KR20210049669A - Ammoxidation catalyst for propylene, manufacturing method of the same catalyst, ammoxidation methode using the same catalyst - Google Patents

Abstract

The present invention relates to a catalyst for ammoxidation of propylene, a method for producing the same, and a method for ammoxidation of propylene using the same. In one embodiment of the present invention, the catalyst is implemented in a structure in which metal oxide is supported in a silica carrier, by using mesopores that are useful for adsorption and desorption of gas, a high reaction surface area can be provided, and ultimately, an effect of increasing the ammoxidation reaction of propylene can be obtained.

Description

Catalyst for ammoxidation of propylene, a method for preparing the same, and a method for ammoxidation of propylene using the same

The present invention relates to a catalyst for ammoxidation of propylene, a method for preparing the same, and a method for ammoxidation of propylene using the same.

The ammoxidation process of propylene is based on a reduction reaction of reacting ammonia and propylene and a mechanism of reoxidation by oxygen, the conversion rate of the reactant (i.e., propylene), and the selectivity of the reaction product (i.e., acrylonitrile). And catalysts of various compositions to increase the yield have been studied.

Specifically, since the Mo (molybdenum)-Bi (bismuth) oxide catalyst was presented, catalysts to which metals having various oxidation states were added have been studied in order to increase the catalytic activity and stability. As a result, depending on the type or amount of metal added, the yield of acrylonitrile is improved compared to the initial study.

However, despite the diversification of the catalyst composition, studies on its structure and physical properties were insufficient, and thus the conversion rate of the reactant (i.e., propylene) and the selectivity of the reaction product (i.e., acrylonitrile) were remarkable during ammoxidation of propylene There was a limit to the height of it.

Specifically, it is common to obtain a catalyst having a secondary particle structure in which metal oxide particles and silica particles are aggregated by co-precipitation of a metal precursor having a desired composition and a nano silica sol, followed by spray drying and firing.

More specifically, the catalyst of the secondary particle structure has metal oxide particles evenly distributed inside and outside, but contains almost no internal pores, so that a portion capable of participating in the ammoxidation reaction of propylene is limited to the external surface portion. will be.

The present invention provides a catalyst for ammoxidation of propylene that can participate in the reaction as well as the outer surface portion (ie, the surface of the catalyst) and the inner surface (pores) thereof, and by using such a catalyst, acrylonitrile in a higher yield It is to manufacture.

Specifically, in one embodiment of the present invention, a catalyst for ammoxidation of propylene having a structure in which a metal oxide of a specific composition is supported on a silica carrier, has a large pore size and volume in such a supported state, and has a large BET specific surface area, is provided. to provide.

The catalyst of one embodiment may have a large effective surface area capable of participating in the reaction, and thus may have high catalytic efficiency and reactivity.

Therefore, by using the catalyst of one embodiment, it is possible to prepare acrylonitrile with higher selectivity and yield while converting propylene at a higher ratio.

1 schematically shows a catalyst prepared using coprecipitation and spray drying.
2 schematically shows a catalyst according to the embodiment.
3 is an SEM image (100 magnification) of the catalyst of Example 1.
4 is an SEM image (100 magnification) of the catalyst of Comparative Example 1.

In the present invention, various transformations can be applied and various embodiments may be provided, and specific embodiments will be illustrated and described in detail. However, this is not intended to limit the present invention to a specific embodiment, it should be understood to include all conversions, equivalents, and substitutes included in the spirit and scope of the present invention. In describing the present invention, when it is determined that a detailed description of a related known technology may obscure the subject matter of the present invention, a detailed description thereof will be omitted.

In addition, terms including ordinal numbers such as first and second to be used hereinafter may be used to describe various elements, but the elements are not limited by the terms. The above terms are used only for the purpose of distinguishing one component from another component. For example, without departing from the scope of the present invention, a first element may be referred to as a second element, and similarly, a second element may be referred to as a first element.

Singular expressions include plural expressions unless the context clearly indicates otherwise. In the present application, terms such as "comprise" or "have" are intended to designate the presence of features, numbers, steps, actions, components, parts, or combinations thereof described in the specification, but one or more other features. It is to be understood that the presence or addition of elements or numbers, steps, actions, components, parts, or combinations thereof does not preclude in advance.

Hereinafter, “particle diameter Dv” means a particle diameter at the v% point of the cumulative volume distribution according to the particle diameter. That is, D50 is the particle diameter at 50% of the cumulative volume distribution according to the particle diameter, D90 is the particle diameter at 90% of the cumulative volume distribution according to the particle diameter, and D10 is at 10% of the cumulative volume distribution according to the particle diameter. It is the particle size.

The Dv can be measured using a laser diffraction method. Specifically, after dispersing the powder to be measured in a dispersion medium, it is introduced into a commercially available laser diffraction particle size measuring device (for example, Microtrac S3500) to measure the difference in the diffraction pattern according to the particle size when the particles pass through the laser beam. Yields D10, D50, and D90 can be measured by calculating the particle diameters at the points at 10%, 50%, and 90% of the cumulative volume distribution according to the particle diameter in the measuring device.

Hereinafter, a catalyst for ammoxidation of propylene according to the embodiment will be described in detail with reference to the drawings.

Catalyst for ammoxidation of propylene

In one embodiment of the present invention, a metal oxide represented by the following formula (1) is supported on a silica carrier; In a state in which the metal oxide is supported on a silica carrier, ^{including pores having a diameter of 5 to 200 nm and a volume of 0.1 to 3.0 cm 3} /g, the BET specific surface area is 50 m ² /g to 1000 m ² /g , To provide a catalyst for ammoxidation of propylene:

[Formula 1]

Mo ₁₂ Bi _a Fe _b A _c B _d C _e O _x

In Formula 1,

A is one or more elements of Ni, Mn, Co, Zn, Mg, Ca, and Ba,

B is one or more elements of Li, Na, K, Rb, and Cs,

C is one or more elements of Cr, W, B, Al, Ca, and V, and

Wherein a to e, and x are a fraction of an atom or group, respectively, a is 0.1 to 5, b is 0.1 to 5, c is 0.01 to 10, d is 0.01 to 2, and e is 0 to 10 , x is 24 to 48.

A generally known catalyst for ammoxidation of propylene is prepared through coprecipitation and spray drying, and is provided in a secondary particle structure in which metal oxide nanoparticles and silica nanoparticles are aggregated (FIG. 1).

This is because, instead of evenly distributed inside and outside of the metal oxide particles, a portion that can participate in the ammoxidation reaction of propylene is limited to the outer surface portion (i.e., the surface of the secondary particles), and provides a small surface area. The amount of ammonia desorbed from the catalyst surface during ammoxidation reaction is large.

On the other hand, the catalyst of the embodiment may be prepared by an impregnation method, and thus may be provided in a structure in which a metal oxide is supported on a silica carrier (FIG. 2).

For example, a silica carrier may be immersed in a metal precursor solution prepared to satisfy a stoichiometric molar ratio of a desired metal oxide, and the metal precursor solution may be impregnated in the silica carrier.

Thereafter, when the solvent (i.e., water) is removed through the drying process, the metal precursor remains on the pore walls of the silica carrier, and the metal precursor is oxidized in the firing process to form a film that continuously coats the pore walls of the silica carrier. have.

The catalyst of one embodiment thus prepared may have less fine powder content and superior durability than a catalyst prepared with the same composition through co-precipitation and spray drying, even if the classification process is not performed as a post-treatment after manufacture.

In addition, the catalyst of one embodiment is a catalyst by controlling the metal oxide composition to further include not only Mo and Bi known to increase the activity of the ammoxidation reaction, but also a metal forming an active point of an appropriate level for the ammoxidation reaction of propylene. It can further increase the activity.

Particularly, in the catalyst of one embodiment, the portion capable of participating in the ammoxidation reaction of propylene by evenly supporting the metal oxide in the inner pores of the silica carrier is not only the outer surface portion (i.e., the surface of the catalyst) but also the inner surface (pore ), there is an advantage.

^{Specifically, the catalyst of the embodiment includes pores having a diameter of 5 to 200 nm and a volume of 0.1 to 3.0 cm 3} /g in a state in which the metal oxide is supported on a silica carrier, and a BET specific surface area of 50 m ² /g to 1000 m ² /g.

Compared to a catalyst prepared through coprecipitation and spray drying and having a secondary particle structure, the pore size and volume are significantly larger, and the BET specific surface area directly connected to the effective surface area capable of adsorbing ammonia gas and propylene gas is much. Means wide.

Hereinafter, the catalyst of the embodiment will be described in more detail,

Catalyst structure

The catalyst of the embodiment may include a silica carrier including second pores; An inner coating layer that continuously coats the walls of the second pores and includes a metal oxide represented by Chemical Formula 1; And first pores located inside the second pores and occupying an empty space excluding the inner coating layer.

Specifically, the catalyst of the embodiment may have an egg-shell structure.

To this end, the silica carrier may include a non-porous core portion; And a porous shell portion positioned on the surface of the non-porous core and including second pores.

More specifically, the porous shell includes a concave portion and a convex portion of a surface, and the concave portion has the second pores open to the surface of the porous shell. It may be formed.

Accordingly, the catalyst of the embodiment may include a coating layer that continuously coats the concave portions and the convex portions of the porous shell and includes a metal oxide represented by Chemical Formula 1; And first pores occupying an empty space excluding the coating layer in the concave portion of the silica carrier.

Due to the above structure, by controlling the second pore characteristics of the silica support, it is possible to control the characteristics of the first pores of the final catalyst.

Specifically, the silica carrier on which the metal oxide is not supported has a D50 size of 20 to 400 μm; Including second pores having a diameter of 10 to 200 nm and a volume of 0.1 to 3 cm ^{3 /g;} The BET specific surface area may be 50 to 1000 m ² /g.

More specifically, the D50 of the silica carrier itself without metal oxide has a lower limit of 20 µm or more, 25 µm or more, 30 µm or more, 35 µm or more, 40 µm or more, or 43 µm or more, and the upper limit is It may be 400 µm or less, 300 µm or less, 200 µm or less, 100 µm or less, 80 µm or less, or 70 µm or less.

In addition, the second pores contained in the silica carrier itself not carrying the metal oxide have a diameter of 10 nm or more, 15 nm or more, or 20 nm or more, and 200 nm or less, 100 nm or less, 50 nm or less, 40 Nm or less, or 30 nm or less; The lower limit of the volume is 0.1 cm ³ /g or more, 0.3 cm ³ /g or more, 0.5 cm ³ /g or more, 0.7 cm ³ /g or more, 0.9 cm ³ /g or more, 1.1 cm ³ /g or more, 1.3 cm ³ / g or more, or 1.5 cm ³ /g or more, and the upper limit is 3 cm ³ /g or less, 2.8 cm ³ /g or less, 2.6 cm ³ /g or less, 2.4 cm ³ /g or less, 2.2 cm ³ /g or less, It can be 2.0 cm ³ /g or less, 1.8 cm ³ /g or less, or 1.6 cm ³ /g or less.

In addition, the silica carrier itself, which is not supported with the metal oxide, has a lower limit of the BET specific surface area of 50 m ² /g or more, 100 m ² /g or more, 150 m ² /g or more, 200 m ² /g or more, or 250 m ² /g or more, 1000 m ² /g or less, 900 m ² /g or less, 800 m ² /g or less, 700 m ² /g or less, 600 m ² /g or less, 500 m ² /g or less , 400 m ² /g or less, or 300 m ² /g or less.

In this case, while the metal oxide is supported on a silica carrier, the catalyst of the embodiment has a D50 size of 30 to 200 μm; It includes first pores having a diameter of 5 nm or more and 200 nm or less and a volume of 0.1 to 3.0 cm ^{3 /g;} The BET specific surface area may be 50 to 1000 m ² /g.

More specifically, in a state in which the metal oxide is supported on a silica carrier, the lower limit of the D50 particle size is 30 µm or more, 35 µm or more, 40 µm or more, 45 µm or more, or 50 µm, while the upper limit is 200 µm or less, 190 It may be µm or less, 180 µm or less, 170 µm or less, 160 µm or less, or 150 µm or less.

In addition, in a state in which the metal oxide is supported on a silica carrier, the first pores included in the catalyst of the embodiment have a lower limit of the diameter of 5 nm or more, 6 nm or more, 7 nm or more, 8 nm or more, or 10 nm. With the above, the upper limit can be set to 200 nm or less, 170 nm or less, 150 nm or less, 130 nm or less, or 100 nm or less; While the lower limit of the volume is 0.1 cm ³ /g or more, 0.2 cm ³ /g or more, 0.3 cm ³ /g or more, 0.4 cm ³ /g or more, 0.5 cm ³ /g or more, or 0.6 cm ³ /g or more, the upper limit is It can be 3.0 cm ³ /g or less, 2.7 cm ³ /g or less, 2.5 cm ³ /g or less, 2.3 cm ³ /g or less, or 2.0 cm ³ /g or less.

In addition, in a state in which the metal oxide is supported on a silica carrier, the catalyst of the embodiment has a lower limit of the BET specific surface area of 50 m ² /g or more, 52 m ² /g or more, 55 m ² /g or more, 57 m ² /g or more, or 60 m ² /g or more, and the upper limit is 1000 m ² /g or less, 900 m ² /g or less, 800 m ² /g or less, 700 m ² /g or less, 600 m ² /g Or less, or 500 m ² /g or less.

For reference, the pore diameter and volume before and after the metal oxide is supported refer to the average pore size and volume derived from the BJH equation through a generally known nitrogen adsorption and desorption experiment. The BET specific surface area before and after the metal oxide is supported can be obtained using a generally known BET measuring device.

The BET specific surface area, the diameter and volume of the first pores provided by the catalyst of the embodiment are improved compared to the catalyst of the secondary particle structure, and accordingly, while converting propylene at a higher ratio, with higher selectivity and yield. Acrylonitrile can be obtained.

Within the ranges presented above, the larger the diameter of the first pore, the larger the volume due to this, and the larger the BET specific surface area may be. However, when the diameter and volume of the entire catalyst are the same, the larger the diameter occupied by the first pores, the easier the inflow of propylene as the reactant and the discharge of acrylonitrile as the product improves the reaction characteristics. The occupied volume decreases, and accordingly, the volume occupied by the metal oxide is relatively reduced, thereby reducing the active point, thereby deteriorating the reactivity.

Accordingly, the diameter and volume of the first pores, the diameter and the BET specific surface area of the catalyst pores including the first pores may be controlled by comprehensively considering the characteristics of the desired catalyst.

Of course, the first porosity of the final catalyst may be affected not only by the second porosity of the silica carrier, but also by the amount of the metal precursor solution impregnated in the silica carrier. A detailed description of this will be described later.

Composition of metal oxides

On the other hand, even if it has the same structure as the catalyst of the embodiment, if the type and content of the components constituting the metal oxide do not satisfy the above formula (1), active sites with insufficient or excessively dense ammoxidation of propylene may be formed. have.

Accordingly, it is necessary to satisfy the type and content of the metal oxide to satisfy the formula (1).

In particular, when the metal oxide is represented by the above-described formula 1-1, the effect of increasing the conversion rate by increasing the rate of movement of the lattice oxygen of molybdenum of Fe, and the formation of a complex oxide with molybdenum of Co improves the partial oxidation reaction characteristics of propylene. As a synergistic effect of increasing the effect of increasing and increasing the selectivity of acrylonitrile by dispersing the active point of the complex oxide including molybdenum of K, the activity in the ammoxidation reaction of propylene may be higher:

[Formula 1-1]

Mo ₁₂ Bi _a Fe _b Co _c K _d O _x

In Formula 1-1,

Wherein a to d, and x are the fractions of an atom or group, respectively, a is 0.1 to 5, specifically 0.1 to 2.0, b is 0.1 to 5, specifically 0.5 to 3.0, c is 0.01 to 10 , Specifically 1 to 10, d is 0.01 to 2, specifically 0.01 to 1.0, x may be 24 to 48, specifically 28 to 45.

Metal oxide: weight ratio of silica carrier

The catalyst of one embodiment is a weight ratio of 10:90 to 15:95, specifically 20:80 to 50:50, such as 15:85 to 35:65 of the metal oxide and the silica support (metal oxide: silica support) Can be included as.

Within this range, the catalyst of the embodiment may have high selectivity of acrylonitrile with high activity.

Method for producing a catalyst for ammoxidation of propylene

In another embodiment of the present invention, a method of preparing the catalyst of the above-described embodiment is provided using an impregnation method.

As briefly described above, the catalyst of one embodiment may be prepared through a series of processes in which a metal precursor solution is supported on the silica carrier using an impregnation method, dried and then calcined.

More specifically, as a method of preparing the catalyst of the embodiment,

Preparing a first precursor solution containing a Mo precursor,

Bi precursor, Fe precursor, A precursor (A = one or more elements of Ni, Mn, Co, Zn, Mg, Ca, and Ba), and B precursor (B = one or more of Li, Na, K, Rb, and Cs Element) preparing a second precursor solution,

Mixing the first and second precursor solutions so that the molar ratio of the metal satisfies the stoichiometric molar ratio of Formula 1 below,

Supporting the mixture of the first and second precursor solutions on a silica carrier,

Drying the silica carrier on which the mixture of the first and second precursor solutions is supported, and

There is provided a method comprising the step of firing the dried material:

[Formula 1]

Mo ₁₂ Bi _a Fe _b A _c B _d C _e O _x

In Formula 1,

A is one or more elements of Ni, Mn, Co, Zn, Mg, Ca, and Ba,

B is one or more elements of Li, Na, K, Rb, and Cs,

C is one or more elements of Cr, W, B, Al, Ca, and V, and

Wherein a to e, and x are the fractions of atoms or groups, respectively, a is 0.1 to 5, b is 0.1 to 5, c is 0.01 to 10, d is 0.01 to 2, and e is 0 to 10 , x is 24 to 48.

Manufacturing process of the first precursor solution

The step of preparing the first precursor solution may be a step of dissolving the Mo precursor in water at 20 to 80° C. to prepare a solution including water and the Mo precursor.

In the step of preparing the first precursor solution, an additive including citric acid, oxalic acid, or a mixture thereof may be used.

In the catalyst manufacturing process using coprecipitation and spray drying, the additive functions as a strength modifier. However, in the above embodiment, the additive makes the first precursor solution transparent, so that a mixture precursor in a completely dissolved state can be prepared.

When the additive is added, the weight ratio of the molybdenum precursor and the additive may satisfy 1:0.1 to 1:1, specifically 1:0.2 to 1:0.7, and the solubility of the molybdenum precursor increases within this range. It can be, but is not limited thereto.

Manufacturing process of the second precursor solution

Meanwhile, the second solution may include the remaining metal precursors except for the Mo precursor included in the first precursor solution.

Specifically, the step of preparing the second precursor solution includes essentially a Bi precursor, an Fe precursor, an A precursor, and a B precursor in water at 20 to 50° C., and optionally, a C precursor (Cr, W, B , Al, Ca, and at least one element of V) may be to prepare a second precursor solution further comprising.

More specifically, in the step of preparing the second precursor solution, the type of metal precursor other than the Mo precursor may be selected in consideration of the composition of the metal oxide in the final catalyst.

For example, in consideration of the metal oxide composition satisfying Formula 1-1, a second precursor solution including water, a Bi precursor, an Fe precursor, a Co precursor, and a K precursor may be prepared.

Processes of preparing the first and second precursor solutions are each independent, and the order of preparation is not limited.

Supporting process of the first and second precursor solution mixture in a carrier

After mixing the first and second precursor solutions, they may be supported on a silica carrier.

Here, the silica carrier including the aforementioned second pores is added to the mixture of the first and second precursor solutions, so that the mixture of the first and second precursor solutions is supported in the first pores in the silica support. I can.

Specifically, the size of the D50 of the silica carrier on which the metal oxide is not supported is 20 to 400 μm; It may include second pores having a diameter of 10 to 200 nm and a volume of 0.1 to 3 cm ^{3 /g.}

In addition, the silica carrier on which the metal oxide is not supported itself may have a BET specific surface area of 50 to 1000 m ² /g, specifically 100 to 700 m ² /g.

When using such a silica carrier, the first pores having a diameter of 5 nm or more and 100 nm or less, specifically 10 to 100 nm, and a volume of 0.2 to 3.0 cm ³ /g, specifically 0.2 to 2.0 cm ^{3 /g, are included.} It is possible to obtain a catalyst.

In addition, as described above, the BET specific surface area of the final gun medium may be 50 to 1000 m ² /g, specifically 60 to 500 m ² /g,

Drying process of the carrier carrying the first and second precursor solution mixtures

Drying the silica carrier on which the mixture of the first and second precursor solutions is supported may include first vacuum drying the silica carrier on which the mixture of the first and second precursor solutions is supported at 120 to 160 mbar, and The first vacuum-dried material may be secondarily vacuum-dried at 30 to 50 mbar to obtain a silica carrier on which a mixture of the first and second precursor solutions is supported.

Specifically, the first vacuum drying is performed at 60 to 80° C. for 1 to 2 hours, and the second vacuum drying is performed at 80 to 100° C. for 15 to 45 minutes, whereby the solvent (ie, water) is removed. , Only the first and second precursors may remain on the walls of the first pores.

The material on which the secondary vacuum drying has been completed can be fired immediately, but by tertiary drying at normal pressure, even the solvent (ie, water) remaining after the secondary vacuum drying can be effectively removed.

Specifically, the third drying may be performed at 100 to 150 °C for 20 to 30 hours.

However, this is only an example, and the solvent (ie, water) is removed, and there is no particular limitation as long as it is a drying condition capable of obtaining a carrier on which the first and second precursors are supported.

Final firing process

Finally, the dried material, that is, the carrier on which the first and second precursors are supported, is calcined for 2 to 5 hours in a temperature range of 500 to 700° C. to finally obtain a catalyst.

However, the drying and firing conditions are only examples, and a condition capable of sufficiently removing the solvent from the internal pores of the carrier and oxidizing the metal precursor is sufficient.

Propylene ammoxidation method

In another embodiment of the present invention, there is provided a method for ammoxidation of propylene, comprising reacting propylene and ammonia in the presence of the catalyst of the above-described embodiment in a reactor.

The catalyst of the embodiment has high activity and stability at high temperature, and is used for ammoxidation reaction of propylene to increase the conversion rate of propylene, selectivity and yield of acrylonitrile.

For matters other than the catalyst of the embodiment, it is possible to refer to matters generally known in the art, and thus a detailed description thereof will be omitted.

Hereinafter, embodiments of the present invention will be described in more detail in the following examples. However, the following examples are merely illustrative of embodiments of the invention, and the contents of the present invention are not limited by the following examples.

Example 1

(1) Manufacturing process of precursor solution

10.592 g of Mo precursor ((NH ₄ ) ₆ Mo ₇ O ₂₄ ) and 3.18 g of citric acid were added and mixed in distilled water at 60° C. to prepare a Mo precursor solution.

Independently, in distilled water at room temperature, 1.819 g of Bi precursor (Fe(NO ₃ ) _3· 5H ₂ O), 9.488 g of Co precursor (Co(NO ₃ ) _2· 6H ₂ O), 2.990 g of Fe precursor ( Fe (NO ₃ ) ₂ 9H ₂ O), and 0.354 g of K precursor (KNO ₃ ) were added, 2.16 g of nitric acid (HNO ₃ ) was added and mixed, and Bi, Fe, Co, and K precursors A mixed solution was prepared.

The Mo precursor solution; And the Bi, Fe, Co, and K precursor mixture solution was mixed to complete a precursor mixture solution of Mo, Bi, Fe, Co, and K.

In the precursor mixture solution, the total amount of distilled water is 54.07 g.

(2) Supporting process of precursor solution in silica carrier (using impregnation method)

Silica (SiO ₂ , SP948, Grace) particles with a D50 particle diameter of 55 µm, an internal pore size of 24.4 nm, a BJH pore volume of 1.58 cm ³ /g according to nitrogen adsorption method, and a BET specific surface area of 283 m ^{2 /g} Was used as a carrier.

The silica carrier was added to the precursor mixture solution of Mo, Bi, Fe, Co, and K, and sequentially stirred at room temperature and 80° C. for 2 hours, respectively, and the Mo, Bi, Fe , Ni, Co, and K precursor mixture solution was sufficiently supported.

(3) Drying and sintering process of the silica carrier loaded with the precursor solution

Thereafter, the silica carrier on which the precursor mixture solution of Bi, Fe, Co, and K is supported is recovered and introduced into a rotary vacuum dryer, followed by primary vacuum drying for 1 hour and 40 minutes under a pressure of 140 mbar and a temperature of 70° C. Then, a second vacuum drying was performed for 30 minutes under a pressure of 40 mbar and a temperature of 90°C.

The material completed until the second vacuum drying is recovered, put into an oven, and dried for a third time for 24 hours under normal pressure and 110°C temperature conditions, and then maintained at 580°C in a box kiln in an air atmosphere. While performing a heat treatment for 3 hours, the catalyst of Example 1 was finally obtained.

(4) Ammoxidation process of flophyllene

In a tubular reactor having an inner diameter of 3/8 inch (inch), 0.05 g of quartz fiber was charged for filling the catalyst, and 0.2 g of the catalyst of Example 1 was charged into the reactor.

As such, the internal pressure of the reactor filled with the quartz fiber and the catalyst was maintained at normal pressure (1 atm), and the internal temperature of the reactor was raised at a temperature increase rate of 10 °C/min, while nitrogen and ammonia gas were flowed as a pretreatment process. Accordingly, after the temperature inside the reactor reached 400° C., which is the temperature at which the ammoxidation reaction is possible, it was maintained in an atmosphere of reducing gas for 15 minutes to allow sufficient pretreatment.

In the reactor where the pretreatment was completed, air was supplied together with propylene and ammonia as reactants, and the ammoxidation process of propylene was performed. At this time, the supply amount of the reactant was configured so that the volume ratio of propylene: ammonia: air = 0.8:1.2:8, and the total weight hourly space velocity (WHSV) of propylene, ammonia, and air was 1.54 h ^-1. .

After completion of the ammoxidation reaction, the product was recovered and analyzed using various equipment to confirm whether acrylonitrile was well produced.

The analysis method, analysis result, etc. will be described in detail in the experimental examples described later.

Examples 2 to 7

(1) catalyst manufacturing process (using the impregnation method)

A precursor solution was prepared according to the composition shown in Table 1 below, and the silica carriers shown in Table 2 were used, but the rest were the same as in Example 1 to prepare each of the catalysts of Examples 2 to 7.

(2) Process of ammoxidation of flophyllene

In addition, instead of the catalyst of Example 1, each catalyst of Examples 2 to 7 was used to perform the ammoxidation process of flophyllene, and then the product was recovered, and analysis was performed in the same manner as in Example 1.

Comparative Example 1

(1) Catalyst manufacturing process (using spray drying after coprecipitation)

First, 10.592 g of Mo precursor ((NH ₄ ) ₆ Mo ₇ O ₂₄ ) and 3.18 g of citric acid were added and mixed in distilled water at 60° C. to prepare a Mo precursor solution.

Independently, in distilled water at room temperature, 1.819 g of Bi precursor (Fe(NO ₃ ) _3· 5H ₂ O), 9.488 g of Co precursor (Co(NO ₃ ) _2· 6H ₂ O), 2.990 g of Fe precursor ( Fe(NO ₃ ) ₂ 9H ₂ O), and 0.354 g of K precursor (KNO ₃ ) were added, 0.83 g of nitric acid (HNO ₃ ) was added and mixed, and Bi, Fe, Co, and K precursors A mixed solution was prepared.

The Mo precursor solution; And the Bi, Fe, Co, and K precursor mixture solution, silica sol 22.530 g (LUDOX AS 40, solid content: 40%) was added and stirred, and then, using a disk-type spray dryer. It was spray-dried under conditions of 120°C (inlet) and 230°C (outlet).

The powder thus obtained was fired at 580° C. for 3 hours, and finally obtained as the catalyst of Comparative Example 1.

(2) Process of ammoxidation of flophyllene

The catalyst of Comparative Example 1 was used instead of the catalyst of Example 1, and the ammoxidation process of flophyllene was performed in the same manner as in Example 1.

After completion of the ammoxidation reaction of Comparative Example 1, the product was recovered, and analysis was performed in the same manner as in Example 1.

Comparative Example 2

(1) Catalyst manufacturing process (using spray drying after coprecipitation)

A precursor solution was prepared according to the composition shown in Table 1 below, and the silica carrier shown in Table 2 was used, but the rest was the same as in Comparative Example 1 to prepare a catalyst of Comparative Example 2.

(2) Process of ammoxidation of flophyllene

In addition, after performing the ammoxidation process of flophyllene using the catalyst of Comparative Example 2 instead of the catalyst of Comparative Example 1, the product was recovered, and analysis was performed in the same manner as in Comparative Example 1.

Comparative Example 3

(1) catalyst manufacturing process (using the impregnation method)

A precursor solution was prepared according to the composition shown in Table 1 below, and the silica carrier shown in Table 2 was used, but the rest were the same as in Example 1 to prepare the catalyst of Comparative Example 3.

(2) Process of ammoxidation of flophyllene

In addition, after performing the ammoxidation process of flophyllene using the catalyst of Comparative Example 3 instead of the catalyst of Example 1, the product was recovered, and analysis was performed in the same manner as in Example 1.

Comparative Example 4

(1) catalyst manufacturing process (using the impregnation method)

First, 10.592 g of Mo precursor ((NH ₄ ) ₆ Mo ₇ O ₂₄ ) and 3.18 g of citric acid were added and mixed in distilled water at 60° C. to prepare a Mo precursor solution.

Independently, 1.091 g of Bi precursor (Fe(NO ₃ ) ₃ ·5H ₂ O), 4.365 g of Co precursor (Co(NO ₃ ) ₂ ·6H ₂ O), 3.636 g of Fe precursor ( Fe(NO ₃ ) ₂ ·9H ₂ O), 2.908 g of Ni precursor (Ni(NO ₃ ) ₂ ·6H ₂ O), 0.045 g of K precursor (KNO ₃ ), 1.954 g of Ce precursor (Ce(NO ₃ ) ₃ ·6H ₂ O), 2.564 g of Mg precursor (Mg(NO ₃ ) ₂ ·6H ₂ O), and 0.037 g of Rb precursor (RbNO ₃ ) were added, and 0.83 g of nitric acid (HNO ₃ ) was added. Then, the mixture was mixed to prepare a mixed solution of Bi, Co, Fe, Ni, K, Ce, Mg, and Rb precursors.

The Mo precursor solution; And the Bi, Co, Fe, Ni, K, Ce, Mg, and Rb precursor mixture solution was mixed to complete a precursor mixture solution of Mo, Bi, Fe, Co, and K.

In the precursor mixture solution, the total amount of distilled water is 27.33 g.

(2) Process of ammoxidation of flophyllene

In addition, after performing the ammoxidation process of flophyllene using the catalyst of Comparative Example 4 instead of the catalyst of Example 1, the product was recovered, and analysis was performed in the same manner as in Example 1.

division Mo precursor solution Dissimilar metal precursor solution Distilled water SiO ₂ Citric acid Mo Bi Co Fe K nitric acid Example 1 3.18 10.592 1.819 9.488 2.990 0.354 2.16 54.07 27.04 Example 2 3.18 10.592 2.425 6.403 2.020 0.177 2.03 50.68 25.338 Example 3 3.18 10.592 1.989 9.313 1.616 0.076 2.10 52.51 26.257 Example 4 3.18 10.592 2.425 6.403 2.020 0.177 4.73 118.25 59.123 Example 5 3.18 10.592 2.425 6.403 2.020 0.177 3.19 79.63 39.817 Example 6 3.18 10.592 1.819 9.488 2.990 0.354 1.25 31.37 15.686 Example 7 3.18 10.592 1.819 9.488 2.990 0.354 0.83 20.65 10.323 Comparative Example 1 3.18 10.592 1.819 9.488 2.990 0.354 0.83 20.65 22.530
(40% Silica sol) Comparative Example 2 3.18 10.592 2.425 6.403 2.020 0.177 2.03 50.68 63.346
(40% Silica sol) Comparative Example 3 1.06 3.531 19.403 - - 1.415 2.60 64.95 32.477

In Table 1, Mo is (NH ₄ ) ₆ Mo ₇ O ₂₄ , Bi is Bi(NO ₃ ) ₃ ·5H ₂ O, Co is Co(NO ₃ ) ₂ ·6H ₂ O, and Fe is Fe( NO ₃ ) ₂ ·9H ₂ O, and K is KNO ₃ . Also, the omitted unit is g.

Meanwhile, Comparative Example 4 in which a number of substances were added to the dissimilar metal precursor solution was omitted from Table 1 for convenience.

division quite Catalyst composition carrier Active substance (metal oxide)
Content and composition Carrier content product name Example 1 Impregnation method 25 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 75wt% SP948 (Grace) Example 2 Impregnation method 25 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 75wt% SP948 (Grace) Example 3 Impregnation method 25 wt% (Mo ₁₂ Bi _0.82 Fe _0.8 Co _6.4 K _0.15 O _x ) 75 wt% SP948 (Grace) Example 4 Impregnation method 12.5wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 87.5 wt% SP948 (Grace) Example 5 Impregnation method 17.5 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 82.5 wt% SP948 (Grace) Example 6 Impregnation method 35 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 65 wt% SP948 (Grace) Example 7 Impregnation method 45 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 55 wt% SP948 (Grace) Comparative Example 1 Coprecipitation 50 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 50 wt% LUDOX_AS40 (Grace) Comparative Example 2 Coprecipitation 25 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 75wt% LUDOX_AS40 (Grace) Comparative Example 3 Impregnation method 25 wt% (Bi ₂ O _3·3 MoO ₃ ) 75wt% SP948 (Grace) Comparative Example 4 Impregnation method 25 wt% (Mo ₁₂ Bi _0.45 Ce _0.90 Fe _1.8 Ni _2.0 Co _3.0 Mg _2.0 K _0.09 Rb _0.05 O _n ) 75wt% SP948 (Grace)

Experimental Example 1: Catalyst Analysis

Each catalyst of Examples 1 to 7 and Comparative Examples 1 to 4 was analyzed according to the following analysis method:

BET specific surface area : Using a BET specific surface area measuring device (manufacturer: BEL Japan, device name: BELSORP_Mini), the specific surface area was evaluated from the amount of nitrogen gas adsorption under liquid nitrogen temperature (77 K), and the evaluation results are shown in Table 3. I got it.

Pore size and volume : Using a BET specific surface area measuring device (manufacturer: BEL Japan, device name: BELSORP_Mini), the adsorption amount measured up to 1 relative pressure (P/P0) under liquid nitrogen temperature (77K) and measured up to 0.03 The pore size and volume were measured from the BJH formula using the amount of desorption, and are shown in Table 3.

Catalyst composition : The catalyst composition can be measured by the ICP method. After weighing 0.01 g of catalyst in a corning tube, 3 ml of nitric acid and 0.1 ml of hydrofluoric acid were added to the sample, and then eluted for at least 1 hour in an ultra-sonicator. To this, 1 ml of saturated boric acid water was added and 50 ml of tertiary distilled water was added to prepare a solution, and then quantitative analysis of each component was performed using ICP-OES quantitative analysis equipment (PerkinElmer, OPTIMA 8300DV). And the composition and formulation thereof are shown in Table 3.

D50: Using a laser diffraction-type particle size analyzer (Microtrac, S3500), after sonication treatment at 30 watts for 1 minute after the sample was introduced, D50 based on volume was derived through particle size analysis, and is shown in Table 3.

division quite Active substance (metal oxide)
Content and composition catalyst
shape Catalyst BET
(m ² /g) Within the catalyst
pore
size
(nm) Within the catalyst
pore
volume
(cm ³ /g) D50
(㎛) Example 1 Impregnation method 25 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) Egg
-shell 105 28.1 0.75 55 Example 2 Impregnation method 25 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) Egg
-shell 125 24.4 0.84 112 Example 3 Impregnation method 25 wt% (Mo ₁₂ Bi _0.82 Fe _0.8 Co _6.4 K _0.15 O _x ) Egg
-shell 128 24.7 0.92 57 Example 4 Impregnation method 12.5wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) Egg
-shell 234 28.3 1.23 62 Example 5 Impregnation method 17.5 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) Egg
-shell 178 25.4 1.15 59 Example 6 Impregnation method Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x : 35 wt% Egg
-shell 106 22.6 0.75 52 Example 7 Impregnation method Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x : 45 wt% Egg
-shell 68 15.5 0.62 50 Comparative Example 1 Coprecipitation 35 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) Uniform 25 8 0.15 30 Comparative Example 2 Coprecipitation 45 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) Uniform 31 9 0.18 50 Comparative Example 3 Impregnation method 25 wt% (Bi ₂ O _3·3 MoO ₃ ) Egg
-shell 45 12.3 0.06 28 Comparative Example 4 Impregnation method 25 wt%
(Mo ₁₂ Bi _0.45 Ce _0.90 Fe _1.8 Ni _2.0 Co _3.0 Mg _2.0 K _0.09 Rb _0.05 O _n ) Egg
-shell 106 24.7 0.94 43

According to Table 3, in the relationship with the catalysts of Comparative Examples 1 and 2 through coprecipitation and spray drying, the impregnation method used to prepare the catalysts of Examples 1 to 7 has a large pore size and volume, and thus It can be seen that it is an advantageous method for preparing a catalyst with a large BET specific surface area.

Here, the catalysts of Comparative Examples 1 and 2 were prepared through coprecipitation and spray drying, and as a result, almost no pores were included, and the BET specific surface area was relatively narrow. On the other hand, the catalysts of Examples 1 to 7 were prepared using the impregnation method, and as a result, had a large number of large pores and had a relatively large BET specific surface area.

As a representative example, for each catalyst of Example 1 and Comparative Example 1, SEM: A Hitachi S-4800 Scanning Electron Microscope was used to obtain a scanning electron microscope (SEM) image at 100 magnification, and each SEM image was shown. 3 (Example 1) and Fig. 4 (Comparative Example 1).

Specifically, the catalyst of Comparative Example 1 generally has a particle diameter of 28 to 50 µm, and instead of forming a secondary particle structure in which metal oxide particles are uniformly distributed inside and outside, it is found that almost no internal pores are included. Able to know.

In contrast, the catalyst of Example 1 generally has a particle diameter of 50 to 112 µm, and a metal oxide coating layer for continuously coating the porous shell portion of the silica carrier is formed, and a plurality of large particles other than the coating layer are formed in the porous shell portion of the silica carrier. It can be seen that there is an empty space (pore).

On the other hand, although the catalyst of Comparative Example 3 was prepared by the impregnation method, the size and volume of the pores, and the BET specific surface area were only equivalent to those of Comparative Examples 1 and 2.

This means that under the influence of a metal oxide containing only Mo and Bi as active metals, a catalyst having a relatively narrow pore size and volume, and a BET specific surface area is prepared.

In the case of the catalyst of Comparative Example 4, it was prepared by the impregnation method and, as active metals included Mo and Bi as well as a plurality of dissimilar metals, it had a BET specific surface area equivalent to that of Examples 1 to 7. However, in order to evaluate the effect of the active metal, it is necessary to further analyze the ammoxidation product.

Experimental Example 2: Analysis of ammoxidation product

Using FID (Flame Ionization Detector and TCD (thermal conductivity detector) equipped chromatography (Gas chromatography, manufacturer: Agilent instrument name: HP 6890 N), each ammoxidation product of Examples and Comparative Examples was analyzed.

Specifically, as FID, products such as ethylene (ehthlene), hydrogen cyanide, acetaldehyde, acetonitrile, and acetonitrile were analyzed, and as TCD _{, NH 3} , O ₂ , Gas products such as CO and CO ₂ and unreacted propylene were analyzed to determine the number of moles of propylene reacted and the number of moles of ammoxidation product in Examples and Comparative Examples, respectively.

By substituting the number of moles of propylene supplied in addition to the analysis results according to the following 1, 2, and 3, the conversion of propylene, the selectivity and yield of acrylonitrile, a product of the ammoxidation reaction of propylene, were calculated, and the calculated value was calculated. It is listed in Table 4:

[Equation 1]

Conversion rate of propylene (%)

=100*(number of moles of ammoxidation of reacted propylene)/(number of moles of supplied propylene)

[Equation 2]

Selectivity of acrylonitrile (%)

=100*(number of moles of acrylonitrile produced)/(number of moles of reacted propylene)

[Equation 3]

Yield of acrylonitrile (%)

=100*(number of moles of acrylonitrile produced)/(number of moles of supplied propylene)

division quite Active substance (metal oxide)
Content and composition Ammoxidation product of propylene
Analysis Propylene
Conversion rate (%) Acrylonitrile
Selectivity (%) Acrylonitrile
Yield (%) Example 1 Impregnation method 25 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 61 76 47 Example 2 Impregnation method 25 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 79 79 63 Example 3 Impregnation method 25 wt% (Mo ₁₂ Bi _0.82 Fe _0.8 Co _6.4 K _0.15 O _x ) 82 86 71 Example 4 Impregnation method 12.5wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 61 80 49 Example 5 Impregnation method 17.5 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 73 82 60 Example 6 Impregnation method 35 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 68 72 49 Example 7 Impregnation method 45 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 65 69 45 Comparative Example 1 Coprecipitation 50 wt% (Mo ₁₂ Bi _0.75 Fe _1.48 Co _6.52 K _0.7 O _x ) 25 37 9 Comparative Example 2 Coprecipitation 25 wt% (Mo ₁₂ Bi _1.0 Fe _1.0 Co _4.4 K _0.35 O _x ) 48 69 33 Comparative Example 3 Impregnation method 25 wt% (Bi ₂ O _3·3 MoO ₃ ) 10 54 5.4 Comparative Example 4 Impregnation method 25 wt%
(Mo ₁₂ Bi _0.45 Ce _0.90 Fe _1.8 Ni _2.0 Co _3.0 Mg _2.0 K _0.09 Rb _0.05 O _n ) 53 64 34

The catalysts of Comparative Examples 1 and 2, as a result of being prepared through coprecipitation and spray drying, contain almost no internal pores, so that a site capable of participating in the reaction is limited to the outer surface portion.

In fact, in the reaction using the catalysts of Comparative Examples 1 and 2, it was confirmed that the conversion rate of propylene was less than 50%, and the yield of acrylonitrile was only less than 35%.

On the other hand, the catalyst of Comparative Example 3, although prepared by the impregnation method, has a small effective surface area capable of participating in the reaction due to the influence of a metal oxide containing only Mo and Bi as active metals.

In fact, in the reaction using the catalyst of Comparative Example 3, it was confirmed that the conversion rate of propylene was only 10%, and the yield of acrylonitrile was only less than 6%.

The catalyst of Comparative Example 4 was prepared by an impregnation method and contained not only Mo and Bi as active metals, but also a large number of dissimilar metals, so that the effective surface area itself capable of participating in the reaction was large.

Nevertheless, during the reaction using the catalyst of Comparative Example 4. The conversion rate of propylene is less than 55%, the selectivity of acrylonitrile is less than 70%, and the yield is only less than 35%. This is inferred from the influence of the formation of an excessively dense active point including Ce, Fe, Ni, Co, Mg, K, and Rb as well as Mo and Bi as active metals, and particularly including Ce.

On the other hand, the catalysts of Examples 1 to 7 contain pores having a large size and volume, and have a large effective surface area capable of participating in the reaction.

In fact, during the reaction using the catalysts of Examples 1 to 7. It was confirmed that the conversion rate of propylene was 60% or more, and the yield of acrylonitrile was significantly increased to 45% or more.

In this regard, the catalyst capable of improving the conversion rate of propylene and the yield of acrylonitrile during the ammoxidation reaction of propylene satisfies the above formula (1), and the metal oxide is supported on a silica carrier. It can be seen that it includes pores having a diameter of 5 to 200 nm and a volume of 0.1 to 3.0 cm ³ /g, and a BET specific surface area of 50 m ² /g to 1000 m ^{2 /g.}

Further, it will be possible to further improve the conversion rate of propylene and the yield of acrylonitrile by adjusting the metal oxide content and composition, etc., with reference to the catalysts of Examples 1 to 7.

Claims (20)

The metal oxide represented by the following formula (1) is a catalyst supported on a silica carrier,
The catalyst,
It contains pores with a diameter of 5 to 200 nm and a volume of 0.1 to 3.0 cm ^{3 /g,}
BET specific surface area of 50 m ² /g to 1000 m ² /g,
Catalyst for ammoxidation of propylene:
[Formula 1]
Mo ₁₂ Bi _a Fe _b A _c B _d C _e O _x
In Formula 1,
A is one or more elements of Ni, Mn, Co, Zn, Mg, Ca, and Ba,
B is one or more elements of Li, Na, K, Rb, and Cs,
C is one or more elements of Cr, W, B, Al, Ca, and V, and
Wherein a to e, and x are a fraction of an atom or group, respectively, a is 0.1 to 5, b is 0.1 to 5, c is 0.01 to 10, d is 0.01 to 2, and e is 0 to 10 , x is 24 to 48.
The method of claim 1,
The catalyst,
A silica carrier including second pores;
An inner coating layer that continuously coats the walls of the second pores and includes a metal oxide represented by Chemical Formula 1; And
Including; first pores located inside the second pores and occupying an empty space excluding the inner coating layer
Catalyst for ammoxidation of propylene.
The method of claim 1,
The catalyst,
BET specific surface area of 60 to 500 m ² /g,
Catalyst for ammoxidation of propylene.
The method of claim 1,
The catalyst,
It includes pores having a diameter of 10 to 100 nm,
Catalyst for ammoxidation of propylene.
The method of claim 1,
The catalyst,
It comprises pores having a volume of 0.6 to 2.0 cm ³ /g,
Catalyst for ammoxidation of propylene.
The method of claim 1,
The catalyst,
The D50 particle diameter is 50 to 200 ㎛,
Catalyst for ammoxidation of propylene.
The method of claim 1,
The metal oxide,
It is represented by the following formula 1-1,
Catalyst for ammoxidation of propylene:
[Formula 1-1]
Mo ₁₂ Bi _a Fe _b Co _c K _d O _x
In Formula 1-1, each definition of a to e, and x is the same as in claim 1.
The method of claim 1,
The weight ratio of the metal oxide and the silica carrier is 15:85 to 35:65,
Catalyst for ammoxidation of propylene.
Preparing a first precursor solution containing a Mo precursor,
Bi precursor, Fe precursor, A precursor (A = one or more elements of Ni, Mn, Co, Zn, Mg, Ca, and Ba), and B precursor (B = one or more of Li, Na, K, Rb, and Cs Element) preparing a second precursor solution,
Mixing the first and second precursor solutions so that the molar ratio of the metal satisfies the stoichiometric molar ratio of Formula 1 below,
Supporting the mixture of the first and second precursor solutions on a silica carrier,
Drying the silica carrier on which the mixture of the first and second precursor solutions is supported, and
Including the step of firing the dried material,
Method for producing a catalyst for ammoxidation of propylene:
[Formula 1]
Mo ₁₂ Bi _a Fe _b A _c B _d C _e O _x
In Formula 1,
A is one or more elements of Ni, Mn, Co, Zn, Mg, Ca, and Ba,
B is one or more elements of Li, Na, K, Rb, and Cs,
C is one or more elements of Cr, W, B, Al, Ca, and V, and
Wherein a to e, and x are the fractions of an atom or group, respectively, a is 0.1 to 5, b is 0.1 to 5, c is 0.01 to 10, d is 0.01 to 2, e is 0 to 10 , x is 24 to 48.
The method of claim 9,
In the step of preparing the second precursor solution,
To prepare a second precursor solution further comprising a C precursor (at least one element of Cr, W, B, Al, Ca, and V),
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 9,
In the step of preparing the second precursor solution,
To prepare a second precursor solution comprising a Bi precursor, a Fe precursor, a Co precursor, and a K precursor,
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 9,
The silica carrier,
It includes pores having a diameter of 10 to 200 nm and a volume of 0.1 to 3 cm ^{3 /g,}
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 9,
The silica carrier,
The BET specific surface area is 50 m ² /g to 1000 m ² /g,
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 9,
Drying the silica carrier on which the mixture of the first and second precursor solutions is supported,
First vacuum drying the silica carrier on which the mixture of the first and second precursor solutions is supported at 120 to 160 mbar, and
Including the step of obtaining a silica carrier on which the mixture of the first and second precursor solutions is supported by secondary vacuum drying the first vacuum-dried material at 30 to 50 mbar,
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 14,
The primary vacuum drying,
That is carried out at 60 to 80 °C,
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 14,
The second vacuum drying,
That is carried out at 80 to 100 °C,
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 14,
It further comprises the step of third drying the second vacuum-dried material at normal pressure,
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 17,
The third drying,
That is carried out at 100 to 150 °C,
Method for producing a catalyst for ammoxidation of propylene.
The method of claim 9,
The step of firing the dried material,
That is carried out at 500 to 700 °C,
Method for producing a catalyst for ammoxidation of propylene.
A method for ammoxidation of propylene, comprising reacting propylene and ammonia in the presence of the catalyst of claim 1 in a reactor.

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