WO2007138962A1 - Combustor - Google Patents
Combustor Download PDFInfo
- Publication number
- WO2007138962A1 WO2007138962A1 PCT/JP2007/060565 JP2007060565W WO2007138962A1 WO 2007138962 A1 WO2007138962 A1 WO 2007138962A1 JP 2007060565 W JP2007060565 W JP 2007060565W WO 2007138962 A1 WO2007138962 A1 WO 2007138962A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- combustion
- ceramic
- fuel
- combustor
- air
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 125
- 239000000446 fuel Substances 0.000 claims abstract description 67
- 239000000919 ceramic Substances 0.000 claims abstract description 63
- 239000003054 catalyst Substances 0.000 claims abstract description 26
- 239000000203 mixture Substances 0.000 claims abstract description 23
- 238000007254 oxidation reaction Methods 0.000 claims abstract description 13
- 230000003647 oxidation Effects 0.000 claims abstract description 12
- 239000000567 combustion gas Substances 0.000 claims description 29
- 241000234435 Lilium Species 0.000 claims description 8
- 230000002093 peripheral effect Effects 0.000 claims description 7
- 239000003973 paint Substances 0.000 claims description 5
- 230000005855 radiation Effects 0.000 claims description 4
- 230000001737 promoting effect Effects 0.000 claims description 3
- 239000012212 insulator Substances 0.000 abstract description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 17
- 239000007789 gas Substances 0.000 description 9
- 239000007788 liquid Substances 0.000 description 8
- 238000010438 heat treatment Methods 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 5
- 230000004913 activation Effects 0.000 description 4
- 239000002245 particle Substances 0.000 description 4
- 238000001704 evaporation Methods 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 238000007084 catalytic combustion reaction Methods 0.000 description 2
- 230000003197 catalytic effect Effects 0.000 description 2
- 239000003344 environmental pollutant Substances 0.000 description 2
- 230000008020 evaporation Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 238000012856 packing Methods 0.000 description 2
- 231100000719 pollutant Toxicity 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 229910021193 La 2 O 3 Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 241001122767 Theaceae Species 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010892 electric spark Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 229910044991 metal oxide Inorganic materials 0.000 description 1
- 150000004706 metal oxides Chemical class 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 239000011225 non-oxide ceramic Substances 0.000 description 1
- 229910052575 non-oxide ceramic Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000002407 reforming Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- 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
- F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
-
- 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
-
- 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
-
- 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
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
- F23C3/002—Combustion apparatus characterised by the shape of the combustion chamber the chamber having an elongated tubular form, e.g. for a radiant tube
Definitions
- the present invention relates to a combustor for obtaining high-temperature gas, for example, for a fuel reformer of a small fuel cell system for home use.
- combustion gas generated from this type of combustor should be free of pollutants, that is, NOx and unburned matter, and have a low residual oxygen content due to complete combustion.
- Air and fuel are mixed at a concentration within the explosion limit range, and this mixed gas is ignited by an ignition means such as an electric spark to form a flame.
- an ignition means such as an electric spark to form a flame.
- a combustor that continuously burns the above-mentioned mixed gas of air and fuel.
- a preheated mixed gas obtained by mixing fuel in preheated air is burned by a combustion catalyst.
- the outside of the heating tube of the main combustor is always heated above the ignition temperature of the fuel by the auxiliary combustor.
- a mixed gas of fuel and air is brought into contact with the heated heating tube. 1: Combustor designed to continue combustion.
- a U-turn is made at the end of the tube to burn the combustion gas that is burned by bringing the mixed gas of fuel and air into contact with the tube heated above the ignition temperature of the fuel.
- the combustor is designed to continue combustion by heating the pipe. (Japanese Patent Laid-Open No. 10-2 6 3 0 9) and the like are known.
- the combustor used in this type of device is required to be small and have a small combustion chamber volume, and the temperature of the surrounding wall surface is about 110 to 180 ° C. Because it is necessary to have a low temperature, complete combustion with a low NOX concentration is required, even though the conditions are very disadvantageous to combustion.
- the small volume of the combustion chamber means that it is susceptible to pressure fluctuations.
- the fuel flow temporarily stops due to pressure fluctuations, the flame disappears, and combustion stops.
- steam generation may cease.
- gaseous fuel and liquid fuel is required in the above-mentioned small-sized home fuel cell system.
- an auxiliary igniter must be used, but after the start of operation, this auxiliary combustor is made unnecessary in as short a time as possible, and combustion stops even if there is a disturbance such as pressure fluctuation. It is necessary to adopt no method.
- the present invention has been made in view of the above, and it is possible to obtain a compact combustion gas that is free from the generation of NOX as a pollutant and does not remain unburned, and that is stable even with a slight disturbance.
- the purpose is to provide a combustor that can To do.
- the first invention is a combustor in which a ceramic combustion cylinder having an oxidation catalyst function is disposed downstream of a bench-lily single-tube fuel / air mixer equipped with an igniter.
- the second invention is a combustor according to the first invention, wherein a vortex generator is provided at the tip of a bench-lily single-tube type fuel 'air mixer so that the mixture becomes a vortex in the ceramic combustion cylinder. is there.
- the downstream end portion of the ceramic combustion cylinder is covered with a cylindrical cover whose head is closed, and a combustion chamber is further provided around the tip of the ceramic combustion cylinder. It is a combustor formed and provided with a combustion gas outflow hole at the cylindrical base end of the cover.
- a fourth invention is the combustor according to the third invention, wherein a radiation promoting paint is applied to the outer peripheral surface of the cover.
- a fifth invention is the combustor according to the third or fourth invention, wherein an oxidation catalyst layer is provided between the ceramic combustion cylinder and the base end portion of the cover.
- the first invention for example, it has a small combustion chamber suitable as a combustor for a boiler used in a fuel reformer of a small-sized domestic fuel cell system that is currently being developed. Combustion efficiency is good and stable combustion is possible A simple combustor can be obtained.
- the air-fuel mixture sufficiently corrodes the oxidation catalyst, a combustor capable of more stable combustion can be obtained.
- combustion of the combustion gas flowing out from the ceramic combustion cylinder is further promoted in the combustion chamber constituted by the cover.
- the radiant heat can be radiated from the outer surface of the cover to the heated part, the heating of the heated part can be promoted.
- the combustion gas flowing out from the combustion chamber in the cover through the through hole passes through the catalyst layer having an oxidation function, it is assumed that the combustion gas burned in the ceramic combustion cylinder is unburned in the combustion gas. Even if a minute remains, the unburned component can be completely burned while passing through the catalyst layer.
- FIG. 1 is a cross-sectional view showing a main part of a first embodiment of a combustor according to the present invention.
- FIG. 2 is a cross-sectional view showing an embodiment of a boiler in which the combustor of the first embodiment of FIG. 1 is used.
- FIG. 3 is a cross-sectional view showing a second embodiment of a combustor according to the present invention and another embodiment of a boiler provided with the same.
- FIG. 1 is a cross-sectional view showing the main part of the combustor of the present invention
- FIG. 2 is a cross-sectional view showing an example of a boiler using the combustor of the present invention.
- 1 is a boiler body composed of an inner cylinder 2 and an outer cylinder 3 arranged concentrically
- 4 is a combustor according to the present invention provided at the lower end of the boiler body 1.
- the high temperature combustion gas generated in the combustor 4 is supplied to the inner surface of the inner cylinder 2 of the boiler body 1 so that the inner surface of the inner cylinder 2 is heated, and the inner cylinder 2 arranged concentrically with the outer cylinder 2
- the water (evaporation medium) supplied in the heat medium jacket 5 formed between the cylinders 3 is heated to generate high-temperature steam.
- a boiler lower flange 6 that closes the heating medium jacket 5 for the evaporation medium is coupled to the lower end of the boiler body 1.
- the combustor 4 is located at the lower end of the boiler body 1 and the cover 10 located at the top of the combustor 4 is located in the inner cylinder 2 of the boiler body 1. It is designed to be joined in the state of rushing into.
- the combustor 4 includes a combustion unit 11 including a ceramic combustion cylinder 14 from which the combustion gas is ejected, and a fuel supply unit 1 2 for supplying a fuel Z air mixture obtained by mixing fuel and air to the combustion unit 11. It is made up of.
- Combustion section 11 is located at the uppermost position and has a combustion chamber forming cover 10 that forms combustion chamber 13 inside, and is disposed at the axial center of the cover, and the upper end is opened into combustion chamber 13.
- the released ceramic combustion cylinder 14 and the outside of the bottom of this ceramic combustion cylinder It is composed of heat insulators 15 5 a, 15 b, 15 c, and a frame 16 surrounding these heat insulators. Is fixed to the combustor flange 7.
- the cover 10 has a bell shape (or a tea tube cap shape), and is provided in a state of covering the heat insulators 15 a, 15 b, and 15 c.
- a slit-like through hole (combustion gas outflow hole) 17 that is long in the vertical direction is provided at the end.
- a catalyst layer 18 made of ceramic small particles having an oxidation function is provided at the height of the through hole 17.
- the upper end of the ceramic combustion cylinder 14 has a predetermined distance L between the upper surface of the catalyst layer 18 and the upper surface of the catalyst layer 18 in the combustion chamber 13 ⁇ with a predetermined distance L from the ceiling inner surface of the cover 10.
- Combustion gas that has H and flows out from the upper end of the ceramic combustion cylinder 14 flows from the combustion chamber 1 3 through the catalyst layer 1 8 through the through hole 1 7 into the inner cylinder 2 of the boiler body 1. It ’s like that.
- the fuel supply unit 12 is fixed to the lower surface of the combustion unit 11 via a packing via a mounting flange 21 provided at the upper end portion thereof via a packing.
- a Venturi tube type mixer 23 is fixed to the mounting flange 21 so as to penetrate therethrough.
- the outlet portion of the bench lily single-tube mixer 2 3 is concentric with the ceramic combustion cylinder 14 of the combustion section 11 1 and its outlet diameter is substantially the same as the inner diameter of the ceramic combustion cylinder 14. The outlet end of this is in contact with the lower end of the ceramic combustion cylinder 14.
- a vortex generator 24 is provided at the contact portion. This eddy current generator 24 directs the mixed air flow from the bench lily single tube mixer 2 3 in the circumferential direction, that is, ceramic fuel. It has a shape that generates a vortex along the inner peripheral surface of the firing tube 14
- a plurality of fuel injection holes 25 are provided on the circumferential surface of the throat portion of the bench lily single tube mixer 23.
- the fuel injection hole 25 is connected to the fuel supply port 26 via a fuel handle 25 a provided in the throat portion of the bench lily single pipe mixer 23.
- An igniter ignition rod conduit 27 is provided at the axial center of the venturi-type mixer 23.
- the ignition rod conduit 27 has an upper end fixed to the center of the vortex generator 24 and a lower end projecting downward from the venturi-type mixer 23.
- An ignition rod 28 is inserted into the ignition rod conduit 27 so that its tip protrudes from the ignition rod conduit 27.
- a cross-shaped pipe fitting 29 is connected to the base end of the Venturi tube mixer 23, and the lower end of the ignition rod conduit 27 is positioned within the pipe fitting 29. Yes.
- one of the two connection ports in the direction orthogonal to the extension line of the connection port of the pipe joint 29 to the bench lily one-pipe mixer 23 is an igniter power rod connection port, A power rod 30 for the igniter is inserted from the end, and the tip thereof is electrically connected to the ignition rod 28 in the connection pipe 29.
- a combustion air supply port 3 1 is connected to the other of the two connection ports.
- a combustion state monitoring port 3 2 that allows the inside of the venturi single-pipe mixer 2 3 to be seen through is connected to the connection port on the extension line of the connection port of the pipe joint 28 with the bench lily single-pipe mixer 2 3. Yes.
- Combustion air is supplied from the air supply port 3 1 of the fuel supply unit 1 2, and the fuel supplied from the fuel supply port 2 6 is supplied to the throat portion of the venturi single-tube mixer 2 3 from the fuel injection port 2 5.
- this air and fuel are mixed from this slot to the outlet of the venturi single-pipe mixer 23 to form a fuel / air mixture (hereinafter referred to as a mixture).
- a mixture fuel / air mixture
- the air-fuel mixture flowing into the ceramic combustion cylinder 14 becomes a vortex along the inner peripheral surface of the ceramic combustion cylinder 14 by the vortex generator 24.
- the igniter power rod 30 is energized to form a spark at the tip of the ignition rod 28 to ignite the mixture.
- the air-fuel mixture starts to burn. After ignition, it is influenced by the mixture ratio of fuel and air in the mixture, but even if the spark is stopped within 2 minutes, the ceramic combustion cylinder 14 is heated above the temperature at which it functions as an oxidation catalyst. If so, the combustion will continue.
- liquid fuel such as kerosene
- the fuel itself is supplied at room temperature, but the combustion air is supplied preheated to about 2 ° 0 to 25 ° C.
- gaseous fuel can also be used.
- the ignited air-fuel mixture starts to combust, and the combustion gas flows upward along the inner peripheral wall of the ceramic combustion cylinder 14.
- the ceramic combustion cylinder 14 itself is heated to a temperature higher than the catalyst activation temperature. This result
- the mixture from the bench-lily single-tube mixer 23 was raised to the catalyst activation temperature or higher.
- Such combustion becomes intense as it goes upward (downstream) of the ceramic combustion cylinder 14, and most of the air-fuel mixture is combusted at the upper end of the ceramic combustion cylinder 14.
- the combustion state at this time is affected by the length of the ceramic combustion cylinder 14.
- the length of the ceramic combustion cylinder 14 is designed such that most of the air-fuel mixture supplied from the fuel supply section 12 is combusted.
- the material of the ceramic combustion cylinder 14 has the following properties.
- the necessary conditions for the above-mentioned ceramic combustion cylinder 14 having an oxidation function are: (1) strong thermal shock resistance, (2) low catalyst activation temperature, (3) high emissivity, (4) High mechanical strength at high temperature, (5) High heat conductivity.
- the ceramics having such properties S i C, S i 3 N 4, Z r 0 2 and Z r O. To which 5 to 20% of other metal oxides are added Is suitable.
- S i C, S i 3 N 4 S i non-oxide ceramics have a catalytic activity temperature of 640 to 6 45 ° C, but other than this, the above conditions are satisfied. It is.
- Zr 0 2 alone has a catalyst activation temperature of 4 65 ° C, but C o O, C r 2 0 3 , Mn0 2 , La 2 O 3 , S n0 2 , ⁇ 2 O 3 , T b O 2 ⁇ Pi M g O a mixture from 5% to 20% is capable of decreasing the catalytic activity temperature from 3 3 0 to 4 9 7 ° about C (9th Symposium on catalytic combustion (See “Catalytic Combustion with Zr 0 2 Composite Oxide” published on May 25, 1990).
- the thermal shock resistance (1) described above is required to be strong is that the amount of heat received from the inside of the ceramic combustion cylinder 14 is large because the combustion speed is high. That is, if the change in the amount of heat received by the ceramic combustion cylinder 14 is large, the temperature change of the ceramic combustion cylinder 14 itself is large, and if the thickness of the ceramic combustion cylinder 14 is increased, the temperature difference inside the ceramic combustion cylinder 14 is large. This is because the ceramic combustion cylinder 14 is destroyed by thermal shock. In order to prevent this, the thermal conductivity of (5) is required to be high. In addition, the high thermal conductivity is suitable for transferring the heat received on the downstream side of the combustion gas to the upstream side, and the high emissivity of (3) exhibits the same effect.
- Combustion gas generated in the ceramic combustion cylinder 14 flows into the combustion chamber 13 from the tip of the ceramic combustion cylinder 14 and moves downward along the inner surface of the cover 10 constituting this combustion chamber 13. Change the boiler through catalyst hole 1 8 through hole 1 7 It flows out into the inner cylinder 2 of the main body 1.
- the combustion gas burned at this time may have insufficient combustion if the volume of the passage through which it passes is small and is surrounded by a cold wall, leaving unburned gas in the combustion gas.
- the combustion gas from the ceramic combustion cylinder 14 flows into the combustion chamber 13, which is a relatively large space formed by the cover 10, and thus burns. Is sufficiently continued to reach a high temperature (1500 to 1700 ° C), and the unburned part of the combustion gas is almost completely combusted.
- the combustion gas in the combustion chamber 13 changes its flow downward along the inner surface of the cover 10 constituting the combustion chamber 13, passes through the catalyst layer 18, and then passes through the hole 1. 7 flows into the inner cylinder 2 of the boiler body 1 and heats the inner surface of the inner cylinder 2. At this time, the combustion gas comes into contact with the small ceramic particles of the catalyst layer 18 so that the unburned components in the combustion gas are completely burned. The presence of the catalyst layer 18 prevents combustion from stopping due to pressure fluctuations in the fuel and combustion air.
- the ceramic small particles having an oxidation function constituting the catalyst layer 18 are preferably SiC hollow particles.
- the inner diameter of the ceramic combustion cylinder 14 is 20 mm.
- the thickness is 2.5 mm
- the length is 40 mm
- the inner diameter of the cover 10 is 5 O mm
- the dimension of H shown in FIG. Is 10 mm and the dimension of L is 15 mm.
- the combustor shown in FIG. 1 is an example applied to a boiler body 1 for a steam generator of a household fuel cell system, and the heat medium jacket 5 of the boiler body 1 is filled.
- the generated water is boiled and the generated steam is led out from the steam pipe connected to the top of the heat medium jacket 5.
- the cover 10 in order to use the cover 10 for a long period of time, it is necessary to transfer the heat received from the high-temperature gas to the heat medium jacket 5 as much as possible.
- the cover made of steel is used.
- a radiation-promoting paint such as a radiation paint with an emissivity of 92% or more
- Applying a radiation-promoting paint, such as a radiation paint with an emissivity of 92% or more, to the outer peripheral surface of 10 generates combustion gas with a theoretical combustion temperature of 1600 ° C in the combustion section 1 1 Even so, the temperature of the wall of the cover 10 can be 9500 ° C or less, so that the cover 10 can withstand long-term use by applying this radiation promoting paint. It becomes.
- FIG. 2 shows an embodiment of a boiler using the combustor 4 according to the present invention.
- a large number of water pipes 3 3, 3 3 are disposed in the inner cylinder 2 of the boiler body 1 and above the combustion section 11. It has a configuration in which a heat exchanging part 3 4 comprising:
- An exhaust pipe 40 is connected to the inside of the inner cylinder 2.
- a water receiving tank 3 5 is provided above the heat exchanging section 3 4, and a water supply pipe 3 6 is connected to the water receiving tank 3 5.
- the inlet 3 3 a of each water pipe 3 3 of the heat exchange section 3 4 is connected to the water receiving tank 3 5, and the outlet is connected to the outlet chamber 3 7.
- the outlet chamber 37 is a space formed between the upper part of the support plate 39 supporting the heat exchanging part 34 and the bottom of the water receiving tank 35, and the air is discharged from the heat medium jacket 5 of the boiler body 1. What has evaporated in the liquid-mixed state and what has evaporated in the gas-liquid mixed state from the outlet of the heat exchange section 34 The gas and liquid are separated in the outlet chamber 37.
- the separated liquid medium (hot water) absorbs heat for circulating and evaporating.
- the vapor of the gas-liquid mixture from which most of the liquid has been separated rises in the space between the inner tube 2 of the boiler body 1 and the outer cylinder part of the water receiving tank 35, and in the upper part of the water receiving tank 35. Gas-liquid separation is performed, and the separated steam is taken out from the steam outlet pipe 41, and the separated hot water is collected in the water receiving tank 35.
- the heat of the combustion gas flowing into the inner cylinder 2 of the boiler body 1 from the combustion section 1 1 of the combustor 4 directly acts on the heat medium jacket 5 from the inner surface of the inner cylinder 2 and heat
- the heat exchanged in the exchanging part 34 can also preheat the water supplied to the heat medium jacket 5 and can effectively use the heat of the combustion gas generated in the combusting part 11.
- the fuel supply section 1 2 is supplied from the venturi one-pipe mixer 2 3 alone.
- the cover 10 for constituting the combustion chamber 13 can be omitted (the cover 10 is omitted). Examples will be described later).
- the cover 10 is disposed on the outlet side of the ceramic combustion cylinder 14.
- the ceramic combustion cylinder 14 If the air-fuel mixture supplied from the venturi-type mixer 2 3 of the fuel supply unit 1 2 can be combusted to a state where there is almost no unburned fuel by appropriately adjusting the length, The cover 10 for constituting the combustion chamber 13 can be omitted.
- FIG. 3 This is shown in FIG. 3 as a second embodiment.
- the outlet side of the ceramic combustion cylinder 14 is provided with a large number of guide passages 19 for deriving the combustion gas from the ceramic combustion cylinder 14 radially outward. It is closed with 15 d of insulation.
- the combustion gas led out of the heat insulator 15 d in the outer circumferential direction is discharged in the upper part of FIG. 3, and a number of vertical descending water pipes 4 are placed in the space between the inner cylinder 2 and the outer cylinder 3.
- the inner cylinder 2 of the boiler main body 1 in which 2 is arranged at intervals in the circumferential direction and the outer walls of a large number of water pipes 33 arranged in the central region of the boiler main body 1 are heated.
- the combustion section 11 cannot be expected to reach a temperature at which the ceramic combustion cylinder 14 functions as an oxidation catalyst.
- the ceramic combustion cylinder 14 is omitted, and instead, in the omitted part, the heat insulator 15 a forms a combustion path having the same diameter as the inner diameter of the ceramic combustion cylinder 14.
- Such a structure is advantageous in terms of cost because it can save the material cost of the ceramic combustion cylinder.
- This structure can also be used for heating a reformer or for starting a fuel cell using a solid oxide.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Spray-Type Burners (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA002649212A CA2649212A1 (en) | 2006-05-30 | 2007-05-17 | Combustor |
US12/302,775 US20090239181A1 (en) | 2006-05-30 | 2007-05-17 | Combustor |
EP07743999A EP2023040A1 (en) | 2006-05-30 | 2007-05-17 | Combustor |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006150258A JP2007322019A (en) | 2006-05-30 | 2006-05-30 | Combustor |
JP2006-150258 | 2006-05-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2007138962A1 true WO2007138962A1 (en) | 2007-12-06 |
Family
ID=38778482
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2007/060565 WO2007138962A1 (en) | 2006-05-30 | 2007-05-17 | Combustor |
Country Status (7)
Country | Link |
---|---|
US (1) | US20090239181A1 (en) |
EP (1) | EP2023040A1 (en) |
JP (1) | JP2007322019A (en) |
KR (1) | KR20090025272A (en) |
CN (1) | CN101443593A (en) |
CA (1) | CA2649212A1 (en) |
WO (1) | WO2007138962A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IT1397333B1 (en) * | 2009-06-26 | 2013-01-10 | Ergo Design S R L | BURNER |
SE537092C2 (en) | 2011-09-08 | 2015-01-07 | Reformtech Heating Holding Ab | Burner |
US9190676B2 (en) * | 2012-09-28 | 2015-11-17 | Fuelcell Energy, Inc. | Flame stabilized mixer-eductor-oxidizer for high temperature fuel cells |
AT520881B1 (en) * | 2018-01-17 | 2020-04-15 | Avl List Gmbh | Method for operating a fuel cell system |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
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JPS6060411A (en) * | 1983-09-12 | 1985-04-08 | Matsushita Electric Ind Co Ltd | Catalytic combustion apparatus |
JPS6117814A (en) * | 1984-07-02 | 1986-01-25 | Matsushita Electric Ind Co Ltd | Catalytic burner |
JPS6426309A (en) | 1987-07-21 | 1989-01-27 | Matsushita Electric Works Ltd | Box assembly having stepped rim |
JPH01200105A (en) * | 1988-02-05 | 1989-08-11 | Nippon Chem Plant Consultant:Kk | Far infrared ray radiation device |
JPH04278108A (en) * | 1991-03-04 | 1992-10-02 | Toho Gas Co Ltd | Injection tube burner using swirl flow combustion |
JPH0733402A (en) * | 1993-07-27 | 1995-02-03 | Hitachi Ltd | Reformer |
JPH08226611A (en) * | 1995-02-23 | 1996-09-03 | Nippon Chem Plant Consultant:Kk | Burning method of fuel |
JP2001342002A (en) * | 2000-05-30 | 2001-12-11 | Kansai Electric Power Co Inc:The | Fuel reformer |
JP2005024181A (en) * | 2003-07-02 | 2005-01-27 | Yamaichi Kinzoku Kk | Burner |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3666625D1 (en) * | 1985-02-21 | 1989-11-30 | Tauranca Ltd | Fluid fuel fired burner |
US4692306A (en) * | 1986-03-24 | 1987-09-08 | Kinetics Technology International Corporation | Catalytic reaction apparatus |
DE69627313T2 (en) * | 1995-12-14 | 2004-02-12 | Matsushita Electric Industrial Co., Ltd., Kadoma | CATALYTIC COMBUSTION DEVICE |
EP1269074B1 (en) * | 2000-03-24 | 2005-08-10 | Webasto Thermosysteme International GmbH | Binary burner with venturi tube fuel atomisation and venturi jets for the atomisation of liquid fuel |
US6325060B1 (en) * | 2000-07-25 | 2001-12-04 | Toyotomi Co. Ltd. | Stack-equipped far infrared space heater |
-
2006
- 2006-05-30 JP JP2006150258A patent/JP2007322019A/en not_active Ceased
-
2007
- 2007-05-17 CN CNA2007800173808A patent/CN101443593A/en active Pending
- 2007-05-17 WO PCT/JP2007/060565 patent/WO2007138962A1/en active Application Filing
- 2007-05-17 KR KR1020087031512A patent/KR20090025272A/en not_active Application Discontinuation
- 2007-05-17 CA CA002649212A patent/CA2649212A1/en not_active Abandoned
- 2007-05-17 US US12/302,775 patent/US20090239181A1/en not_active Abandoned
- 2007-05-17 EP EP07743999A patent/EP2023040A1/en not_active Withdrawn
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JPS6060411A (en) * | 1983-09-12 | 1985-04-08 | Matsushita Electric Ind Co Ltd | Catalytic combustion apparatus |
JPS6117814A (en) * | 1984-07-02 | 1986-01-25 | Matsushita Electric Ind Co Ltd | Catalytic burner |
JPS6426309A (en) | 1987-07-21 | 1989-01-27 | Matsushita Electric Works Ltd | Box assembly having stepped rim |
JPH01200105A (en) * | 1988-02-05 | 1989-08-11 | Nippon Chem Plant Consultant:Kk | Far infrared ray radiation device |
JPH04278108A (en) * | 1991-03-04 | 1992-10-02 | Toho Gas Co Ltd | Injection tube burner using swirl flow combustion |
JPH0733402A (en) * | 1993-07-27 | 1995-02-03 | Hitachi Ltd | Reformer |
JPH08226611A (en) * | 1995-02-23 | 1996-09-03 | Nippon Chem Plant Consultant:Kk | Burning method of fuel |
JP2001342002A (en) * | 2000-05-30 | 2001-12-11 | Kansai Electric Power Co Inc:The | Fuel reformer |
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"Catalytic Combustion by Zr02 compound oxide", 9TH SYMPOSIUM ON CATALYTIC COMBUSTION, 25 May 1990 (1990-05-25) |
Also Published As
Publication number | Publication date |
---|---|
CA2649212A1 (en) | 2007-12-06 |
KR20090025272A (en) | 2009-03-10 |
CN101443593A (en) | 2009-05-27 |
JP2007322019A (en) | 2007-12-13 |
US20090239181A1 (en) | 2009-09-24 |
EP2023040A1 (en) | 2009-02-11 |
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