fig1 to 3 show some embodiments of the invention for the case that the hydrolysis catalyst and reduction catalyst are applied in the form of superimposed layers onto the channel walls of the flow channels of the honeycomb . in the figures there is shown a schematic representation of the structured catalyst including a channel wall ( 1 ) of the inert honeycomb , a reduction layer ( 2 ) and a hydrolysis layer ( 3 ), which stands in direct contact with the exhaust gas . the honeycomb has an inlet face ( 4 ) and an outlet face ( 5 ). in fig1 both coatings are uniformly applied over the entire length l of the honeycomb . fig2 in contrast , shows an embodiment in which the hydrolysis layer ( 3 ) is applied only over 50 % of the length of the honeycomb starting from the inlet face . fig3 shows the same arrangement as fig2 but the rear half of the reduction layer was additionally coated with , for example , vanadium pentoxide ( 6 ). the coating concentrations necessary to fulfill the task of catalysis are between about 50 and 250 grams of catalysis per liter of catalyst body ( g / l ) for the reduction catalyst . the hydrolysis catalyst is used in concentrations from 10 to 160 , preferably 40 to 120 g / l . below 10 g / l the hydrolysis activity is to low , while above 160 g / l the reduction layer lying under the hydrolysis layer can no longer fully develop its activity . an aqueous coating dispersion was prepared from the powdered coatings to make the coatings . the inert carrier can be provided with a layer of the corresponding substances , for example , by immersion into this coating dispersion . after application of the coating dispersion the coating is dried and is usually calcined at temperatures between 200 and 600 ° c . for a time of 1 - 5 h . after this , additional active components can be applied to the coating by impregnation with solutions of suitable precursor compounds . the techniques that are used in this case are well known to the specialist . after the application of the first reduction layer the hydrolysis catalyst is applied in the same way . the hydrolysis layer can also be applied to the face of the inlet face by spraying it one or more times . in this case the coating concentration of the hydrolysis catalyst decreases continuously from the inlet phase along the catalyst body until it is zero . by varying the amount of coating or by controlled spraying of selected regions of the face , which is exposed to a high aerosol or exhaust gas load in operation , the concentration of the coating of the hydrolysis layer can be matched to the distribution of the aerosol of the compound that can be hydrolyzed to ammonia over the cross section of the exhaust gas stream . in each case according to the case of application , it can be enough to coat only about 10 to 90 % of the inlet face with the hydrolysis catalyst . high - surface - area materials like active aluminum oxides and titanium dioxide in anatase form with specific surfaces ( measured in accordance with din 66132 ) between 40 and 300 m 2 / g are preferably used as powdered solids . aluminum oxide and titanium oxide can be thermally stabilized by suitable additions such as lanthanum oxide , barium oxide , tungsten oxide , silicon oxide , molybdenum oxide and niobium oxide . suitable materials are commercially available . in applying the hydrolysis layer care must be taken that this layer allows sufficient diffusion of the nitrogen oxides to the reduction layer . optionally , the porosity of this top layer can be increased by adding particularly coarse solids or other pore - forming agents . the following examples serve for further illustration of the invention . the materials listed below were used to make the catalysts . the precise composition of the catalyst can be found in table 1 . anatase ; bet surface & gt ; 80 m 2 / g ( dt 51 from rhone 1 . 1 wt % fe 2 o 3 ; modulus = 28 1 . 5 wt % fe 2 o 3 ; modulus = 30 length , 62 cm − 2 cell density and wall thickness of 0 . 2 mm an aqueous coating dispersion with a solid content of 40 wt % was prepared to produce the catalyst k 1 in accordance with the invention . the dispersion contained 80 wt % titanium dioxide and 20 wt % aluminum oxide , with respect to dry weight . then a honeycomb of type a was coated with the oxide mixture by immersing it in the coating dispersion , after which it was dried in a stream of air at 120 ° c . and calcined in air for one hour at 500 ° c . the coating concentration applied in this way was 160 g / l of honeycomb . in a second step the coated honeycomb was coated with 5 g v 2 o 5 per liter , 26 g wo 3 / l and 3 g nb 2 o 5 / l . for this the honeycomb was impregnated with a solution of the precursor compound vanadyl oxalate , ammonium metatungstate and niobium - ammonium complex . the impregnated oxide precursors were decomposed after air drying at 120 ° c . in a stream of air at 500 ° c . over a period of one hour . this completed the preparation of the reduction layer . in another step the honeycomb was coated again with an oxide coating ( hydrolysis layer ) of tio 2 / wo 3 ( 80 wt %) and aluminum oxide ( 20 wt %) by means of a second coating dispersion . the amount of coating applied in this step was 60 g / l of support . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined for a period of one hour at 500 ° c . in air . to make catalyst k 2 in accordance with the invention , a titanium oxide powder was first impregnated with vanadyl sulfate corresponding to a v 2 o 5 content of 5 wt % by the method of pore volume impregnation . the impregnated material was dried for 15 h at 120 ° c . and then calcined for 3 h at 400 ° c . in air . the resulting tio 2 / v 2 o 5 powder was processed with aluminum oxide to form a coating dispersion ( 80 wt % tio 2 / v 2 o 5 and 20 wt % al 2 o 3 ) and applied in a concentration of 160 g / l to a honeycomb . the oxide coating was dried for 30 min at 120 ° c . in a stream of air and then calcined for 1 h at 500 ° c . in air and then calcined for 1 h at 500 ° c . in air . to prepare the reduction layer , the honeycomb was coated with 26 g wo 3 per liter ( from ammonium metasulfate ) and 3 g nb 2 o 5 / l ( from niobium - ammonium complex ) by impregnation with soluble precursors . the decomposition of the impregnated oxide precursors took place , after drying at 120 ° c . in a stream of air , at 500 ° c . for 1 h . in another step the hydrolysis layer described in example 1 was applied . to make the catalyst k 3 in accordance with the invention , tio 2 / wo 3 was impregnated with a v 2 o 5 content of 3 . 2 wt % by spraying with an alkaline ( ph = 8 to 11 ) solution of ammonium metavanadate in a mixer . the resulting wet powder was then calcined in air for 3 h at 400 ° c . then a honeycomb support was coated with the oxide mixture of tio 2 / v 2 o 5 / wo 3 ( 80 wt %) and aluminum oxide ( 20 wt %) ( reduction layer ). the amount of coating applied in this way was 180 g / l of support . the oxide coating was dried in a stream of air for 30 min at 120 ° c . and then calcined in air for 1 h at 500 ° c . in another step the hydrolysis layer described in example 1 was applied . to make the catalyst k 4 in accordance with the invention , first la 2 o 3 - stabilized titanium dioxide ( 10 wt % la 2 o 3 ) was impregnated by the pore volume impregnation method with vanadyl oxalate corresponding to a v 2 o 5 content of 3 . 2 wt % and with ammonium metatungstate corresponding to a wo 3 content of 10 wt %. the impregnating material was dried for 15 h at 120 ° c . and then calcined in air for 3 h at 400 ° c . then a honeycomb support was coated with the oxide mixture of tio 2 / v 2 o 5 / wo 3 / la 2 o 3 ( 80 wt %) and aluminum oxide ( 20 wt %) ( reduction layer ). the applied amount of coating was 180 g / l of support . the oxide coating was dried in a stream of air for 30 min at 120 ° c . and then calcined in air for 1 h at 500 ° c . the hydrolysis layer described in example 1 was applied in another step . to make the catalyst k 5 in accordance with the invention , first titanium dioxide was impregnated by pore volume impregnation with ammonium polymolybdate corresponding to an moo 5 content of 5 . 5 wt %. the impregnated material was dried for 15 h at 120 ° c . and then calcined in air for 4 h at 480 ° c . then a honeycomb support was coated with the oxide mixture of tio 2 / moo 3 ( 80 wt %) and aluminum oxide ( 20 wt %) ( reduction layer ) the applied amount of coating was 180 g / l of support . the oxide coating was dried in a stream of air for 30 min at 120 ° c . and then calcined in air for 4 h at 300 ° c . in a second step the coated support was then impregnated with 5 g v 2 o 5 ( from vanadyl oxalate ) and 3 g ( nb 2 o 5 ( from niobium - ammonium complex ) per liter of support . the impregnated oxide precursors were decomposed , after air drying at 120 ° c . in a stream of air for 2 h at 500 ° c . in another step the hydrolysis layer described in example 1 was applied . another catalyst was made as in example 3 ( catalyst k 6 ). the coating amounts of the reduction layer and the hydrolysis , however , were each adjusted to 120 g / l of support . a support was provided with the reduction layer of example 3 . a hydrolysis layer of titanium dioxide ( 80 wt %) and aluminum oxide ( 20 wt %) was applied to this layer ( catalyst k 7 ). the amount of coating applied in this step was 60 g / l . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined in air for 1 h at 500 ° c . a support was provided with the reduction layer of example 3 . a hydrolysis layer of aluminum silicate was applied to this layer ( catalyst k 8 ). the amount of coating was 60 g / l of support . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined in air for 2 h at 300 ° c . a support was provided with the reduction layer of example 3 . a hydrolysis layer of aluminum silicate and tio 2 / wo 3 in a 1 : 1 ratio by weight was applied to this layer . the amount of coating of the hydrolysis layer was 60 g / l of support . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined in air for 2 h at 300 ° c . a support was provided with the reduction layer of example 3 . a hydrolysis layer of sulfatized zirconium oxide ( 80 wt %) and aluminum oxide ( 20 wt %) was applied to this layer . the amount of coating was 60 g / l of support . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined in air for 2 h at 500 ° c . a support was provided with the reduction layer of example 3 . a hydrolysis layer of high surface area silicon dioxide ( aerosil ®; 80 wt %) and aluminum oxide ( 20 wt %) was applied to this layer . the amount of coating was 60 g / l of support . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined in air for 2 h at 500 ° c . another catalyst was made in accordance with example 3 . a ceramic honeycomb of type b was used as support . another catalyst was prepared as in example 3 . a metallic honeycomb of type c was used as support . another catalyst was prepared as in example 3 . the hydrolysis layer , however , was applied only over 50 % of the length of the support starting from the inlet face of the honeycomb . another catalyst was prepared as in example 1 . after calcining the hydrolysis layer the catalyst was coated in an additional step with 0 . 5 g v 2 o 5 ( from vanadyl oxalate ) per liter of support only over 50 % of the length of the honeycomb starting from the outlet face . the impregnated oxide precursors were decomposed , after drying at 120 ° c . in a stream of air , for 1 h at 500 ° c . another catalyst was prepared in accordance with example 3 . however , the reduction layer was additionally post - impregnated in an additional step with 2 g v 2 o 5 / l of support ( from vanadyl oxalate ) over 50 % of the length of the honeycomb starting from the exit face . the hydrolysis layer was applied only over 50 % of the length of the honeycomb starting from the inlet face . the impregnated oxide precursors were decomposed , after drying at 120 ° c . in a stream of air for 1 h at 500 ° c . a tio 2 / wo 3 / v 2 o 5 complete extrudate with a cell density of 31 cells per cm 2 and a wall thickness of 0 . 35 mm was coated with a coating of tio 2 / wo 3 ( 80 wt %) and aluminum oxide ( 20 wt %) ( hydrolysis layer ) for catalyst k 17 in accordance with the invention . the amount of coating applied in this step was 60 g / l of support . then the coating was dried in a stream of air at 30 min at 120 ° c . and calcined in air for 2 h at 500 ° c . to produce the catalyst k 18 in accordance with the invention , an aqueous coating suspension with a solids content of 40 wt % was prepared . the dispersion contained , with respect to dry weight , 80 wt % fe zsm - 5 ( modulus 28 , 1 . 1 wt % fe 2 o 3 ) and 20 wt % aluminum oxide . then a honeycomb of type a was coated with the oxide mixture by immersing it in the coating suspension and it was then dried at 120 ° c . in a stream of air . this was followed by a 4 - hour calcination at 300 ° c . in air . the amount of coating applied in this way ( reduction layer ) was 180 g / l of support . in an additional step the support was coated with the hydrolysis layer in accordance with example 1 . the amount of coating applied in this step was 60 g / l of support . to prepare the catalyst k 19 in accordance with the invention , an aqueous coating dispersion with a solids content of 40 wt % was prepared . the dispersion contained , with respect to dry , 80 wt % fe mordenite ( modulus 30 , 1 . 5 wt % fe 2 o 3 ) and 20 wt % aluminum oxide . then a honeycomb was coated with the oxide mixture by immersing it in the coating dispersion and drying it in a stream of air at 120 ° c . this was followed by a 4 - hour calcination at 300 ° c . in air . the amount of coating applied in this way ( reduction layer ) was 120 g / l of support . in an additional step the coated support was again provided with an oxide coating of aluminum silicate ( hydrolysis layer ). the amount of coating applied in this step was 80 g / l of support . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined for 2 h at 300 ° c . in air . an additional catalyst was prepared as in example 1 . after calcination of the reduction layer the face of the catalyst body was coated in an additional step with an oxide coating ( hydrolysis layer ) of tio 2 / wo 3 ( 80 wt %) and aluminum oxide ( 20 wt %). the coating dispersion was sprayed evenly over the entire inlet face by means of a paint spray gun . the amount of coating applied in this step was 40 g / l of support with respect to the sprayed element of volume . then the coating was dried for 30 min for 120 ° c . in a stream of air and calcined for a period of 1 h at 500 ° c . in air . an additional catalyst was prepared as in example 22 . after drying the hydrolysis layer the face of the catalyst was sprayed again in an additional step with the coating dispersion for the hydrolysis layer . however , a template was used to coat only a central region of the inlet face ( about 50 % of the total area ). the amount of coating applied in this step was 20 g / l of support with respect to the sprayed element of volume . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined in air for a period of 1 h at 500 ° c . an additional catalyst as in example 1 was prepared . after calcining the reduction layer , the face of the catalyst body was again coated in an additional step with an oxide coating ( hydrolysis layer ) of tio 2 / wo 3 ( 80 wt %) and aluminum oxide ( 20 wt %). the additional coating was applied by brief immersion of the catalyst body in the coating dispersion and then blowing it out from the outlet face . the depth of immersion was only 10 millimeters . the amount of coating applied in this step was 30 g / l of support with respect to the coated element of volume . then the coating was dried in a stream of air for 30 min at 120 ° c . and calcined in air for a period of 1 h at 500 ° c . further variations and modifications of the foregoing will be apparent to those skilled in the art and are intended to be encompassed by the claims appended hereto . german priority application 100 22 842 . 9 is relied on and incorporated herein by reference .