blowers, the sum of the cross sections of the holes in the flame barrier 2 should be selected to be from 3% to 4%, in order to still ensure highly safe operation while at the same time achieving minimal pressure losses in the flame barrier 2 .
- the widening of the operating range which is achieved with the perforated flame barrier 2 made from the material described above for the first time allows the use of the porous burner 1 for the conversion of hydrogen in industrial burners and in particular in fuel cell systems.
- the fuel cell systems it is possible on the one hand to shorten the cold-start time and on the other hand to reduce the system complexity, since there is no need for an additional burner.
- NO x is the only potential pollutant during the combustion of hydrogen, since carbon-based pollutants, such as carbon monoxide or particulates, cannot be formed.
- Possible application areas in which low-emission hydrogen burners are required even now include the chemical industry and use as afterburners and heating burners in fuel cell systems.
- non-premix or catalytic burners which are used for the combustion of hydrogen, as opposed to premix combustion systems.
- the fuel is only mixed with the air in the reaction area, so that a flashback fundamentally cannot occur.
- this concept involves relatively high NO x emissions, since irrespective of the overall air excess there are always zones with a stoichiometric mixture composition and therefore high temperatures.
- catalytic burners have the drawback that for many applications they are too susceptible to contamination and temperature fluctuations and have an insufficient power modulation.
- An additional problem is that they have to be operated with high excesses of air in order to avoid overheating of the catalyst. It is likely that with the state of the art as it stands, the desired low NO x emissions can only be achieved using premix combustion systems.
- porous burner technology has further properties which make the use of a porous burner for the combustion of hydrogen an attractive option.
- the temperature in the combustion zone can be influenced in a targeted way.
- the temperature field within the combustion zone is very homogeneous. Both these advantages allow very low NO x emissions which cannot be achieved even by most other premix burners. Further advantages of porous burners over other premix burners are the high surface loading which can be achieved and the geometric flexibility in terms of the configuration of the combustion zone.
- the power can only be modulated in the range of 1:2. It has been possible to demonstrate in tests that during the combustion of hydrogen the flame front penetrates into the porous material of the flame barrier, moves through the material in the direction of the mixing space and leads to a flashback. In practice the extremely high risk of flashbacks, which greatly restricts the operating range, constitutes a significant obstacle to the implementation of premix hydrogen burners.
- the present invention addresses this problem.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gas Burners (AREA)
- Fuel Cell (AREA)
Abstract
Description
- This claims the benefit of German patent application DE 10 2005 027 698.9, filed Jun. 15, 2006 and which is hereby incorporated by reference herein.
- The present invention relates to a porous burner having a mixing space for mixing reducing agent and oxidizing agent, and an adjoining combustion space, which is filled with a porous material, a flame barrier with holes being arranged between the mixing space and the combustion space. Furthermore, the present invention relates to the use of a porous burner of this type.
- WO 95/01532 A1 has disclosed a burner which includes a combustion space filled with a porous material and a mixing space. This burner also has a flame barrier or flame trap between the mixing space and the burner space.
- Premix combustion techniques, such as porous burner technology, require flame stabilization, which prevents a flashback of the flame front to the mixing space. Therefore, a flame barrier is arranged between the mixing space and the combustion space filled with a porous material. The conventional flame barriers used in porous burners are optimized for use with hydrocarbon-based fuels, such as natural gas or gasoline. They typically comprise generally ceramic fiber plates with parallel holes. The thickness of these fibers is generally approximately 3.0-3.5 μm, while their length is approximately 2-3 mm, and the fibers comprise 95-97% Al2O3. During production, they are arranged in such a manner that the plates which are formed have a high material porosity and, as a result, a low thermal conductivity and a high strength under the high spatial and temporal temperature gradients which occur. These perforated flame barriers, as described in the above-mentioned WO document, allow operation with a high power modulation (1:25) over a wide range of air/fuel ratios using hydrocarbon-containing fuels.
- The typical material porosity of flame barriers of this type is approx. 90%. For the explanations given here, the material porosity is in each case determined from the quotient (ρF−ρT/ρF, where ρF stands for the density of the nonporous solid, ρT stands for the density of the porous material of the same composition under the same external conditions, e.g. standard conditions. In the context in which it is used here, therefore, the material porosity indicates the proportion of “empty” volume in the material.
- Examples of structures and applications for porous burners of this type can be found, for example, in
-
- Durst, F., Kesting, A., Möβbauer, S., Pickenäcker, K., Pickenäcker O., Trimis, D., (1997), Der Porenbrenner—Konzept, Technik und Anwendungsgebiete [The Porous Burner—Concept, technique, and fiels of application], Gaswärme International, Vol. 46, No. 6, pp. 300-307;
- or in
- Diezinger, S., Talukdar, P., von Issendorff F., Trimis, D., (2005), Verbrennung von niederkalorischen Gasen in Porenbrennern [Combustion of low calorific gases porous burners], Gaswärme International, Vol. 54, No. 3, pp. 187-192.
- An object of the invention is to provide a porous burner as a premix burner which allows flashback-free use with hydrogen or hydrogen-rich gas.
- The present invention provides a porous burner having a mixing space for mixing reducing agent and oxidizing agent, and an adjoining combustion space, which is filled with a porous material, a flame barrier with holes being arranged between the mixing space and the combustion space, characterized in that the flame barrier includes a porous material with a material porosity of less than 60%, this material having a density of greater than 1300 kg/m3. On account of the use of materials with a significantly lower material porosity and a correspondingly higher density than with conventional flame barriers, it has been possible to considerably extend the operating range and power modulation of porous burners during combustion, in particular of hydrogen and hydrogen-rich gas.
- The flame barriers according to the invention then can permit reliable operation with hydrogen and air, for example at a surface loading of 1300 kW/m2 and with a considerably lower air/fuel ratio of λ=1.8. This limit air/fuel ratio may be reduced accordingly for higher surface loading levels. Moreover, the novel design may allow a power modulation of 1:10.
- The widening of the operating range using the flame barrier according to the present invention opens up the possibility of new application areas and increases the versatility for existing application areas.
- Further advantageous configurations of the invention are described in the exemplary embodiment which is explained in more detail below with reference to the drawing, in which:
- the sole appended FIGURE shows a diagrammatic cross section through a porous burner.
- The text which follows is intended to present a
porous burner 1 having aflame barrier 2 according to the present invention, as well as the resulting options with regard to flexibility and widening the operating range, by way of example, on the basis of an afterburner or heating burner for a hydrogen-operated fuel cell system, for example based on a polymer membrane as electrolyte (PEM), for mobile applications. Naturally, theporous burner 1 is not restricted to an application of this nature. - In particular in mobile applications, the time taken to reach a steady operating state is a crucial factor. This time can be considerably reduced by heating. Either an electrical heating system or a burner which generates a hot exhaust-gas stream by burning, the system fuel hydrogen can be used for this purpose. The use of burners has the advantage that considerably shorter starting times can be achieved than with electrical systems, in particular since in many mobile applications insufficient electrical energy is available.
- Since systems of this type impose very high demands on the discharge of emissions, the burners which are to be used, however, have to satisfy extremely high demands. In this context, widening of the air/fuel ratio range in the direction of low air/fuel ratios is crucial, since otherwise the exhaust-gas temperatures remain too low to significantly shorten the starting time. An additional range of applications for a starting burner of this type can be opened up by increasing the power modulation range.
- The exhaust gases which are formed during what is known as purging, i.e. the blow-off of hydrogen-containing gases from the fuel cell or from an anode hydrogen circuit thereof, when shutting down or from time to time during operation, typically have a hydrogen content of between 5% and 10% by volume. One way of avoiding emission of these exhaust gases into the atmosphere is afterburning. However, the chemical energy contained in this exhaust gas is well below the thermal power required when starting. The use of a single burner both as a starting burner and for the afterburning is therefore only possible if this burner can be reliably operated with a sufficient load spread.
- The only appended FIGURE shows a diagrammatic cross section through the
porous burner 1 having the perforatedflame barrier 2. Theflame barrier 2 is located between amixing space 3, in which air as oxidizing agent and hydrogen or hydrogen-rich gas as reducing agent/fuel are premixed, and acombustion space 4. As is customary inporous burners 1, thecombustion space 4 is filled with a porous material, in which the actual combustion takes place. This porous material could, for example, be an SiC foam with 10 ppi (pores per inch). In addition, all other conceivable configurations of thecombustion space 4 which have already been used in previous porous burners are also possible. Theporous burner 1 illustrated here differs from known porous burners only by virtue of theflame barrier 2 or the material from which the latter is formed. - The material used for the
flame barrier 2 is typically ceramic produced by a slip casting. To minimize the shrinkage during the production process, this material, in addition to the powder fraction, may contain less than 30%, preferably less than 15%, e.g. approx. 10%, by mass of fibrous constituents. These fibrous constituents have the additional advantage of increasing the stability of the material. To keep the material porosity at a sufficiently low level, however, it would also be possible to dispense with adding fibers altogether. - The
flame barrier 2 should have a density of at least 1300 kg/m3 and a material porosity, as defined above, of less than 60%. In this context, a typical material-based upper limit for the density can be specified as 2000 kg/m3, while the typical manufacturing-related lower limit for the material porosity can be specified as 40%. - In tests which have been carried out, values of the order of magnitude of ρ=1750 kg/m3 as the density and approx. 50% as the material porosity have proven ideal. Mixtures of Al2O3 and SiO2, preferably in a mass ratio of approx. 80% to approx. 20%, have been identified as a suitable material. This material is also able to withstand the temperatures of up to 1700° C. which occur in the region of the
flame barrier 2, and here in particular in its region facing thecombustion space 4. - With materials of this type for the perforated
flame barrier 2, in a test carried out using hydrogen, it was possible to achieve safe operation under surface loading of 1300 kW/m2 at an air/fuel ratio of λ=1.8. This limit air/fuel ratio is reduced further accordingly at higher surface loading levels. Moreover, the new type of flame barrier also allows power modulation of 1:10. - A perforated
flame barrier 2 made from material of this type was used in tests. The holes in theflame barrier 2 were made with a diameter of d=0.5 mm. A likewise sufficient functionality is achieved with hole diameters of up to d=0.8 mm. For manufacturing reasons, hole diameters of less than approx. d=0.35 mm are scarcely feasible, even though a good functionality would be expected. - The sum of the cross sections of the holes in the
flame barrier 2 should not exceed 5% of the total area of theflame barrier 2. Particularly good results can be achieved between 1% and 4%. The sum of the cross sections of the holes within the tests undertaken were, for example, approx. 1.4% of the total area of theflame barrier 2. This effectively avoided a flashback on the part of the flame front. However, since the pressure losses caused by theflame barrier 2 also increase with a decrease in cross-sectional area of the holes, in practice theporous burner 1 or theflame barrier 2 should be optimized on the basis of the pressure losses which are just still tolerable within the context given above. For example, if a high pressure is available, it is generally possible for the sum of the cross sections of the holes in theflame barrier 2 to be selected from 1% to 2% for ultrahigh security against flashbacks. If, on the other hand, the air and/or hydrogen is delivered at only a low excess pressure, for example by means of blowers, the sum of the cross sections of the holes in theflame barrier 2 should be selected to be from 3% to 4%, in order to still ensure highly safe operation while at the same time achieving minimal pressure losses in theflame barrier 2. - The widening of the operating range which is achieved with the
perforated flame barrier 2 made from the material described above for the first time allows the use of theporous burner 1 for the conversion of hydrogen in industrial burners and in particular in fuel cell systems. In the fuel cell systems, it is possible on the one hand to shorten the cold-start time and on the other hand to reduce the system complexity, since there is no need for an additional burner. - The advantages of the invention are further clarified below.
- Many scenarios foresee hydrogen as one of the energy carriers of the future, since it allows the generation of heat and power with very low pollutant emissions. NOx is the only potential pollutant during the combustion of hydrogen, since carbon-based pollutants, such as carbon monoxide or particulates, cannot be formed. Possible application areas in which low-emission hydrogen burners are required even now include the chemical industry and use as afterburners and heating burners in fuel cell systems.
- At present, it is primarily non-premix or catalytic burners which are used for the combustion of hydrogen, as opposed to premix combustion systems. In the case of non-premix burners, the fuel is only mixed with the air in the reaction area, so that a flashback fundamentally cannot occur. However, this concept involves relatively high NOx emissions, since irrespective of the overall air excess there are always zones with a stoichiometric mixture composition and therefore high temperatures. By contrast, catalytic burners have the drawback that for many applications they are too susceptible to contamination and temperature fluctuations and have an insufficient power modulation. An additional problem is that they have to be operated with high excesses of air in order to avoid overheating of the catalyst. It is likely that with the state of the art as it stands, the desired low NOx emissions can only be achieved using premix combustion systems.
- In addition to the general benefits of premix burner designs, porous burner technology has further properties which make the use of a porous burner for the combustion of hydrogen an attractive option. With porous burners, the temperature in the combustion zone can be influenced in a targeted way. Moreover, on account of the high heat transport, the temperature field within the combustion zone is very homogeneous. Both these advantages allow very low NOx emissions which cannot be achieved even by most other premix burners. Further advantages of porous burners over other premix burners are the high surface loading which can be achieved and the geometric flexibility in terms of the configuration of the combustion zone.
- The present invention addresses the flashback problem found with porous premix burners. It has been found that when other porous premix burners are operated with hydrogen or hydrogen-rich gases, as are formed for example when hydrogen is obtained by reforming hydrocarbon-containing starting materials (methane, methanol, gasoline, etc.), a flashback of the flame into the mixing space occurs within a short time. Safe, i.e. flashback-free, steady-state operation is only possible if the air excess is greatly increased. The extent of the rise in the air/fuel ratio required depends mainly on the surface loading. Safe operation at a surface loading of 1300 kW/m2, which is customary for porous burners, with the conventional flame barrier configuration is only possible beyond an air/fuel ratio of approximately λ=3.0. Furthermore, the power can only be modulated in the range of 1:2. It has been possible to demonstrate in tests that during the combustion of hydrogen the flame front penetrates into the porous material of the flame barrier, moves through the material in the direction of the mixing space and leads to a flashback. In practice the extremely high risk of flashbacks, which greatly restricts the operating range, constitutes a significant obstacle to the implementation of premix hydrogen burners. The present invention addresses this problem.
Claims (16)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102005027698A DE102005027698A1 (en) | 2005-06-15 | 2005-06-15 | Porous burner for combustion of hydrogen, has mixing space for mixing reducing and oxidizing agents, combustion space filled with porous material, and flame barrier containing another porous material of preset porosity and density |
| DE102005027698.9 | 2005-06-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20060286498A1 true US20060286498A1 (en) | 2006-12-21 |
Family
ID=37489646
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/447,726 Abandoned US20060286498A1 (en) | 2005-06-15 | 2006-06-06 | Porous burner having a flame barrier |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US20060286498A1 (en) |
| JP (1) | JP2006349337A (en) |
| DE (1) | DE102005027698A1 (en) |
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| CN102401381A (en) * | 2010-09-16 | 2012-04-04 | 哈尔滨北辰电站设备有限公司 | Mixing device with pore plates |
| CN106524143A (en) * | 2016-11-10 | 2017-03-22 | 江苏大学 | Burner applied to microthermophotovoltaic system |
| WO2020182902A1 (en) * | 2019-03-12 | 2020-09-17 | Bekaert Combustion Technology B.V. | Method to operate a modulating burner |
| WO2021078949A1 (en) * | 2019-10-25 | 2021-04-29 | Bekaert Combustion Technology B.V. | Surface stabilized fully premixed gas premix burner for burning hydrogen gas, and method for starting such burner |
| US20210348755A1 (en) * | 2018-10-17 | 2021-11-11 | Beckett Thermal Solutions Ltd. | Method for forming a gas burner membrane |
| EP4101825A1 (en) * | 2021-06-11 | 2022-12-14 | Orkli, S. Coop. | Burner surface |
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| EP3540310A1 (en) * | 2018-03-12 | 2019-09-18 | H.J.Th.M. Taris Beheer B.V. | A method for heat transport and regulation |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1830826A (en) * | 1925-08-17 | 1931-11-10 | Cox Frederick John | Refractory diaphragm for use in surface-combustion apparatus |
| US3912443A (en) * | 1972-09-25 | 1975-10-14 | Foseco Int | Radiant gas burners |
| US5522723A (en) * | 1993-07-02 | 1996-06-04 | Franz Durst | Burner having porous material of varying porosity |
| US5749721A (en) * | 1993-07-22 | 1998-05-12 | Gossler Thermal Ceramics Gmbh | Ceramic combustion support element for surface burners and process for producing the same |
| US6331366B1 (en) * | 1999-06-23 | 2001-12-18 | International Fuel Cells Llc | Operating system for a fuel cell power plant |
-
2005
- 2005-06-15 DE DE102005027698A patent/DE102005027698A1/en not_active Withdrawn
-
2006
- 2006-06-06 US US11/447,726 patent/US20060286498A1/en not_active Abandoned
- 2006-06-13 JP JP2006164107A patent/JP2006349337A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1830826A (en) * | 1925-08-17 | 1931-11-10 | Cox Frederick John | Refractory diaphragm for use in surface-combustion apparatus |
| US3912443A (en) * | 1972-09-25 | 1975-10-14 | Foseco Int | Radiant gas burners |
| US5522723A (en) * | 1993-07-02 | 1996-06-04 | Franz Durst | Burner having porous material of varying porosity |
| US5749721A (en) * | 1993-07-22 | 1998-05-12 | Gossler Thermal Ceramics Gmbh | Ceramic combustion support element for surface burners and process for producing the same |
| US6331366B1 (en) * | 1999-06-23 | 2001-12-18 | International Fuel Cells Llc | Operating system for a fuel cell power plant |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102401381A (en) * | 2010-09-16 | 2012-04-04 | 哈尔滨北辰电站设备有限公司 | Mixing device with pore plates |
| CN106524143A (en) * | 2016-11-10 | 2017-03-22 | 江苏大学 | Burner applied to microthermophotovoltaic system |
| US20210348755A1 (en) * | 2018-10-17 | 2021-11-11 | Beckett Thermal Solutions Ltd. | Method for forming a gas burner membrane |
| US12379106B2 (en) * | 2018-10-17 | 2025-08-05 | Beckett Thermal Solutions Ltd. | Method for forming a gas burner membrane |
| WO2020182902A1 (en) * | 2019-03-12 | 2020-09-17 | Bekaert Combustion Technology B.V. | Method to operate a modulating burner |
| CN113557390A (en) * | 2019-03-12 | 2021-10-26 | 贝卡尔特燃烧技术股份有限公司 | Method for operating an adjustable burner |
| US12135128B2 (en) | 2019-03-12 | 2024-11-05 | Bekaert Combustion Technology B.V. | Method to operate a modulating burner |
| WO2021078949A1 (en) * | 2019-10-25 | 2021-04-29 | Bekaert Combustion Technology B.V. | Surface stabilized fully premixed gas premix burner for burning hydrogen gas, and method for starting such burner |
| 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 |
| US12305856B2 (en) | 2019-10-25 | 2025-05-20 | Bekaert Combustion Technology B.V. | Surface stabilized fully premixed gas premix burner for burning hydrogen gas, and method for starting such burner |
| KR102862099B1 (en) * | 2019-10-25 | 2025-09-22 | 베카에르트 컴버스천 테크놀러지 비.브이. | Surface-stabilized fully premixed gas premixed burner for combusting hydrogen gas, and method for starting such burner |
| EP4101825A1 (en) * | 2021-06-11 | 2022-12-14 | Orkli, S. Coop. | Burner surface |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2006349337A (en) | 2006-12-28 |
| DE102005027698A1 (en) | 2006-12-21 |
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