WO2013024783A1 - H2 burner and h2 burner combustion method - Google Patents
H2 burner and h2 burner combustion method Download PDFInfo
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- WO2013024783A1 WO2013024783A1 PCT/JP2012/070334 JP2012070334W WO2013024783A1 WO 2013024783 A1 WO2013024783 A1 WO 2013024783A1 JP 2012070334 W JP2012070334 W JP 2012070334W WO 2013024783 A1 WO2013024783 A1 WO 2013024783A1
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- catalyst
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- 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
- F23C13/00—Apparatus in which combustion takes place in the presence of catalytic material
- F23C13/06—Apparatus in which combustion takes place in the presence of catalytic material in which non-catalytic combustion takes place in addition to catalytic combustion, e.g. downstream of a catalytic element
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
- F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
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- 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
- F23C2201/00—Staged combustion
- F23C2201/30—Staged fuel supply
- F23C2201/301—Staged fuel supply with different fuels in stages
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- 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
- F23C2900/13002—Catalytic combustion followed by a homogeneous combustion phase or stabilizing a homogeneous combustion phase
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- 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
- F23C2900/99006—Arrangements for starting combustion
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- 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23N—REGULATING OR CONTROLLING COMBUSTION
- F23N2227/00—Ignition or checking
- F23N2227/40—Catalytic ignition
Definitions
- the present invention relates to an H 2 burner and a combustion method of the H 2 burner.
- H 2 gas has a wide combustion range and a high combustion speed due to its physical properties, it is difficult to apply combustion techniques such as hydrocarbon gas, reformed gas, or city gas, which have been widely used so far. As an industrial heating source, the field of use has been limited. In addition, since H 2 gas is more easily combusted than other fuels, countermeasures against backfire and countermeasures for suppressing NO X generation have become important issues in general hydrogen combustion.
- H 2 gas continues to burn at a relatively low temperature compared to other fuels, it is known that when H 2 gas is burned using a catalyst, it becomes a stable and efficient burner. .
- H 2 gas is said to be an effective combustion catalyst for many metals and metal oxides compared to hydrocarbon-based gas.
- H 2 gas is an extreme method for automatically igniting liquid hydrogen. Low temperature catalytic combustion methods have been introduced.
- a direct ignition type pilot burner using an ignition transformer is used for ignition of an industrial combustion furnace.
- a fuel having a combustion rate of about several tens of cm / sec such as hydrocarbon gas or city gas
- H 2 gas as the fuel
- the pilot burner needs to be burned for a certain period of time until it is transferred to the main burner not only when used as a continuous pilot for ignition but also when used as a timed pilot. Therefore, the inventors of the present application have intensively studied about using a burner that uses H 2 gas as fuel and burns using a catalyst. However, if combustion is continued for a certain period of time by the catalyst, the catalyst deteriorates due to sintering, oxidation, or the like. And the high temperature resistance of the support has reached its limit and the catalyst has deteriorated.
- the invention according to claim 1 is an H 2 burner having two different gas flow paths, wherein the first flow path includes the H 2 gas and the first combustion-supporting gas.
- the second flow path is configured to flow H 2 gas or the second combustion-supporting gas, and the tip of the second flow path is the first flow path.
- a flame formed at the tip of the flow path is disposed at a position where the flame can be transferred, and a catalyst that can be ignited by supplying H 2 gas and a first combustion-supporting gas to the first flow path. Is a burner for H 2 .
- the invention according to claim 2 is the H 2 burner according to claim 1, wherein the catalyst contains at least one of Pt, Pd, PdO, and PtO 2 .
- the invention according to claim 3 is characterized in that a detection mechanism capable of detecting the formation of a flame is provided at the tip of the first flow path. 2 burner.
- the invention according to claim 4 is a combustion method of an H 2 burner having two different gas flow paths, and a catalyst is provided in the first flow path, wherein the first flow path H 2 gas and a first combustion-supporting gas are caused to flow through and are ignited by the catalyst to form a flame at the tip of the first flow path, and H 2 in the second flow path of the H 2 burner.
- the invention according to claim 5 is characterized in that after a flame is formed at the tip of the first flow path, H 2 gas or a second combustion-supporting gas is flowed into the second flow path. It is a combustion method of H 2 burner according to claim 4.
- the invention according to claim 6 is characterized in that the catalyst contains at least one of Pt, Pd, PdO or PtO 2.
- the H 2 burner of the present invention is provided with a catalyst that can be ignited by supplying H 2 gas and a combustion-supporting gas to the first flow path. Accordingly, by the first flow path flowing a combustion-supporting gas and H 2 gas, it was possible to ignite using a catalyst without using a transformer or the like. As a result, since ignition is performed without using a transformer, H 2 gas is used as fuel, but no detonation or the like occurs, and safety is ensured. Further, the tip of the second channel is formed at a position where it can be transferred from the tip of the first channel. Therefore, a fire is formed by the catalyst provided in the first flow path, and at the same time or around that time, H 2 gas or combustion-supporting gas is flowed into the second flow path.
- the catalyst formed in the first flow path contains at least one of Pt, Pd, PdO, and PtO 2 . Thereby, it can ignite in a catalyst efficiently.
- a detection mechanism capable of detecting the formation of flame is provided at the tip of the first flow path. As a result, it is possible to accurately detect whether or not a fire is formed at the tip of the first flow path, and it is possible to accurately stop the supply of gas to the first flow path.
- the method of combustion H 2 burner of the present invention is ignited by supplying H 2 gas and combustion-supporting gas to the catalyst formed in the first flow path. Therefore, since no transformer is used for ignition, detonation or the like does not occur and safety is ensured. Further, in the combustion method of the H 2 burner according to the present invention, ignition is performed by the catalyst, and simultaneously with or around that time, H 2 gas or a combustion-supporting gas is caused to flow through the second flow path to transfer the seed flame. Of the gas flowing through the first flow path, the flow of the same type of gas as that flowing through the second flow path is stopped. As a result, combustion of H 2 gas in the catalyst can be stopped, and deterioration of the catalyst can be prevented. Even if the flow of one of the H 2 gas and the combustion-supporting gas flowing in the first flow path is stopped, the same gas flows in the second flow path. A flame can be formed continuously at the tip.
- FIG. 1 is a cross-sectional view showing an example of the H 2 burner of the present embodiment.
- FIG. 2A is a cross-sectional view showing an example of the H 2 burner of this embodiment
- FIG. 2B is a side view of the H 2 burner as viewed from the front end side.
- FIG. 3 is a perspective view showing a part of another example of the H 2 burner of the present embodiment.
- FIG. 4 is a view showing a heat treatment apparatus using the H 2 burner of the present embodiment.
- FIG. 5 is a view showing a flare stack using the H 2 burner of the present embodiment.
- FIG. 6 is a graph showing the relationship between the H 2 concentration on the catalyst and the time until confirmation of ignition in one example of the present invention.
- FIG. 7 is a graph showing the minimum ignition energy depending on the concentration of the hydrogen-air mixture.
- FIG. 8 is a cross-sectional view showing a part of the H 2 burner used in one embodiment of the present invention.
- FIG. 9 is a graph showing the relationship between the air flow rate and the maximum temperature achieved in one embodiment of the present invention.
- H 2 burner and combustion method H 2 burner of the present invention will be described with reference to the drawings.
- FIG. 1 is a cross-sectional view showing an H 2 burner 1 according to an embodiment of the present invention.
- the H 2 burner 1 is a pipe-like structure having two different gas flow paths A and B inside.
- the outer tube 2 and the inner tube 2 are arranged in the outer tube 2.
- the tube 3, the catalyst 4 formed on the tip 3 a side of the inner tube 3, and the inner tube 5 disposed in the inner tube 3 are configured.
- the outer tube 2 is a pipe-shaped hollow tube body, and an inner tube 3 is disposed on the inner side, and an opening 2 c is formed at the tip 2 a of the outer tube 2. Further, the downstream side of the opening 2c is a combustion portion 6, which is configured so that a flame F can be formed.
- a combustion-supporting gas supply device 7 is connected to one end 2 b (rear end) of the outer tube 2 opposite to the tip 2 a via a pipe 8, and the outer tube 2 is connected to the combustion portion 6. It is formed so as to be able to supply a combustion-supporting gas (second combustion-supporting gas).
- the inner tube 3 is a pipe-shaped hollow tube body, and is arranged in the outer tube 2 with the same axial direction as that of the outer tube 2, and a flame (not shown) is provided at the tip 3 a of the inner tube 3. It is configured so that it can be formed.
- An H 2 gas supply device 9 is connected to one end 3b (rear end) side of the inner tube 3 opposite to the tip 3a via a pipe 10, and the inner tube 3 is connected to the catalyst 4 and the combustion portion 6. It is formed so that H 2 gas can be supplied.
- the inside of the inner tube 3 on the tip 3a side is filled with a catalyst 4 (catalyst layer), and the tip 3a of the inner tube 3 is formed in a nozzle shape having a plurality of ejection holes 3c. .
- the arrangement position of the inner tube 3 may be any position as long as the flame formed at the tip 3a of the inner tube 3 can be transferred to the tip 2a of the outer tube 2.
- the position of the distal end 3a of the inner tube 3 can be a position retracted from the position of the distal end 2a of the outer tube 2, or can be a protruding position.
- the flame formation region by the tip 3a of the inner tube 3 overlaps at least partly with the formation region of the flame F by the tip 2a of the outer tube 2
- the flame formed at the tip 3a of the inner tube 3 Since it can be transferred to the tip 2a of the outer tube 2, the position of the tip 3a of the inner tube 3 can be arbitrarily adjusted with respect to the position of the tip 2a of the outer tube 2 so as to satisfy this positional relationship.
- the catalyst 4 may be any catalyst that can be ignited by supplying H 2 gas and a combustion-supporting gas, and any one or more of Pt, Pd, PdO, and PtO 2 If a material containing is used, it becomes possible to ignite efficiently. In particular, when Pd or PdO is used as a catalyst, it is useful as an H 2 dissociation catalyst even if the flow rate of supplied combustion-supporting gas is changed, and the flow rate of H 2 gas is excessive. However, since it has sufficient ignition performance, it is more preferable.
- the catalyst 4 reaches a temperature of 500 to 800 degrees at the maximum.
- an inner pipe 5 is further arranged inside the inner pipe 3 on the upstream side of the catalyst 4.
- the inner tube 5 is a pipe-shaped hollow tube body, and is arranged in the inner tube 3 with the same axial direction as the inner tube 3 and the outer tube 2.
- a combustion-supporting gas supply device 21 is connected to one end 5b (rear end) side of the inner pipe 5 opposite to the front end 5a via a pipe 22, and the inner pipe 5 includes the catalyst 4 and the combustion portion 6. It is formed so as to be able to supply a combustion-supporting gas (first combustion-supporting gas). Further, the arrangement position of the inner tube 5 may be any position as long as the tip 5a of the inner tube 5 can spray the combustion-supporting gas to the catalyst 4.
- the flow path A (second flow path) is formed in the space between the outer tube 2 and the inner tube 3 disposed in the outer tube 2, and the inner tube 3.
- a flow path C is formed in the space between the inner pipe 5 and the inner pipe 5 disposed in the inner pipe 3, and a flow path D is formed in the inner pipe 5.
- a flow path B (first flow path) formed by joining the flow path C and the flow path D is formed. That is, the flow path A is configured so that the combustion-supporting gas flows, the flow path B includes the H 2 gas and the combustion-supporting gas, the flow path C includes the H 2 gas, and the flow path D includes the combustion support gas.
- the H 2 burner 1 detects a flame in a space located inside the outer tube 2 and downstream of the tip 3a of the inner tube 3.
- a detection mechanism 23 may be provided. Thereby, it is possible to quickly and accurately detect whether or not a flame is formed in the inner tube 3. Examples of the detection mechanism 23 include a frame rod, a thermometer, and a UV sensor.
- the H 2 burner 1 of the present embodiment is configured as described above.
- the combustion-supporting gas supply device 7 is connected to the outer tube 2
- the H 2 supply device 9 is connected to the inner tube 3
- the combustion-supporting gas supply device 21 is connected to the inner tube 5. It is not limited to such an aspect.
- an H 2 gas supply device may be connected to the outer tube 2.
- a combustion-supporting gas supply device may be connected to the inner pipe 3 and an H 2 gas supply device may be connected to the inner pipe 5.
- combustion-supporting gas is caused to flow through the flow path D in the inner tube 5 using the combustion-supporting gas supply device 21, and the space between the inner tube 3 and the inner tube 5 using the H 2 gas supply device 9.
- H 2 gas is allowed to flow through the channel C formed in Note that the combustion-supporting gas supplied by the combustion-supporting gas supply device 21 may be air or oxygen, for example.
- the gas flowing through the flow channel C and the gas flowing through the flow channel D merge into the flow channel B formed on the distal end 3a side of the inner tube 3 so that the H 2 gas and the combustion-supporting gas flow.
- the H 2 gas and the combustion-supporting gas are also supplied to the catalyst 4 provided on the tip 3a side of the inner tube 3.
- the H 2 gas starts to burn (ignites) in the catalyst 4, and a flame (not shown) is formed at the tip 3 a of the inner tube 3 that is the tip of the flow path B.
- the flow rate of the gas flowing in the flow path C and the flow path D is any if the temperature of H 2 and the combustion-supporting gas that have passed through the catalyst 4 exceeds 530 ° C., which is the spontaneous ignition temperature of H 2. Such a flow rate may be used and may be determined appropriately.
- a flame When a flame is formed at the tip of the flow path B, it is supported at the flow path A formed between the outer pipe 2 and the inner pipe 3 by using the support gas supply device 7 at the same time or around that time. Flow flammable gas. As a result, the flame formed at the tip of the channel B is transferred to the tip 2a of the outer tube 2 that is the tip of the channel A, and a flame F is formed at the tip of the channel A.
- combustion-supporting gas supplied from the combustion-supporting gas supply device 7 may be air or oxygen, for example, and is necessarily the same gas as the combustion-supporting gas supplied from the combustion-supporting gas supply device 21. There is no.
- the detection mechanism 23 when the detection mechanism 23 is provided in the outer tube 2, it is possible to accurately detect whether or not a flame is formed at the tip of the flow path B by the detection mechanism 23.
- the supply of the combustion-supporting gas can be stopped with high accuracy.
- stopping the supply of the same type of gas means, for example, that the combustion-supporting gas supplied to the flow path A is air and the combustion support gas supplied to the flow path B is oxygen. It also includes stopping the supply of the combustion-supporting gas (in this case, oxygen) supplied to B.
- a catalyst 4 that can be ignited by supplying H 2 gas and combustion-supporting gas to the flow path B is provided.
- the combustion-supporting gas and the H 2 gas to the flow path B, it becomes possible to ignite using the catalyst 4 without using a transformer or the like.
- the tip end of the flow path A is formed at a position where it can be transferred from the front end of the flow path B.
- the catalyst 4 provided in the flow path B forms a fire, and at the same time or around that time, the combustion supporting gas is supplied to the flow path A, and the fire is transferred to the tip of the flow path A. Then, the catalyst deterioration can be prevented by stopping the supply of the combustion-supporting gas to the flow path B. That is, after the seed fire is formed by the catalyst and it is transferred, both the H 2 gas and the combustion-supporting gas pass through the catalyst by stopping the supply of the combustion-supporting gas supplied to the catalyst. The time can be shortened, and the deterioration of the catalyst can be prevented by stopping the combustion with the catalyst. Further, even if the flow of the combustion-supporting gas to the flow path B is stopped, since the combustion support gas that is the same gas is supplied from the flow path A, the flame is continuously formed at the end of the flow path A. can do.
- ignition is performed by supplying H 2 gas and combustion-supporting gas to the catalyst 4 formed in the flow path B. Therefore, since no transformer is used for ignition, detonation or the like does not occur and safety is ensured. Further, it is ignited by the catalyst 4 to form a seed flame at the tip of the flow path B. At the same time or around that, a combustion-supporting gas is caused to flow through the flow path A, and the seed fire is transferred to the tip of the flow path A The flow of the combustion-supporting gas to the flow path B is stopped.
- the H 2 burner 1 described above has a configuration in which the inner tube 3 is disposed inside the outer tube 2, but two different flow paths can be formed and formed at the tip of the first flow path. As long as the fired flame can be transferred to the tip of the second flow path, the burner may have any structure, and may be composed of two separated tubes. As an example composed of two tube bodies, for example, as shown in FIG. 3, the inner tube 3 disposed inside the outer tube 2 may be disposed beside the outer tube 2.
- both the H 2 gas and the combustion-supporting gas are provided in the inner tube 3 without providing the inner tube 5.
- the H 2 gas and the combustion-supporting gas are supplied to the catalyst 4 without mixing the H 2 gas and the combustion-supporting gas in advance.
- the possibility of backfire during ignition is low.
- both the H 2 gas and the combustion-supporting gas are simply supplied into the inner pipe 3 without providing the inner pipe 5, these gases are mixed in advance, so as to appropriately prevent backfire. It is preferable to take measures.
- the heating target gas heating device 24 using the H 2 burner according to the present embodiment is roughly composed of a main burner 25 and an H 2 burner 1 provided at the tip of the main burner 25. It is configured.
- the main burner 25 is formed so as to surround the outer periphery of the piping 27 that supplies the target gas to the combustion portion 26 that is the space of the tip portion of the main burner 25, and the jet outlet 28 a that supplies fuel to the combustion portion 26.
- a main burner main body 28 provided with.
- the main burner body 28 is connected to a pipe 29 for introducing fuel into the main burner body 28.
- the H 2 burner 1 that is a pilot burner is ignited. Then, the gas to be heated is supplied from the pipe 27 of the main burner 25 and the fuel is supplied from the main burner body 28, and the main burner 25 is ignited using the flame of the H 2 burner 1. In this way, a flame (not shown) is formed in the combustion portion 26 at the tip of the main burner 25, and the target gas is heated.
- H 2 gas when used as the fuel for the main burner, the pilot burner is ignited in advance as described above in order to prevent explosion due to mixing of H 2 gas and combustion-supporting gas in the furnace. Fuel will be introduced.
- a device for introducing a fuel such as a hydrocarbon-based gas different from the fuel for the main burner into the pilot burner, and A device for detecting the leakage was necessary. For this reason, there is a disadvantage that the cost required for the ignition operation of the main burner increases.
- the H 2 burner 1 of the present embodiment if the H 2 burner 1 of the present embodiment is used, it is possible to ignite safely while using H 2 gas as a fuel. Therefore, a supply device for fuel other than H 2 and a device for detecting leakage thereof are provided. It becomes unnecessary and the expense concerning ignition of the main burner 25 can be suppressed.
- the flare stack 41 includes a discharge tower 43 connected to a storage facility 42 for a desired gas to be burned, and a H 2 burner 1 provided at the tip of the discharge tower 43. .
- the H 2 burner 1 When gas is burned using the flare stack 41, the H 2 burner 1 is first ignited. Then, the desired gas to be combusted from the storage facility 42 may be sent to the emission tower 43 and the desired gas may be ignited and combusted at the tip of the emission tower 43 using the flame of the H 2 burner 1.
- the H 2 gas may be used as fuel for the H 2 burner, so the fuel for the burner and facilities for supplying it are also provided. This eliminates the need for cost reduction.
- the flame using H 2 gas as a fuel is less likely to blow out as compared with the case where a hydrocarbon-based gas is used as a fuel like a conventional burner, when the H 2 burner 1 is used, Even when the wind speed in the discharge tower 43 is increased, it functions without blowing off.
- the use of the H 2 burner 1 makes it possible to reduce the inner diameter of the discharge tower 43 compared to the case of using a conventional burner.
- the flare stack 41 itself can be downsized.
- Example 1 In Example 1, using the same H 2 burner and burner 1 for H 2 as described above, the H 2 gas in the outer tube 2 at a flow rate of 10L / min, the inner tube 5 H 2 gas 1.5 L / The time required for ignition was measured when the flow rate of air supplied to the inner tube 3 was changed at a flow rate of min.
- the catalyst used was Pd and the ambient and initial gas temperatures were 20 ° C. The results are shown in FIG. Note that the ignition was confirmed using a thermometer installed on the distal end side in the outer tube 2.
- Example 2 In Example 2, using the same H 2 burner with H 2 burner 1 described in the embodiment, Pd as a catalyst, Pt, for the case of using each of PdO and PtO 2, were compared in ignition performance . Specifically, the H 2 gas in the outer tube 2 at a flow rate of 10L / min, H 2 gas into the inner tube 5 was supplied at a flow rate of 2L / min, while changing the flow rate of air supplied to the inner tube 3 However, the performance was compared by measuring the maximum temperature reached 30 seconds after the ignition operation. In addition, the measurement of the maximum temperature was performed using the temperature sensor 44 installed in the outer wall of the front-end
- H 2 and combustion-supporting gas that has passed through the catalyst is present in the range of air air volume indicating a temperature above 530 ° C. autoignition point of H 2, H 2 gas It was found that it had the performance necessary for ignition. Further, Pd or PdO is when used as a catalyst, since the H 2 and combustion-supporting gas that has passed through the catalyst over a wide range of air flow rate reaches a temperature above 530 ° C., as a very H 2 dissociation catalyst It turns out that it is useful.
- Example 2 Although the temperature rose to 750 ° C. at the maximum, no backfire was confirmed under any conditions, and by adopting a structure in which H 2 gas and combustion-supporting gas were not mixed in advance, H 2 It was confirmed that ignition could be performed without backfire even when the temperature of the battery rose.
- the H 2 gas is used as a fuel because it ignites without using a transformer by flowing a combustion-supporting gas and H 2 gas through the first flow path of the H 2 burner. No detonation occurs and safety is ensured. Accordingly, the present invention can be suitably used in H 2 burner and combustion method.
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- Combustion & Propulsion (AREA)
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Abstract
Description
本願は、2011年8月17日に日本に出願された特願2011-178212号に基づき優先権を主張し、その内容をここに援用する。 Recently, in order to prevent global warming has become a serious, solar, wind, geothermal, ocean, although focused on renewable energy hydropower etc. are gathered, not only it does not emit carbon dioxide by combustion H 2 Gas is also expected to be used effectively as an ideal fuel.
This application claims priority based on Japanese Patent Application No. 2011-178212 for which it applied to Japan on August 17, 2011, and uses the content here.
また、H2ガスは、他の燃料と比べ燃焼しやすいので、一般的な水素燃焼においては、逆火に対する対策やNOX発生抑制に対する対策が重要な課題となっていた。 However, since H 2 gas has a wide combustion range and a high combustion speed due to its physical properties, it is difficult to apply combustion techniques such as hydrocarbon gas, reformed gas, or city gas, which have been widely used so far. As an industrial heating source, the field of use has been limited.
In addition, since H 2 gas is more easily combusted than other fuels, countermeasures against backfire and countermeasures for suppressing NO X generation have become important issues in general hydrogen combustion.
また、H2ガスは、炭化水素系ガスと比較すると、多くの金属や金属酸化物が有効な燃焼触媒になると言われており、特殊な例ではあるが、液体水素の自動着火方法として、極低温触媒燃焼方法が紹介されたことがある。 On the other hand, since H 2 gas continues to burn at a relatively low temperature compared to other fuels, it is known that when H 2 gas is burned using a catalyst, it becomes a stable and efficient burner. .
In addition, H 2 gas is said to be an effective combustion catalyst for many metals and metal oxides compared to hydrocarbon-based gas. As a special example, H 2 gas is an extreme method for automatically igniting liquid hydrogen. Low temperature catalytic combustion methods have been introduced.
ここで、パイロットバーナの燃料として、炭化水素系ガスや都市ガスのように燃焼速度が数十cm/sec程度の燃料を用いるのであれば問題はないが、燃料としてH2ガスを用いる場合は、その燃焼速度が2.6m/secと速いため安全性に問題があった。
特に、燃焼炉内のパージ不良や未着火時のように、燃料と空気の混合気体が充満した状態で再着火すると、爆轟が生じる可能性があり、危険であった。 By the way, in general, a direct ignition type pilot burner using an ignition transformer is used for ignition of an industrial combustion furnace.
Here, there is no problem if a fuel having a combustion rate of about several tens of cm / sec, such as hydrocarbon gas or city gas, is used as the fuel for the pilot burner, but when using H 2 gas as the fuel, Since the burning speed was as fast as 2.6 m / sec, there was a problem in safety.
In particular, if reignition is performed in a state in which a mixed gas of fuel and air is filled, such as in the case of poor purge in the combustion furnace or unignited, detonation may occur, which is dangerous.
そこで、本願発明者らは、H2ガスを燃料とし、触媒を用いて燃焼させるバーナを用いることについて鋭意検討したが、触媒によって一定時間燃焼を継続させると、触媒が焼結や酸化等によって劣化したり、担体の高温耐性が限界に達して触媒が劣化したりするという問題があることを突き止めた。 Further, the pilot burner needs to be burned for a certain period of time until it is transferred to the main burner not only when used as a continuous pilot for ignition but also when used as a timed pilot.
Therefore, the inventors of the present application have intensively studied about using a burner that uses H 2 gas as fuel and burns using a catalyst. However, if combustion is continued for a certain period of time by the catalyst, the catalyst deteriorates due to sintering, oxidation, or the like. And the high temperature resistance of the support has reached its limit and the catalyst has deteriorated.
また、第1の流路の先端から火移り可能な位置に第2の流路の先端が形成されている。
したがって、第1の流路に設けられた触媒によって種火を形成し、それと同時にもしくはそれと前後して、第2の流路にH2ガスまたは支燃性ガスを流し、第2の流路の先端に種火を火移りさせ、その後に第2の流路に流すガスと同様の種類のガスを、第1の流路に流すことを停止させることで、触媒の劣化を防止することができる。すなわち、触媒によって種火が形成され、それを火移りさせた後に、触媒に供給するH2ガスまたは支燃性ガスの片方の供給を停止することで、触媒でのH2ガスの燃焼を停止させることができ、触媒の劣化を防止することができる。また、H2ガスまたは支燃性ガスの片方について、第1の流路に流すことを停止しても、それと同じガスが第2の流路から供給されるので、第2の流路の先端において火炎を継続して形成することができる。 The H 2 burner of the present invention is provided with a catalyst that can be ignited by supplying H 2 gas and a combustion-supporting gas to the first flow path. Accordingly, by the first flow path flowing a combustion-supporting gas and H 2 gas, it was possible to ignite using a catalyst without using a transformer or the like. As a result, since ignition is performed without using a transformer, H 2 gas is used as fuel, but no detonation or the like occurs, and safety is ensured.
Further, the tip of the second channel is formed at a position where it can be transferred from the tip of the first channel.
Therefore, a fire is formed by the catalyst provided in the first flow path, and at the same time or around that time, H 2 gas or combustion-supporting gas is flowed into the second flow path. It is possible to prevent the catalyst from deteriorating by stopping the flow of the same kind of gas as the gas flowing through the second flow path to the first flow path after stopping the seed flame at the tip. . That, is formed pilot flame by the catalyst, after it is flame diffusion, by stopping one of the supply of H 2 gas or combustion-supporting gas supplied to the catalyst, stopping the combustion of the H 2 gas at the catalyst And the deterioration of the catalyst can be prevented. Further, even if one of the H 2 gas and the combustion-supporting gas is stopped from flowing into the first flow path, the same gas is supplied from the second flow path, so that the tip of the second flow path The flame can be continuously formed in
また、本発明のH2用バーナの燃焼方法では、触媒によって着火し、それと同時にまたはそれと前後して、第2の流路にH2ガスまたは支燃性ガスを流して種火を火移りさせ、第1の流路に流すガスのうち、第2の流路に流すガスと同様の種類のガスについては、流すことを停止している。この結果、触媒でのH2ガスの燃焼を停止することができ、触媒の劣化を防止することができる。また、第1の流路に流していたH2ガスまたは支燃性ガスの片方について、流すことを停止しても、それと同じガスを第2の流路に流すので、第2の流路の先端において、火炎を継続して形成することができる。 Further, the method of combustion H 2 burner of the present invention is ignited by supplying H 2 gas and combustion-supporting gas to the catalyst formed in the first flow path. Therefore, since no transformer is used for ignition, detonation or the like does not occur and safety is ensured.
Further, in the combustion method of the H 2 burner according to the present invention, ignition is performed by the catalyst, and simultaneously with or around that time, H 2 gas or a combustion-supporting gas is caused to flow through the second flow path to transfer the seed flame. Of the gas flowing through the first flow path, the flow of the same type of gas as that flowing through the second flow path is stopped. As a result, combustion of H 2 gas in the catalyst can be stopped, and deterioration of the catalyst can be prevented. Even if the flow of one of the H 2 gas and the combustion-supporting gas flowing in the first flow path is stopped, the same gas flows in the second flow path. A flame can be formed continuously at the tip.
図1は、本発明の一実施形態であるH2用バーナ1を示す断面図である。
H2用バーナ1は、内部に2つの異なるガスの流路A,Bを有するパイプ状の構造体であり、図1に示すように、外管2と、外管2内に配置された内管3と、内管3の先端3a側に形成された触媒4と、内管3内に配置された内管5と、を有した構成となっている。 <H 2 burner>
FIG. 1 is a cross-sectional view showing an H 2 burner 1 according to an embodiment of the present invention.
The H 2 burner 1 is a pipe-like structure having two different gas flow paths A and B inside. As shown in FIG. 1, the
内管3の先端3aとは反対側の一端3b(後端)側には、H2ガス供給装置9が配管10を介して接続されており、内管3は、触媒4及び燃焼部分6にH2ガスを供給することが可能なように形成されている。 The
An H 2
特に、PdまたはPdOを触媒として用いた場合は、供給される支燃性ガスの流量を変化させても、H2解離触媒として有用であり、また、H2ガスの流量が過多な状態であっても、十分な着火性能を有するので、より好ましい。
なお、触媒4は、最高で500~800度の温度に達する。 The
In particular, when Pd or PdO is used as a catalyst, it is useful as an H 2 dissociation catalyst even if the flow rate of supplied combustion-supporting gas is changed, and the flow rate of H 2 gas is excessive. However, since it has sufficient ignition performance, it is more preferable.
The
内管5は、パイプ状の中空管体であって、内管3や外管2と軸線方向を同一にしつつ内管3内に配置されている。 Further, an
The
すなわち、流路Aは支燃性ガスが、流路BはH2ガスおよび支燃性ガスが、流路CはH2ガスが、流路Dは支燃性ガスが、それぞれ流れるように構成されている。 Thus, in the H 2 burner 1, the flow path A (second flow path) is formed in the space between the
That is, the flow path A is configured so that the combustion-supporting gas flows, the flow path B includes the H 2 gas and the combustion-supporting gas, the flow path C includes the H 2 gas, and the flow path D includes the combustion support gas. Has been.
本実施形態のH2用バーナ1は、以上のような構成をしている。 Further, as shown in FIGS. 2A and 2B, the H 2 burner 1 detects a flame in a space located inside the
The H 2 burner 1 of the present embodiment is configured as described above.
次に、上記したH2用バーナ1を用いたH2用バーナの燃焼方法について説明する。
まず、支燃性ガス供給装置21を用いて、内管5内の流路Dに支燃性ガスを流し、H2ガス供給装置9を用いて内管3と内管5との間の空間に形成された流路CにH2ガスを流す。
なお、支燃性ガス供給装置21が供給する支燃性ガスは、例えば空気や酸素であってもよい。 <Combustion method of H 2 burner>
Next, a combustion method of the H 2 burner using the above-described H 2 burner 1 will be described.
First, the combustion-supporting gas is caused to flow through the flow path D in the
Note that the combustion-supporting gas supplied by the combustion-supporting
まず、H2分子が触媒4上に吸着し、このH2分子が触媒4上でH原子に解離する。そして、解離してできたH原子が酸素と反応することによって反応熱が生じる。その結果、この反応熱を発火エネルギーとしてH2が燃焼状態に移行すると考えられている。 Although the details of the ignition principle of H 2 gas by the
First, H 2 molecules are adsorbed on the
なお、触媒でのH2ガスの燃焼時間が長いと、触媒の劣化が激しくなることからから、支燃性ガスの供給の停止は、流路Bの先端に種火が形成されてから、または流路Aの先端に火炎Fが形成されてから、間をおかず、略同時に行われるのが好ましい。 When the flame F is formed at the front end of the flow path A, the flow of the combustion-supporting gas to the flow path C and eventually to the flow path B is stopped by the combustion support
Note that if the combustion time of H 2 gas in the catalyst is long, the deterioration of the catalyst becomes severe. Therefore, the supply of the combustion-supporting gas is stopped after the seed flame is formed at the tip of the flow path B, or After the flame F is formed at the front end of the flow path A, it is preferable that the steps be performed substantially at the same time.
流路AにH2ガスを流すようにしてもよい。また、流路BにH2ガスと支燃性ガスの両方を流すことができるのであれば、流路Cおよび流路Dに流すガスの選択は適宜決定すればよい。 In the embodiment described above, flowing combustion-supporting gas into the flow path A and the flow path D, the case has been described where the flow of H 2 gas to the flow path C, not necessarily limited to this embodiment.
The flow path A may flow H 2 gas. In addition, if both the H 2 gas and the combustion-supporting gas can be flowed to the flow path B, the selection of the gas to be flowed to the flow path C and the flow path D may be appropriately determined.
また、流路Bの先端から火移り可能な位置に、流路Aの先端が形成されている。したがって、流路Bに設けられた触媒4によって種火を形成し、それと同時にもしくはそれと前後して、流路Aに支燃性ガスを供給し、流路Aの先端に種火を火移りさせ、その後に支燃性ガスの流路Bへの供給を停止することで、触媒の劣化を防止することができる。すなわち、触媒によって種火が形成され、それを火移りさせた後に、触媒に供給する支燃性ガスの供給を停止することで、H2ガスと支燃性ガスの両方ともが触媒を通過する時間を短くすることができ、触媒での燃焼を停止することで、触媒の劣化を防止することができる。また、支燃性ガスを流路Bに流すことを停止しても、それと同じガスである支燃性ガスが流路Aから供給されるので、流路Aの先端において火炎を継続して形成することができる。 In the H 2 burner 1 of the present embodiment, a
Further, the tip end of the flow path A is formed at a position where it can be transferred from the front end of the flow path B. Therefore, the
また、触媒4によって着火して流路Bの先端に種火を形成し、それと同時にもしくはそれと前後して流路Aに支燃性ガスを流し、流路Aの先端に種火を火移りさせ、支燃性ガスを流路Bに流すのを停止している。この結果、支燃性ガスの供給を停止しているので、触媒でのH2ガスの燃焼を短くすることができ、触媒の劣化を防止することができる。また、支燃性ガスを流路Bに流すことを停止しても、流路Aに支燃性ガスを流すので、火炎Fを継続して形成することができる。 In the combustion method of the H 2 burner 1 of the present embodiment, ignition is performed by supplying H 2 gas and combustion-supporting gas to the
Further, it is ignited by the
2つの管体から構成される例としては、例えば図3に示すように、上記した外管2の内部に配置されていた内管3を、外管2の横に配置してもよい。 The H 2 burner 1 described above has a configuration in which the
As an example composed of two tube bodies, for example, as shown in FIG. 3, the
ここで、内管3の内部に内管5を設けた場合は、予めH2ガスと支燃性ガスとを混合することなく、触媒4にH2ガスと支燃性ガスを供給するので、点火の際に逆火が起きる可能性が低い。これに対し、内管5を設けず、単に内管3内にH2ガスと支燃性ガスの両方を供給する場合は、これらのガスが予め混合されるので、適宜逆火を防ぐための措置を採るのが好ましい。 In the above embodiment, the case where the
Here, when the
図4に示すように、本実施形態のH2用バーナを用いた加熱対象ガスの加熱処理装置24は、メインバーナ25と、メインバーナ25の先端に設けられたH2用バーナ1とから概略構成されている。 <Heat treatment method of target gas>
As shown in FIG. 4, the heating target
ここで、従来は、パイロットバーナ用の燃料としてH2ガスを用いることができなかったことから、パイロットバーナには、メインバーナの燃料とは異なった炭化水素系ガス等の燃料を導入する装置およびその漏洩を検知する装置が必要であった。そのため、メインバーナの点火動作に必要なコストが嵩むという不都合があった。
一方、本実施形態のH2用バーナ1を用いれば、H2ガスを燃料として用いながらも、安全に点火することができるため、H2以外の燃料の供給装置およびその漏洩を検知する装置が不要となり、メインバーナ25の点火にかかる費用を抑制することができる。 In general, when H 2 gas is used as the fuel for the main burner, the pilot burner is ignited in advance as described above in order to prevent explosion due to mixing of H 2 gas and combustion-supporting gas in the furnace. Fuel will be introduced.
Here, conventionally, since H 2 gas could not be used as the fuel for the pilot burner, a device for introducing a fuel such as a hydrocarbon-based gas different from the fuel for the main burner into the pilot burner, and A device for detecting the leakage was necessary. For this reason, there is a disadvantage that the cost required for the ignition operation of the main burner increases.
On the other hand, if the H 2 burner 1 of the present embodiment is used, it is possible to ignite safely while using H 2 gas as a fuel. Therefore, a supply device for fuel other than H 2 and a device for detecting leakage thereof are provided. It becomes unnecessary and the expense concerning ignition of the
次に、本実施形態のH2用バーナ1を用いたフレアースタックのメリットについて説明する。
図5に示すように、フレアースタック41は、燃焼させる所望のガスの貯蔵設備42と接続された放出塔43と、放出塔43の先端に設けられたH2用バーナ1とから構成されている。 <Flare stack>
Next, the merit of the flare stack using the H 2 burner 1 of the present embodiment will be described.
As shown in FIG. 5, the
そのため、電気を供給する設備が必要であり、また、フレアースタックを保安設備としても用いる際には、停電時に備えてバッテリーや非常用発電機といった予備電源を用意する必要があった。 Here, in the case of the conventional flare stack, since a normal pilot burner was used as the burner installed at the tip of the emission tower, it was necessary to ignite using electric energy such as an ignition plug.
Therefore, a facility for supplying electricity is necessary, and when using the flare stack as a safety facility, it is necessary to prepare a spare power source such as a battery or an emergency generator in preparation for a power failure.
この結果、同流量のガスをフレアースタック41で処理しようとした場合、H2用バーナ1を用いると、従来のバーナを使用する場合と比較して放出塔43の塔内径を小さくすることが可能となり、フレアースタック41自体の小型化が可能となる。 Furthermore, since the flame using H 2 gas as a fuel is less likely to blow out as compared with the case where a hydrocarbon-based gas is used as a fuel like a conventional burner, when the H 2 burner 1 is used, Even when the wind speed in the
As a result, when the gas of the same flow rate is to be processed by the
実施例1では、上記したH2用バーナ1と同様なH2用バーナを用いて、外管2にH2ガスを10L/minの流量で、内管5にH2ガスを1.5L/minの流量で供給し、内管3に供給する空気の流量を変化させた際の、着火までに要する時間を測定した。使用した触媒はPdであり、周囲および初期ガス温度は20℃とした。結果を図6に示す。なお、着火の確認は、外管2内の先端側に設置された温度計を用いて行った。 (Example 1)
In Example 1, using the same H 2 burner and
これは、H2濃度ごとにおけるスパークによる最小発火エネルギーの測定結果(図7参照)とよく合致しており、触媒上でH2の燃焼が行われていることが認められる。 As shown in FIG. 6, when the H 2 concentration on the catalyst is about 20 to 30% by volume, the time required for ignition is shortened.
This is in good agreement with the measurement result of the minimum ignition energy by spark for each H 2 concentration (see FIG. 7), and it is recognized that H 2 is burned on the catalyst.
実施例2では、実施形態で説明したH2用バーナ1と同様なH2用バーナを用い、触媒としてPd,Pt,PdOおよびPtO2のそれぞれを用いた場合について、着火性能の比較を行った。具体的には、外管2にH2ガスを10L/minの流量で、内管5にH2ガスを2L/minの流量で供給し、内管3内に供給する空気の流量を変化させながら、点火動作後30秒で到達する最高温度を計測することで、性能比較を行った。なお、最高温度の測定は、図8に示すように、内管3の先端3aの外壁に設置した温度センサー44を用いて行った。結果を図9に示す。 (Example 2)
In Example 2, using the same H 2 burner with H 2
また、PdまたはPdOを触媒として用いた場合は、空気流量の広い範囲において触媒を通過したH2と支燃性ガスとが530℃以上の温度に到達することから、H2解離触媒として非常に有用であることが分かる。 As shown in FIG. 9, in any of the catalyst, H 2 and combustion-supporting gas that has passed through the catalyst is present in the range of air air volume indicating a temperature above 530 ° C. autoignition point of H 2, H 2 gas It was found that it had the performance necessary for ignition.
Further, Pd or PdO is when used as a catalyst, since the H 2 and combustion-supporting gas that has passed through the catalyst over a wide range of air flow rate reaches a temperature above 530 ° C., as a very H 2 dissociation catalyst It turns out that it is useful.
Claims (6)
- 2つの異なるガスの流路を有するH2用バーナであって、
第1の流路は、H2ガスおよび第1の支燃性ガスが流れるように構成されており、
第2の流路は、H2ガスまたは第2の支燃性ガスが流れるように構成されており、
前記第2の流路の先端は、前記第1の流路の先端に形成される火炎が火移り可能な位置に配置されており、
前記第1の流路には、H2ガスと第1の支燃性ガスを供給することで着火可能な触媒が設けられていることを特徴とするH2用バーナ。 An H 2 burner having two different gas flow paths,
The first flow path is configured so that the H 2 gas and the first combustion-supporting gas flow,
The second flow path is configured such that H 2 gas or second combustion-supporting gas flows,
The tip of the second channel is arranged at a position where a flame formed at the tip of the first channel can be transferred,
The H 2 burner, wherein the first flow path is provided with a catalyst that can be ignited by supplying H 2 gas and a first combustion-supporting gas. - 前記触媒が、Pt、Pd、PdOまたはPtO2のいずれか一種類以上を含有することを特徴とする請求項1に記載のH2用バーナ。 The burner for H 2 according to claim 1, wherein the catalyst contains at least one of Pt, Pd, PdO, and PtO 2 .
- 前記第1の流路の先端に、火炎の形成を検知可能な検知機構が設けられていることを特徴とする請求項1または請求項2に記載のH2用バーナ。 3. The H 2 burner according to claim 1, wherein a detection mechanism capable of detecting formation of a flame is provided at a tip of the first flow path.
- 2つの異なるガスの流路を有し、第1の流路に触媒が設けられているH2用バーナの燃焼方法であって、
前記第1の流路にH2ガスおよび第1の支燃性ガスを流し、前記触媒によって着火させて第1の流路の先端に火炎を形成する工程と、
前記H2用バーナの第2の流路にH2ガスまたは第2の支燃性ガスを流す工程と、
前記第1の流路の先端に形成された火炎を前記第2の流路の先端に火移りさせる工程と、
H2ガスおよび第1の支燃性ガスのうち、前記第2の流路に流すガスと同様の種類のガスについて、前記第1の流路に流すことを停止する工程と、
を有することを特徴とするH2用バーナの燃焼方法。 A combustion method for an H 2 burner having two different gas flow paths, wherein a catalyst is provided in the first flow path,
Flowing a H 2 gas and a first combustion-supporting gas through the first flow path, and igniting with the catalyst to form a flame at the tip of the first flow path;
A step of flowing H 2 gas or a second combustion assisting gas to the second flow path of the H 2 burner,
Transferring the flame formed at the tip of the first channel to the tip of the second channel;
Of the H 2 gas and the first combustion-supporting gas, a step of stopping the flow of the same kind of gas as the gas flowing through the second flow path into the first flow path;
A combustion method of a burner for H 2 characterized by comprising: - 前記第1の流路の先端に火炎を形成した後に、前記第2の流路にH2ガスまたは第2の支燃性ガスを流すことを特徴とする請求項4に記載のH2用バーナの燃焼方法。 5. The H 2 burner according to claim 4, wherein after a flame is formed at a tip of the first flow path, H 2 gas or a second combustion-supporting gas is allowed to flow through the second flow path. Combustion method.
- 前記触媒が、Pt、Pd、PdOまたはPtO2のいずれか一種類以上を含有することを特徴とする請求項4または請求項5に記載のH2用バーナの燃焼方法。 The combustion method of the burner for H 2 according to claim 4 or 5, wherein the catalyst contains at least one of Pt, Pd, PdO, and PtO 2 .
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JP2019039590A (en) * | 2017-08-24 | 2019-03-14 | トヨタ自動車株式会社 | Nozzle for hydrogen gas combustion |
JP2019039608A (en) * | 2017-08-25 | 2019-03-14 | トヨタ自動車株式会社 | Nozzle for hydrogen gas combustion |
US11428405B2 (en) | 2020-06-29 | 2022-08-30 | AMF Den Boer B.V. | Hydrogen gas burner |
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Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6551375B2 (en) * | 2016-12-07 | 2019-07-31 | トヨタ自動車株式会社 | Hydrogen gas burner structure and hydrogen gas burner apparatus equipped with the same |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02259331A (en) * | 1989-03-30 | 1990-10-22 | Central Res Inst Of Electric Power Ind | Combustion device for catalytic combustion type gas turbine |
JPH0321651U (en) * | 1989-07-05 | 1991-03-05 | ||
JPH11509307A (en) * | 1995-06-12 | 1999-08-17 | シーメンス アクチエンゲゼルシヤフト | Burners with catalytic introduction combustion, especially for gas turbines |
JP2001065815A (en) * | 1999-08-31 | 2001-03-16 | Denso Corp | Combustion device |
JP2007163044A (en) * | 2005-12-14 | 2007-06-28 | Osamu Hirota | Injection flame burner, furnace and flame generation method |
JP2009079881A (en) * | 2007-09-27 | 2009-04-16 | Jfe Steel Kk | Pilot burner and its ignition detecting method |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3737247C1 (en) * | 1987-11-03 | 1989-03-02 | Zettner Michael L | Burner |
US5634784A (en) * | 1991-01-09 | 1997-06-03 | Precision Combustion, Inc. | Catalytic method |
DE4416650A1 (en) * | 1994-05-11 | 1995-11-16 | Abb Management Ag | Combustion process for atmospheric combustion plants |
DE4426351B4 (en) * | 1994-07-25 | 2006-04-06 | Alstom | Combustion chamber for a gas turbine |
US5950434A (en) * | 1995-06-12 | 1999-09-14 | Siemens Aktiengesellschaft | Burner, particularly for a gas turbine, with catalytically induced combustion |
JP3619626B2 (en) * | 1996-11-29 | 2005-02-09 | 株式会社東芝 | Operation method of gas turbine combustor |
US7121097B2 (en) * | 2001-01-16 | 2006-10-17 | Catalytica Energy Systems, Inc. | Control strategy for flexible catalytic combustion system |
JP2004163030A (en) * | 2002-11-14 | 2004-06-10 | Calsonic Kansei Corp | Hydrogen combustor |
JP4299868B2 (en) * | 2006-07-28 | 2009-07-22 | クロリンエンジニアズ株式会社 | Hydrogen combustion equipment |
-
2012
- 2012-08-09 WO PCT/JP2012/070334 patent/WO2013024783A1/en active Application Filing
- 2012-08-09 CN CN201280035371.2A patent/CN103732991B/en active Active
- 2012-08-09 JP JP2013528993A patent/JP5732135B2/en active Active
- 2012-08-09 KR KR1020147001810A patent/KR101974819B1/en active IP Right Grant
- 2012-08-14 TW TW101129319A patent/TWI550234B/en active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH02259331A (en) * | 1989-03-30 | 1990-10-22 | Central Res Inst Of Electric Power Ind | Combustion device for catalytic combustion type gas turbine |
JPH0321651U (en) * | 1989-07-05 | 1991-03-05 | ||
JPH11509307A (en) * | 1995-06-12 | 1999-08-17 | シーメンス アクチエンゲゼルシヤフト | Burners with catalytic introduction combustion, especially for gas turbines |
JP2001065815A (en) * | 1999-08-31 | 2001-03-16 | Denso Corp | Combustion device |
JP2007163044A (en) * | 2005-12-14 | 2007-06-28 | Osamu Hirota | Injection flame burner, furnace and flame generation method |
JP2009079881A (en) * | 2007-09-27 | 2009-04-16 | Jfe Steel Kk | Pilot burner and its ignition detecting method |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2019039590A (en) * | 2017-08-24 | 2019-03-14 | トヨタ自動車株式会社 | Nozzle for hydrogen gas combustion |
JP2019039608A (en) * | 2017-08-25 | 2019-03-14 | トヨタ自動車株式会社 | Nozzle for hydrogen gas combustion |
CN109424958A (en) * | 2017-09-05 | 2019-03-05 | 丰田自动车株式会社 | Nozzle arrangements for hydrogen gas combustor device |
EP3450843A1 (en) * | 2017-09-05 | 2019-03-06 | Toyota Jidosha Kabushiki Kaisha | Nozzle structure for hydrogen gas burner apparatus |
JP2019045092A (en) * | 2017-09-05 | 2019-03-22 | トヨタ自動車株式会社 | Nozzle structure for hydrogen gas burner device |
CN111810950A (en) * | 2017-09-05 | 2020-10-23 | 丰田自动车株式会社 | Nozzle structure for hydrogen burner device |
US11098893B2 (en) | 2017-09-05 | 2021-08-24 | Toyota Jidosha Kabushiki Kaisha | Nozzle structure for hydrogen gas burner apparatus |
US11428405B2 (en) | 2020-06-29 | 2022-08-30 | AMF Den Boer B.V. | Hydrogen gas burner |
Also Published As
Publication number | Publication date |
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CN103732991B (en) | 2016-03-02 |
JP5732135B2 (en) | 2015-06-10 |
TW201319469A (en) | 2013-05-16 |
CN103732991A (en) | 2014-04-16 |
KR101974819B1 (en) | 2019-08-23 |
JPWO2013024783A1 (en) | 2015-03-05 |
KR20140051907A (en) | 2014-05-02 |
TWI550234B (en) | 2016-09-21 |
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