US20030235523A1 - Method for methane oxidation and, apparatus for use therewith - Google Patents
Method for methane oxidation and, apparatus for use therewith Download PDFInfo
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- US20030235523A1 US20030235523A1 US10/178,130 US17813002A US2003235523A1 US 20030235523 A1 US20030235523 A1 US 20030235523A1 US 17813002 A US17813002 A US 17813002A US 2003235523 A1 US2003235523 A1 US 2003235523A1
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- catalytic burner
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- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 title claims abstract description 95
- 238000000034 method Methods 0.000 title claims abstract description 29
- 238000007254 oxidation reaction Methods 0.000 title abstract description 29
- 230000003647 oxidation Effects 0.000 title abstract description 24
- 239000000446 fuel Substances 0.000 claims abstract description 65
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract description 37
- 239000001301 oxygen Substances 0.000 claims abstract description 37
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 37
- 230000001590 oxidative effect Effects 0.000 claims abstract description 33
- 239000007800 oxidant agent Substances 0.000 claims abstract description 31
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910002091 carbon monoxide Inorganic materials 0.000 claims abstract description 16
- 238000002485 combustion reaction Methods 0.000 claims abstract description 13
- 239000001257 hydrogen Substances 0.000 claims abstract description 7
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 7
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 6
- 239000003054 catalyst Substances 0.000 claims description 27
- 230000003197 catalytic effect Effects 0.000 claims description 24
- 239000000470 constituent Substances 0.000 claims description 22
- 239000012530 fluid Substances 0.000 claims description 20
- 238000006243 chemical reaction Methods 0.000 claims description 16
- 238000002407 reforming Methods 0.000 claims 5
- 238000006555 catalytic reaction Methods 0.000 claims 1
- 230000005855 radiation Effects 0.000 abstract description 6
- 238000009792 diffusion process Methods 0.000 description 10
- 239000011148 porous material Substances 0.000 description 10
- 239000000203 mixture Substances 0.000 description 9
- 239000007789 gas Substances 0.000 description 8
- 230000007246 mechanism Effects 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 6
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 5
- 239000000376 reactant Substances 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000003345 natural gas Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- 238000007084 catalytic combustion reaction Methods 0.000 description 2
- 230000001276 controlling effect Effects 0.000 description 2
- 239000006185 dispersion Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000003344 environmental pollutant Substances 0.000 description 2
- 229930195733 hydrocarbon Natural products 0.000 description 2
- 150000002430 hydrocarbons Chemical class 0.000 description 2
- 229910052697 platinum Inorganic materials 0.000 description 2
- 231100000719 pollutant Toxicity 0.000 description 2
- NLOAOXIUYAGBGO-UHFFFAOYSA-N C.[O] Chemical compound C.[O] NLOAOXIUYAGBGO-UHFFFAOYSA-N 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- GQPLMRYTRLFLPF-UHFFFAOYSA-N Nitrous Oxide Chemical class [O-][N+]#N GQPLMRYTRLFLPF-UHFFFAOYSA-N 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000010411 cooking Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- XLYOFNOQVPJJNP-ZSJDYOACSA-N heavy water Substances [2H]O[2H] XLYOFNOQVPJJNP-ZSJDYOACSA-N 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Images
Classifications
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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
-
- 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
- F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
- F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
- F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
-
- 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
- F23C2900/03002—Combustion apparatus adapted for incorporating a fuel reforming device
-
- 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
- F23C2900/06041—Staged supply of oxidant
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery
Abstract
The invention is a method and apparatus for use therewith for the combustion of methane. The method employs reformation of methane and oxygen in fuel-rich proportions into carbon monoxide and hydrogen and residual methane. The carbon monoxide, hydrogen and residual methane is then combined with oxidant in fuel lean proportions to continue oxidation in a porous media that absorbs some of the heat of oxidation and radiates the heat as infrared radiation.
Description
- The present invention is generally directed to catalytic combustion, and more specifically to a method and an apparatus for use therewith for the reformation of methane into partial oxidation products and the oxidation of those products at a temperature below the adiabatic temperature thereof.
- Methane is an abundant hydrocarbon that is used as a source of fuel in numerous applications, such as industrial radiant heaters, gas turbines, home furnaces and cooking equipment. While methane can be made available in a relatively pure form, it is more commonly provided as a constituent of natural gas, of which it is the primary component.
- Natural gas is typically combusted in an open flame, a process referred to as diffusion burning, which generates certain pollutants. One particularly undesirable class of pollutants formed during diffusion burning is nitrous oxides, i.e. NOx. In diffusion burning, NOx can be formed by any one of three possible mechanisms: thermal, prompt, and fuel bound. The production of NOx by the thermal and the prompt mechanisms, however, far exceeds that produced from the fuel bound mechanism. Consequently, efforts to reduce NOx pollution focus on reducing NOx formation by the thermal and/or the prompt mechanisms.
- NOx produced by the thermal mechanism, i.e. thermal NOx, is often the dominant mechanism. Thermal NOx is formed when the heat being released by diffusion burning is sufficient to provide the necessary energy for the nitrogen in the air to combine with the oxygen in the air. Generally, at flame temperatures below 1700 K, the production of thermal NOx is insignificant. However, as flame temperatures increase, the production of thermal NOx increases sharply.
- Thermal NOx production can be controlled by regulating reactant stoichiometry. To burn a fuel it must be mixed with an oxidant. For example, to burn methane oxygen must be provided. The ratio of the fuel and oxidant, that is methane and oxygen, is the reactant's stoichiometry. Reactant stoichiometry is expressed in terms of a fuel/oxidant equivalence ratio, or where the oxidant is oxygen as a constituent of air—fuel/air ratio. The fuel/oxidant equivalence ratio is the ratio of the actual fuel/oxidant ratio to the stoichiometric fuel/oxidant ratio. For example in the case of methane (CH4), the combustion reaction is CH4+2O2→CO2+2H2O. Therefore, a stoichiometric fuel/oxidant ratio is one part CH4 and two parts O2. Thus, if a mixture had this ratio of CH4 and O2, the reactant stoichiometry as expressed by the fuel/oxidant ratio of the mixture would be 1.0 (an actual mixture having these proportions would be referred to as stoichiometric).
- A mixture having an equivalence ratio greater than 1.0 is fuel rich, i.e., in the case of the above methane reaction more than one part fuel for each two parts of oxygen, and a mixture having an equivalence ratio less than 1.0 is fuel lean, i.e. in the case of the above methane reaction less than one part fuel for each two parts of oxygen. When combustion is adiabatic, stoichiometric mixtures burn relatively hotter than non-stoichiometric mixtures and the further away the mixture is from stoichiometric the relatively cooler it burns.
- NOx production by the prompt mechanism, i.e. prompt NOx, is a fuel-rich, gas-phase phenomenon. The reaction is quick and completes within the diffusion flame. The production of NOx by the prompt mechanism can only be controlled if the diffusion flame is eliminated, in whole or in part.
- NOx formation from the combustion of methane could be greatly reduced if methane could be combusted at temperatures below 1700 degrees K and diffusion flame could be avoided. It is well known in the art that if methane is catalytically combusted, i.e. oxidized in the presence of a catalyst, the energy within the methane can be released without the formation, or limited formation, of thermal and/or prompt NOx.
- A problem, however, with the catalytic combustion of methane is that methane is a very stable molecule. Thus, it is more difficult to oxidize than higher order hydrocarbons, such as propane. Methane can be catalytically combusted under fuel lean conditions producing combustion temperatures below 1700 degrees K. When a palladium-based catalyst is used the reaction may become unstable due to properties of Pd-PdO transformation of the catalyst. Hysteresis in the catalyst activity makes controlling the reaction extremely difficult. Platinum based catalysts on the other hand can provide more stable operation. However, volatility of Pt at the desired temperatures under lean conditions is very high. Thus, platinum catalyst lacks durability.
- Based on the foregoing, it is an object of the present invention to develop a method and an apparatus for the combustion of methane that overcomes the problems and drawbacks associated with the prior art.
- The present invention is directed in one aspect to a method for the combustion of methane. In the method, a fluid stream including fuel having methane and oxygen that is in fuel rich proportions, i.e. having a fuel/oxidant equivalence ratio greater than 1.0, is provided. The fluid stream flows into a reformation reactor having a catalyst therein that promotes the reformation of methane (CH4) into carbon monoxide (CO) and hydrogen (H2).
- The catalyst reforms at least a portion of the methane in the fluid stream into carbon monoxide and hydrogen creating an exhaust stream exiting the reformation reactor having various fuel constituents therein, such as unreformed methane, CO and H2. The exhaust stream is then divided into a plurality of exhaust streamlets by passing the exhaust stream into a manifold having a plurality of discrete discharges. As a portion of the exhaust gas exits through a discharge, an exhaust streamlet is formed. Sufficient oxygen is then added to the exhaust streamlet such that the fuel constituents therein and the oxygen are in fuel-lean proportions. Same amount of oxygen should be added to each streamlet, such that variations in the equivalence ratios between the streamlets are small. The exhaust and second fluid are added together, not mixed. In the present invention, it is desired that the exhaust and the second fluid enter the porous media as distinct flow steams. It is understood however, that the two fluids will be in contact along an interface and that incidental diffusion of one fluid into another will occur. It is expected that if sufficient time is provided the diffusion combustion would occur at the interface before the two streamlets can mix. To avoid gas phase flame oxidation of the exhaust stream, which is undesirable in this invention, combined stream formed after adding the second stream to the exhaust stream should be passed into the porous media before combustion takes place. Finally, at least a portion of the CO, H2 and CH4 in the exhaust streamlets is oxidized by passing the combined stream through a porous media that absorbs and then radiates some of the heat generated by the oxidation.
- A catalytic burner suitable for performing the above method includes a reformation reactor incorporating a catalyst. A manifold that receives the exhaust stream from the reformation reactor and passes the exhaust stream through a plurality of discharges forming part of the manifold thereby creating a plurality of exhaust streamlets. The exhaust streamlets then enter a flow path where the exhaust streamlets are directed into a proximally located porous media. Means for introducing a second fluid into the flow path are also provided.
- The reformation reactor is a partial oxidation reactor. In a partial oxidation reactor, the catalyst and its associated geometry, e.g. substrate and dispersion thereon, defines an activity relative to the flow rate, i.e., residence time, of the methane/oxygen thereover such that when the catalyst and the methane/oxygen interact partial oxidation products and not complete oxidation products are predominantly formed. In the case of methane and oxygen, partial oxidation products are H2 and CO, while the compete oxidation products are H2O and CO2. An example of a reformation reactor for methane suitable for this application is disclosed in U.S. Pat. No. 5,648,582, the disclosure of which is incorporated herein in its entirety.
- As those skilled in the art will appreciate, the selectivity, i.e. the ability to produce one product in favor of another, in the reformation process can be manipulated by controlling the temperature of the fluid stream. In the case of a fluid stream including methane and oxygen in fuel rich proportions, preheating of the fluid stream increases the selectivity in the reformation of methane in favor of H2 and CO versus CO2 and H2O. Therefore, an enhancement to both the method and the catalytic burner incorporates heating the fuel stream prior to its entry into the reformation reactor.
- The exhaust and the second fluid are mixing and reacting inside the porous media to further oxidize at least part of the exhaust stream to the complete oxidation products. The porous media absorbs some of the heat created by the exothermic oxidation reaction and emits it in the form of IR radiation, assuring that the temperature remains below the adiabatic flame temperature defined by the reactant stoichiometry of the fuel constituents and oxygen. A porous media can be any media through which a gas can flow, while continuously encountering solid surfaces. In other words, porous media is comprised of alternating regularly or randomly empty volumes and filled volumes. Empty volumes should form a continuous network, such that the porous media remains permeable to permit the flow of a fluid therethrough. The porous media should have a pore size, which describes the average size of the empty volume (if the pores size in not round the smaller dimension), that is generally uniform, but small deviations are acceptable. Porous media having a few large empty volumes and otherwise generally uniform smaller volumes could be problematic. The precise pore size, porosity (ratio of open volume to total volume) and material is application dependent.
- The material for the porous media should be chosen to withstand the temperatures generated in the exothermic oxidation process and effectively emit heat in the form of infrared radiation (IR). Pore size and porosity are chosen large enough to minimize pressure drop induced by the porous media but small enough when compared to the total volume in which the oxidation reaction between the exhaust and the second stream takes place.
- As those skilled in combustion will readily appreciate, the reformation reactor requires that the catalyst therein be at a certain temperature to perform the reformation. The catalyst can be brought to this temperature by any one or a combination of well know procedures, such as heating the fluid stream, or direct heating of the catalyst.
- Regardless of the method chosen, the exhaust gas will have a temperature upon exiting the catalyst equal to the operational temperature chosen for the reformation reactor plus the exothermal resulting from the exothermic oxidation process taking place therein. It should be remembered that the proportions of fuel constituents to oxygen within the exhaust stream are still be quite rich, i.e., the initial stream had fuel rich proportions and oxidant was consumed along with fuel creating a progressively richer fuel stream as it passed through the reformation reactor. Therefore, although the fuel constituents in the exhaust gas will be quite hot, oxidation will not occur within the exhaust stream until additional oxidant is added.
- Where the fuel/oxygen stoichiometry, flow rate and IR radiation are such that porous media is hot enough, oxidation of fuel inside the porous media will occur upon contact with an oxidant. Where the porous media is not hot enough to support oxidation on contact with an oxidant, the porous media can utilize a suitable oxidation catalyst to sustain the oxidation reaction. It is understood that a catalyst can be used even if the fuel constituents are hot enough to support combustion.
- FIG. 1 is a side view of the catalytic burner of the present invention.
- FIG. 2 is a top view of the manifold of the present invention taken along line2-2 of FIG. 1.
- FIG. 3. is a side view of a second embodiment of the catalytic burner of the present invention.
- FIG. 4 is a top view of the catalytic burner taken along the line4-4 of FIG. 3 showing the heat exchanger.
- As shown in FIG. 1, the catalytic burner, generally referred to by the
reference number 10, is comprised of areformation reactor 12, a manifold 14 and aporous media 16. An inlet stream 18 enters thereformation reactor 12 by means of aflow path 20 creating an exhaust stream 24. The manifold 14 andreformation reactor 12 are connected by aflow path 26 such that the exhaust stream 24 enters the manifold 14 to exit through a plurality of discharges 28 (See FIG. 2).Exhaust streamlets 30 are formed by thedischarges 28. Thedischarges 28 are positioned proximate theporous media 16, and connected by aflow path 32, such that upon exiting thedischarges 28 theexhaust streamlets 30 enter aninlet face 15 of theporous media 16. - An
oxidant 34 flows around the manifold 14 permitting theoxidant 34 to flow into theflow path 35 connecting the discharges 24 to theporous media 16. As shown in FIG. 2, thedischarges 28 are positioned to disperse uniformly the exhaust stream 24 asexhaust streamlets 30 over adispersion area 36, defined by a perimeter 38. The hub and spoke design of the manifold 14 assists in distributing theexhaust streamlets 30 uniformly under theporous media 16 across theinlet face 15, but the manifold 14 and discharges 28 therefrom could be of any design, such as port injectors positioned in thehousing 12, thus the invention should not be considered limited to the manifold 14 shown. - The
flow path 32 andmanifold 14 should cooperate to uniformly disperse theoxidant 34 and exhaust stream 24 across theinlet face 15 of the porous media 6. It is a feature of this invention that theoxidant 34 andexhaust streamlets 30 be associated, but not mixed in theflow path 32. Associated means that the exhaust streamlets 30 andoxidant 34 are brought in contact but are not provided sufficient time to inter-defuse, and therefore, the exhaust streamlets 30 andoxidant 34 generally enter theporous media 16 as discrete streams. - In the method of the present invention, the inlet stream18 has methane and oxygen in fuel rich proportions. Preferably, the oxygen is provided as a constituent of air. If desired, the methane can be provided as a constituent of a blended fuel, such as natural gas. Preferably, the methane and oxygen are highly mixed. The operational perimeters of the
reformation reactor 12, including the catalyst therein, are selected such that some, or for all practical purposes all, of the methane is converted primarily into CO and H2 instead of CO2 and H2O. This creates an exhaust stream 24 from thereformation reactor 12 having therein at least the fuel constituents CO, and H2. - The fuel constituents in the exhaust stream24 define an adiabatic temperature. The exhaust stream 24 is then divided into
exhaust streamlets 30. Theexhaust streamlets 30 are then associated with additional oxygen, generally as a constituent of air, in fuel lean proportion (exhaust stream to oxygen). It is preferred that exhaust and oxygen are mixed in a proportion close to stoichiometric with small excess oxygen. Theexhaust streamlets 30 and additional oxygen then pass into theporous media 16 where mixing and oxidation, which is exothermic, takes place. Theporous media 16 is constructed of materials that absorb some of the heat of reaction, such that the oxidation occurring in theporous media 16 is below the adiabatic temperature of the fuel constituents. The heat of reaction absorbed by theporous media 16 is radiated therefrom in the form of infrared radiation. - As discussed above and shown in FIGS. 1 and 2, the
catalytic burner 10 has a plurality ofdischarges 28 that divide the exhaust stream 24 intoexhaust streamlets 30. In the context of the method, the exhaust stream 24, which is in fuel rich proportion, has associated with it a certain amount of energy. The energy density of the exhaust stream is proportional to the amount of fuel passing through a certain cross-sectional area per unit of time, i.e. to the volumetric flow rate of the exhaust stream 24. U.S. Pat. No. 5,648,582 suggests that one essential feature of thereformation reactor 12 is that the inlet stream 18 enters the reactor at very high space velocity and the reformation reaction occurs at short residence time. This provides that flow space velocity and associated energy density in the exhaust stream 24 will also be high. If the exhaust stream 24 were to be exposed to additional oxidant as a single stream, excessive amount of heat, associated with the oxidation reaction, would be released in a small volume of theporous media 16. This excessive heat could cause deterioration, or failure, of theporous media 16. The manifold 14 distributes the exhaust stream 24 over the larger cross-sectional area, effectively decreasing the energy density in the stream. The energy density associated withindividual exhaust streamlets 30 and any diffusion flame that maybe associated therewith is considerably lower and may be adjusted depending on the application. Thedischarges 28 can also act as diffusers to reduce further the power density, i.e., power per area, of the exhaust stream 24. - FIG. 3 is a second embodiment of the catalytic burner which is similar to the previous embodiment, therefore, like reference number preceded by the
number 1 are used to indicate like elements. In this embodiment, thecatalytic burner 110 is positioned in aninterior area 140 of a housing 142. Also positioned within theinterior area 140 is aheat exchanger 144. Thereformation reactor 112 is positioned within theporous media 116 as opposed to under it. In this embodiment, theinlet stream 118 enters aheat exchanger 144 positioned within theinterior area 140 adjacent theporous media 116. Theporous media 116 has acatalyst 146 deposited on the surface thereof. Thecatalyst 146 is selected to support the continued oxidation of the H2, CO and CH4 in the exhaust streamlets 130. Theinlet stream 118 flows through theheat exchanger 144 prior to entering thereformation reactor 112. - As explained above, in the method of the present invention an oxidation reaction occurs in the
porous media 116. As such, some of the heat ofreaction 147 leaves theporous media 116 and is conducted into contact withheat exchanger 144, where some of the heat of reaction is transferred into theinlet stream 118 flowing therein. Referring to FIG. 4, theheat exchanger 144 is comprised of a tube 148 that has been formed into a flat coil about a center point on an axis designated by the letter A. - The
heat exchanger 144 could be of any other design, which allows part of heat released inporous media 116 to be transferred into theinlet stream 118, thus, the invention should not be considered limited to theheat exchanger 144 shown. - Continuing with FIG. 3, the manifold114 is adapted to receive the exhaust stream 130 from the
reformation reactor 112. In this embodiment, the means for introducing additional oxidant 134 between thedischarges 128 and theporous media 116 is by the introduction of additional oxidant 134 into the housing 142 below thedischarges 128. Depending upon the method of operation, the flow of additional oxidant 134 may be by natural convection or a pump, such as a fan. In most cases, the introduction point is not critical as oxygen as a constituent of air will be the oxidant 134 and the air will naturally flow to the desired location. Therefore, the means could include passages in the housing, or the additional oxidant 134 could flow from a point above theporous media 116 into the housing 142. - In this embodiment, the
reformation reactor 112 is shown positioned within theporous media 116. This is not a requirement of the invention, as thereformation reactor 112 could be positioned anywhere including outside the interior area 40. - In the method of the present invention, this embodiment is designed to provide the additional step of preheating of the
inlet gas stream 118 using some of the heat of reaction produced by the exothermic reaction in theporous media 116. Preheating theinlet stream 118 offers the advantage of increasing the selectively to CO and H2 within thereformation reactor 12. This is but one method of preheating, therefore the invention should not be considered so limited. Preheating of theinlet stream 118 by other means such as electric resistance are considered within the scope of the invention. Preheating of the inlet stream can assist in starting the catalytic burner. - The
porous media porous media porous media additional oxidant 34, 134, extract heat from the ongoing oxidation, and radiate infrared radiation. Further, theporous media oxidant 34, 134 are divided into small pockets. In other words, the exhaust stream 24, 124 andoxidant 34, 134 cannot reform into a large volume. These requirements mean that preferably the pores within theporous media - Although the present invention has been described in considerable detail with reference to certain preferred versions thereof, other versions are possible, particularly versions having more than two catalysts. Therefore, the spirit and scope of the invention should not be limited to the description of the preferred versions contained herein.
Claims (20)
1. A method for combustion of a fuel including methane, the method comprising the steps of:
providing a fluid stream that includes fuel and oxygen in fuel rich proportions to a reformation reactor having a catalyst therein upon which at least a portion of the fuel stream contacts;
reforming, via catalytic reaction, at least a portion of the methane in the fuel into carbon monoxide and hydrogen to form an exhaust stream having various fuel constituents therein;
associating oxygen with the exhaust stream, the oxygen being provided in quantities that cause the ratio of oxygen and the fuel constituents in the exhaust stream to be in fuel lean proportions;
oxidizing at least a portion of the fuel constituents in the exhaust stream within a porous media creating a heat of reaction; and
radiating at least a portion of the heat of reaction from the porous media.
2. The method of claim 1 having the additional step of preheating the fluid stream prior to the reforming step.
3. The method of claim 1 wherein the porous media has a catalyst positioned on the surface thereof.
4. A method for combustion of a fuel including methane, the method comprising the steps of:
providing a fluid stream including fuel and oxygen in fuel rich proportions;
reforming at least a portion of the methane in the fluid stream into carbon monoxide and hydrogen to create an exhaust stream from the catalyst having various fuel constituents therein;
associating oxygen with the exhaust stream, the oxygen having a volume in fuel lean proportions to the fuel constituents within the exhaust stream;
oxidizing at least a portion of the fuel constituents within a porous media creating a heat of reaction; and
radiating at least a portion of the heat of reaction from the porous media.
5. The method of claim 4 having the additional step of preheating the fluid stream prior to the reforming step.
6. The method of claim 4 having an additional step of dispersing the exhaust stream prior to associating with oxygen.
7. A catalytic burner comprising:
a reformation reactor having a catalyst therein suitable for the converting of at least a portion of the methane in the fuel stream including methane and oxygen in fuel rich proportions to carbon monoxide and hydrogen for creating an exhaust stream;
a manifold having a plurality of discharges, the manifold in fluid communication with the exhaust stream and defining a plurality discharges;
a porous media:
means defining a flow path between at least some of the discharges and the porous media; and
means for introducing oxygen into the flow path such that the exhaust stream and oxygen are in fuel lean proportions.
8. The catalytic burner of claim 7 wherein the porous media is a plurality of stacked short-channel screens.
9. The catalytic burner of claim 7 wherein the porous media has a catalyst positioned on the surface thereof.
10. The catalytic burner of claim 7 further comprising a heat exchanger, downstream of the porous media for receiving and passing the fuel therethrough.
11. The catalytic burner of claim 8 wherein the heat exchanger is a spiral shape tube.
12. The catalytic burner of claim 7 wherein the manifold includes a hub having a plurality of spokes extending therefrom.
13. The catalytic burner of claim 7 wherein at least a portion of the reformation reactor is positioned within the porous media.
14. A catalytic burner comprising:
a reformation reactor for reforming an inlet stream;
a manifold having a plurality of discharges;
means defining a first flow path between the reformation reactor and the manifold;
a porous media:
means defining a second flow path between at least some of the discharges and the porous media; and
means for introducing oxidant into the second flow path.
15. The catalytic burner of claim 14 wherein the porous media is a plurality of stacked short-channel screens.
16. The catalytic burner of claim 14 wherein the porous media has a catalyst positioned on the surface thereof.
17. The catalytic burner of claim 14 further comprising a heat exchanger located downstream of the porous media.
18. The catalytic burner of claim 17 wherein the heat exchanger is a spiral shape tube.
19. The catalytic burner of claim 14 wherein the manifold a hub having a plurality of spokes extending therefrom.
20. The catalytic burner of claim 14 wherein at least a portion of the reformation reactor is positioned within the porous media.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/178,130 US20030235523A1 (en) | 2002-06-24 | 2002-06-24 | Method for methane oxidation and, apparatus for use therewith |
AU2003247767A AU2003247767A1 (en) | 2002-06-24 | 2003-06-23 | Method for methane oxidation and apparatus for use therewith |
PCT/US2003/020929 WO2004001294A2 (en) | 2002-06-24 | 2003-06-23 | Method for methane oxidation and apparatus for use therewith |
US11/476,995 US20060242903A1 (en) | 2002-06-24 | 2006-06-27 | Apparatus for use for methane oxidation |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/178,130 US20030235523A1 (en) | 2002-06-24 | 2002-06-24 | Method for methane oxidation and, apparatus for use therewith |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/476,995 Division US20060242903A1 (en) | 2002-06-24 | 2006-06-27 | Apparatus for use for methane oxidation |
Publications (1)
Publication Number | Publication Date |
---|---|
US20030235523A1 true US20030235523A1 (en) | 2003-12-25 |
Family
ID=29734596
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/178,130 Abandoned US20030235523A1 (en) | 2002-06-24 | 2002-06-24 | Method for methane oxidation and, apparatus for use therewith |
US11/476,995 Abandoned US20060242903A1 (en) | 2002-06-24 | 2006-06-27 | Apparatus for use for methane oxidation |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/476,995 Abandoned US20060242903A1 (en) | 2002-06-24 | 2006-06-27 | Apparatus for use for methane oxidation |
Country Status (3)
Country | Link |
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US (2) | US20030235523A1 (en) |
AU (1) | AU2003247767A1 (en) |
WO (1) | WO2004001294A2 (en) |
Cited By (9)
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---|---|---|---|---|
US8684303B2 (en) | 2008-06-02 | 2014-04-01 | United Technologies Corporation | Gas turbine engine compressor arrangement |
US8747055B2 (en) | 2011-06-08 | 2014-06-10 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US8756908B2 (en) | 2012-05-31 | 2014-06-24 | United Technologies Corporation | Fundamental gear system architecture |
US9840969B2 (en) | 2012-05-31 | 2017-12-12 | United Technologies Corporation | Gear system architecture for gas turbine engine |
US10138809B2 (en) | 2012-04-02 | 2018-11-27 | United Technologies Corporation | Geared turbofan engine with a high ratio of thrust to turbine volume |
US10221770B2 (en) | 2012-05-31 | 2019-03-05 | United Technologies Corporation | Fundamental gear system architecture |
US10451004B2 (en) | 2008-06-02 | 2019-10-22 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US11021997B2 (en) | 2011-06-08 | 2021-06-01 | Raytheon Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US11970984B2 (en) | 2023-02-08 | 2024-04-30 | Rtx Corporation | Gas turbine engine with power density range |
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US4054407A (en) * | 1975-12-29 | 1977-10-18 | Engelhard Minerals & Chemicals Corporation | Method of combusting nitrogen-containing fuels |
US5160254A (en) * | 1991-10-04 | 1992-11-03 | Radian Corporation And The Board Of Regents | Apparatus and method for combustion within porous matrix elements |
US5431559A (en) * | 1993-07-15 | 1995-07-11 | Maxon Corporation | Oxygen-fuel burner with staged oxygen supply |
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US3270798A (en) * | 1961-09-19 | 1966-09-06 | Universal Oil Prod Co | Catalytic radiant heat treating apparatus |
NL7314826A (en) * | 1972-12-11 | 1974-06-13 | ||
US6946111B2 (en) * | 1999-07-30 | 2005-09-20 | Conocophilips Company | Short contact time catalytic partial oxidation process for recovering sulfur from an H2S containing gas stream |
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2002
- 2002-06-24 US US10/178,130 patent/US20030235523A1/en not_active Abandoned
-
2003
- 2003-06-23 WO PCT/US2003/020929 patent/WO2004001294A2/en not_active Application Discontinuation
- 2003-06-23 AU AU2003247767A patent/AU2003247767A1/en not_active Abandoned
-
2006
- 2006-06-27 US US11/476,995 patent/US20060242903A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
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US4054407A (en) * | 1975-12-29 | 1977-10-18 | Engelhard Minerals & Chemicals Corporation | Method of combusting nitrogen-containing fuels |
US5160254A (en) * | 1991-10-04 | 1992-11-03 | Radian Corporation And The Board Of Regents | Apparatus and method for combustion within porous matrix elements |
US5431559A (en) * | 1993-07-15 | 1995-07-11 | Maxon Corporation | Oxygen-fuel burner with staged oxygen supply |
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US8684303B2 (en) | 2008-06-02 | 2014-04-01 | United Technologies Corporation | Gas turbine engine compressor arrangement |
US11731773B2 (en) | 2008-06-02 | 2023-08-22 | Raytheon Technologies Corporation | Engine mount system for a gas turbine engine |
US11286883B2 (en) | 2008-06-02 | 2022-03-29 | Raytheon Technologies Corporation | Gas turbine engine with low stage count low pressure turbine and engine mounting arrangement |
US10451004B2 (en) | 2008-06-02 | 2019-10-22 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US9752511B2 (en) | 2011-06-08 | 2017-09-05 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US11635043B2 (en) | 2011-06-08 | 2023-04-25 | Raytheon Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US8747055B2 (en) | 2011-06-08 | 2014-06-10 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US11698007B2 (en) | 2011-06-08 | 2023-07-11 | Raytheon Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US11073106B2 (en) | 2011-06-08 | 2021-07-27 | Raytheon Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US8899915B2 (en) | 2011-06-08 | 2014-12-02 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US11021997B2 (en) | 2011-06-08 | 2021-06-01 | Raytheon Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US11021996B2 (en) | 2011-06-08 | 2021-06-01 | Raytheon Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US11047337B2 (en) | 2011-06-08 | 2021-06-29 | Raytheon Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US9631558B2 (en) | 2012-01-03 | 2017-04-25 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US11053843B2 (en) | 2012-04-02 | 2021-07-06 | Raytheon Technologies Corporation | Geared turbofan engine with a high ratio of thrust to turbine volume |
US11448124B2 (en) | 2012-04-02 | 2022-09-20 | Raytheon Technologies Corporation | Geared turbofan engine with a high ratio of thrust to turbine volume |
US10138809B2 (en) | 2012-04-02 | 2018-11-27 | United Technologies Corporation | Geared turbofan engine with a high ratio of thrust to turbine volume |
US10221770B2 (en) | 2012-05-31 | 2019-03-05 | United Technologies Corporation | Fundamental gear system architecture |
US8756908B2 (en) | 2012-05-31 | 2014-06-24 | United Technologies Corporation | Fundamental gear system architecture |
US9840969B2 (en) | 2012-05-31 | 2017-12-12 | United Technologies Corporation | Gear system architecture for gas turbine engine |
US11773786B2 (en) | 2012-05-31 | 2023-10-03 | Rtx Corporation | Fundamental gear system architecture |
US11970984B2 (en) | 2023-02-08 | 2024-04-30 | Rtx Corporation | Gas turbine engine with power density range |
Also Published As
Publication number | Publication date |
---|---|
WO2004001294A2 (en) | 2003-12-31 |
WO2004001294A3 (en) | 2005-06-02 |
AU2003247767A1 (en) | 2004-01-06 |
US20060242903A1 (en) | 2006-11-02 |
AU2003247767A8 (en) | 2004-01-06 |
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