Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
  • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
  • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
  • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
  • F05B2230/00—Manufacture
  • F05B2230/60—Assembly methods
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
  • F05B2230/00—Manufacture
  • F05B2230/60—Assembly methods
  • F05B2230/604—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
  • F05B2230/606—Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation

Definitions

• This invention relates to improved support structures for securing monolithic catalyst structures used in high temperature reactions, such as catalytic combustion, within a reaction chamber or reactor.
• the present invention is directed to a method for using the improved support structure in high temperature catalytic processes, like catalytic combustion for gas turbine power plants.
• a variety of high temperature processes are known which employ monolithic catalyst structures to promote the desired reactions, for example partial oxidation of hydrocarbons, complete oxidation of hydrocarbons for emissions control, catalytic mufflers in automotive emissions control and catalytic combustion of fuels for further use in gas turbines, furnaces and the like.
• Typical of such catalytic systems are the catalysts used in thermal combustion units for gas turbines to provide low emissions and high combustion efficiency. To achieve high turbine efficiency, a high gas temperature is required.
• the catalyst monolith employed which is typically a unitary or bonded metallic or ceramic structure made up of a multitude of longitudinally disposed channels for passage of the combustion gas mixture, with at least a portion of the channels being coated on their internal surfaces with a combustion catalyst.
• the high gas flow rates characteristic of combustion units in gas turbines place a significant axial load or force on the catalyst structure pushing in the direction of the gas flow due to the resistance to gas flow, i.e., friction, in the longitudinally disposed channels of the catalyst structure.
• a multistage monolithic catalyst structure such as that described in U.S. Patent No. 5,183,401 to Dalla Betta et al. is employed as a 20 inch diameter catalyst in a catalytic combustion reactor where air/fuel mixture flow rate is about 50 lbs/second at a pressure drop through the catalyst of 4 psi
• the total axial load on the catalyst would be about 1 ,260 lbs.
• an uncooled support structure constructed out of high temperature resistant metal or ceramic which can serve as a superior means for securing a monolithic catalyst structure, comprising a multiplicity of longitudinally disposed channels for passage of a flowing gas mixture, within a reactor designed for high temperature reactions and high gas flow rates or through puts, without creating an undue pressure drop or otherwise interfering with the catalytic reaction.
• This uniquely effective support structure comprises a monolithic honeycomb or open cellular support structure having cellular openings at least as large as the channels in the catalyst structure, said cellular openings being in fluid communication with the catalyst structure channels and being formed by thin strips or ribs of high temperature resistant metal or ceramic that are bonded together to afford a unitary structure which abuts against and extends over the entire outlet face of the catalyst structure, with its peripheral edge being secured to the reactor wall in a manner so that any axial force placed on the open cellular support structure will be transferred to the reactor wall.
• the monolithic honeycomb or open cellular support structure of the invention possesses sufficient strength when secured to the reactor wall to withstand the axial load or force placed on it by the catalyst structure operating at high temperatures and at high gas flow rates, such that any axial movement or deformation of the catalyst structure is minimized.
• the inherent strength of the open-celled structure allows for the use of rather thin strips or ribs of metal or ceramic in the structural framework and this, coupled with the use of open cells which are at least as large as the catalytic reactor channel openings, enables the support structure of the invention to be used advantageously in high gas flow rate applications where pressure drop across the support structure is to be avoided, e.g., catalytic combustion of a fuel/air mixture for subsequent use in a gas turbine.
• honeycomb -like or open-celled nature of the support structure of the invention provides a multiplicity of support strips or ribs which abut against the catalyst structure over its entire end face or cross-section, and therefore, the axial load of the catalyst structure is spread more uniformly over the entire monolithic support structure and localized deformations in the catalyst structure are avoided.
• the monolithic open-celled support structures of the invention are most desirably placed at the outlet end or side of the catalyst structure to secure the catalyst structure against axial movement in the direction of gas flow through the catalyst structure, their very low resistance to gas flow through the support structure also makes them attractive candidates for supporting the inlet side of the catalyst structure against any backward movement in the event of sudden gas flow upsets.
• the support structure of the invention can be placed at the outlet end of one or more of the catalyst stages and thus function as an interstage support relieving axial force on subsequent catalyst stages.
• one aspect the invention is directed to a support structure for securing within a reaction chamber a catalyst structure made up of a multiplicity of longitudinally disposed channels with inlet and outlet ends for passage of a flowing gas mixture, said support structure comprising a monolithic open cellular structure wherein the walls of the cells are formed by strips of a high temperature resistant metal or ceramic material to afford cellular openings which are at least as large as the openings formed by the catalyst structure channels at their inlet and outlet ends, said monolithic open cellular structure being:
• Another aspect of the invention is focused on an improved process for catalytic combustion or partial combustion of a fuel which is particularly applicable to gas turbine applications, wherein the monolithic open cellular support structure of the invention is utilized to secure the combustion catalyst structure within the combustor or reaction chamber.
• This process comprises the steps of:
• aspects of the invention include a method for securing the monoHthic catalyst structure in a reactor or reaction chamber using the monoHthic open ceUular structure of the invention and support structures according to the invention used as interstage supports for multistage catalytic processes employing monoHthic catalysts. 97/47926
• FIG. 1 is a side view of a catalytic combustion reactor in a gas turbine combustor.
• FIG. 2A and 2B depict the fabrication of a monoHthic catalyst structure which may be usefully secured within a reactor using the monoHthic support structure of the invention.
• FIGS. 3A and 3B show component parts and a partial cross-section of the inventive support structure.
• FIGS. 4A through 4E depict end views of various configurations of the inventive catalyst support structure.
• FIGS. 5, 6, 7 and 8 are schematic representations of catalytic reactors according to the invention.
• FIGS. 9A and 9B show schematically the effects of axial load due to high gas flow through the catalyst structure on the inventive support structure.
• This invention comprises an uncooled support structure for securing the position of a monoHthic catalyst structure within a reaction chamber or reactor where the catalyst structure is subject to high temperatures and large axial loads due to high gas flow rates through the catalyst.
• this invention is directed to a method using this support in a catalytic combustion process. More particularly, this invention is directed to a support structure which Hmits the axial movement of a relatively flexible monoHthic catalyst structure within a combustion reactor. In addition to Hmiting the axial movement of the catalyst structure, the support structure increases the strength of the catalyst against the force imposed by the gas flow through the catalyst.
• FIG. 1 A typical catalytic combustion reactor is shown in FIG. 1.
• a catalyst structure (10) is positioned in a combustion reactor (1) downstream of a preburner (4) and perpendicular to the flow of an oxygen- containing gas, typically an air and fuel mixture, the fuel being introduced to the monoHthic catalyst structure via fuel injector (5).
• the catalyst structure is positioned in this manner to obtain a uniform flow of air/fuel mixture through the catalyst, and to allow the mixture to pass through passageways which extend longitudinally through the catalyst structure.
• the "outlet side” (9) of the catalyst structure is the side where the partiaHy or completely combusted air/fuel mixture exits the catalyst structure. Therefore, the “inlet side” of the catalyst structure is the side where the uncombusted air/fuel mixture is initially introduced to the catalyst structure.
• the catalyst structure can be made according to any of the weU-known designs, particularly monoHthic catalyst structures comprising a multipHcity of parallel longitudinal channels or passageways at least partiaHy coated with catalyst. Typical catalyst structures are disclosed in a variety of pubHshed references including U.S. Patent Nos.
• the catalyst structure may be fabricated from a metalHc or ceramic substrate in the form of honeycombs, spiral roUs of corrugated sheet, columnar (or "handful of straws") or other configurations having longitudinal channels or passageways permitting high gas space velocities with minimal pressure drops across the catalyst structure.
• a spiral catalyst structure such as that illustrated in FIG. 2A and 2B may suitably be used.
• This structure is fabricated by crimping a sheet of metal foil (20) into a corrugated or wavy pattern with depressions (21) and ridges (22) and then rolling it together with a fiat metal sheet (24) to form a large spiral (25) of alternate layers of corrugated sheet (20) and flat sheet (24) as a cyHndrical unit.
• the corrugated and/or flat sheets are typicaUy coated on one or both sides with a platinum group metal, preferably paUadium and/or platinum, prior to being rolled together to form the spiral catalyst structure.
• While the illustrated catalyst structure involves a metal foil corrugated in a straight channel structure combined with a flat foil, other suitable spiral catalyst structures include those obtained when two or more corrugated foils having straight or herringbone corrugation patterns are wound together in non-nesting fashion.
• the catalyst structure supports of the invention are particularly useful in the case of metal spiral catalyst structures since they have a tendency to telescope or deform in the direction of gas flow when exposed to high gas flow rates at temperatures which are sufficiently high, e.g., 1,000°C or more, to soften or otherwise weaken the metal structure.
• the support structure of the invention is comprised of a monoHthic open ceUed or honeycomb-like structure formed by thin strips or ribs of high temperature resistant metal or ceramic which abuts against one end of the catalyst structure, and extends in a direction perpendicular to the longitudinal axis of the catalyst structure to essentially cover an end face (at either the inlet end or outlet end or both) of the catalyst structure with the support structure being secured on its periphery to the reactor waU.
• the strips or ribs making up the support structure are bonded together to form a unitary structure having cellular openings at least as large as the catalyst structure channel openings.
• the cellular openings in the support structure are also positioned to be in fluid communication with the channels of the catalyst structure thus affording essentiaUy unaltered gas flow from the catalyst structure through the support structure.
• the support structure of the invention surprisingly shows a high level of structural integrity and strength in resisting the axial force placed to it by the catalyst structure's tendency to move or deform in the direction of gas flow through the catalyst structure.
• a typical pressure drop through the catalyst of 4 psi can result in an axial load or force in the direction of gas flow of about 600 to about 1,600 lbs.
• the support structures of the invention show only very minimal flexing or bowing and any locaHzed deformation of the catalyst structure is essentially eHminated due to the uniform nature of the support provided by the multiple strips or ribs making up the open-ceUed support monoHth.
• the support structures of the invention have the dual advantage of being able to support a rather large axial load while stiU having a very open structure with very low resistance to gas flow through the structure.
• the monoHthic open ceUular support structure of the invention can be either ceramic or metalHc as weU as any other structural material which is designed to provide significant structural integrity and strength under high temperatures and high loads.
• High temperature resistant metallic materials which can be usefuUy employed in the support structures of the invention include high temperature resistant steel alloys such as nickel, cobalt or chromium alloys or other alloys rated for the required temperature service as weU as inter-metalHc materials and metal-ceramic composites. Of course, different materials can be employed depending on the location of the support structure and the temperature and axial force to which it wfll be subjected.
• a support structure employed at the inlet end of the catalyst structure will not be subject to the same temperatures and forces that are appHed to the outlet end of the final catalyst stage and therefore the materials of construction can be different.
• Preferred metalHc materials of construction include FeCrAI alloys which typically contain about 20% Cr and about 5% Al with the balance being Fe such as Alfa TV available from AUegheny Ludlum (Pittsburgh, Pennsylvania), RiverHte R20-5SR from Kawasaki Steel (Kobe, Japan) and Aluchrom Y from VDM (Werdohl, Germany).
• NiCrAl aUoys nickel based super alloys containing about 20% Cr and about 5% Al with the balance being Ni, such as Haynes 214 from Haynes International (Kokomo, Indiana).
• Suitable ceramic materials include Celcor cordierite from Corning Glass Works (Corning, New York) and Cordierite monoHthic substrates available from NGK Locke, Inc. (Southfield, Michigan).
• the support structure of the invention can be constructed or fabricated using any conventional technique for forming monoHthic honeycomb-like structures, made up of strips or ribs of ceramic or metallic material which are bonded together to form a unitary structure.
• the structure can be cast as a single unit in the appropriate mold or the structure can be formed by bonding together a series of strips or ribs which have been previously molded or bent to afford the desired ceUular opening configuration when they are bonded together.
• FIGS. 3A and 3B iUustrate the fabrication of a portion of a support structure according to the invention wherein the structure is a metal monoHth having hexagon-shaped ceUular openings.
• This support structure is made up of thin metal strips (30) which have been formed into corrugated strips having flat surfaced ridges (31) and vaUeys (32). These corrugated strips are laid together to form the hexagonal or honeycomb structure shown in FIG.
• the iUustrated honeycomb-Hke structure can be surrounded on its periphery with a circular strip of the metal (not shown) which is bonded to the peripheral portions of the honeycomb in the same fashion as the corrugated strips making up the honeycomb are bonded together.
• a circular strip of metal or metal frame is employed to give the support structure a circular cross-section which is essentiaUy co-extensive with the cross section of the cyHndrical catalyst structure in a direction perpendicular to the gas flow through the catalyst structure.
• brazing In cases where metal strips make up the support structure, it is preferable to use a brazing technique to bond the strips to one another since this appears to give a stronger, more unitary structure than welding does, however the use of welding as a method of bonding the strips together is not precluded. Welding and brazing may also be used in combination as the method of bonding the strips together.
• the ceUular openings in the support structure of the invention may have a variety of shapes provided they are reasonably uniform in cross-sectional area and aUow for sufficient contact between adjacent strips or ribs defining the edges of the ceUular openings that a strong bond between the strips or ribs can be created.
• the ceUs of the open ceUular structure can be polygonal, elliptical or circular in shape, with polygonal ceUs in the shape of trapezoids, triangles, rectangles, squares or hexagons being preferred.
• the ceUular openings are of a hexagon shape from a standpoint of ease of manufacture and the strength of bonds which can be created between adjacent strips or ribs. In this regard, FIGS.
• FIG. 4A through 4E iUustrate end views of several different open ceU configurations which may be usefully employed in the support structure of the invention for a cyHndrical catalyst structure Hke that shown in FIG. 2B.
• FIG. 4A shows the cross-section of a support structure having hexagonal ceUular openings (40) surrounded by and bonded to the circular strip (41) which frames the support structure whUe
• FIG. 4B shows a simUar cross-section for a support structure having square ceUular openings (42) surrounded by a circular frame (43).
• FIG. 4C iUustrates the cross-section of a support structure according to the invention in which the ceUular openings (44) are circular in shape again in a circular frame (45).
• FIGS. 4D and 4E show support structures of the invention having trapezoidal ceUular openings (46) or triangular ceUular openings (48) surrounded in each case by a circular frame (47) and (49).
• the ceUular openings in the support structure of the invention regardless of their specific shape, be sized such that they are at least as large in cross-sectional area as the cross- sectional area of the individual longitudinal channels making up the catalyst structure.
• the ceUular openings are from 1.1 to 200 times as large as the catalyst structure openings which are in fluid communication with the ceUular openings to minimize pressure drop or other flow disruption problems.
• the open ceUs or ceUular openings of the support structure of the invention wiU have an average ceU size or cross-sectional area of from about 0.03 in 2 to about 2.0 in 2 with average ceU sizes in the range of about 0.05 in 2 to about 0.2 in 2 being most preferred.
• the thickness of the strips or ribs making up the support structure of the invention (defined as the cross-sectional dimension of any individual strip measured in a direction perpendicular to the gas flow) and the width of the strips or ribs making up the inventive support structure (defined as the dimension of the strip measured longitudinaUy in the direction of gas flow) will be determined by a variety of factors relating to the size of the reaction chamber and catalyst structure and the process parameters under which the support structure wiU be used.
• the metal or ceramic strip thickness will depend on the flow blockage (pressure drop) which can be tolerated, the axial load to be supported, the diameter of the catalyst structure, the ceU size of the open ceUular structure and the anticipated temperatures which wiU be encounted in use.
• the width of the support structure according to the invention wiU be dependent on factors such as the axial load to be supported, the size of the catalyst structure, the anticipated temperature which will be encountered and the space aUowed in the reaction chamber for the support structure.
• the strips or ribs making up the support structure should be from about 0.5 to about 20 times as thick as the waUs of the longitudinaUy disposed channels of the catalyst structure.
• the strip thickness is preferably between about 1 to about 10 times as thick as the catalyst channel waUs and for ceramic structures the strip or rib thickness is between about 2 to about 20 times as thick as the channel waUs of the catalyst structure.
• the strip thickness of metal support structures of the invention suitably range between about 0.0001 in. to about 0.10 in. with metal strip thickness of between about 0.002 in. and 0.03 in. being preferred and from about 0.005 in. to about 0.02 in. being most preferred.
• metal strip width in the support structure of the invention of between about 0.25 in. to about 3 in., whereas if a ceramic support structure is employed the strip or rib width is suitably between about 0.75 in. and about 4 in. In each case, however, the specific width and thickness selected will depend to some degree on the local stresses and the actual yield and creep strength of the material of construction selected.
• the thickness of the strips or ribs which make up the support structure of the invention coupled with the ceU density or ceUular opening size in the structure have a direct effect on the extent to which the gas flow to or from the catalyst structure is blocked by the support structure.
• these factors are controUed so that the flow blockage provided by any single support structure according to the invention is less than about 25 percent.
• the flow blockage is between about 5 and 15 percent so as to not unduly disrupt the gas flow properties of the gaseous reaction mixture.
• the flow passages in the support structure are preferably straight channels with relatively smooth waUs to minimize turbulence in the gas flow and to obtain the lowest resistance to gas flow.
• FIGS. 5, 6 and 7. Typical appHcations of the support structure of the invention in catalytic reactors are shown in FIGS. 5, 6 and 7.
• FIG. 5 which depicts a single stage catalytic reactor, such as that utilized in catalytic combustion systems
• the gaseous reaction mixture (50) is passed into the catalytic reactor having a reaction chamber defined by the reactor waU (51), which in the case of a catalytic combustor would be the combustor Hner waU, and containing a catalyst structure (52) comprising a multipHcity of paraUel longitudinal channels for passage of the gaseous reaction mixture.
• the catalyst structure is secured within the reaction chamber by means of the monoHthic open ceUular support structure of the invention (53) which is secured to the reactor waU by means of a Hp or ridge (54) that is attached to or part of the reactor waU and protrudes in an inward direction forming a ledge on which the outside or peripheral edge of the support structure sets or rests. In this manner, any axial load placed on the support structure by gas flow through the catalyst structure is transferred from the support structure to the reactor waU.
• FIG. 6 illustrates a simflar reaction system except a two-stage catalytic reactor is employed.
• the gaseous reaction mixture (60) again flows into a catalytic reactor having a reaction chamber defined by the reactor waU (61) but in this case there are two monoHthic catalyst structures (62) and (63) comprising a first and second stage catalytic reaction system and in each case the catalyst structure is secured in the reaction chamber by means of a support structure of the invention (64) and (65) positioned to abut against the outlet end or face of each of the two catalyst structures.
• FIG. 7 shows a two stage catalytic reactor with no interstage support but which is secured at its inlet side and on its outlet side with the support structure of the invention.
• the gaseous reaction mixture (70) is passed into a catalytic reactor having a reaction chamber defined by the reactor waU (71) and containing a multistage catalyst comprising two catalytic monoHths (72) and (73) which abut against each other, each having a multipHcity of paraUel longitudinal channels which are in fluid communication with channels in the other catalyst stage.
• the two stage catalyst structure is secured within the reaction chamber by means of the support structure of the invention which is placed at both the outlet end (74) of the second stage of the catalyst structure and the inlet end (75) of the first stage of the catalyst structure to essentiaUy sandwich the catalyst structure within the reaction chamber and secure it from axial movement in either direction.
• Both the support structure at the outlet end and the support structure at the inlet end of the two stage system are secured by a Hp or ridge (76) and (77) which extends inwardly from the reactor waU thus serving to transfer any axial force to the reactor waU.
• an inwardly protruding Hp or ridge on the reactor waU on which the support structure of the invention rests or sits has clear operating advantages over, for example, actuaUy welding or otherwise fixing and immobilizing the periphery of the support to the reactor waU.
• the ridge or Hp can accommodate support structures which do not extend aU the way to the reactor waU thus affording a free space to accommodate the thermal expansion of the support which can occur on contact with the hot gas flow.
• the support structure of the invention is sized and a ridge or Hp is used such that the support can expand by up to 2% of its diameter in a peripheral direction without pressing against or contacting the reactor waU.
• the Hp or ridge on the reactor waU on which the downstream or outlet side of the support structure rests or sets as shown in FIGS. 5, 6 and 7 can be dupHcated in a position immediately before the inlet side or surface of the support structure to, in effect, form a slot in which the support structure can fit but stiU have the freedom to undergo thermal expansion.
• FIG. 8 An alternate but preferred method of securing the support structure of the invention to the reactor waU is shown in FIG. 8 which iUustrates a single stage catalytic reactor in which the gaseous reaction mixture (80) is passed 97/47926
• the support structure which does not extend aU the way to the reactor waU is, attached to the reactor wall by means of rivets (84) which extend through the reactor waU into a series of cavities in the support structure which are sufficient in depth to aUow for thermal expansion of the support structure on exposure to the hot reaction gas. That is, the rivet penetrates into the support structure for a sufficient length to hold the support structure securely whUe leaving an adequate open area at the end of the rivet to aUow for differential thermal expansion of the support structure.
• one of the important and surprising advantages of the support structure of the invention is the superior strength which it exhibits when subject to high axial loads or forces as a result of high gas flows through the monoHthic catalyst structure which it supports. That is, when a high axial load is placed on the support structure, the support structure will show a tendency to flex or bow in the same direction as the axial force is being exerted and in the case of the support structure of the invention, a surprising resiHence to such bowing or deformation is observed even when the structure is subject to high thermal stress in addition to high axial loads. For the support structures of the invention this is LUustrated by FIGS.
• FIG. 9A and 9B showing a catalytic reactor where the catalyst structure (90) is secured within the reaction chamber waU (91) by means of the support structure of the invention (92) at the outlet side of the catalyst structure, which support structure, in turn, is secured to the reactor waU by means of a Hp or ridge (93) protruding inwardly into the reaction chamber.
• the gas flow (94) through the catalyst structure is such that the axial force exerted on the support structure causes a deflection or bending of the support structure (shown in exaggerated form in FIG. 9B) in the direction of gas flow.
• this deflection can be expressed and quantified as the deformation index for any given support structure
• the "deformation index” is defined as the ratio (numeric) of the deflection or bowing in the support structure which occurs at a standard or typical load from axial gas flow on the catalyst, that is, 4 psi, which is typical for catalytic combustion appHcations, divided by the length of the diameter (or approximate diameter for non-circular supports) of the support structure.
• the deflection or bowing is measured as shown in FIG. 9B as the difference between the bow in the support in an unstressed condition versus the bow which occurs under the standard axial load, i.e., 4 psi.
• this deformation index is suitably between about 0.00001 and about 0.05 and preferably in the range of about 0.001 to about 0.02.
• the support structure of the invention can be used in a process for the catalytic combustion of a hydrocarbonaceous or other combustible fuel, e.g., methane, ethane, H2 ⁇ r CO/H2 mixtures.
• a hydrocarbonaceous or other combustible fuel e.g., methane, ethane, H2 ⁇ r CO/H2 mixtures.
• an oxygen-containing gas such as air
• This oxygen/fuel mixture is passed as a flowing gas through a monoHthic catalyst structure that is positioned within a reaction chamber to combust the oxygen/fuel mixture and form a hot, partiaUy or completely combusted, gas product.
• a variety of catalyst structures can be used in this process.
• a catalyst structure having integral heat exchange surfaces as described in U.S. Patent No. 5,250,489, entitled “Catalyst Structure Having Integral Heat Exchange,” or a graded paUadium-containing partial combustion process catalyst as described in U.S. Patent Nos. 5,248,251 and 5,258,349 both entitled “Graded PaUadium- Containing Partial Combustion Catalyst and Process for Using It,” may be used in this invention.
• the process may involve complete combustion of the fuel or partial combustion of the fuel as described in the co-pending appHcation, U.S. Serial No.
• the process may be a multistage process in which the fuel is combusted stepwise using specific catalysts and catalyst structures in the various stages, as described in U.S. Patent No. 5,232,357, entitled “Multistage Process for Combusting Fuel Mixtures Using Oxide Catalysts in the Hot Stage.”
• U.S. Patent No. 5,232,357 entitled “Multistage Process for Combusting Fuel Mixtures Using Oxide Catalysts in the Hot Stage.”
• the above six patents and one patent appHcation are herein incorporated by reference.
• This process also involves stabilizing the position of the catalyst structure in the reaction chamber so as to prevent the axial movement of the catalyst structure.
• the catalyst structure is stabiHzed in the reaction chamber by means of a monoHthic open ceUular structure in which the waUs of the ceUs are formed by strips of a high temperature resistant metal or ceramic material to afford ceUular openings which are at least as large as the openings formed by the catalyst structure channels at their inlet and outlet ends, said monoHthic open ceUular structure being:

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• 1996
  • 1996-06-10 EP EP96921479A patent/EP1009955A1/de not_active Withdrawn
  • 1996-06-10 CA CA002257874A patent/CA2257874A1/en not_active Abandoned
  • 1996-06-10 WO PCT/US1996/009910 patent/WO1997047926A1/en not_active Ceased

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