IMPROVED LAYERED CATALYST COMPOSITION

Abstract: A catalyst composition contains a catalytic material having an undercoat layer containing a mixture of a fine particulate undercoat refractory metal oxide and a sol such as a silica sol, the undercoat providing good adherence to substrates, such as metal substrates, on which the catalytic material is disposed. An overlayer is coated over the underlayer and contains an overlayer refractory metal oxide, which may be the same as or different from the undercoat refractory metal oxide, and on which is dispersed one or more catalytic metal components, such as palladium and manganese components. The metal substrate may be made of, e.g., aluminum or titanium or alloys thereof, and provides a low pressure drop and lightweight catalyst, making the catalyst especially well adapted for use in aircraft to abate ozone in cabin air. A method of making the catalyst composition includes applying the undercoat to the substrate and calcining it, impregnating the overlayer refractory metal oxide with one or more catalytic metal components and depositing the overlayer over the undercoat, and calcining it.

Description: IMPROVED LAYERED CATALYST COMPOSITION BACKGROUND OF THE INVENTION Field of the Invention The present invention relates to an improved catalyst comj.osition comprising a layered catalytic material dis¬ persed on a substrate, the catalytic material containing one or more catalytic metal components, and to a method of making the catalyst composition. More particularly, the present invention relates to a catalyst composition as aforesaid comprising an undercoat on which is dispersed an overlayer comprising at least one catalytic metal compo¬ nent, for example, a palladium catalytic component. The catalyst composition of the present invention is particu¬ larly well suited for the abatement of ozone and other noxious substances in an airstream. Description of Related Art U.S. Patent 4,206,083 of J.C. Chang discloses the co-precipitation of platinum, palladium and manganese ox¬ ide on a ceramic support, such as a cordierite support, in order to provide a catalyst suitable for the reduction of ozone content of air intended for human respiration. The Chang Patent refers to U.S. Patent 3,269,801 as evidence that it had been long recognized that ozone is present in the atmosphere in toxic concentrations at altitudes of about 9 to 46 kilometers. Aircraft flying at those alti¬ tudes scoop in cabin air from the outside atmosphere which, because it is very much compressed, is raised in temperature to several hundred degrees Centigrade. Such air is treated to reduce the ozone concentration of it to below 1 part per million ("ppm") to render it fit for use as cabin air. U.S. Patent 5,187,137 to S. Terui et al discloses an ozone abatement catalyst comprising a composition contain¬ ing manganese oxide and metallic palladium and/or palla¬ dium oxide as the essential ingredients, formed as a thin film on a support. The method of preparing the catalyst includes coating on a support a slurry containing manga¬ nese oxide, metallic palladium and/or a palladium com¬ pound, and an inorganic oxide sol as a binder, for exam- pie, an alumina sol, silica sol, titania sol or zirconia sol. See column 2, line 53 through column 3, line 5 and column 4, lines 16-19. At column 3, line 62 to column 4, line 3, the Terui et al Patent discloses that the support, i.e., the substrate on which the catalytic material is disposed, may be a cordierite or other similar inorganic support, or it may be a metal support. U.S. Patent 4,900,712 of A. Bar-Ilan et al discloses a catalytic washcoat in which one or more catalytically active non-noble metal oxides ("dopants") such as iron ox- ide are deposited from neutral aqueous colloidal solutions thereof onto preformed high surface area crystalline alu¬ mina. The neutral colloidal compounds are said to provide a uniform, thin coating of the non-noble dopants on the alumina particles and to avoid the use of noxious elements such as nitrates or chlorides, thereby substantially elim¬ inating any air pollution hazard. See the paragraph bridging columns 3 and 4 of the Patent, and column 5, lines 23-26. The reference to eliminating air pollution hazards appears to be with reference to the manufacture of the catalyst, see column 1, lines 29-41. U.S. Patent 4,343,776 issued to W.F. Carr discloses an ozone abatement catalyst containing at least one plati¬ num group metal (platinum, palladium or rhodium) or cata¬ lytically active compound thereof and an oxide or alumi- nate of at least one non-precious Group VIII metal (iron, cobalt or nickel). By applying the non-precious metal oxide as an alumina slip prior to application of the plat¬ inum group metal component to the substrate, the platinum group metal, e.g., palladium, is preferentially exposed to the ozone. See column 2, line 53 to column 4, line 19. The carrier or support, i.e., the substrate, may be any one of a wide range of materials, including aluminum, as described at column 2, line 56 to column 3, line 3. U.S. Patent 5,250,489 to R.A. Dalla Betta et al dis¬ closes a catalyst structure configured to provide heat ex¬ change in which the support, i.e., substrate, is a metal¬ lic support which may comprise aluminum or aluminum al- loys, provided the latter are used at temperatures which will not deform or m^lt the material. See column 6, lines 16-22. However, other materials, including aluminum-con¬ taining steels, are preferred (column 5, line 46 et seq) . U.S. Patent 5,080,882 of M. Yoshimoto et al discloses an ozone decomposition catalyst disposed on a thin porous carrier (substrate) material which has micropores of pref¬ erably not less than 30 microns in diameter for ozone abatement, in order to prevent substantial pressure loss. See column 2, lines 5-15. Any suitable known ozone cata- lyst may be utilized, including oxides of manganese, iron, silver, nickel or copper and a noble metal such as plati¬ num or palladium or a mixture of two or more of these. See column 2, line 16 et seq. SUMMARY OF THE INVENTION In accordance with the present invention there is provided a catalyst composition comprising a catalytic ma¬ terial coated on a substrate, in which the catalytic mate¬ rial comprises an undercoat layer and an overlayer. The undercoat layer comprises a mixture of a fine particulate refractory metal oxide and a sol selected from silica, alumina, zirconia and titania sols, and the overlayer com¬ prises a refractory metal oxide support on which is dis¬ persed at least one catalytic metal component. In accordance with another aspect of the present in¬ vention there is provided an ozone abatement catalyst com¬ position comprising a catalytic material coated on a sub¬ strate, in which the catalytic material comprises an un¬ dercoat layer and an overlayer. The undercoat layer com- prises a mixture of a fine particulate undercoat refrac¬ tory metal oxide and a silica sol, and the overlayer com¬ prises an overlayer refractory metal oxide support on which is dispersed a catalytic metal component comprising a catalytically effective palladium component, for exam¬ ple, a palladium component and a manganese component. One aspect of the present invention provides that the undercoat comprises from about 5 to 50 percent by weight of the refractory metal oxide and from about 50 to 95 per¬ cent by weight of the silica sol. Another aspect of the invention provides for the catalyst composition to be a non-chloride composition. Another aspect provides that the catalytic material further comprises a chloride ion scavenger, for example, a silver compound. Yet another aspect of the present invention provides that the sub¬ strate comprises a body having a plurality of gas flow passages extending therethrough, the passages being de¬ fined by walls on which the catalytic material is coated, and the loading of the underlayer does not exceed about 0.3 g/in 3 . Other aspects of the present invention include the following aspects, alone or in combination: the catalytic metal component may comprise a palladium component and a manganese component; the fine particulate refractory metal oxide of the undercoat and the refractory metal oxide of the overlayer may, but need not, be the same refractory metal oxide, for example, a silica-alumina. Yet another aspect of the present invention provides that the substrate may comprise a metal substrate made of a metal selected from the class consisting of aluminum, aluminum alloys, titanium and titanium alloys. A method aspect of the present invention provides a method of preparing a catalyst composition comprising the following steps. An undercoat layer comprising a mixture of a fine particulate undercoat refractory metal oxide and a silica sol is applied to a substrate by contacting the substrate with an undercoat slurry of the undercoat re¬ fractory metal oxide and silica sol in a liquid medium, for example, an aqueous liquid medium, and thereafter heating the applied undercoat to fix it to the substrate. An overlayer comprising an overlayer refractory metal ox¬ ide is applied to the undercoat obtained in the foregoing step by contacting the su ~e containing the undercoat with an overlayer slurry o. "layer refractory metal ox¬ ide particles in a liquid v. ., for example, an aqueous liquid medium, and thereaft ating the applied overlay- er slurry to fix it to the i. coat. At least one cata¬ lytic metal component is apjrl * to the overlayer refrac¬ tory metal oxide. Another aspect of the method of the present invention includes applying the catalytic metal component by impreg- nating the overlayer refractory metal oxide with a solu¬ tion of one or more salts comprising a precursor of one or more catalytic: metal components, for example, a palladium amine salt such as one selected from the group consisting of palladium tetraamine hydroxide and palladium tetraamine acetate or palladium nitrate. As used herein and in the claims, reference to a cat¬ alytic metal component includes any suitable catalytically active form of the component, for example, and without limitation, as the elemental metal, as an alloy and as a metal oxide or other compound. Other aspects of the invention are disclosed in the following description. DETAILED DESCRIPTION OF THE INVENTION AND PREFERRED EMBODIEMENTS THEREOF It is well-known that many suitable substrates (some¬ times referred to in the art as "supports" or "carriers") may be utilized to support catalyst compositions thereon. For example, it is known to utilize substrate bodies, often referred to as "honeycombs", comprising a monolithic body having a plurality of fine, parallel gas flow chan¬ nels extending therethrough. Such substrates may be ex¬ truded from ceramic-like compositions such as cordierite or other similar highly refractory materials. Although such cordierite or other ceramic-like substrates are use¬ ful in many applications, they are heavier than some metal substrates and, because the walls thereof are usually thicker than the walls of metal substrates, cause a higher pressure drop in gases forced through them than do similar catalysts in which the substrate is formed of a metal. Further, cordierite and other such substrate bodies are more susceptible to mechanical and thermal shock damage than are metal substrates. A suitable catalytic material is applied to the sub¬ strate by coating, the gas flow passages of the substrate with the catalytic material. Conventionally, such cata¬ lytic material comprises a fine particulate refractory metal oxide, such as a high surface area alumina, on which is dispersed one or more catalytic metal components. One problem with the utilization of metal substrates is the difficulty of adhering the coating of catalytic ma¬ terial to the metal substrate with sufficient strength to prevent or minimize spalling of the coating of catalytic material from the substrate. The present invention over¬ comes this problem by applying an undercoat layer which comprises a mixture of a fine particulate refractory metal oxide and a sol, such as a silica sol, an alumina sol, a zirconia sol or a titania sol. Such sols tend to shrink and crack upon drying. Further, the catalyst, even if it is not subjected to high temperatures in use, usually must be heated to a high temperature, e.g., 400° to 550°C, to adhere or fix the coating of catalytic material to the substrate. Heating under such conditions tends to aggra¬ vate the shrinkage and cracking of a coating of silica or other sol on the substrate, leaving discontinuities in the coating which will render the coating subject to spalling or flaking off the substrate. The combination of, prefer- ably, a minor amount of a fine particulate refractory met¬ al oxide with the sol has been found to eliminate or at least reduce the tendency of the sol undercoat to crack upon drying and/or heating. Up to about a 1 to 1 weight ratio of the refractory metal oxide to the sol may be used. Thus, the proportion of sol to fine refractory met¬ al oxide in the undercoat may be from about 1 to 20 parts by weight sol (dry solids basis) to one part by weight of undercoat refractory metal oxide. -1- W k hout wishing to be bound by any particular theory, it is lieved that the interspersion of the refractory metal ide in the sol tends to prevent or reduce shrink¬ age a ' racking of the undercoat upon drying and heating of V. 1 layer on the metal substrate. On the other hand, .e addition of minor amounts of sols or binders to the overlayer containing the catalytic metal component, i.e., the catalytically active component, does not improve adhesion of the washcoat to the substrate and may adverse- ly affect the catalytic activity of the composition. Another difficulty encountered with metal substrates is their tendency to corrode, especially if the catalytic material contains significant quantities of chlorides. Therefore, one aspect of the present invention provides that the catalytic material either be substantially chlo¬ ride free or at least comprise a non-chloride composition in which any chlorides present are only those which result from trace impurities in the materials forming the cata¬ lytic composition. Thus, reference herein and in the claims to a catalyst composition which is "a non-chloride composition" means catalyst compositions made of non-chlo¬ ride materials and containing no more than trace quanti¬ ties of chlorides present as impurities. Such trace im¬ purities usually cannot be economically removed. A scav- enger may be utilized in the catalytic material of the present invention, for example in the undercoat layer, to scavenge any trace or residual chloride ions which may be present. Silver compounds such as silver oxide provide a suitable chloride scavenger material by reacting with the chlorides to form a water-insoluble species, silver chlo¬ ride. Ozone abatement catalysts, especially those contain¬ ing a palladium catalytic component, are effective at tem¬ peratures as low as about 100°F (37.7°C), although the rate of ozone abatement is increased if the air or other gas stream being treated is heated to a higher tempera¬ ture. Nonetheless, in some applications it is highly de¬ sirable to have the catalyst composition be effective over a broad range of inlet gas temperatures, on the order of about 100° to 300°F (21.1° to 148.9°C). For effective low temperature operation it is desirable that a high density of the noble catalytic metal, such as palladium, be at- tained in highly dispersed form on the refractory metal oxide support. It has been found that the desired high density of palladium catalytic component is enhanced if the soluble palladium salt used to -impregnate the over- layer refractory metal oxide particles is a solution of a palladium amine salt, such as palladium tetraamine hydrox¬ ide or palladium tetraamine acetate, or palladium nitrate. The use of such salts, especially in combination with a high porosity refractory metal oxide support as described below is found to give higher densities of palladium with improved dispersion on the overlayer refractory metal ox¬ ide than that attainable under similar conditions with other palladium salts, such as palladium acetate or palla¬ dium chloride. Of course, as noted above, palladium chlo¬ ride is preferably not used in any case in order to render the catalyst composition a non-chloride composition and thereby ameliorate or prevent corrosion of metal sub¬ strates on which the catalyst composition is carried. The Substrate As indicated above, metal substrates have certain ad¬ vantages over cordierite or other ceramic-like substrates, including reduced pressure drop and, for certain metals, lower weight per unit of volume. Metal substrates are conventionally made by spiral-winding a flat and corru- gated metal strip into a coil with the corrugations run¬ ning parallel to the longitudinal axis of the coil to pro¬ vide a plurality of fine, parallel gas flow passages ex¬ tending through the metal substrate. The coil is stabi¬ lized to prevent "telescoping" of the spiral-wound metal strips by the utilization of pins or other mechanical fas¬ teners driven through the coil or by brazing or spot or resistance welding the wound metal strip layers to each other. Such brazing or welding may take place either at one or both end faces, throughout the body, or at selected portions of the body, as is well-known in the art. For ozone abatement catalysts intended for use on aircraft in order to abate ozone in air destined for use as cabin atmosphere, it is particularly important that the catalyst be of as low weight as possible. It has been found that a highly satisfactory catalyst of light weight can be made in accordance with the teachings of the pres¬ ent invention by utilizing a metal substrate in which the metal is aluminum or an aluminum alloy such as an alumi¬ num-magnesium alloy. Alternatively, the metal substrate may be made of titanium or a titanium alloy. However, aluminum is lighter than titanium, less expensive and easier to weld or braze in order to form a satisfactory metal substrate. Accordingly, metal substrates made of aluminum or aluminum alloys are, to that degree, prefer¬ red. In particular, an aluminum-magnesium alloy provides greater hardness, strength and corrosion resistance than aluminum, but cannot readily be brazed due to the magne- sium content. Accordingly, aluminum-magnesium alloy metal substrates would have to rely on pins or other mechanical fasteners to provide a rigid metal substrate structure. Generally, any suitable substrate material may be em¬ ployed, including cordierite or other ceramic-like mate- rials, as well as suitable metals other than aluminum, ti¬ tanium and their alloys, such as Inconel metals, e.g., Inconel 625, and suitable stainless steels such as 304, 316 and 404 stainless steels. Generally, the metal sub¬ strates have substantially thinner walls than cordierite or other ceramic-like substrates and yet provide adequate mechanical strength and better resistance to thermal shock than do cordierite or similar substrates, and to that ex¬ tent are preferred. The thinner walls of metal substrates as compared to cordierite substrates assist in reducing the pressure drop sustained by a gas forced through the substrate. The metal strip or foil used to manufacture the metal substrate of the catalyst preferably has a thickness of from about 1 to 3 mils and, in one embodiment, may be con¬ figured to have about 400 cells (gas flow channels) per square inch (62 cells per square centimeter) of end face area. Metal substrates useful in the present invention may be configured to have anywhere from 100 to 600 cells per square inch (15.5 to 93.0 cells per square centimeter) of end face area, preferably from 300 to 500 cells per square inch (46.5 to 77.5 cells per square centimeter). The Undercoat One difficulty which results from the utilization of metal substrates is that of obtaining adequate adherence of the coating of catalytic material to the substrate. This problem may be overcome in accordance with the teach- ings of the present invention by the provision of a highly adherent bonding undercoat over which an overlayer con¬ taining one or more catalytic metal components is applied. A suitable undercoat is made from a low chloride sol which contains less than 50 ppm by weight of chlorides. Other suitable sols such as low chloride alumina, titania and zirconia sols may also be employed in the compositions of the present invention. An undercoat washcoat may be prepared by combining the sol with a fine particulate refractory metal oxide. In order to distinguish the refractory metal oxide used in the undercoat from that which may be used in the overlayer described below, the refractory metal oxide used in the undercoat is in the claims and sometimes herein referred to as the "undercoat refractory metal oxide". The under- coat refractory metal oxide may comprise, for example, particles of a particle size such that 90% by volume of the particles are 2 microns or less in diameter. The re¬ fractory metal oxide particles, for example, activated alumina particles coated with silica, are mixed with the silica sol in an aqueous medium and, optionally, a chlo¬ ride scavenger such as particulate silver oxide may be added thereto. The slurry may contain from about 5 to 50 percent by weight refractory metal oxide particles and from about 50 to 95 percent by weight (dry solids basis) of the sol and the total solids content (dry basis) of the slurry utilized may be from about 10 to 30 percent by weight of the total weight of the slurry. It will be ap- predated that any suitable refractory metal oxide parti¬ cles may be employed, such as activated alumina particles (comprising predominantly gamma-alumina although other phases such as delta and theta are usually present), sili¬ ca particles, zirconia particles or titania particles, or mixtures or composites of one or more of the foregoing. The metal substrate, for example, an aluminum or alu¬ minum alloy substrate, is dipped into the slurry so that the fine gas flow passages of the honeycomb are completely coated by the slurry. Alternatively, slurry may be drawn through the fine gas flow panels by suction. Excess slurry may be blown out of the gas flow channels with com¬ pressed air. The coated substrate may be dried in air and then calcined in air at a temperature of about 300°C to 600°C for a period of from about one-quarter to two hours, in order to fix the undercoat to the substrate. Optionally, the metal strips from which the metal substrate is prepared may be chemically treated or other¬ wise have their surfaces roughened to promote better ad¬ herence between the undercoat and the metal. The Overlayer The catalytic metal component or components are dis¬ persed on the overlayer, which may comprise refractory metal oxide particles which serve as a support on which the one or more catalytic metal components are dispersed. The overlayer is deposited on the undercoat, either di¬ rectly or with an intermediate layer between the undercoat and the overlayer. The refractory metal oxide used in the overlayer may be the same as or different from the refrac- tory metal oxide used in the undercoat. In order to dis¬ tinguish it from the refractory metal oxide used in the undercoat, the refractory metal oxide used in the overlay¬ er is in the claims and sometimes herein referred to as the "overlayer refractory metal oxide". Any suitable re¬ fractory metal oxide, such as any of those identified above as suitable for the undercoat refractory metal ox¬ ide, may be used as the overlayer refractory metal oxide to provide a support for the catalytic metal component or components. Generally, particles of high surface area, e.g., from about 100 to 500 square meters per gram ("m 2 /g") surface area, preferably from about 150 to 450 m 2 /g, more preferably from about 200 to 400 m 2 /g, are de- sired so as to better disperse the catalytic metal compo¬ nent or components thereon. The overlayer refractory metal oxide also desirably has a high porosity of pores up to 1456 Angstroms radius, e.g., from about 0.75 to 1.5 cubic centimeters per gram ("cc/g"), preferably from about 0.9 to 1.2 cc/g, and a pore size range of at least about 50% of the porosity being provided by pores of 50 to 1000 Angstroms in radius. For example, the overlayer refrac¬ tory metal oxide may be a silica alumina comprising from about 1 to 10 percent by weight silica and from about 90 to 99 percent by weight alumina. The overlayer refractory metal oxide may be impreg¬ nated with one or more suitable catalytic metal salts, such as a palladium salt, preferably a palladium amine salt such as palladium tetraamine acetate, palladium tet- raamine hyroxide or palladium nitrate, then dried and cal¬ cined in air. The resulting impregnated refractory metal oxide powder may then be slurried with distilled water and other catalytic metal components may be added to the slur¬ ry. For example, a soluble non-chloride manganese salt, e.g., manganese nitrate, may be added to further impreg¬ nate the overlayer refractory metal oxide powder with a precursor of manganese or manganese oxide. The contents of the overlayer slurry are thoroughly blended and the undercoated substrate is then coated with the overlayer slurry of metal- and/or metal compound-impregnated over- layer refractory metal oxide in a manner similar to that in which the undercoat was applied. The coated substrate is then dried and calcined to provide a catalyst in accor- dance with the present invention. The palladium and man¬ ganese catalytic metal components have been found to be particularly effective for the abatement of ozone in air- streams, even at relatively low operating temperatures. Alternatively, a slurry of the overlayer refractory metal oxide may be coated over the undercoat, dried and calcined and the thus overlayered substrate immersed in one or more solutions of suitable catalytic metal salts, dried and calcined. Obviously, different catalytic metal components may be utilized depending on the intended use of the catalyst. In some embodiments, catalytic metal components which are useful for the abatement of ozone may be supplemented with other catalytic metal components. The palladium and man- ganese oxide components which are preferred for an ozone abatement catalyst may also be useful for other pollut¬ ants. For example, a manganese catalytic component is known to react with hydrogen sulfide and may release the sulfur as sulfur dioxide if elevated temperatures are at- tained. In addition, the oxidation of carbon monoxide and hydrocarbons can take place with a palladium and manganese catalytic component-containing catalyst as the catalyst heats up somewhat during operation. Obviously, heating means may be supplied to heat the catalyst itself or the gas stream being introduced to the catalyst. Carbon mon¬ oxide and hydrocarbons are generated by tobacco smoke so the preferred ozone abatement catalyst of the invention may be employed to treat not only makeup air introduced from outside the aircraft (or other vehicle) but to treat recycled cabin air which might contain the products of to¬ bacco combustion. Generally, the catalysts of the inven¬ tion will find a variety of uses. For example, those em¬ bodiments of the invention useful for ozone abatement may be used to treat not only the cabin atmosphere of air- craft, trains, buses and other vehicles, but to abate ozone in equipment, such as xerographic copy machines, which generate ozone. The catalyst of the present inven¬ tion may also be employed for air handling systems for residences, office and factory buildings, public build¬ ings, hospitals and the like. Such systems can conveni¬ ently include means to heat the air being introduced into the catalyst and/or to heat the catalyst itself in order to enhance conversion efficiency. In air handling sys¬ tems, the substrate on which the catalyst is coated need not be a honeycomb-type carrier or other substrate specif¬ ically configured to support a catalyst, but the catalytic material could be applied to any portion of the air hand- ling system in which the air sustains turbulent flow. Thus, a catalytic material may be applied to the blades of an air handling fan or compressor, to a grill, louvers or other air-directing structure disposed immediately down¬ stream (as sensed in the direction of air movement) from the blades of the fan or compressor, or on other struc¬ tures over which the air of the air handling system is forced in turbulent flow. For applying the catalyst to such structures, for example, fan blades, the fan blades would be sandblasted or otherwise treated to remove any paint or finish and to roughen the surface to accept the catalyst composition to be applied thereto. After such treatment, the fan blades or other structure (louvers, grills, etc.) may be coated, for example, with an under¬ coat and overlayer to provide a catalytic material coating as described elsewhere herein. For an ozone abatement catalyst, the catalyst loading is preferably from about 150 to 250 grams of palladium per cubic foot of catalyst volume. (The catalyst volume is the volume of the finished catalyst and therefore includes the void spaces provided by the fine gas flow passages of the metal substrate. All references herein and in the claims to a grams per cubic foot ("g/ft 3 ") or grams per cubic inch ("g/in 3 ") loading or quantity refer to the weight per unit volume of the catalyst composition, i.e., the catalytic material coated onto the substrate.) The high (150 to 250 g/ft 3 ) loading of palladium catalytic component provides a catalyst which can decompose 90 to 95 percent of the ozone content of a treated gas (air) stream by employing, for example, a five-segment or seven-segment catalyst and an inlet temperature of the gas (e.g., air) of 70° to 100°F (21.1° to 37.7°C). The individual seg¬ ments are from 0.5 to 1.5 inches in length (the length of the gas flow passages) and are desirably spaced apart about 0.063 to 0.25 inches (0.160 to 0.635 centimeters) from each other in order to provide turbulence-inducing empty spaces between adjacent segments to break up laminar flow of the gas being treated. The use of multiple, spaced-apart segments of catalyst is a known expedient in the art. The empty spaces between adjacent catalyst seg¬ ments also promote mixing of the gas stream being treated thereby increasing the effectiveness of the catalytic ac¬ tion, especially at the relatively low temperatures at which ozone abatement is often carried out. The following example illustrates the preparation of an ozone abatement catalyst in accordance with the present invention. Example 1 Preparation of the Undercoat 1. A jet-milled silica-alumina support containing 5.5 weight percent silica dispersed on gamma-alumina par¬ ticles, based on the combined weight of the silica and gamma-alumina is slurried in distilled water. This mate¬ rial was measured as having a surface area of 271 m 2 /g, an average pore radius of 74 Angstroms, and a total porosity of 1.00 cc/g. This material was ball milled to a particle size distribution of more than 90 percent by volume of the particles having a particle size of 2 microns diameter or less. The material is milled to a solids content in ex¬ cess of 30% with approximately 0.5% by weight of acetic acid added on a solids basis. 2. A "chloride-free" silica sol containing less than 10 parts per million by weight ( "ppm") chloride has a par- ticle size of about 200 Angstroms and a 27 to 28% true solids basis. 3. The materials of steps 1 and 2 are blended to- gether in a ratio of three parts by weight of the silica sol (dry solids basis) to one part by weight of the sili¬ ca-alumina support in distilled water to approximately an 18% solids concentration measured at 150° to 200°F. Dis¬ tilled water is added as needed to provide the desired solids content. The viscosity of the resultant undercoat slurry is approximately 80 to 100 cps and the pH is be¬ tween 8 to 9. 4. A series of metal substrates were made of alumi- num and aluminum-magnesium alloys 3003, 5056 and 3104 (al¬ loy numbering system of the American Aluminum Associa¬ tion) . Flat and corrugated metal strips of these metals having a thickness of about 1 to 2 mils were spiral-wound to fabricate cylindrical metal substrates in which the flat and the corrugated strip alternated to provide about 400 cells per square inch (62.0 cells per square cm) of end face area. The metal substrates were about 0.85 inches (2.15 cm) long and 8.2 inches (20.83 cm) in diame¬ ter. The substrates were dipped into the above undercoat slurry and the cells (gas flow passages) were cleared with an air knife to the desired wet weight target. 5. The substrates were then dried with forced air at about 100°C and then calcined at 450°C for 1 hour in air. Following calcination, an air gun was used to remove resi¬ dual particles on the surface of the substrate. These undercoated substrates have a target loading of about 0.25 g/in 3 of an undercoat layer, with a 0.2 to 0.3 g/in 3 ex¬ pected range, the undercoat layer comprising a 3:1 weight ratio of silica sol (dry solids basis) to silica-alumina refractory metal oxide. Preparatic the Overlayer This preparation us- - following materials: pal¬ ladium tetraamine acetat- tion, a silica-alumina re- fractory metal oxide, an .ganous nitrate solution. All solutions are prepared w Λictilled water. 6. A jet-milled silica-alumina powder, the same sil¬ ica-alumina used to prepare the undercoat, serves as the overlayer refractory metal oxide to provide a support for the metal catalytic components. By the incipient wetness technique, the support is impregnated with a solution of palladium acetate, Pd(NH 3 ) 4 (CH 3 COOH) 2 , in distilled water. By "incipient wetness technique" is meant that the amount of palladium tetraamine acetate solution applied to the silica-alumina powder is limited to avoid the formation of a distinct liquid phase, so that although the powder is thoroughly wetted by the solution, a slurry is not formed. The palladium tetraamine acetate solution contains about 12.3 weight percent palladium salt. The palladium salt solution is applied to the silica-alumina powder using a dispensing buret/drop column and is not diluted during the impregnation. After impregnation of the silica-alumina powder with the palladium salt solution, the powder is dried and calcined in a clean furnace at 450°C for one hour in air. The Pd metal loading on the silica-alumina support for this catalyst is targeted at 250 g Pd/ft 3 , the silica-alumina loading is targeted at 1.2 g/in 3 and the MnO loading is targeted at 0.07 g/in 3 . The target over- layer loading is thus about 1.41 g/in 3 , including the Pd. The Pd metal concentration on the silica-alumina support, i.e., on the overlayer refractory metal oxide, was 12.06 weight percent palladium metal. 7. The impregnated silica-alumina powder obtained in step 6 was then slurried in distilled water using a shear mixer and ball mill with a manganous nitrate solution and containing about 21.65% MnO equivalent in distilled water. The resulting overlayer slurry is then blended to approxi¬ mately 32 to 34% solids concentration at 150° to 200°F. Viscosity can range from 200 to 279 cps and the pH range is 4.8 to 5.3 at room temperature. 8. The substrates coated with the underlayer as de¬ scribed above are coated with the overlayer slurry to the desired wet weight target by being dipped into the over- layer slurry after which the cells (gas flow passages) are cleared with an air knife. The coated substrate is then dried and calcined at 450°C for one hour in air. The heating decomposes the palladium salt to Pd or PdO and the manganese salt to an oxide of manganese. The finished catalysts obtained in accordance with Example 1 may be mounted in a conventional manner within a suitable canister, which may be made of a suitable metal such as stainless steel or titanium or a titanium alloy. As is conventional in the art, the canister will normally have truncated cone-shaped inlet and outlet sections with the bases of the cones adjacent the opposite end faces of the cylindrical substrate, to facilitate connecting the canistered catalyst in a pipe or duct through which the air or other gas to be treated is flowed. As indicated above, usually the catalysts of the present invention will be provided in a number of segments, typically five to seven or eight segments spaced apart one from the other and suitably mounted within the canister. As is known in the art, at least with respect to ceramic-type substrate catalysts, a ceramic fiber blanket, such as that sold under the trademark CERABLANKET by Thermal Ceramics or under the trademark DURABLANKET S by the Carborundum Com¬ pany may be employed. Such ceramic blankets are available in several different thicknesses and densities. The ce¬ ramic blanket is wrapped about the exterior surface of the catalyst segments in order to both provide thermal insula¬ tion and help to maintain the segments firmly mounted in place within the canister. As is also known in the art, instead of a ceramic blanket a resilient wire mesh may be utilized. If needed, suitable retaining rings or the like may also be utilized to securely mechanically retain the catalyst segments in place within the canister. By providing an aluminum or aluminum alloy substrate (or a substrate made of another lightweight metal, such as titanium or a titanium alloy) a lightweight catalyst, which is particularly well adapted for use in aircraft by virtue of its low weight, may be attained. By utilizing a thin outer shell made of a strong lightweight metal such as titanium, further weight reductions may be attained. It has been found that the use of, for example, an alumi¬ num or aluminum alloy substrate in a thin gauge titanium metal canister effects a reduction in the weight of the canistered catalyst to about 50 percent of the weight of a comparable conventional cordierite substrate catalyst. Example 2 Catalysts in accordance with the present invention made in accordance with Example 1 but comprising a palla¬ dium catalytic component loading of from 150 to 250 grams per cubic foot and a manganese oxide loading of from 0.03 to 0.30 grams per cubic inch in a catalyst composition having a catalyst bed volume of 331 cubic inches have been found to provide the following conversion efficiencies of ozone to oxygen at the indicated air inlet temperatures to the catalyst. (By conversion efficiency is meant the vol¬ ume percentage of the original amount of ozone present which is converted to oxygen. ) The inlet space velocity was in all cases 131,000 standard cubic feet per minute ("SCFM") (131,000 cubic feet per minute measured at stan¬ dard conditions of temperature (72°F = 22.2°C) and pres¬ sure (one atmosphere). TABLE II Air Stream Percent Conversion Inlet Temp. per Catalyst Stage 70°F (21.1°C) 80-90% 100°F (37.7°C) 99% 200°F (93.3°C) 99% 300°F (148.9°C) 90% Example 3 A comparison was made of an ozone abatement catalyst in accordance with an embodiment of the present invention and a prior art comparative ozone abatement catalyst. The comparative catalyst was prepared as follows. A slurry was made by dispersing in water the silica alumina used to make the overlayer slurry in Example 1, together with man¬ ganese nitrate and a colloidal alumina binder. The alumi¬ na sol was used in an amount equal to 5% by weight of the silica-alumina refractory metal oxide powder. The result- ant slurry was applied to a Corning 400 c/in 2 cordierite 8-10 mil wall monolith substrate by dipping the substrate in the slurry, removing excess slurry with high pressure air, drying at 100°C and calcining at 450°C for 2 hours. The resulting honeycomb had deposited on it 1.53 g/in 3 of silica-alumina/alumina sol and 0.07 g/in 3 of manganese oxide. A solution of Na 2 PdCl 4 and NaHC0 3 was made at a con¬ centration designed to give the catalyst composition units a Pd concentration of 250 g/ft 3 after submerging the coated units in the Pd solution at room temperature for 2 hours. A hot (90°C) sodium formate solution was prepared in a separate tank in which the Pd catalyzed units were placed and reduced for 30 minutes. After the reduction, the units were washed chloride free, as determined by testing the effluent of the wash water with Ag(N0 3 ) 2 . The units were then heat treated at 200°C. This comparative catalyst is designated Catalyst C and has the following composition: 250 g/ft 3 Pd, 0.07 g/in 3 MnO and 1.52 g/in 3 of combined silica-alumina refractory metal oxide and alu¬ mina sol. The catalyst in accordance with an embodiment of the present invention was an aluminum substrate catalyst of Example 1. This catalyst is designated Catalyst I and had the composition set forth in Example 1. Catalysts C and I were tested under the following conditions: air containing 1.5 parts per million by vol¬ ume ozone was introduced into the catalysts C and I at an inlet temperature of 300°F (148.9°C) and a space velocity of 131,000 SCFM. The results shown in TABLE III were attained. TABLE III Catalyst Catalyst C I Ozone Conversion (%) 90 to 93 94.9 Pressure Drop Across the Catalyst (psi) 0.95 0.65 Pd Loading (g/ft 3 ) 250 170 The data show that Catalyst I, the catalyst of the present invention, provided a higher ozone conversion that compar¬ ative Catalyst C despite the fact that Catalyst I con¬ tained a significantly low loading of the palladium cata- lytic component than did Catalyst C. Catalyst I also im¬ posed a significantly lower pressure drop on the airstream being treated than did Catalyst C. Without wishing to be bound by any particular theory it is believed that the combination of the high density of palladium loading (at- tained by utilizing palladium tetraamine salts to impreg¬ nate the overlayer refractory metal oxide) and the porosi¬ ty and high surface area of the overlayer refractory metal oxide results in the increased conversion efficiency at- tained by Catalyst I of the invention. The effect of the undercoat layer on loss of the washcoat (the term "washcoat" refers to the entire coat¬ ing, i.e., the undercoat and the overlayer) from the sub- strate was demonstrated as follows. Example 4 Additional catalyst samples were prepared by follow¬ ing the procedure in Example 1, except that the amount of the slurry solids in the undercoat was adjusted to give loadings as shown in TABLE IV. The application of the overlayer was held constant at 1.5 g/in 3 . The slurries were applied to an aluminum honeycomb having 400 cells per square inch of end face area. Washcoat loss is measured by weighing the catalyst composition units before and af¬ ter exposure to high pressure air flow from an air gun used to remove loose material. From the data it can be seen that the overlayer will have very poor adherence without an undercoat. However, if the undercoat loading is increased above 0.3 g/in 3 , the coating process becomes very difficult. TABLE IV Undercoat Loading Overlayer Loading Total Washcoat g/in 3 q/in 3 Loss % None 1.5 > 50 0.1 - 0.2 1.5 10 0.2 - 0.3 1.5 1 - 2 0.3 - 0.5 1.5 Difficult to coat > 0.5 1.5 Impossible to coat The effect of the manganese catalytic metal component on ozone conversion was demonstrated as follows. Example 5 Following the procedure outlined in Example 1, the undercoat was applied to an aluminum substrate having 400 cells per square inch of end face. The overlayer manga¬ nese oxide loading was varied by changing the amount of manganese nitrate added to the slurry. The study was con¬ ducted with samples containing from no manganese oxide to 0.70 g/in 3 of manganese oxide. Cores 1 inch in diameter by 0.85 inches in length were taken from the catalyst unit and evaluated in a laboratory reactor in a gas stream con¬ taining 2 ppm by volume ozone in air at a space velocity of 20 SCFM. The percent conversion of ozone was noted at different inlet air temperatures. As can be seen from TABLE IV, the addition of manganese to the palladium top¬ coat dramatically increases the catalyst activity at lower temperatures for decomposing ozone. TABLE V Percent Ozone Conversion Manganese Oxide Loading in Gas Inlet Temperature Overlayer g/in 3 100°F 200°F 300°F None 27.5 38.2 40.6 0.025 35.0 40.0 41.9 0.044 33.6 40.0 41.9 0.70 36.3 42.0 44.9 Example 6 To evaluate the effect of different palladium salts on the degree of dispersion of the palladium catalytic metal component, a study was performed in which the Pd catalytic metal precursor used was varied in carrying out setp 6 of the procedure of Example 1. The dispersion of the resultant 12.06% Pd content on the resulting silica- alumina refractory metal oxide powder was measured using a CO chemisorption technique. From TABLE VI it can be seen that the highest dispersions were achieved with palladium nitrate, palladium tetraamine acetate, and palladium tet¬ raamine hydroxide used as the palladium precursors. It should be noted that the palladium nitrate gave variable results due to an exotherm generated during the decomposi- tion which took place during calcining and which proved to be difficult to control. The results presented in TABLE VI represent the best result obtained for palladium ni¬ trate. TABLE VI Palladium Precursor % Dispersion Palladium Tetraamine Nitrate 10 Palladium Citrate Complex '' 12 Palladium Nitrate 30 Palladium Tetraamine Acetate 45 Palladium Tetraamine Hydroxide 65 While the invention has been described with reference to specific preferred embodiments thereof, it will be ap¬ preciated by those skilled in the art that upon a reading and understanding of the foregoing numerous variations to the preferred embodiments may be attained which, nonethe- less, lie within the spirit and scope of the appended claims.

Claims: THE CLAIMS What is claimed is: 1. A catalyst composition comprising a catalytic material coated on a substrate, the catalytic material compribing: (a) an undercoat layer comprising a mixture of a fine particulate refractory metal oxide and a sol selected from the class consisting of one or more of sili¬ ca, alumina, zirconia and titania sols; and (b) an over- layer comprising a refractory metal oxide support on which is dispersed at least one catalytic metal component. 2. An ozone abatement catalyst composition compris¬ ing a catalytic material coated on a substrate, the cata¬ lytic material comprising: (a) an undercoat layer com¬ prising a mixture of a fine particulate undercoat refrac¬ tory metal oxide and a sol selected from the class con¬ sisting of one or more of silica, alumina, zirconia and titania sols; and (b) an overlayer comprising an overlayer refractory metal oxide support on which is dispersed a catalytic metal component comprising a catalytically ef¬ fective palladium component. 3. The composition of claim 1 or claim 2 wherein the undercoat layer comprises from about 5 to 50 percent by weight of the fine particulate refractory metal oxide and from about 50 to 95 percent by weight of the sol. 4. The composition of claim 3 wherein the sol is a silica sol. 5. The composition of claim 4 wherein at least one of the undercoat and overlayer refractory metal oxides comprises activated alumina. 6. The composition of claim 4 wherein at least one of the undercoat and overlayer refractory metal oxides comprises a silica-alumina. 7. The composition of claim 1 or claim 2 wherein the catalyst composition is a non-chloride composition. 8. The composition of claim 7 wherein " the catalytic material further comprises a chloride ion scavenger. 9. The composition of claim 1 or claim 2 wherein the substrate comprises a body having a plurality of gas flow passages extending therethrough the passages being defined by walls on which the catalytic material is coated, and the loading of the underlayer does not exceed about 0.3 g/in 3 . 10. The composition of claim 7 wherein the catalytic metal component comprises a palladium component and a man¬ ganese component. 11. The composition of claim 1 or claim 2 wherein the fine particulate refractory metal oxide of the undercoat and the refractory metal oxide of the overlayer are the same refractory metal oxide. 12. The composition of claim 8 wherein the refractory metal oxide is a silica alumina comprising from about 5 to 50 percent by weight silica and from about 50 to 95 per¬ cent by weight alumina. 13. The composition of claim 9 wherein the refractory metal oxide has a porosity of from about 0.75 to 1.5 cc/g, of pores of up to 1456 Angstroms in radius. 14. The composition of claim 1 or claim 2 wherein the particulate refractory metal oxide of the undercoat layer is of a size such that at least 90 percent by volume of the particles have a diameter of not more than about 2 microns. 15. The catalyst composition of claim 1 or claim 2 wherein the substrate comprises a metal substrate made of a metal selected from the class consisting of aluminum, aluminvm alloys, titanium and titanium alloys. 16. The catalyst composition of claim 1 or claim 2 wherein the sol is a silica sol. 17. The composition of claim 1 or claim 2 wherein the catalytic metal component comprises a palladium component and a manganese component. 18. The catalyst composition of claim 1 or claim 2 wherein the catalytic metal component comprises a palladi¬ um component dispersed on the overlayer refractory metal oxide by impregnating the overlayer refractory metal oxide with a palladium salt selected from the group consisting of palladium tetraamine salts and palladium nitrate. 19. The catalyst composition of claim 18 wherein the palladium salt is selected from the group consisting of palladium tetraamine hydroxide and palladium tetraamine acetate. 20. The catalyst composition of claim 18 containing from about 150 to 250 g/ft 3 of the palladium component. 21. The catalyst composition of claim 20 wherein the catalyst composition further comprises a manganese compo¬ nent. 22. A method of preparing a catalyst composition com¬ prising: (a) applying to a substrate an undercoat layer comprising a mixture of a fine particulate undercoat re¬ fractory metal oxide and a sol selected from the group consisting of silica, alumina, zirconia and titania sols by contacting the sμbstrate with an undercoat slurry of the undercoat refractory metal oxide and the sol in a liquid medium and thereafter heating the applied undercoat to fix it to the substrate; (b) applying to the undercoat obtained in step (a) an overlayer comprising an overlayer refractory metal oxide, by contacting the substrate con¬ taining the undercoat with an overlayer slurry of over- layer refractory metal oxide particles in a liquid medium and thereafter heating the applied overlayer slurry to fix it to the undercoat; and (c) applying at least one catalytic metal compo¬ nent to the overlayer refractory metal oxide. 23. The method of claim 22 wherein step (c) is car¬ ried out by impregnating the overlayer refractory metal oxide with a solution of one or more salts comprising a precursor of one or more catalytic metal components. 24. The method of claim 22 or claim 23 wherein the catalytic metal components comprise a palladium component and, optionally, a manganese component. 25. The method of claim 23 wherein the precursor com¬ prises a palladium salt selected from the group consisting of palladium tetraamine salts and palladium nitrate. 26. The method of claim 25 wherein the precursor is selected from the group consisting of palladium tetraamine hydroxide and palladium tetraamine acetate. 27. The method of claim 22 wherein the liquid medium of the undercoat slurry is an aqueous medium and the liq¬ uid medium of the overlayer slurry is an aqueous medium and further comprising impregnating the overlayer refrac¬ tory metal oxide with one or more palladium salts selected from the group consisting of palladium tetraamine salts and palladium nitrate to provide the catalytic metal com¬ ponent.

Inventors: DETTLING JOSEPH C, GALLIGAN MICHAEL P, DETTLING, JOSEPH, C., GALLIGAN, MICHAEL, P.
Applicants: ENGELHARD CORP, ENGELHARD CORPORATION
Application year: 1995
Main classification: B01J37
IPC codes: B01D53, B01J23, B01J37