EP0558669B1 - Multistage process for combusting fuel mixtures - Google Patents

Multistage process for combusting fuel mixtures Download PDF

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Publication number
EP0558669B1
EP0558669B1 EP92902114A EP92902114A EP0558669B1 EP 0558669 B1 EP0558669 B1 EP 0558669B1 EP 92902114 A EP92902114 A EP 92902114A EP 92902114 A EP92902114 A EP 92902114A EP 0558669 B1 EP0558669 B1 EP 0558669B1
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Prior art keywords
catalyst
temperature
catalytic
stage
gas
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EP92902114A
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German (de)
English (en)
French (fr)
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EP0558669A1 (en
EP0558669A4 (ko
Inventor
Kazunori Tsurumi
Nobuyasu Ezawa
James C. Schlatter
Sarento G. Nickolas
Ralph A. Dalla Betta
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Tanaka Kikinzoku Kogyo KK
Catalytica Inc
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Tanaka Kikinzoku Kogyo KK
Catalytica Inc
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Priority claimed from US07/617,980 external-priority patent/US5232357A/en
Priority claimed from US07/618,301 external-priority patent/US5183401A/en
Priority claimed from US07/617,977 external-priority patent/US5281128A/en
Application filed by Tanaka Kikinzoku Kogyo KK, Catalytica Inc filed Critical Tanaka Kikinzoku Kogyo KK
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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
    • F23C2900/13002—Catalytic combustion followed by a homogeneous combustion phase or stabilizing a homogeneous combustion phase

Definitions

  • This invention is a combustion process having a series of stages in which a fuel/oxygen-gas-containing mixture is combusted stepwise using a series of specific catalysts and catalytic structures and, optionally, a final homogeneous combustion zone to produce a combusted gas at a selected temperature preferably between 1050° and 1700°C.
  • a selected temperature preferably between 1050° and 1700°C.
  • the choice of catalysts and the use of specific structures, including those employing integral heat exchange results in a catalyst and its support which are stable due to their comparatively low temperature, do not deteriorate, and yet the product combustion gas is at a temperature suitable for use in a gas turbine, furnace, boiler, or the like, but has low NO x content. Neither fuel nor air is added to the combustion process except in the initial stage.
  • NO x an equilibrium mixture mostly of NO, but also containing very minor amounts of NO 2
  • NO x an equilibrium mixture mostly of NO, but also containing very minor amounts of NO 2
  • removal of NO x once produced once it is a difficult task because of its relative stability and its low concentration in most exhaust gases.
  • One solution used in automobiles is the use of carbon monoxide chemically to reduce NO x to nitrogen while oxidizing the carbon monoxide to carbon dioxide.
  • the need to react two pollutants also speaks to a conclusion that the initial combustion reaction was inefficient.
  • Ceramic or metal oxide supports are clearly well-known.
  • the structures formed do not readily melt or oxidize as would a metallic support.
  • a ceramic support carefully designed for use in a particular temperature range can provide adequate service in that temperature range. Nevertheless, many such materials can undergo phase changes or react with other components of the catalyst system at temperatures above 1100°C, e.g., the gamma alumina phase changes to the alpha alumina form in that region.
  • such ceramic substrates are olefin fragile, subject to cracking and failure as a result of vibration, mechanical shock, or thermal shock. Thermal shock is a particular problem in catalytic combustors used in gas turbines. During startup and shutdown, large temperature gradients can develop in the catalyst leading to high mechanical stresses that result in cracking and fracture.
  • Japanese Kokai 60-053724 teaches the use of a ceramic columnar catalyst with holes in the column walls to promote equal distribution of fuel gas and temperature amongst the columns lest cracks appear.
  • High temperatures are also detrimental to the catalytic layer resulting in surface area loss, vaporization of metal catalysts, and reaction of catalytic components with the ceramic catalyst components to form less active or inactive substances.
  • platinum group metals platinum, palladium, ruthenium, iridium, and rhodium; sometimes alone, sometimes in mixtures with other members of the group, sometimes with non-platinum group promoters or co-catalysts.
  • combustion catalysts include metallic oxides, particularly Group VIII and Group I metal oxides.
  • metallic oxides particularly Group VIII and Group I metal oxides.
  • ABO 3 particularly oxides formulated as La 1-x Me x MnO 3 , where Me denotes Ca, Sr, or Ba.
  • a number of the three stage catalyst combination systems discussed above also have post-combustion steps.
  • a series of Japanese Kokai assigned to Nippon Shokubai Kagaku (“NSK”) (62-080419, 62-080420, 63-080847, 63-080848, and 63-080549) disclose three stages of catalytic combustion followed by a secondary combustion step.
  • Nippon Shokubai Kagaku (62-080419, 62-080420, 63-080847, 63-080848, and 63-080549) disclose three stages of catalytic combustion followed by a secondary combustion step.
  • the catalysts used in these processes are quite different from the catalysts used in the inventive process.
  • these Kokai suggest that in the use of a post-combustion step, the resulting gas temperature is said to reach only "750°C to 1100°C".
  • the inventive process when using the post catalyst homogeneous combustion step may be seen to reach substantially higher adiabatic combustion temperatures.
  • the patent to Furuya et al . (U.S. Patent No. 4,731,989) discloses a single stage catalyst with injection of additional fuel followed by post-catalyst combustion.
  • the low fuel/air ratio mixture feed to the catalyst limits the catalyst substrate temperature to 900°C or 1000°C.
  • additional fuel is injected after the catalyst and this fuel is burned homogeneously in the post catalyst region. This process is complicated and requires additional fuel injection devices in the hot gas stream exiting the catalyst.
  • the inventive device described in our invention does not require fuel injection after the catalyst; all of the fuel is added at the catalyst inlet.
  • an important aspect in the practice of our inventive process is the use of integral heat exchange structures --preferably metal and in at least in the latter catalytic stage or stages of combustion.
  • the concept is to position a catalyst layer on one surface of a wall in the catalytic structure which is opposite a surface having no catalyst. Both sides are in contact with the flowing fuel-gas mixture. On one side reactive heat is produced; on the other side that reactive heat is transferred to the flowing gas.
  • the process of the invention is a combustion process in which the fuel is premixed at a specific fuel/air ratio to produce a combustible mixture having a desired adiabatic combustion temperature.
  • the combustible mixture is then reacted in a series of catalyst structures and in a homogeneous combustion zone.
  • the combustion is staged so that catalyst and bulk gas temperatures are controlled at a relatively low value by catalyst choice and structure.
  • the palladium catalyst self-limiting temperature and the homogeneous combustion initiation temperature are equal or are sufficiently compatible that a "hot end" combustion catalyst stage may be eliminated.
  • the process produces an exhaust gas of a very low NO x concentration but at a temperature suitable for use in a gas turbine, boiler, or furnace.
  • Figure 1 is a graph showing the relationship of pressure to homogeneous combustion temperature and palladium temperatures.
  • Figures 2A and 2B show close-up, cutaway views of a catalyst structure wall having catalyst only on one side.
  • FIGS 3A, 3B, 3C, 4A, 4B, 5, 6A, and 6B all show variations of the integral heat exchange catalyst structure which may be used in the catalytic stages of the inventive process.
  • Figure 7 is a schematic representation of the three stage catalyst test reactor used in the examples.
  • Figures 8 and 9 are graphs of various operating temperatures as a function of preheat temperature.
  • Figure 10 is a graph of various operating temperatures during a long term steady state operation test.
  • Figure 11 is a graph of various operating temperatures during a typical start up procedure.
  • the process of the invention is a combustion process in which the fuel is premixed at a specific fuel/air ratio to produce a combustible mixture having a desired adiabatic combustion temperature.
  • the combustible mixture is then reacted in two or more discrete catalyst structures and in a homogeneous combustion zone.
  • the combustion is staged so that catalyst and bulk gas temperatures are controlled at a relatively low value through catalyst choice and structure.
  • the present invention provides a process comprising:
  • the catalytic structure comprises a catalyst support, preferably a corrugated metal structure, having catalyst with a diffusion barrier situated thereon so that a portion of the combustible mixture is inhibited in its contact with catalyst.
  • the temperature at which the palladium catalyst "self-limits" rises and the temperature at which the fuel mixture undergoes homogeneous combustion decreases.
  • the partial pressure of O 2 rises (be it through an increase in overall pressure or increase in O 2 concentration)
  • the theoretical pressure needed to complete homogeneous combustion declines to a level where the palladium catalyst will initiate that combustion.
  • the two lines meet between four and five atmospheres.
  • the homogeneous combustion reaction will completely combust in about eleven microseconds.
  • the palladium limiting temperature and the homogeneous combustion temperature area equal or sufficiently compatible that a third stage "hot end" combustion catalyst may, if so desired, be eliminated.
  • the process produces an exhaust gas of a very low NO x concentration but at a temperature suitable for use in a gas turbine, boiler, or furnace.
  • This process may be used with a variety of fuels and at a broad range of process conditions.
  • normally gaseous hydrocarbons e.g., methane, ethane, and propane
  • methane ethane
  • propane propane
  • the fuels may be liquid or gaseous at room temperature and pressure.
  • Examples include the low molecular weight hydrocarbons mentioned above as well as butane, pentane, hexane, heptane, octane, gasoline, aromatic hydrocarbons such as benzene, toluene, ethylbenzene; and xylene; naphthas; diesel fuel, kerosene; jet fuels; other middle distillates; heavy distillate fuels (preferably hydrotreated to remove nitrogenous and sulfurous compounds); oxygen-containing fuels such as alcohols including methanol, ethanol, isopropanol, butanol, or the like; ethers such as diethylether, ethyl phenyl ether, MTBE, etc.
  • Low-BTU gases such as town gas or syngas may also be used as fuels.
  • the fuel is typically mixed into the combustion air in an amount to produce a mixture having a theoretical adiabatic combustion temperature greater than the catalyst or gas phase temperatures actually occurring in the catalysts employed in this inventive process.
  • the adiabatic combustion temperature is above 900°C, and most preferably above 1000°C.
  • Non-gaseous fuels should be vaporized prior to their contacting the initial catalyst zone.
  • the combustion air may be at atmospheric pressure or lower (-0.25 atm of air) or may be compressed to a pressure of 35 atm or more of air.
  • Stationary gas turbines (which ultimately could use the gas produced by this process) often operate at gauge pressures in the range of eight atm of air to 35 atm of air.
  • this process may operate at a pressure between -0.25 atm of air and 35 atm of air, preferably between zero atm of air and 17 atm of air.
  • the oxygen-containing gas is air and is compressed to a pressure of at least 4 atmospheres (gauge). In an alternative embodiment, the pressure is zero to 35 atm. (gauge) of air.
  • the fuel/air mixture supplied to the first zone should be well mixed and heated to a temperature high enough to initiate reaction on the first zone catalyst; for a methane fuel on a typical palladium catalyst a temperature of at least about 325°C is usually adequate.
  • This preheating may be achieved by partial combustion, use of a pilot burner by heat exchange, or by compression.
  • the first zone in the process contains a catalytic amount of palladium on a monolithic catalyst support offering low resistance to gas flow.
  • the support is preferably metallic.
  • Palladium is very active at 325°C and lower for methane oxidation and can "light-off" or ignite fuels at low temperatures. It has also been observed that in certain instances, after palladium initiates the combustion reaction, the catalyst rises rapidly to temperatures of 750°C to 800°C at one atm of air or about 940°C at ten atm total pressure of air. These temperatures are the respective temperatures of the transition points in the thermogravimetric analysis (TGA) of the palladium/palladium oxide reaction shown below at the various noted pressures.
  • TGA thermogravimetric analysis
  • This self-limiting phenomenon maintains the catalyst substrate temperature substantially below the adiabatic combustion temperature. This prevents or substantially decreases catalyst degradation due to high temperature operation.
  • the palladium metal is added in an amount sufficient to provide significant activity.
  • the specific amount added depends on a number of requirements., e.g., economics, activity, life, contaminant presence, etc.
  • the theoretical maximum amount is likely enough to cover the maximum amount of support without causing undue metal crystallite growth and concomitant loss of activity.
  • maximum catalytic activity requires higher surface coverage, but higher surface coverage can promote growth between adjacent crystallites.
  • the form of the catalyst support must be considered. If the support is used in a high space velocity environment, the catalyst loadings likely should be high to maintain sufficient conversion even though the residence time is low. Economics has as its general goal the use of the smallest amount of catalytic metal which will do the required task. Finally, the presence of contaminants in the fuel would mandate the use of higher catalyst loadings to offset the deterioration of the catalyst by deactivation.
  • the palladium metal content of this catalyst composite is typically quite small, e.g., from 0.1% to about 25% by weight, and preferably from 0.01% to about 20% by weight.
  • the palladium may be incorporated onto the support in a variety of different methods using palladium complexes, compounds, or dispersions of the metal.
  • the compounds or complexes may be water or hydrocarbon soluble. They may be precipitated from solution.
  • the liquid carrier generally needs only to be removable from the catalyst carrier by volatilization or decomposition while leaving the palladium in a dispersed form on the support.
  • the palladium complexes and compounds suitable in producing the catalysts used in this invention are palladium chloride, palladium diammine dinitrite, palladium tetrammine chloride, palladium 2-ethylhexanoic acid, sodium palladium chloride, and other palladium salts or complexes.
  • the preferred supports for this catalytic zone are metallic. Although other support materials such as ceramics and the various inorganic oxides typically used as supports: silica, alumina, silica-alumina, titania, zirconia, etc., and may be used with or without additions such as barium, cerium, lanthanum, or chromium added for stability. Metallic supports in the form of honeycombs, spiral rolls of corrugated sheet (which may be interspersed with flat separator sheets), columnar (or "handful of straws"), or other configurations having longitudinal channels or passageways permitting high space velocities with a minimal pressure drop are desirable in this service.
  • the catalyst is deposited, or otherwise placed, on the walls within the channels or passageways of the metal support in the amounts specified above.
  • the catalyst may be introduced onto the support in a variety of formats: the complete support may be covered, the downstream portion of the support may be covered, or one side of the support's wall may be covered to create an integral heat exchange relationship such as that discussed with regard to the later stages below.
  • the preferred configuration is complete coverage because of the desire for high overall activity at low temperatures but each of the others may be of special use under specific circumstances.
  • Several types of support materials are satisfactory in this service: aluminum, aluminum containing or aluminum-treated steels, and certain stainless steels or any high temperature metal alloy, including nickel alloys where a catalyst layer can be deposited on the metal surface.
  • the preferred materials are aluminum-containing steels such as those found in U.S. Patent Nos. 4,414,023 to Aggen et al ., 4,331,631 to Chapman et al ., and 3,969,082 to Cairns, et al .
  • These steels, as well as others sold by Kawasaki Steel Corporation (River Lite 20-5 SR), disclose Anlagen Deutchse Metalltechnike AG (Alumchrom I RE), and Allegheny Ludlum Steel (Alfa-IV) contain sufficient dissolved aluminum so that, when oxidized, the aluminum forms alumina whiskers or crystals on the steel's surface to provide a rough and chemically reactive surface for better adherence of the washcoat.
  • the washcoat may be applied using an approach such as is described in the art, e.g., the application of gamma-alumina sols or sols of mixed oxides containing aluminum, silicon, titanium, zirconium, and additives such as barium, cerium, lanthanum, chromium, or a variety of other components.
  • a primer layer may be applied containing hydrous oxides such as a dilute suspension of pseudo-boehmite alumina as described in U.S. Patent 4,729,782 to Chapman et al .
  • the primed surface is then coated with a zirconia suspension, dried, and calcined to form a high surface area adherent oxide layer on the metal surface.
  • the washcoat may be applied in the same fashion one would apply paint to a surface, e.g., by spraying, direct application, dipping the support into the washcoat material, etc.
  • Aluminum structures are also suitable for use in this invention and may be treated or coated in essentially the same manner.
  • Aluminum alloys are somewhat more ductile and likely to deform or even to melt in the temperature operating envelope of the process. Consequently, they are less desirable supports but may be used if the temperature criteria can be met.
  • a low or non-catalytic oxide may then be applied as a diffusion barrier to prevent the temperature "runaway" discussed above.
  • This barrier layer can be alumina, silica, zirconia, titania, or a variety of other oxides with a low catalytic activity for combustion of the fuel or mixed oxides or oxides plus additives similar to those described for the washcoat layer.
  • Alumina is the least desirable of the noted materials.
  • the barrier layer can range in thickness from 1% of the washcoat layer thickness to a thickness substantially thicker than the washcoat layer, but preferably from 10% to 100% of the washcoat layer thickness.
  • the first stage combustion catalyst comprises palladium on a metallic support and additionally a barrier layer covering at least a portion of the palladium.
  • the barrier layer is preferably zirconia.
  • the barrier layer or layers may be applied using the same application techniques one would use in the application of paint.
  • This catalyst structure should be made in such a size and configuration that the average linear velocity through the channels in the catalyst structure is greater than about 0.2 m/second and no more than about 40 m/second throughout the first catalytic zone structure.
  • This lower limit is an amount larger than the flame front speed for methane and the upper limit is a practical one for the type of supports currently commercially available. These average velocities may be somewhat different for fuels other than methane.
  • the first catalytic zone is sized so that the bulk outlet temperature of the gas from that zone is no more than about 800°C, preferably in the range of 450°C to 700°C and, most preferably, 500°C to 650°C.
  • the second zone in the process takes partially combusted gas from the first zone and causes further controlled combustion to take place in the presence of a catalyst structure having heat exchange capabilities.
  • the catalyst may comprise materials selected from Mendelev Groups IB, VI, VIII noble metals.
  • the second stage catalyst comprises palladium, particularly if the pressure of the process is higher than about four atmospheres. Whatever the pressure, the catalyst comprises a Group VIII noble metal such as platinum or palladium. If the catalyst contains palladium it may optionally contain up to an equivalent amount of one or more catalyst adjuncts selected from Group IB or Group VIII noble metals.
  • the preferred adjunct catalysts are silver, gold, ruthenium, rhodium, platinum, iridium, or osmium. Most preferred are silver and platinum.
  • This zone may operate adiabatically with the heat generated in the partial combustion of the fuel resulting in a rise in the gas temperature. Neither air nor fuel is added between the first and second catalytic zone.
  • the catalyst structure in this zone is similar to that used in the first catalytic zone except that the catalyst preferably is applied to at least a portion of only one side of the surface forming the walls of the monolithic catalyst support structure.
  • Figure 2A shows a cutaway of a the high surface area metal oxide washcoat (10), and active metal catalyst (12) applied to one side of the metal substrate (14).
  • This structure readily conducts the reaction heat generated at the catalyst through interface between the washcoat layer (10) and gas flow (16) in Figure 2B. Due to the relatively high thermal conductivity of the washcoat (10) and metal (14), the heat is conducted equally along pathway (A) as well as (B), dissipating the reaction heat equally into flowing gas streams (16) and (18).
  • Metal sheets coated on one side with catalyst, and the other surface being non-catalytic, can be formed into rolled or layered structures combining corrugated (20) and flat sheets (22) as shown in Figures 3A through 3C to form long open channel structures offering low resistance to gas flow.
  • a corrugated metal strip (30) coated on one side with catalyst (32) can be combined with a separator strip (34) not having a catalytic coating to form the structure shown in Figure 4A.
  • corrugated (36) and flat strips (38) both coated with catalyst on one side prior to assembly into a catalyst structure can be combined as shown in Figure 4B.
  • the structures form channels with catalytic walls (40 in Figure 4A and 42 in Figure 4B) and channels with non-catalytic walls (44 in Figure 4A and 46 in Figure 4B).
  • Catalytic structures arranged in this manner with catalytic channels and separate non-catalytic channels are termed limited-integral-heat-exchange structures ("L-IHE"). These structure have the unique ability to limit the catalyst substrate temperature and outlet gas temperature.
  • the corrugated (42) and flat sheets (44) coated on one side with catalyst can be arranged according to Figure 5 where the catalytic surface of each sheet faces a different channel so that all channels have a portion of their walls' catalyst coated and all walls have one surface coated with catalyst and the opposite surface non-catalytic.
  • the Figure 5 structure will behave differently from the Figure 4A and Figure 4B structures.
  • the walls of the Figure 5 structure form an integral heat exchange but, since all channels contain catalyst, there is then a potential for all the fuel to be catalytically combusted. As combustion occurs at the catalyst surface, the temperature of the catalyst and support will rise and the heat will be conducted and dissipated in the gas flow on both the catalytic side and the non-catalytic side.
  • the structures shown in Figures 4A and 4B have equal gas flow through each of the catalytic channels and non-catalytic channels.
  • the maximum gas temperature rise with these structures will be that produced by 50% combustion of the inlet fuel.
  • FIG. 4A and 4B may be modified to control the fraction of fuel and oxygen reacted by varying the fraction of the fuel and oxygen mixture that passes through catalytic and non-catalytic channels.
  • Figure 6A shows a structure where the corrugated foil has a structure with alternating narrow (50) and broad (52) corrugations. Coating this corrugated foil on one side results in a large catalytic channel (54) and a small non-catalytic channel (56). In this structure approximately 80% of the gas flow would pass through catalytic channels and 20% through the non-catalytic channels. The maximum outlet gas temperature would be about 80% of the temperature rise expected if the gas went to its adiabatic combustion temperature.
  • the palladium at one atm of air pressure will limit the wall temperature to 750°C to 800°C and the maximum outlet gas temperature will be about ⁇ 800°C.
  • the palladium limiting is controlling the maximum outlet gas temperature and limiting the wall temperature.
  • the situation is different at ten atmospheres of air pressure.
  • the palladium limiting temperature is about 930°C.
  • the wall will be limited to 900°C by the L-IHE structure. In this case, the L-IHE structure is limiting the wall and gas temperature.
  • the temperature of gas leaving the second stage is typically between 750 and 950°C, for example between 750 and 800°C.
  • the catalyst structure in this zone should have the same approximate catalyst loading, on those surfaces having catalysts, as does the first zone structure. It should be sized to maintain flow in the same average linear velocity as that first zone and, if a third catalytic stage is desired, sized to reach a bulk outlet temperature of no more than 800°C, preferably in the range of 600°C to 800°C and most preferably between 700°C and 800°C.
  • the catalyst can incorporate a non-catalytic diffusion barrier layer such as that described for the first catalytic zone.
  • the second catalytic zone should be designed such that the bulk temperature of the gas exiting the zone is above its autoignition temperature (if the homogenous combustion zone is desired).
  • the support and catalyst temperature are maintained at the moderation temperature mandated by the relative sizing of the catalytic and non-catalytic channels, the inlet temperature, the theoretical adiabatic combustion temperature, and the length of the second zone.
  • the linear velocity of the gas in the second catalytic zone is the same as that of the first zone.
  • the process of the invention may additionally comprise combusting any remaining uncombusted fuel in a third stage to produce a gas having a temperature greater than that of the gas leaving the second stage but no greater than about 1700°C.
  • the third zone in the process takes the partially combusted gas from the second zone and causes a further controlled combustion to take place in the presence of a catalyst preferably having integral heat exchange capabilities and, desirably, comprising a metal-oxygen catalytic material or comprising platinum as the catalytic material.
  • the first and/or third stage combustion catalyst is on a support having integral heat exchange surfaces.
  • the metal-oxygen material desirably contains one or more metals selected from those found in Mendelev Group VIII and Group I. These materials are desirable because of their reactive stability at the higher temperatures.
  • Other combustion catalysts such as palladium, rhodium, osmium, iridium, and the like, may be used in place of or in addition to platinum.
  • the zone may be essentially adiabatic in operation and, by catalytic combustion of at least a portion of the fuel, further raises the gas temperature to a point where homogeneous combustion may take place or where the gas may be directly used in a furnace or turbine.
  • the catalyst structure in this zone may be the same as used in the second zone.
  • the catalyst used in this zone desirably comprises a metal-oxygen catalytic materials or platinum.
  • Suitable metal-oxygen catalytic materials include those selected from Mendelev Group V (particularly Nb or V), Group VI (particularly Cr), Group VIII transition (particularly Fe, Co, Ni), and first series lanthanides (particularly Ce, Pr, Nd, Sa, Tb, La) metal oxides or mixed oxides.
  • the catalytic materials may be chosen from Perovskite-form materials of the form ABO 3 where A is selected from Group IIA or IA metals (Ca, Ba, Sr, Mg, Be, K, Rb, Na, or Cs); and B is selected from Group VIII transition metals, Group VIB, or Group IB (particularly Fe, Co, Ni, Mn, Cr, Cu).
  • A is selected from Group IIA or IA metals (Ca, Ba, Sr, Mg, Be, K, Rb, Na, or Cs)
  • B is selected from Group VIII transition metals, Group VIB, or Group IB (particularly Fe, Co, Ni, Mn, Cr, Cu).
  • Impregnation of the support with a solution of salts or complexes of the desired metal or metals followed by a calcination step is suitable. These materials are typically active as combustion catalysts only at temperatures above 650°C but exhibit reasonable stability in that range. These materials do not show temperature limiting behavior as does palladium; the catalyst substrate can rise
  • the second and third stage catalysts comprise palladium.
  • the third stage catalyst preferably comprises palladium, rhodium, osmium, iridium or platinum.
  • the outlet gas temperature of the third zone will be the average of the inlet temperature and the adiabatic combustion temperature as described earlier.
  • the wall temperature and gas temperature will be limited to equations (1) and (2) given earlier. Incomplete reaction in the catalytic channels will result in a lower outlet gas temperature.
  • the outlet temperature from the third zone will be 1050°C (i.e., the average 800°C and 1300°C). This exit gas temperature will result in rapid homogeneous combustion.
  • the structure of the third zone may take many forms and the catalyst can be applied in a variety of ways to achieve at least partial combustion of the fuel entering the third zone. As an example, use of the structures described above with regard to Figure 6A and 6B would result respectively in the conversion of 80% or 20% of the gas mixture entering the third zone.
  • the outlet gas temperature from the third zone may be adjusted by catalyst support design.
  • the third zone should be designed such that the bulk temperature of the gas exiting the third zone is above its autoignition temperature (if the fourth zone homogenous combustion zone is desired).
  • the support and catalyst temperature are maintained at the moderate temperature mandated by the relative sizing of the catalytic and non-catalytic channels, the inlet temperature, the theoretical adiabatic combustion temperature, and the length of the third zone.
  • the linear velocity of the gas in the third catalytic zone is in the same range as those of the first and second zones although clearly higher because of the higher temperature.
  • the temperature of the combustible mixture discharged from the first stage is between 500°C and 650°C, that discharged from the second stage is between 750° and 800°C, and that discharged from the third stage is between 850° and 1050°C.
  • the gas which has exited the earlier combustion zones may be in a condition suitable for subsequent use if the temperature is correct; the gas contains substantially no NO x and yet the catalyst and catalyst supports have been maintained at a temperature which permits their long term stability.
  • a higher temperature is required.
  • many gas turbines are designed for an inlet temperature of about 1260°C. Consequently, an homogeneous combustion zone may be an appropriate addition.
  • the process of the invention may additionally comprise the step of combusting any remaining uncombusted fuel in a fourth zone to produce a gas having a temperature greater than that of the gas leaving the third stage but no greater than about 1700°C.
  • the homogenous combustion zone need not be large.
  • the gas residence time in the zone normally should not be more than about eleven or twelve milliseconds to achieve substantially complete combustion (i.e., ⁇ ten ppm carbon monoxide) and to achieve the adiabatic combustion temperature.
  • the Table below shows calculated residence times both for achievement of various adiabatic combustion temperatures (as a function of fuel/air ratio) as well as achievement of combustion to near completion variously as a function of fuel-(methane)/air ratio, temperature of the bulk gas leaving the third catalyst zone, and pressure. These reaction times were calculated using a homogeneous combustion model and kinetic rate constants described by Kee et al . (Sandia National Laboratory Report No. SAND 80-8003).
  • the residence time to reach the adiabatic combustion temperature and complete combustion is less than five milliseconds.
  • a bulk linear gas velocity of less than 40 m/second would result in a homogeneous combustion zone of less than 0.2 m in length.
  • the process uses a number of carefully crafted catalyst structures and catalytic methods to produce a working gas which contains substantially no NO x and is at a temperature comparable to normal combustion processes. Yet, the catalysts and their supports are not exposed to deleteriously high temperatures which would harm those catalysts or supports or shorten their useful life.
  • This example shows the assembly of a three stage catalyst system.
  • Thermocouples were located in this system at the positions shown.
  • the thermocouples located in the catalyst sections were sealed inside a channel with ceramic cement to measure the temperature of the catalyst substrate.
  • the gas thermocouples were suspended in the gas stream.
  • the insulated catalyst section of Figure 7 was installed in a reactor with a gas flow path of 50 mm diameter. Air at 150 SLPM was passed through an electric heater, a static gas mixer, and through the catalyst system. Natural gas at 67 SLPM was added just upstream of the static mixer. The air temperature was slowly increased by increasing power to the electric heater. At 368°C, exit the gas temperatures from stages 1, 2, and 3 began to rise as shown in Figure 8.
  • the gas temperature from stage 1 was constant at about 530°C
  • the gas exiting stage 2 was about 780°C
  • the gas exiting stage 3 at approximately 1020°C.
  • Homogeneous combustion occurred after the catalyst giving a gas temperature of about 1250°C; a temperature near the adiabatic combustion temperature of this fuel/air ratio.
  • the substrate temperatures for the three stages are shown in Figure 9.
  • stage 1 the stage 1 catalyst lit off at a low temperature and substrate temperature self-limited at about 750°C.
  • This catalyst cell density and gas flow rate produced an intermediate gas temperature of 540°C.
  • stage 2 also self-limited the substrate temperature to 780°C and produced a gas temperature of 750°C.
  • Stage 3 limited the wall temperature at 1100°C.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Catalysts (AREA)
  • Liquid Carbonaceous Fuels (AREA)
  • Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
  • Hydrogen, Water And Hydrids (AREA)
EP92902114A 1990-11-26 1991-11-26 Multistage process for combusting fuel mixtures Expired - Lifetime EP0558669B1 (en)

Applications Claiming Priority (9)

Application Number Priority Date Filing Date Title
US61797690A 1990-11-26 1990-11-26
US617980 1990-11-26
US617976 1990-11-26
US617977 1990-11-26
US618301 1990-11-26
US07/617,980 US5232357A (en) 1990-11-26 1990-11-26 Multistage process for combusting fuel mixtures using oxide catalysts in the hot stage
US07/618,301 US5183401A (en) 1990-11-26 1990-11-26 Two stage process for combusting fuel mixtures
US07/617,977 US5281128A (en) 1990-11-26 1990-11-26 Multistage process for combusting fuel mixtures
PCT/US1991/008917 WO1992009849A1 (en) 1990-11-26 1991-11-26 Multistage process for combusting fuel mixtures

Publications (3)

Publication Number Publication Date
EP0558669A1 EP0558669A1 (en) 1993-09-08
EP0558669A4 EP0558669A4 (ko) 1994-01-19
EP0558669B1 true EP0558669B1 (en) 1998-09-16

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EP92902114A Expired - Lifetime EP0558669B1 (en) 1990-11-26 1991-11-26 Multistage process for combusting fuel mixtures

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EP (1) EP0558669B1 (ko)
JP (1) JP3364492B2 (ko)
KR (1) KR100261783B1 (ko)
AT (1) ATE171258T1 (ko)
AU (1) AU9143891A (ko)
CA (1) CA2096951A1 (ko)
DE (1) DE69130225T2 (ko)
ES (1) ES2121004T3 (ko)
RU (1) RU2161755C2 (ko)
TW (1) TW198743B (ko)
WO (1) WO1992009849A1 (ko)

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US5474441A (en) * 1989-08-22 1995-12-12 Engelhard Corporation Catalyst configuration for catalytic combustion systems
CA2150106A1 (en) * 1993-03-01 1994-09-15 Jennifer S. Feeley Improved catalytic combustion system including a separator body
EP0686249A1 (en) * 1993-03-04 1995-12-13 Engelhard Corporation Improved substrate configuration for catalytic combustion system
US5746194A (en) * 1995-12-01 1998-05-05 Carrier Corporation Catalytic insert for NOx reduction
FR2742680B1 (fr) * 1995-12-22 1998-01-16 Inst Francais Du Petrole Catalyseur de combustion et procede de combustion utilisant un tel catalyseur
FR2743008B1 (fr) * 1995-12-28 1998-01-30 Inst Francais Du Petrole Procede de combustion catalytique a plusieurs zones catalytiques successives
FR2743616B1 (fr) 1996-01-15 1998-02-27 Inst Francais Du Petrole Systeme de combustion catalytique a injection etagee de combustible
FR2743511B1 (fr) * 1996-01-15 1998-02-27 Inst Francais Du Petrole Procede de combustion catalytique a injection etagee de combustible
JPH1052628A (ja) * 1996-06-07 1998-02-24 Toyota Motor Corp ディーゼルエンジンの排ガス浄化用触媒装置
NL1004051C2 (nl) * 1996-09-17 1998-03-18 Gastec Nv Katalytische stralingsbrander.
DE69939011D1 (de) 1998-03-09 2008-08-14 Osaka Gas Co Ltd Verfahren zur entfernung von methan aus abgasen
GB2354587B (en) * 1999-08-06 2003-10-22 Sanyo Electric Co Battery unit
DE10329162A1 (de) * 2003-06-27 2005-01-13 Alstom Technology Ltd Katalytischer Reaktor und zugehöriges Betriebsverfahren
US7444820B2 (en) * 2004-10-20 2008-11-04 United Technologies Corporation Method and system for rich-lean catalytic combustion
DE102014110534A1 (de) * 2014-07-25 2016-01-28 Continental Automotive Gmbh Verfahren zur Erzeugung einer Diffusionssperrschicht auf einem Metallblech und bei einer Abgasbehandlungseinheit
UA111056C2 (uk) * 2015-10-19 2016-03-10 Компанія "Палметіно А.Т." Спосіб ефективного спалювання палива без доступу атмосферного повітря та пристрій для його здійснення

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GB1469527A (en) * 1973-03-30 1977-04-06 Atomic Energy Authority Uk Manufacture of catalysts
JPS60243549A (ja) * 1984-05-05 1985-12-03 ゲゼルシヤフト、フユール、ゲレーテバウ、ミツト、ベシユレンクテル、ハフツング ガスの触媒燃焼用のセンサの製造方法
EP0198948A3 (en) * 1985-04-11 1988-09-21 Nippon Shokubai Kagaku Kogyo Co., Ltd Catalytic combustor for combustion of lower hydrocarbon fuel
US4870824A (en) * 1987-08-24 1989-10-03 Westinghouse Electric Corp. Passively cooled catalytic combustor for a stationary combustion turbine

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ES2121004T3 (es) 1998-11-16
AU9143891A (en) 1992-06-25
EP0558669A1 (en) 1993-09-08
JP3364492B2 (ja) 2003-01-08
CA2096951A1 (en) 1992-05-27
TW198743B (ko) 1993-01-21
RU2161755C2 (ru) 2001-01-10
ATE171258T1 (de) 1998-10-15
EP0558669A4 (ko) 1994-01-19
KR100261783B1 (ko) 2000-07-15
DE69130225T2 (de) 1999-04-08
DE69130225D1 (de) 1998-10-22
JPH07500659A (ja) 1995-01-19
WO1992009849A1 (en) 1992-06-11

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