Catalyst for the oxidation of acrolein and methacrolein to acrylic acid and methacrylic acid, respectively
This is a continuation of application Ser. No. 800,722, filed May 26, 1977, now abandoned. 
    
    
     The present invention relates to a new catalyst for the gas phase oxidation of acrolein and methacrolein to give acrylic acid and methacrylic acid, respectively, in which an active catalyst layer is applied to an inert carrier core. 
     A large number of catalysts containing molybdenum oxide have been disclosed for the gas phase oxidation of acrolein and methacrolein to acrylic acid and methacrylic acid, respectively. As additional activating components, these catalysts in most cases contain vanadium and/or tungsten and may or may not contain iron and/or copper and/or manganese and/or nickel and/or phosphorus as well as niobium and/or tantalum and/or bismuth and/or antimony and/or tin and/or thorium and/or cerium, alkali metals, especially sodium, potassium and cesium, and thallium. Such catalysts are disclosed, for example, in U.S. Pat. No. 3,567,772, Canadian Pat. No. 941,384, British Pat. No. 1,353,864, U.S. Pat. No. 3,773,692, British Pat. No. 1,337,865, British Pat. No. 1,387,776 and German Laid-Open Application DOS No. 2,517,148. They may be represented by the general formula Mo 12  A a  B b  C c  D d  P e  O x  where A is V and/or W, B is Cu and/or Fe and/or Mn and/or Ni and/or Cr, C is Nb and/or Ta and/or Bi and/or Sb and/or Sn and/or U and/or Th and/or Ce, D is Li and/or Na and/or K and/or Rb and/or Cs and/or Tl, and a is from 0.1 to 18, b is from 0 to 8, c is from 0 to 10, d is from 0 to 2, e is from 0 to 5 and x is from 36 to 136. Oxidic catalysts of this nature may be employed for the gas phase oxidation of acrolein and methacrolein, either unsupported or supported, and in the latter case the inert carriers used are mostly aluminum oxides, silicon dioxide and their mixtures, silicon carbide, titanium dioxide and also zirconium dioxide. To manufacture catalysts of this nature, the common procedure is to mix mixtures of aqueous solutions of salts of the components, eg. of ammonium molybdate, ammonium vanadate, ammonium tungstate and nitrates of iron, copper or manganese, and impregnate the carrier with the mixture, from which the water may or may not have been evaporated completely or partially, or to coat the carrier with the composition. If the composition contains water, the material is dried and calcined, after the water has been evaporated off, the calcination being carried out in most cases at above 150° C., especially at from 180° to 600° C. This gives oxide catalysts which carry the active catalyst composition on the inner and/or outer surface of the carrier. A disadvantage of the supported oxide catalysts thus obtained is that they are sensitive to mechanical stresses resulting from friction, as occurs, eg. in the calcination stages of the process of manufacture or when filling reactor tubes. In addition, their activity and selectivity is in many cases not fully satisfactory. Finally, the active composition is frequently not distributed uniformly over the surface of the carrier. The manufacture of supported catalysts by applying a mixture of the active metal oxides to carriers was proposed in British Pat. No. 1,296,922. 
     U.S. Pat. No. 3,956,377 discloses a special process for the manufacture of oxide catalysts, in the form of layers, for the gas phase oxidation of acrolein and methacrolein to acrylic acid and methacrylic acid respectively, in which, for example, molybdenum oxide, vanadium oxide and tungsten metal powder are suspended in water by heating under reflux, the resulting slurry is evaporated and the residue is dried for several days at 115° C. The active catalyst composition thus obtained is then applied to the carrier, which has been pre-moistened with water, the application being effected by tumbling the moist carrier with a powder of the active catalyst. Catalysts manufactured in this way are frequently non-selective. 
     We have found that catalysts for the oxidation of acrolein and methacrolein with oxygen-containing gases to give acrylic acid and methacrylic acid, respectively, which catalysts consist of a conventional molded carrier, the surface of which is coated with an active catalyst composition of the general formula Mo 12  A a  B b  C c  D d  O x , where A is V and/or W, B is Cu and/or Fe and/or Mn and/or Ni and/or Cr, C is Nb and/or Ta and/or Bi and/or Sb and/or Sn and/or Th and/or Ce and/or U, D is Li and/or Na and/or K and/or Rb and/or Cs and/or Tl and a is from 0.1 to 18, b is from 0 to 8, c is from 0 to 10, d is from 0 to 2 and x is from 36.25 to 135 are particularly advantageous if the catalyst composition, before applying to the carrier, is manufactured from thermally easily decomposed salts of the components by mixing aqueous solutions, slurries or moist solid masses of the salts of the components, drying the mixture and calcining the dried composition at from 140° to 600° C., and is comminuted, for example by milling to a particle size of less than 150 μm, and applied, as a mixture with water, as a layer from 10 to 1,500 μm thick, to the premolded carrier, which has a rough surface. 
     Suitable carriers for the manufacture of the new oxide catalysts are the conventional inert carriers, for example highly calcined aluminum oxides (preferably in the α-phase), natural and synthetic silicates and aluminosilicates, eg. mullite and steatite, silicon carbide and zirconium oxides and/or titanium oxides. The inner surface area of the carriers may be varied within wide limits and is in general from less than 1 to 20 m 2  /g, eg. frequently from 1 to 20 m 2  /g, especially from 1 to 10 m 2  /g. The porosity is generally not critical and is mostly from 1 to 65%, and from 50 to 85% of the pores have a diameter of from 20 to 1,500 μm. The carriers are pre-molded in the conventional manner and are preferably spherical, but it is also possible to employ, for example, pre-molded carriers in the shape of rings or cylinders. The mean diameter of the pre-molded carrier is in most cases from 2 to 10 mm, preferably from 2 to 7 mm and especially from 3 to 6 mm. The materials have a rough surface, the recesses being mostly from 10 to 1,500 μm, especially from 20 to 750 μm. 
     Preferred active catalyst compositions for oxidizing acrolein to acrylic acid are those of the formula Mo 12  A a  B b  C c  D d  O x , where A is vanadium and/or tungsten, especially vanadium and tungsten, B is copper, iron, chromium and/or manganese, especially copper, or copper in combination with one or more of the other components B, C is antimony, niobium, tantalum and/or tin, D is lithium, sodium, potassium, rubidium, cesium and/or thallium and a is from 2 to 18, preferably from 0.5 to 12 for vanadium, from 0.2 to 6 for tungsten and from 2.5 to 18 for vanadium+tungsten, b is from 0.5 to 8, and for copper is preferably from 0.5 to 6, especially from 1 to 5, c is from 0 to 10 and d is from 0 to 0.5, preferably from 0 to less than 0.1, and x is from 41 to 127.75. 
     The component of group C as a rule does not improve the catalyst properties as far as the oxidation of acrolein to acrylic acid is concerned. This is also true of the component of group D, and higher concentrations of alkali metal oxides (d&gt;0.5) in general reduce the activity, so that as a rule alkali metals are only present in the active catalyst composition in such concentration in such concentrations as result from using raw materials of commercial purity; for example, commercial grades of ammonium molybdate or molybdic acid of technical catalyst quality frequently contain up to 200, sometimes up to 500, ppm of potassium, whilst technical-grade carriers may contain up to 0.5% by weight of sodium and/or potassium. 
     The starting materials for the manufacture of the active catalyst composition are, in general, thermally easily decomposed salts of the components, of which an intimate mixture is prepared by, for example, mixing their aqueous solutions and then dehydrating the solution and drying the residue. Thereafter, the mixture is converted to the oxides by one or more calcinations at above the decomposition point of the salts and below or at the optimum final calcination temperature, this process being carried out in the absence of the molded carrier. Preferred easily decomposed salts are the ammonium salts of the oxy-acids of molybdenum, vanadium and tungsten, vanadyl oxalate, and the nitrates, oxalates, hydroxides, carbonates, sulfates, acetates and/or formates of the cationic components, of which aqueous solutions are preferably prepared at an elevated temperature, eg. at from 50° to 100° C., and preferably at a pH of from 2 to 6. On mixing, suspensions are in most cases obtained, which can be dried and can then, if necessary after addition of water, be homogenized, eg. by kneading, and densified. The calcination is carried out at from 140° to 600°  C., preferably from 180° to 450° C. and especially from 230° to 420° C. In a preferred embodiment of the manufacture of the catalysts, the dehydrated mixtures of the easily decomposed salts are first calcined at from 180° to 350° C., especially at from 230° to 300° C., and then at from 350° to 600° C., preferably at from 370° to 450° C., and especially at from 380° to 420° C., in air. For the manufacture of certain active catalyst compositions, eg. those containing iron, it is sometimes of advantage to carry out the calcination in an inert atmosphere (eg. nitrogen) or a slightly reducing atmosphere (eg. a gas mixture containing propylene and/or acrolein). 
     After calcining the oxide mixture and comminuting it to a particle size of less than 150 μm, the active catalyst composition, preferably mixed with a wetting liquid which evaporates easily, is applied to the pre-molded carrier, the particle size of the pulverulent active catalyst composition being less than 150 μm, preferably less than 80 μm and especially less than 50 μm. The composition may be applied, for example, by granule coating or spraying the pre-molded, eg. spherical, carrier with a suspension of the active catalyst composition in water, the carrier being at from room temperature, ie. about 20° C., to 300° C. The thickness of the layer of active catalyst composition on the carrier surface should be from 10 to 1,500 μm, preferably from 20 to 750 μm and especially from 50 to 400 μm, corresponding to the finished catalyst containing from about 0.05 to 0.60 kg of active catalyst composition per liter (Bulk volume) of finished catalyst. 
     When applying the active catalyst composition to the premolded carrier it can be of advantage to add small amounts, in general from 0.5 to 20, preferably from 1 to 10, percent by weight of materials which improve the adhesion of the active composition to the carriers. Suitable materials of this nature are inorganic hydroxo salts and compounds which in aqueous solution hydrolyze to give hydroxides by hydroxo complexes and which are catalytically inert or are in any case a constituent of the active catalyst composition. Examples are aluminum chloride, molybdenum sulfide and/or basic aluminum salts, eg. basic aluminum nitrate. However, in the case of the active catalysts having the compositions stated above to be preferred, the addition of such materials is in general not necessary. 
     The carriers coated with the active composition are then dried, if necessary, at below 180° C., preferably below 150° C. In the case of granule coating, the pulverulent active catalyst composition is fed, at constant speed, onto the vigorously agitated, continuously moistened carrier in a rotary mixer or on a granulating disc. 
     The catalysts of the invention are outstandingly suitable for oxidizing acrolein and methacrolein with oxygen-containing gases, under otherwise conventional conditions, to give acrylic acid and methacrylic acid, respectively. The catalysts of the invention are distinguished by a particularly high selectivity and activity when used for the industrial manufacture of acrylic acid by oxidizing acrolein; surprisingly, the selectivity and activity achieved in tubes with diameters useful for production purposes, ie. 15 mm and above, are greater, under comparable conditions, than those achieved with catalysts disclosed in, for example, U.S. Pat. No. 3,956,377. Furthermore, the new catalysts show lower abrasion losses of catalytic composition, for example whilst being packed into a reactor, and have a particularly uniform composition and uniform thickness of the active layer. They are especially suitable for use with high space velocities of greater than 2,000 h -1  and low water vapor concentrations of less than 20% by volume, and with linear gas velocities of greater than 100 cm/sec. especially in tubes having a diameter of from 15 to 40 mm at from 200° to 350°  C. In the case of tubes having diameters greater than 20 mm it can be of advantage to dilute the catalyst with from 10 to 60% by volume of moldings of an inert material or of a catalyst of lower activity, so that in the direction of flow the activity increases from a value of from 40 to 80% of the maximum to 100% of the latter. 
    
    
     In the Examples which follow, parts are by weight, bearing the same relation to parts by volume as one kilogram to the liter. To test the catalytic properties of the catalysts from Examples 1 to 14, 40 ml of one of the catalysts are packed into a tube of 15 mm internal diameter and the tube is then heated to the test temperature in a salt bath. Per hour, 3.4 liters (S.T.P.) of acrolein, 28 liters (S.T.P.) of air, 30 liters (S.T.P.) of nitrogen and 25 liters (S.T.P.) of steam are passed through the tube. The analysis of the off-gas gives the conversions of acrolein and yields of acrylic acid, acetic acid and carbon oxides (CO x ) shown in the Tables. 
     EXAMPLES 1 to 9 
     (Active composition Mo 12  V 4 .6 W 2 .4 Cu 2 .2 O 56 .9 ; various carriers) 
     Manufacture of the catalysts: 
     65 parts of ammonium paratungstate, 54 parts of ammonium metavanadate and 212 parts of ammonium heptamolybdate are dissolved, in this sequence, in 2,500 parts of water at 95° C. A solution of 54 parts of copper nitrate in 125 parts of water is then added, the mixture is evaporated and the residue is dried at 110° C. It is then kneaded, with addition of 50 parts of water, for 31/2 hours, dried for 4 hours at 250° C. in a rotary oven, and calcined for 3 hours at 395° C. The calcined composition is milled to a particle size less than 150 μm. 
     30 parts of the active pulverized catalyst composition mixed with from 10 to 30 parts of water are applied to 100 parts by volume (bulk volume) of magnesium silicate spheres of diameter 3 mm, and then dried at 100° C. (Example 1). To manufacture the catalysts of Examples 2 to 9, 100 parts by volume of the carriers stated for these Examples are used, and in other respects the procedure described above is followed. The catalysts are tested as described above; the results, together with the abrasion loss, are shown in Table 1. The abrasion loss is the proportion of active catalyst composition, in percent by weight of the composition present on the carrier, which is abraded under the following conditions: 50 parts by volume of catalyst are tumbled for 5 minutes at constant speed on a covered disc and the proportion abraded is then sieved off and weighed. 
     
                                           TABLE 1                                 
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                                   Catalyst:                              
                                   parts                                  
                  Carrier          of active                              
     Active            Proportion                                         
                               Inner                                      
                                   composition                            
                                         mean                             
     composition  Open (in %) of                                          
                               surface                                    
                                   per part by                            
                                         thickness                        
     particle size                                                        
                  porosity,                                               
                       macropores of                                      
                               area                                       
                                   volume of                              
                                         of layer                         
Example                                                                   
     in μm                                                             
            Nature                                                        
                  %    20-1,500 μm                                     
                               m.sup.2 /g                                 
                                   carrier                                
                                         μm                            
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1    &lt;80    Mg silicate                                                   
                   0    0      &lt;&lt;1 0.300 130                              
            spheres                                                       
            3-3.5 mm                                                      
2    &lt;80    SiO.sub.2                                                     
                  &gt;50   8      622 0.300 175                              
            spheres                                                       
            3.5 mm                                                        
3    &lt;50    α-Al.sub.2 O.sub.3                                      
                   3   about 50                                           
                                0.04                                      
                                   0.15   70                              
            3-5 mm                                                        
Al.sub.2 O.sub.3ha.                                                       
     34     84    &lt;1   0.300   125                                        
            spheres                                                       
            3-3.5 mm                                                      
5    &lt;80    α-Al.sub.2 O.sub.3                                      
                  34   84      &lt;1  0.300 125                              
            spheres                                                       
            3-3.5 mm                                                      
6    &lt;80    α-Al.sub.2 O.sub.3                                      
                  34   84      &lt;1  0.224 105                              
            spheres                                                       
            3-3.5 mm                                                      
7    &lt;50    α-Al.sub.2 O.sub.3                                      
                  34   84      &lt;1  0.182  90                              
            spheres                                                       
            3-3.5 mm                                                      
8    &lt;80    mullite                                                       
                  25   63      4.5 0.258 215                              
            spheres                                                       
            5-6 mm                                                        
9    &lt;50    mullite                                                       
                  25   63      4.5 0.15  130                              
            spheres                                                       
            5-6 mm                                                        
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 The surface recesses are &lt;10 μm for the carrier of Example 1, &lt;20 μ
 for the carrier of Example 2, from 50 to 250 μm for the carriers of   
 Examples 3 to 7 and from 20 to 300 μm for the carriers of Examples 8  
 and 9.                                                                   
Activity test                                                             
Bath                                                                      
temperature  Conversion                                                   
                    yield, mole %      Abrasion loss,                     
Ex.  °C.                                                           
             mole % acrylic acid                                          
                           acetic acid                                    
                                  CO.sub.x                                
                                       % by weight                        
__________________________________________________________________________
1    289     99.5   93     2      4.5  7                                  
2    275     94.5   84     1.7    8.5  5                                  
3    282     99.1   93     1.6    4.5  2                                  
4    279     97.4   92     1.4    4    3                                  
5    275     98.4   93     0.9    4.5  2                                  
     277     ˜100                                                   
6    295     98.5   92     1.5    5    2                                  
7    298     97.5   91.5   1.2    4.7  0.2-0.7                            
8    284     99     92.9   1.1    5    1.5                                
9    305     96.7   89.5   1.9    5.3  0.5                                
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     EXAMPLES 10 to 14 
     (Catalysts obtained from various active compositions) 
     Catalyst compositions of various constitutions (cf. Table 3) are manufactured by the method described for Examples 1 to 9, using the easily decomposed salts shown in Table 2. After calcining, the active composition is in each case milled to a particle size of less than 80 μm and sprayed, as an aqueous suspension with a weight ratio of active catalyst composition to water of from 1:1 to 1:2, onto the carrier spheres at from 25° to 80° C. The activity of the catalysts is tested as described above and the results are summarized in Table 3 below. 
     
                       TABLE 2                                                     
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                Parts by weight in Example                                
Easily decomposed salt                                                    
                  10     11     12   13   14                              
______________________________________                                    
iron(III) nitrate 44.5   222.   --   --   --                              
Mn-acetate-tetrahydrate                                                   
                  --     --     30   --   --                              
SnO.sub.2         --     --     --   22.5 --                              
Ammonium dichromate                                                       
                  --     --     --   --   7.5                             
Copper(II) nitrate                                                        
                  28.5   54     28.5 28.5 54                              
Ammonium heptamolybdate              212                                  
Ammonium metavanadate                                                     
                  54     35     54   54   54                              
Ammonium paratungstate                                                    
                  65     32.3   65   65   65                              
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                                           TABLE 3                                 
__________________________________________________________________________
                                    Parts of                              
                                    active                                
                                    composi-                              
                                    tion per                              
                   Particle         part by                               
     Active composition                                                   
                   size             volume of                             
Example                                                                   
     formula       μm                                                  
                        Carrier     carrier                               
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10   Mo.sub.12 V.sub.4.6 W.sub.2.4 Cu.sub.1.2 Fe.sub.1.1 O.sub.57.6       
                   &lt;50  α-Al.sub.2 O.sub.3, 3-4 mm,                 
                                    0.3                                   
                        inner surface area                                
                        &lt;1 m.sup.2 /g                                     
                        porosity = 34%                                    
                        proportion of pores                               
                        of 20-1,500 μm = 84%,                          
                        surface recesses from                             
                        20 to 300 μm                                   
11   Mo.sub.12 V.sub.3 W.sub.1.2 Cu.sub.2.2 O.sub.49.3                    
                   &lt;50  α-Al.sub.2 O.sub.3, 3-4 mm,                 
                                    0.3                                   
                        inner surface area                                
                        &lt;1 m.sup.2 /g,                                    
                        porosity = 34%                                    
                        proportion of pores                               
                        of 20-1,500 μm = 84%,                          
                        surface recesses from                             
                        20 to 300 μm                                   
12   Mo.sub.12 V.sub.4.6 W.sub.2.4 Cu.sub.1.2 Mn.sub.1.2 O.sub.57.1       
                   &lt;20  α-Al.sub.2 O.sub.3, 3-4 mm,                 
                                    0.3                                   
                        inner surface area                                
                        &lt;1 m.sup.2 /g,                                    
                        porosity = 34%                                    
                        proportion of pores                               
                        of 20-1,500 μm = 84%,                          
                        surface recesses from                             
                        20 to 300 μm                                   
13   Mo.sub.12 V.sub.4.6 W.sub.2.4 Cu.sub.1.2 Sn.sub.1.2 O.sub.58.3       
                   &lt;20  α-Al.sub.2 O.sub.3, 3-4 mm,                 
                                    0.3                                   
                        inner surface area                                
                        &lt;1 m.sup.2 /g,                                    
                        porosity = 34%                                    
                        proportion of pores                               
                        of 20-1,500 μm = 84%                           
                        surface recesses from                             
                        20 to 300 μm                                   
14   Mo.sub.12 V.sub.4.6 W.sub.1.2 Cu.sub.2.2 Cr.sub.0.6 O.sub.54.2       
                   &lt;20  α-Al.sub.2 O.sub.3, 3-4 mm,                 
                                    0.3                                   
                        inner surface area                                
                        &lt;1 m.sup.2 /g,                                    
                        porosity = 34%                                    
                        proportion of pores                               
                        of 20-1,500 μm = 84%,                          
                        surface recesses from                             
                        20 to 300 μm                                   
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Activity test                                                             
Thickness                                                                 
of layer,  Bath   Conversion,                                             
                         yield, mole %                                    
Ex.  μm temperature                                                    
                  mole % acrylic acid                                     
                                acetic acid                               
                                      CO.sub.x                            
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10   125   298    97     90     1.5   5.5                                 
           302    100    91.5   2     7                                   
11         284    99.4   93     1.6   4.8                                 
12         290    99.3   92     1.1   6.2                                 
13         292    48.2   90.2   1.6   6.1                                 
14         288    98     91     1.4   5.6                                 
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     EXAMPLE 15 
     1,000 ml of a spherical catalyst (sphere diameter about 5.3 mm), manufactured as described in Example 8, were packed into a steel tube of 4 m length and 25 mm diameter and the surrounding salt bath was heated at 286° C. (2nd stage). A catalyst specific for the conversion of propylene to acrolein was packed into an upstream reactor (first stage). This latter catalyst was precipitated by the method of Example 1 of German Laid-Open Application DOS No. 2,338,111, dried, calcined at 300° C., mixed with 2% by weight of graphite powder, molded to give 3×3 mm pellets and calcined for 11/2 hours at 580° C. It has the composition Mo 12  BiIn 0 .1 Fe 2  Ni 6 .5 P 0 .06 Si 10  O 6 .03 and contained, relative to the above formula, 0.05 atom of potassium, as a natural impurity of the ammonium molybdate used as the raw material. The catalyst in the upstream reactor was diluted with 200 ml of  3 mm spheres of magnesium silicate in such a way that the proportion by volume of the catalyst increased linearly in the direction of flow from 60% to 100%. A mixture of 105 liters (S.T.P.) of fresh propylene, 1,000 liters (S.T.P.) of fresh air and 1,200 liters (S.T.P.) of purified off-gas from the second stage reactor was passed hourly over the catalyst of the upstream reactor. The gaseous mixture from the upstream reactor was then passed to the catalyst tube. According to analysis of the material leaving the catalyst tube (second stage), the yield of acrylic acid, based on fresh propylene employed, was 80.8 mole % and the yield of carbon oxides resulting from combustion of acrolein and propylene in the second stage was 3.5 mole %. Based on the acrolein (and acrylic acid) produced in the first stage, the yield of acrylic acid and carbon oxides was calculated to be, respectively, 93 and 3.9 mole %, the acrolein conversion being 98%. 
     EXAMPLE 16 
     The experiment of Example 15 is repeated, except that the second part of the reactor is packed with 832 ml of a catalyst manufactured as described in Example 5. The spherical catalyst (diameter about 3.5 mm) was diluted with 168 ml of 3 mm steatite spheres in such a way that the proportion by volume of the catalyst-coated spheres increased linearly in the direction of flow from 60% by volume to 100%. At a bath temperature of 283° C., yields of acrylic acid and CO of, respectively, 82.3 and 2.5 mole % based on fresh propylene employed, or of 95% and 2.9%, based on acrolein and acrylic acid formed in the first stage, were obtained. The acrolein conversion was 98 mole %. 
     COMPARATIVE EXPERIMENTS 
     (A) 65 parts of ammonium paratungstate, 54 parts of ammonium metavanadate and 212 parts of ammonium heptamolybdate are dissolved, in the stated sequence, in 2,500 parts of water at 95° and a solution of 54 parts of copper nitrate in 125 parts of water is added to the solution, followed by 605 parts of α-aluminum oxide having a particle size of from 40 to 150 μm. The mixture is evaporated whilst being stirred, and is dried and calcined at from 230° to 250° C. Spheres of from 3 to 3.5 mm diameter are molded from the resulting calcined active composition, and are further calcined for 3 hours at 400° C. in air in a rotary oven. The activity of the catalyst (A) is tested as described immediately before Example 1. The results are shown in Table 4 below. 
     (B) 65 parts of ammonium paratungstate, 54 parts of ammonium metavanadate and 212 parts of ammonium heptamolybdate are dissolved, in the stated sequence, in 2,500 parts of water at 95° C., a solution of 54 parts of copper nitrate in 125 parts of water is added and 625 parts of α-aluminum oxide spheres of diameter from 3 to 3.5 mm, of the type described in Example 5, are impregnated with the mixture. They are then dried at 110° C. and calcined for 5 hours at 400° C. in a rotary oven. The catalyst (B) is tested as described immediately before Example 1; the results are shown in Table 4 below. 
     (C) 65 parts of ammonium paratungstate, 54 parts of ammonium metavanadate and 212 parts of ammonium heptamolybdate are dissolved, in the stated sequence, in 2,500 parts by weight of water at 95° C. and a solution of 54 parts of copper nitrate in 125 parts of water is added. 625 parts of α-aluminum oxide spheres of diameter from 3 to 3.5 mm, of the type described in Example 5, are sprayed with the mixture at 100°-110° C., whereupon the water evaporates. The impregnated spheres are then calcined for 4 hours at from 230° to 250° C. followed by 3 hours at 400° C. in a rotary oven. The catalyst obtained is tested as described immediately before Example 1; the results are shown in Table 4 below. 
     (D) Example 5 is repeated except that the particle size of the active composition is from 310 to 600 μm. The catalyst obtained is tested as described immediately before Example 1; the results obtained are shown in Table 4 below. 
     (E) Example 6 of German Laid-Open Application DOS No. 2,526,238 was repeated. To do this, 216 parts of MoO 3 , 34.1 parts of V 2  O 5 , 27.59 parts of tungsten powder, 60.43 parts of Cu (NO 3 ) 2 .3 H 2  O and 8.42 parts of SnO were suspended in 1,000 parts of water and the mixture was boiled under reflux for 20 hours. The suspension was then evaporated and the residue dried for 3 days at 115° C. A coherent dry mass was obtained, which was milled to give a powder. 45 parts of powder were applied to 100 parts of Al 2  O 3  (SA 5.252 Alundum) of mean particle size 1/8 inch. The catalyst was tested as described immediately before Example 1. The results are shown in Table 4. 
     
                       TABLE 4                                                     
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Com-           Activity test                                              
para-  Abrasion                                                           
               Bath                                                       
tive  loss     tempera- Con-   Yield, mole %                              
Ex-   % by     ture     version                                           
                               acrylic                                    
                                     acetic                               
ample weight   °C.                                                 
                        mole % acid  acid  CO.sub.x                       
______________________________________                                    
A     3        275      99     87    3     9                              
B     .sup.(1) 268      97     88    2.3   6.6                            
C     12-15    330      99     87    3     8                              
D     &gt;20.sup.(2)                                                         
               305      97     90.5  1.5   5                              
E     1-3      290      20.5   9     0.8   10.7                           
               320      55.6   42    1.6   12                             
______________________________________                                    
 .sup.(1) A high proportion of the spheres was stuck together by the      
 deposit of active composition, to form larger agglomerates and the       
 catalyst was therefore industrially unusable in this form.               
 .sup.(2) (low adhesion of the active shell)