FORCED DYNAMIC OPERATION FOR ACRYLONITRILE MANUFACTURE
20250263364 ยท 2025-08-21
Inventors
- William Epling (Charlottesville, VA, US)
- Zhuoran Gan (Oak Ridge, TN, US)
- Lars Christian Grabow (Houston, TX, US)
- James Frank Brazdil (Leland, NC, US)
Cpc classification
C07C253/26
CHEMISTRY; METALLURGY
International classification
C07C253/26
CHEMISTRY; METALLURGY
B01J23/887
PERFORMING OPERATIONS; TRANSPORTING
Abstract
In one aspect, the disclosure relates to a process for acrylonitrile manufacture using forced dynamic operation over transition metal promoted bismuth molybdate-based catalysts. The forced dynamic operation leverages catalyst lattice oxygen in ammoxidation of propene to improved acrylonitrile productivity and yield. This abstract is intended as a scanning tool for purposes of searching in the particular art and is not intended to be limiting of the present disclosure.
Claims
1. A method for manufacturing an acrylic compound or intermediate, the method comprising alternately flowing a first gas phase and a second gas phase over a catalyst in a reactor; wherein the first gas phase, the second gas phase, or both comprise propene, ammonia, and oxygen; wherein the catalyst comprises a transition metal promoted bismuth molybdate catalyst; wherein at least one reactor input or condition is modified periodically using forced dynamic operation (FDO); and wherein the acrylic compound or intermediate comprises acrylonitrile, acrolein, acrylic acid, or any combination thereof.
2. The method of claim 1, wherein the oxygen is provided as substantially pure oxygen gas.
3. The method of claim 1, wherein the oxygen is provided as a component of a mixed gas composition.
4. The method of claim 1, further comprising a third gas phase.
5. The method of claim 4, wherein the third gas phase comprises propene, ammonia, oxygen, or any combination thereof.
6. The method of claim 1, wherein the at least one reactor input comprises composition of the first gas phase, composition of the second gas phase, flow rate of the first gas phase, flow rate of the second gas phase, duty cycle of the reactor, reaction temperature, cycle period of the reactor, or any combination thereof.
7. The method of claim 1, wherein the first gas phase comprises propene, ammonia, and oxygen in a molar ratio of about 1:1:2.
8. The method of claim 1, wherein the second gas phase is selected from oxygen or a combination of propene, ammonia, and oxygen in a molar ratio of from about 1:1:6 to about 1:1:67.
9. The method of claim 8, wherein the second gas phase is oxygen and wherein the oxygen is present in a molar amount of from about 0.5 to about 67 times a molar amount of propene in the first gas phase.
10. The method of claim 1, wherein the first gas phase, the second gas phase, and, if present, the third gas phase, or any combination thereof further comprise an inert gas.
11. The method of claim 6, wherein the cycle period of the reactor is from about 0.1 min to about 2 hours.
12. The method of claim 6, wherein the duty cycle of the reactor is from about 50% to about 95%.
13. The method of claim 6, wherein the reaction temperature is from about 300 C. to about 500 C.
14. The method of claim 1, wherein the transition metal promoted bismuth molybdate catalyst has a formula M.sub.aFe.sub.bBi.sub.cMo.sub.12O.sub.x, wherein M comprises a transition metal, an alkaline earth metal, an alkali metal, or any combination thereof; wherein 0<a+b11; wherein 0<c<3; and wherein x has a value such that an amount of oxygen in the catalyst balances a charge of M, Fe, Bi, and Mo combined.
15. The method of claim 14, wherein a is from 0.1 to 10.9 and b is from 0.1 to 10.9
16. The method of claim 14, wherein M comprises Ni, Co, Mn, Mg, Zn, Cr, or any combination thereof.
17. The method of claim 14, wherein the catalyst comprises Ni.sub.11Fe.sub.0Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.10.5Fe.sub.0.5Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.10Fe.sub.1Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.8Fe.sub.3Bi.sub.1Mo.sub.12O.sub.x, or any combination thereof.
18. The method of claim 1, wherein the catalyst further comprises a support material.
19. The method of claim 18 wherein the support material comprises silica.
20. The method of claim 18, wherein the support material is present at from about 20 wt % to about 80 wt % of the catalyst.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0007] Many aspects of the present disclosure can be better understood with reference to the following drawings. The components in the drawings are not necessarily to scale, emphasis instead being placed upon clearly illustrating the principles of the present disclosure. Moreover, in the drawings, like reference numerals designate corresponding parts throughout the several views.
[0008]
[0009]
[0010]
[0011]
[0012]
[0013]
[0014]
[0015]
[0016]
[0017]
[0018]
[0019]
[0020]
[0021]
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
[0032]
[0033]
[0034]
[0035]
[0036]
[0037]
[0038] Additional advantages of the invention will be set forth in part in the description which follows, and in part will be obvious from the description, or can be learned by practice of the invention. The advantages of the invention will be realized and attained by means of the elements and combinations particularly pointed out in the appended claims. It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.
DETAILED DESCRIPTION
[0039] In one aspect, the present disclosure relates to the manufacture of acrylonitrile (ACN) using forced dynamic operation (FDO) in the ammoxidation of propene over transition metal promoted bismuth molybdate-based catalysts.
[0040] Forced dynamic operation (FDO), or periodic operation of a reactor, is a technique that involves periodically changing reactor inputs or the reactor environment. In one aspect, in FDO, one or more reactant concentrations to the reactor are purposefully varied as a function of time, or the reactor or reactant gas mixture temperature are varied as a function of time, or the reactor pressure is varied as a function of time. This can also be called modulation, cycling, or periodic forcing. In one aspect, the goals of FDO include improving selectivity and yield of the desired product and/or enhancing reaction rate. In another aspect, FDO can be used to regenerate a catalyst, such that activity can be re-attained. In a further aspect, one method of FDO is realized through composition forcing or feed modulation, e.g., step-changes in reactor inlet concentration in a periodic manner. FDO has proven advantageous in many reactions such as NH.sub.3 synthesis, methane combustion, and especially, partial oxidation of hydrocarbons. In an aspect, in partial oxidation reactions, oxygen in the catalyst or lattice oxygen plays a major role, in that the desired product is selectively produced, not becoming completely oxidized to H.sub.2O and CO.sub.2. Further in this aspect, the catalyst functions as an oxygen carrier allowing the partial oxidation reaction to be divided into two separate steps: reduction of the catalyst by hydrocarbon and NH.sub.3 in one step and re-oxidation by gaseous O.sub.2 in another step. In one aspect, such a process is perfectly aligned with FDO with feed modulation.
[0041] In another aspect, some promoted BMO catalysts have been developed for ammoxidation of propene and show high yield towards ACN in steady-state operation (SSO) processes. In one aspect, disclosed herein is a method for producing BMO-based catalyst formulations that are efficient for FDO, which can provide improved ACN productivity and/or yield compared to SSO. As defined herein, steady-state operation (SSO) refers to continuous operation in the presence of a catalyst for at least about one hour under approximately constant feed composition, temperature, pressure and other process conditions. In some aspects, SSO can refer to other time periods, such as continuous operation in the presence of a catalyst for at least about 10 min, 20 min, 30 min, 40 min, 50 min, 1 hour, 1.25 hours, 1.5 hours, or 2 hours. In a further aspect, the FDO parameters can be tuned for a catalyst, or a catalyst tuned for the parameters. In one aspect, FDO aged catalyst retains performance and properties closer to fresh catalyst as opposed to SSO aged catalyst, thus prolonging the useful lifetime of the catalyst. In another aspect, FDO can have lower energy requirements than SSO. In still another aspect, FDO offers additional advantages versus SSO including, but not limited to substantial variable manufacturing cost reduction and enhanced process efficiency due to (i) increased yield and selectivity to acrylonitrile, (ii) reduced raw material usage for propene and ammonia feedstocks, and (iii) increased operational time interval for catalyst change-out due to enhanced catalyst lifetime. In some aspects, NiFe and/or CoFe promoted BMO show better acrylonitrile production under FDO. In an aspect, during SSO, the rate of catalyst reduction and reoxidation must be equal. Further in this aspect, FDO has performance benefits over SSO, because the catalyst reduction and reoxidation occur in different reaction environments, which can be independently optimized to increase the rate of reduction or oxidation. As the rate of reduction and oxidation is an intrinsic catalyst property, the catalyst composition can be tuned to favor reduction or oxidation reactions. In one aspect, and without wishing to be bound by theory, for best overall performance, the catalyst composition must produce rates of catalyst reduction and oxidation that match the periods of the reduction and oxidation cycle of FDO. The rate of catalyst reduction and oxidation, can be approximately quantified by measuring its dynamic oxygen storage capacity (DOSC). In another aspect, practical benefits of FDO over SSO include temporal separation of the oxidant (O.sub.2) from the hydrocarbon and NH.sub.3, which greatly expands the accessible reductant-to-oxidant ratios and allows safe operation within the flammability limit of the overall feed mixture.
[0042] In one aspect, disclosed herein is a method for manufacturing an acrylic compound or intermediate, the method including alternately flowing a first gas phase and a second gas phase over a catalyst in a reactor; wherein the first gas phase, the second gas phase, or both include propene, ammonia, and oxygen; wherein the catalyst includes a transition metal promoted bismuth molybdate catalyst; wherein at least one reactor input or condition is modified periodically using forced dynamic operation (FDO); and wherein the acrylic compound or intermediate is selected from acrylonitrile, acrolein, acrylic acid, or any combination thereof.
[0043] In another aspect, the at least one reactor input can be composition of the first gas phase, composition of the second gas phase, flow rate of the first gas phase, flow rate of the second gas phase, duty cycle of the reactor, reaction temperature, cycle period of the reactor, or any combination thereof. In one aspect, the flow rate of the first gas phase and the flow rate of the second gas phase can be the same. In another aspect, the cycle period of the reactor can be from about 0.1 min to about 2 hours, or can be about 0.1, 0.5, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, or about 20 min, or can be about 0.5, 1, 1.5, or about 2 hours, or a combination of any of the foregoing values, or a range encompassing any of the foregoing values. In another aspect, the duty cycle of the reactor can be from about 50% to about 95%, or can be about 50, 55, 60, 65, 70, 75, 80, 85, 90, or about 95%, or a combination of any of the foregoing values, or a range encompassing any of the foregoing values. In one aspect, the reaction temperature can be from about 300 C. to about 500 C., or can be about 300, 305, 310, 315, 320, 325, 330, 335, 340, 345, 350, 355, 360, 365, 370, 375, 380, 385, 390, 395, 400, 405, 410, 415, 420, 425, 430, 435, 440, 445, 450, 455, 460, 465, 470, 475, 480, 485, 490, 495, or about 500 C., or can be from about 320 C. to about 450 C., or a combination of any of the foregoing values, or a range encompassing any of the foregoing values.
[0044] In one aspect, the FDO strategy consists of at least two alternating phases, but can consist of three or more phases in other aspects. In one example of a two phase system, one phase has a propene:ammonia:oxygen ratio of 1:1:2, while the other phase consists of O.sub.2 only. In some aspects, O.sub.2 can be provided as substantially pure O.sub.2, or can be provided as an oxygen-containing gas or mixed gas composition such as, for example, air. Further in this aspect, the O.sub.2 concentration in phase 2 is in the range of the equivalent of from about 0.5 to about 67 times the propene concentration in phase 1, or can be about 0.5, 1, 2, 5, 10, 15, 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, or about 67 times the propene concentration in phase one, or a combination of any of the foregoing values, or a range encompassing any of the foregoing values. In yet another aspect, the feed mixtures are all balanced by an inert gas such as, for example, N.sub.2, in the two or three or more phases.
[0045] In another aspect, the FDO strategy consists of 2 alternating phases; one phase has a propene:ammonia:oxygen ratio of 1:1:2, while the other phase has a propene:ammonia:oxygen ratio of from about 1:1:2 to 1:1:80 or from about 1:1:6 to 1:1:67.
[0046] In an aspect, the catalyst for ammoxidation of propene in FDO, includes a support material such as a silica support and a mixed-oxide complex having the following formula:
M.sub.aFe.sub.bBi.sub.cMo.sub.12O.sub.x
wherein M can be selected nickel, cobalt, manganese, magnesium, zinc, chromium, or any combination thereof. In one aspect, M is Ni. In another aspect, 0<a+b11, or 5<a+b11, or a+b=1. Further in this aspect, a or b can be 0. In an alternative aspect, a can be from about 0.1 to about 10.9 and b can be from about 0.1 to about 10.9. In a further aspect, 0<c<3, or 1<c<2, or c is about 1. In still another aspect, x can be the total oxygen number that meets the requirement of the valence of the elements. In one aspect, the catalyst can be Ni.sub.11Fe.sub.0Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.10.5Fe.sub.0.5Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.10Fe.sub.1Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.8Fe.sub.3Bi.sub.1Mo.sub.12O.sub.x, or any combination thereof.
[0047] In one aspect, the catalyst includes a support material such as, for example, a silica support. Further in this aspect, the content of the support material can be from about 20 wt % to about 80 wt %, or can be 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, 70, 75, or about 80 wt %, of a combination of any of the foregoing values, or a range encompassing any of the foregoing values.
[0048] In an aspect, provided herein is a process for low-volume, de-centralized acrylonitrile manufacture. However, in another aspect, the current disclosure is also applicable to the production of acrolein (ACO) by the partial oxygenation of propene, or further to acrylic acid production.
[0049] Many modifications and other embodiments disclosed herein will come to mind to one skilled in the art to which the disclosed compositions and methods pertain having the benefit of the teachings presented in the foregoing descriptions and the associated drawings. Therefore, it is to be understood that the disclosures are not to be limited to the specific embodiments disclosed and that modifications and other embodiments are intended to be included within the scope of the appended claims. The skilled artisan will recognize many variants and adaptations of the aspects described herein. These variants and adaptations are intended to be included in the teachings of this disclosure and to be encompassed by the claims herein.
[0050] Although specific terms are employed herein, they are used in a generic and descriptive sense only and not for purposes of limitation.
[0051] As will be apparent to those of skill in the art upon reading this disclosure, each of the individual embodiments described and illustrated herein has discrete components and features which may be readily separated from or combined with the features of any of the other several embodiments without departing from the scope or spirit of the present disclosure.
[0052] Any recited method can be carried out in the order of events recited or in any other order that is logically possible. That is, unless otherwise expressly stated, it is in no way intended that any method or aspect set forth herein be construed as requiring that its steps be performed in a specific order. Accordingly, where a method claim does not specifically state in the claims or descriptions that the steps are to be limited to a specific order, it is no way intended that an order be inferred, in any respect. This holds for any possible non-express basis for interpretation, including matters of logic with respect to arrangement of steps or operational flow, plain meaning derived from grammatical organization or punctuation, or the number or type of aspects described in the specification.
[0053] All publications mentioned herein are incorporated herein by reference to disclose and describe the methods and/or materials in connection with which the publications are cited. The publications discussed herein are provided solely for their disclosure prior to the filing date of the present application. Nothing herein is to be construed as an admission that the present invention is not entitled to antedate such publication by virtue of prior invention. Further, the dates of publication provided herein can be different from the actual publication dates, which can require independent confirmation.
[0054] While aspects of the present disclosure can be described and claimed in a particular statutory class, such as the system statutory class, this is for convenience only and one of skill in the art will understand that each aspect of the present disclosure can be described and claimed in any statutory class.
[0055] It is also to be understood that the terminology used herein is for the purpose of describing particular aspects only and is not intended to be limiting. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which the disclosed compositions and methods belong. It will be further understood that terms, such as those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the specification and relevant art and should not be interpreted in an idealized or overly formal sense unless expressly defined herein.
[0056] Prior to describing the various aspects of the present disclosure, the following definitions are provided and should be used unless otherwise indicated. Additional terms may be defined elsewhere in the present disclosure.
Definitions
[0057] As used herein, comprising is to be interpreted as specifying the presence of the stated features, integers, steps, or components as referred to, but does not preclude the presence or addition of one or more features, integers, steps, or components, or groups thereof. Moreover, each of the terms by, comprising, comprises, comprised of, including, includes, included, involving, involves, involved, and such as are used in their open, non-limiting sense and may be used interchangeably. Further, the term comprising is intended to include examples and aspects encompassed by the terms consisting essentially of and consisting of. Similarly, the term consisting essentially of is intended to include examples encompassed by the term consisting of.
[0058] As used in the specification and the appended claims, the singular forms a, an and the include plural referents unless the context clearly dictates otherwise. Thus, for example, reference to a BMO catalyst, a metal, or a gas, include, but are not limited to, mixtures or combinations of two or more such BMO catalysts, metals, or gases, and the like.
[0059] It should be noted that ratios, concentrations, amounts, and other numerical data can be expressed herein in a range format. It will be further understood that the endpoints of each of the ranges are significant both in relation to the other endpoint, and independently of the other endpoint. It is also understood that there are a number of values disclosed herein, and that each value is also herein disclosed as about that particular value in addition to the value itself. For example, if the value 10 is disclosed, then about 10 is also disclosed. Ranges can be expressed herein as from about one particular value, and/or to about another particular value. Similarly, when values are expressed as approximations, by use of the antecedent about, it will be understood that the particular value forms a further aspect. For example, if the value about 10 is disclosed, then 10 is also disclosed.
[0060] When a range is expressed, a further aspect includes from the one particular value and/or to the other particular value. For example, where the stated range includes one or both of the limits, ranges excluding either or both of those included limits are also included in the disclosure, e.g. the phrase x to y includes the range from x to y as well as the range greater than x and less than y. The range can also be expressed as an upper limit, e.g. about x, y, z, or less and should be interpreted to include the specific ranges of about x, about y, and about z as well as the ranges of less than x, less than y, and less than z. Likewise, the phrase about x, y, z, or greater should be interpreted to include the specific ranges of about x, about y, and about z as well as the ranges of greater than x, greater than y, and greater than z. In addition, the phrase about x to y, where x and y are numerical values, includes about x to about y.
[0061] It is to be understood that such a range format is used for convenience and brevity, and thus, should be interpreted in a flexible manner to include not only the numerical values explicitly recited as the limits of the range, but also to include all the individual numerical values or sub-ranges encompassed within that range as if each numerical value and sub-range is explicitly recited. To illustrate, a numerical range of about 0.1% to 5% should be interpreted to include not only the explicitly recited values of about 0.1% to about 5%, but also include individual values (e.g., about 1%, about 2%, about 3%, and about 4%) and the sub-ranges (e.g., about 0.5% to about 1.1%; about 5% to about 2.4%; about 0.5% to about 3.2%, and about 0.5% to about 4.4%, and other possible sub-ranges) within the indicated range.
[0062] As used herein, the terms about, approximate, at or about, and substantially mean that the amount or value in question can be the exact value or a value that provides equivalent results or effects as recited in the claims or taught herein. That is, it is understood that amounts, sizes, formulations, parameters, and other quantities and characteristics are not and need not be exact, but may be approximate and/or larger or smaller, as desired, reflecting tolerances, conversion factors, rounding off, measurement error and the like, and other factors known to those of skill in the art such that equivalent results or effects are obtained. In some circumstances, the value that provides equivalent results or effects cannot be reasonably determined. In such cases, it is generally understood, as used herein, that about and at or about mean the nominal value indicated 10% variation unless otherwise indicated or inferred. In general, an amount, size, formulation, parameter or other quantity or characteristic is about, approximate, or at or about whether or not expressly stated to be such. It is understood that where about, approximate, or at or about is used before a quantitative value, the parameter also includes the specific quantitative value itself, unless specifically stated otherwise.
[0063] As used herein, the term effective amount refers to an amount that is sufficient to achieve the desired modification of a physical property of the composition or material. For example, an effective amount of a feed gas refers to an amount that is sufficient to achieve the desired improvement in the property modulated by the formulation component, e.g. achieving the desired level of conversion of starting materials to acrylonitrile. The specific level in terms of wt % in a composition required as an effective amount will depend upon a variety of factors including the identities and amounts of other feed or carrier gases present, scale of the reaction, temperature and pressure of the reaction, and the like.
[0064] As used herein, the terms optional or optionally means that the subsequently described event or circumstance can or cannot occur, and that the description includes instances where said event or circumstance occurs and instances where it does not.
[0065] A transition metal promoted bismuth molybdate catalyst as used herein is a catalyst containing bismuth and molybdate ions in its crystal lattice alongside one or more transition metals including, but not limited to, Fe, Ni, Co, Mn, Zn, Cr, and combinations thereof. In some aspects, a transition metal promoted bismuth molybdate catalyst can also include an alkali metal and/or an alkaline earth metal such as, for example, Mg, as long as it also contains at least one transition metal. As used herein and as defined by convention by the International Union of Pure and Applied Chemistry (IUPAC), the term transition metal refers to one or more elements in Groups 3 to 12, inclusive, in the Periodic Table of Elements.
[0066] Unless otherwise specified, temperatures referred to herein are measured at atmospheric pressure (i.e. one atmosphere).
[0067] Now having described the aspects of the present disclosure, in general, the following Examples describe some additional aspects of the present disclosure. While aspects of the present disclosure are described in connection with the following examples and the corresponding text and figures, there is no intent to limit aspects of the present disclosure to this description. On the contrary, the intent is to cover all alternatives, modifications, and equivalents included within the spirit and scope of the present disclosure.
ASPECTS
[0068] The present disclosure can be described in accordance with the following numbered aspects, which should not be confused with the claims.
[0069] Aspect 1. A method for manufacturing an acrylic compound or intermediate, the method comprising alternately flowing a first gas phase and a second gas phase over a catalyst in a reactor; [0070] wherein the first gas phase, the second gas phase, or both comprise propene, ammonia, and oxygen; [0071] wherein the catalyst comprises a transition metal promoted bismuth molybdate catalyst; [0072] wherein at least one reactor input or condition is modified periodically using forced dynamic operation (FDO); and [0073] wherein the acrylic compound or intermediate comprises acrylonitrile, acrolein, acrylic acid, or any combination thereof.
[0074] Aspect 2. The method of aspect 1, wherein the oxygen is provided as substantially pure oxygen gas.
[0075] Aspect 3. The method of aspect 1, wherein the oxygen is provided as a component of a mixed gas composition.
[0076] Aspect 4. The method of aspect 3, wherein the mixed gas composition comprises air.
[0077] Aspect 5. The method of any one of aspects 1-4, further comprising a third gas phase.
[0078] Aspect 6. The method of aspect 5, wherein the third gas phase comprises propene, ammonia, oxygen, or any combination thereof.
[0079] Aspect 7. The method of any one of aspects 1-6, wherein the at least one reactor input comprises composition of the first gas phase, composition of the second gas phase, flow rate of the first gas phase, flow rate of the second gas phase, duty cycle of the reactor, reaction temperature, cycle period of the reactor, or any combination thereof.
[0080] Aspect 8. The method of any one of aspects 1-7, wherein the first gas phase comprises propene, ammonia, and oxygen in a molar ratio of about 1:1:2.
[0081] Aspect 9. The method of any one of aspects 1-8, wherein the second gas phase is selected from oxygen or a combination of propene, ammonia, and oxygen.
[0082] Aspect 10. The method of aspect 9, wherein the second gas phase is propene, ammonia, and oxygen in a molar ratio of from about 1:1:6 to about 1:1:67.
[0083] Aspect 11. The method of aspect 9, wherein the second gas phase is oxygen and wherein the oxygen is present in a molar amount of from about 0.5 to about 67 times a molar amount of propene in the first gas phase.
[0084] Aspect 12. The method of any one of aspects 1-11, wherein the first gas phase, the second gas phase, and, if present, the third gas phase, or any combination thereof further comprise an inert gas.
[0085] Aspect 13. The method of aspect 12, wherein the inert gas comprises N.sub.2.
[0086] Aspect 14. The method of any one of aspects 7-13, wherein the flow rate of the first gas phase and the flow rate of the second gas phase are the same.
[0087] Aspect 15. The method of any one of aspects 7-14, wherein the cycle period of the reactor is from about 0.1 min to about 2 hours.
[0088] Aspect 16. The method of any one of aspects 7-15, wherein the duty cycle of the reactor is from about 50% to about 95%.
[0089] Aspect 17. The method of any one of aspects 7-16, wherein the reaction temperature is from about 300 C. to about 500 C.
[0090] Aspect 18. The method of any one of aspects 1-17, wherein the catalyst has a formula M.sub.aFe.sub.bBi.sub.cMo.sub.12O.sub.x, wherein M comprises a transition metal, an alkaline earth metal, an alkali metal, or any combination thereof; [0091] wherein 0<a+b11; [0092] wherein 0<c<3; and [0093] wherein x has a value such that an amount of oxygen in the catalyst balances a charge of M, Fe, Bi, and Mo combined.
[0094] Aspect 19. The method of aspect 18, wherein a is from 0.1 to 10.9.
[0095] Aspect 20. The method of aspect 18 or 19, wherein b is from 0.1 to 10.9.
[0096] Aspect 21. The method of any one of aspects 18-20, wherein M comprises Ni, Co, Mn, Mg, Zn, Cr, or any combination thereof.
[0097] Aspect 22. The method of aspect 21, wherein M is Ni.
[0098] Aspect 23. The method of any one of aspects 18-22, wherein the catalyst comprises Ni.sub.11Fe.sub.0Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.10.5Fe.sub.0.5Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.10Fe.sub.1Bi.sub.1Mo.sub.12O.sub.x, Ni.sub.8Fe.sub.3Bi.sub.1Mo.sub.12O.sub.x, or any combination thereof.
[0099] Aspect 24. The method of any one of aspects 1-23, wherein the catalyst further comprises a support material.
[0100] Aspect 25. The method of aspect 24 wherein the support material comprises silica.
[0101] Aspect 26. The method of aspect 24 or 25, wherein the support material is present at from about 20 wt % to about 80 wt % of the catalyst.
EXAMPLES
[0102] The following examples are put forth so as to provide those of ordinary skill in the art with a complete disclosure and description of how the compounds, compositions, articles, devices and/or methods claimed herein are made and evaluated, and are intended to be purely exemplary of the disclosure and are not intended to limit the scope of what the inventors regard as their disclosure. Efforts have been made to ensure accuracy with respect to numbers (e.g., amounts, temperature, etc.), but some errors and deviations should be accounted for. Unless indicated otherwise, parts are parts by weight, temperature is in C. or is at ambient temperature, and pressure is at or near atmospheric.
Example 1: Ni.SUB.8.Fe.SUB.3.Bi.SUB.1.Mo.SUB.12.O.SUB.50.+20 wt % SiO.SUB.2.
[0103] Solution A was prepared by dissolving 0.69 g Bi(NO.sub.3).sub.3.Math.5H.sub.2O into 10 ml diluted HNO.sub.3 solution (3 ml 70% HNO.sub.3 mixed with 7 ml deionized water).
[0104] Solution B was prepared by dissolving 1.71 g Fe(NO.sub.3).sub.3.Math.9H.sub.2O into 100 ml deionized water, then adding 3.29 g Ni(NO.sub.3).sub.2.Math.6H.sub.2O.
[0105] Solution C was prepared by dissolving 3 g (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O into 50 ml deionized water. 2.94 g 34 wt % sodium-free silica sol having a SiO.sub.2 particle diameter of 22 nm was added to the resulting solution.
[0106] Solution B was mixed with solution A, then solution C was added to B dropwise then heated to 80 C. with 250 rpm stirring overnight. The resulting slurry was heated for another 6 h at 120 C. to dryness.
[0107] The precursor solid was collected and calcined in air at 290 C. for 3 h, then 425 C. for 3 h, then 560 C. for 3 h, with a ramping rate between temperatures of 5 C./min. The catalyst is denoted as Ni.sub.8Fe.sub.3-BMO.
Example 2: Ni.SUB.10.Fe.SUB.1.Bi.SUB.1.Mo.SUB.12.O.SUB.49.+20 wt % SiO.SUB.2
[0108] The catalyst was prepared following the procedure in Example 1, where the amount of Bi(NO.sub.3).sub.3.Math.5H.sub.2O 0.7 g, that of Fe(NO.sub.3).sub.2.Math.9H.sub.2O was 0.58 g, that of Ni(NO.sub.3).sub.2.Math.6H.sub.2O was 4.17 g, that of (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was 3.04 g, with others being the same as Example 1. The catalyst is denoted as Ni.sub.10Fe.sub.1-BMO.
Example 3: Ni.SUB.10.5.Fe.SUB.0.5.Bi.SUB.1.Mo.SUB.12.O.SUB.50.+20 wt % SiO.SUB.2
[0109] The catalyst was prepared following the procedure in Example 1, where the amount of Bi(NO.sub.3).sub.3.Math.5H.sub.2O 0.7 g, that of Fe(NO.sub.3).sub.2.Math.9H.sub.2O was 0.29 g, that of Ni(NO.sub.3).sub.2.Math.6H.sub.2O was 4.39 g, that of (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was 3.04 g, with others being the same as Example 1. The catalyst is denoted as Ni.sub.10.5Fe.sub.0.5-BMO.
Example 4: Ni.SUB.11.Fe.SUB.0.Bi.SUB.1.Mo.SUB.12.O+20 wt % SiO.SUB.2
[0110] The catalyst was prepared following the procedure in Example 1, where the amount of Bi(NO.sub.3).sub.3.Math.5H.sub.2O 0.7 g, that of Fe(NO.sub.3).sub.2.Math.9H.sub.2O was 0, that of Ni(NO.sub.3).sub.2.Math.6H.sub.2O was 4.6 g, that of (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was 3.05 g, with others being the same as Example 1. The catalyst is denoted as Ni.sub.11Fe.sub.0-BMO.
Example 5: Co.SUB.8.Fe.SUB.3.Bi.SUB.1.Mo.SUB.12.O.SUB.50.+20 wt % SiO.SUB.2
[0111] The catalyst was prepared following the procedure in Example 1, where the amount of Bi(NO.sub.3).sub.3.Math.5H.sub.2O 0.69 g, that of Fe(NO.sub.3).sub.2.Math.9H.sub.2O was 1.73 g, that of (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was 3.03 g, 3.33 g Co(NO.sub.3)2.Math.6H.sub.2O was added to solution B, with others being the same as Example 1. The catalyst is denoted as Co.sub.8Fe.sub.3-BMO.
Comparative Example 1: Bi.SUB.2.Mo.SUB.3.O.SUB.12.+20 wt % SiO.SUB.2
[0112] Solution A was prepared by dissolving 9.6 g Bi(NO.sub.3).sub.3.Math.5H.sub.2O into 0.2 M citric acid (CA) solution with ratio 1 Bi:1 CA, then adding 12.6 ml nitric acid (NA), with 10 NA:1 CA.
[0113] Solution B was prepared by dissolving 5.3 g (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O into 0.3 M CA solution, with ratio 1 Mo:1 CA, then adding 6.5 g 34 wt % sodium-free silica sol having a SiO.sub.2 particle diameter of 22 nm.
[0114] Solution B was slowly added to solution A while heated to 80 C. with stirring at 250 rpm overnight, the slurry was further heated to 120 C. for 6 h to dryness.
[0115] The resulting solid was grinded and calcined in air at 500 C. for 6 h with a ramping rate to said temperature of 5 C./min. The catalyst is denoted as -BMO.
Comparative Example 2: Ni.SUB.1.Mo.SUB.1.O.SUB.4.+20 wt % SiO.SUB.2
[0116] 3.23 g (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was dissolved into 200 ml deionized water, then 5.32 g Ni(NO.sub.3).sub.2.Math.6H.sub.2O was added, and then 2.94 g 34 wt % sodium-free silica sol having a SiO.sub.2 particle diameter of 22 nm was added to the resulting solution. The heating and calcination procedures were the same as Example 1. The catalyst is denoted as NiMO.
Comparative Example 3: Fe.SUB.2.Mo.SUB.3.O.SUB.12.+20 wt % SiO.SUB.2
[0117] The catalyst was prepared following the procedure in Comparative example 2, where the amount of (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was 3.27 g, that of Fe(NO.sub.3).sub.3.Math.9H.sub.2O was 5 g, with the others being the same as Comparative example 2. The catalyst is denoted as FeMO.
Comparative Example 4: Ni.SUB.1.Bi.SUB.1.Mo.SUB.3.O.SUB.11.5.+20 wt % SiO.SUB.2
[0118] The catalyst was prepared following the procedure in Example 1, where the amount of Bi(NO.sub.3).sub.3.Math.5H.sub.2O 2.62 g, that of Ni(NO.sub.3).sub.2.Math.6H.sub.2O was 1.6 g, that of (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was 2.86 g, with others being the same as Example 1 except no Fe precursor was added. The catalyst is denoted as Ni-BMO.
Comparative Example 5: Fe.SUB.1.Bi.SUB.1.Mo.SUB.3.O.SUB.12.+20 wt % SiO.SUB.2
[0119] The catalyst was prepared following the procedure in Example 1, where the amount of Bi(NO.sub.3).sub.3.Math.5H.sub.2O 2.61 g, that of Fe(NO.sub.3).sub.2.Math.9H.sub.2O was 2.17 g, that of (NH.sub.4).sub.6Mo.sub.7O.sub.24.Math.4H.sub.2O was 2.85 g, with others being the same as Example 1 except no Ni precursor was added. The catalyst is denoted as Fe-BMO.
Comparative Example 6: INEOS-BMO
[0120] A commercial silica supported multi-component (including but not limited to Ni, Fe, Cr) promoted bismuth molybdate-based catalyst was provided by INEOS Nitriles USA LLC (Lima, Ohio). The catalyst is denoted as INEOS-BMO.
Example 7: Characterization and Yield
[0121] X-ray diffraction (XRD) was carried out with a PANalytical Empyrean X-ray diffractometer using Cu K radiation operated at 40 kV and 40 mA. Dynamic oxygen storage capacity measurements were performed using C.sub.3H.sub.6 as a probe molecule, with alternating exposures of C.sub.3H.sub.6:N.sub.2:O.sub.2:N.sub.2=2 min:3 min:2 min:3 min, C.sub.3H.sub.6=1500 ppm and O.sub.2=3000 ppm, total flowrate=300 sccm, T=330 C.
[0122] Catalytic performance measurements. The propene ammoxidation reaction experiments were performed in a horizontal quartz tube reactor with an internal diameter of 11 mm. The quartz tube reactor resided in a Thermo Scientific Lindberg Blue M electric furnace. The catalyst was pelletized and sieved to 40-60 mesh (250-425 m) pellets, mixed with nitric acid washed SiO.sub.2 of the same size and placed between two quartz wool plugs. Two K-type thermocouples were placed at the end of the two quartz wool plugs to measure the temperature upstream and downstream of the catalyst. Forced dynamic operation was achieved by the set-up illustrated in
[0123] The catalyst was pretreated with 10% O.sub.2/N.sub.2 at 500 C. for 1 h in a flowrate of 100 sccm before reaction. In disclosed process, the total flowrate in the reactor is usually 50 sccm. This results in a contact time=2.3 s. Due to the constraints of the FTIR analyzer (the inlet flowrate needs to be >200 sccm), the FTIR inlet is diluted with additional 250 sccm N.sub.2 flow, making the total flowrate 300 sccm. Thus, the gas concentrations reflected in the figures are diluted 6 times (to obtain the real concentrations, the values plotted should be multiplied by 6). A series of temperature programmed reactions were done from 200-500 C. using Ni.sub.8Fe.sub.3-BMO, Co.sub.8Fe.sub.3-BMO, and INEOS-BMO to evaluate the catalytic performance at steady-state. The feed conditions were, C.sub.3H.sub.6:NH.sub.3:O.sub.2=1500 ppm:1500 ppm:3000 ppm, with balance N.sub.2, total flowrate=50 sccm, C.sub.3H.sub.6 GHSV=0.65 h.sup.1. The ramping rate between temperatures was 5 C./min and the dwell time is 2 h at each temperature. The results are shown in
[0124]
[0125]
[0126]
[0127]
TABLE-US-00001 TABLE 1 Fe.sup.3+/Fe.sup.2+ and Ni.sup.3+/Ni.sup.2+ Ratios Sample Fe.sup.3+/Fe.sup.2+ Ni.sup.3+/Ni.sup.2+ Fresh 0.791 0.68 SSO Aged 0.827 0.75 FDO Aged 0.774 0.626
[0128] Quantification from the XPS scans is presented in Tables 2 and 3 below. This quantification is derived from the average of two-point scans.
TABLE-US-00002 TABLE 2 Elemental Analysis of NiFeBMO Samples Sample Bi Mo Si Ni Fe O C Fresh 1.26 7.9 14.45 5.56 2.75 44.28 23.78 FDO (aged) 0.59 9.125 18.9 6.265 3.685 54.61 5.415 SSO (aged) 0.86 8.48 18.79 5.58 4.065 53.8 8.415
TABLE-US-00003 TABLE 3 Bismuth Ratios in NiFeBMO Samples NiFeBMO Bi/Mo Bi/Ni Bi/Fe Fresh 0.159 0.226 0.458 FDO (aged) 0.108 0.158 0.268 SSO (aged) 0.101 0.154 0.211
[0129]
[0130]
TABLE-US-00004 TABLE 4 Phases Detected in Various Catalysts Catalyst Phase(s) Detected by XRD Bi.sub.2Mo.sub.3O.sub.12 -Bi.sub.2Mo.sub.3O.sub.12 NiMoO.sub.4 -NiMoO.sub.4, -NiMoO.sub.4 Fe.sub.2MoO.sub.12 Fe.sub.2Mo.sub.3O.sub.12, MoO.sub.3 NiBiMo.sub.3O.sub.x -Bi.sub.2Mo.sub.3O.sub.12, -Bi.sub.2Mo.sub.2O.sub.9, -NiMoO.sub.4, -NiMoO.sub.4 FeBiMo.sub.3O.sub.3 -Bi.sub.2Mo.sub.3O.sub.12, Fe.sub.2Mo.sub.3O.sub.12, Bi.sub.3FeMo.sub.2O.sub.12 Ni.sub.11BiMo.sub.12O.sub.x -Bi.sub.2Mo.sub.3O.sub.12, -NiMoO.sub.4, -NiMoO.sub.4 Ni.sub.10.5Fe.sub.0.5BiMo.sub.12O.sub.x -Bi.sub.2Mo.sub.3O.sub.12, -NiMoO.sub.4, -NiMoO.sub.4 Ni.sub.10FeBiMo.sub.12O.sub.x -Bi.sub.2Mo.sub.3O.sub.12, FeMoO.sub.4, Fe.sub.2Mo.sub.3O.sub.12, -NiMoO.sub.4, -NiMoO.sub.4 Ni.sub.8Fe.sub.3BiMo.sub.12O.sub.x -Bi.sub.2Mo.sub.3O.sub.12, FeMoO.sub.4, Fe.sub.2Mo.sub.3O.sub.12, -NiMoO.sub.4, -NiMoO.sub.4
Example 8: Performance Under FDO Modes
[0131] With the information gained from the temperature programmed reactions, FDO testing was done with the Ni.sub.8Fe.sub.3-BMO at 330 C., where the ACN yield is decent and the NH.sub.3 conversion has not reached 100%, at which point the ACN selectivity will be limited. The FDO evaluations were begun with a normal feed-O.sub.2 regen FDO scheme described in Table 5, with varied duty cycle from 50% to 90%. In this FDO scheme, the ACN will only be produced in phase 1. Since the feed conditions are the same as SSO, it is referred to as normal feed phase. In phase 2, the C.sub.3H.sub.6 and NH.sub.3 were cut-off, only O.sub.2 was present. In
TABLE-US-00005 TABLE 5 Gas concentrations in the normal feed-O.sub.2 regen FDO scheme Phase 1 Phase 2 C.sub.3H.sub.6 NH.sub.3 O.sub.2 C.sub.3H.sub.6 NH.sub.3 O.sub.2 1500 ppm 1500 ppm 3000 ppm 0 0 3000 ppm
[0132] The ACN productivity can be further increased by increasing the O.sub.2 concentration in the regeneration phase. Shown in
[0133] The best FDO scheme above with elevated O.sub.2 input in the O.sub.2 regen phase (O.sub.2=10%) was applied at higher temperatures, 360 C. and 390 C. (
[0134] The overshoot phenomenon of a desired product in FDO schemes that rely on O.sub.2 regeneration is believed to be related to lattice oxygen on/in the catalyst in certain partial oxidation reactions. The area where the ACN trace in FDO is higher than the SSO is defined as the ACN spike region, using Ni.sub.8Fe.sub.3-BMO as an example shown in
[0135]
[0136]
[0137]
[0138]
[0139]
[0140]
[0141] SSO was conducted under C.sub.3H.sub.6:NH.sub.3:O.sub.2=1500:1500:3000 ppm at 330 C. for 3 days. FDO cycling was carried out between C.sub.3H.sub.6:NH.sub.3:O.sub.2=1500:1500:3000 ppm and O.sub.2=3000 ppm at 330 C. for 3 d.
[0142]
[0143]
[0144]
[0145]
[0146]
[0147]
Example 9: Processes Leveraging Excess O.SUB.2
[0148] To further explore the disclosed processes in relation to FDO, a new strategy was introduced, the feed gas conditions are listed in Table 6. Here two schemes that leverage a high concentration O.sub.2 were proposed where C.sub.3H.sub.6 and NH.sub.3 are not cut-off in phase 2. The impact of O.sub.2 concentration in SSO on the Ni.sub.8Fe.sub.3-BMO was investigated first at 330 C. The O.sub.2 concentration is varied from 500 ppm to 10%, with C.sub.3H.sub.6 and NH.sub.3 fixed to 1500 ppm, total flowrate=50 sccm, C.sub.3H.sub.6 GHSV=0.65 h.sup.1. The investigation was done with separate runs, each run with an increased O.sub.2 concentration. The catalyst was pretreated with 10% O.sub.2/N.sub.2 before every run, each run lasts 4 h, the ACN productivity was recorded after 2 h. From the ammoxidation reaction, the stoichiometric ratio of O.sub.2/C.sub.3 is 1.5:1, hence 2250 ppm O.sub.2 should be supplied with 1500 ppm C.sub.3H.sub.6, theoretically. But in practice O.sub.2/C.sub.3 is usually in slight excess (2:1). The results in
TABLE-US-00006 TABLE 6 FDO schemes leveraging excess O.sub.2 Cycling Phase 1 Phase 2 scheme C.sub.3H.sub.6 NH.sub.3 O.sub.2 C.sub.3H.sub.6 NH.sub.3 O.sub.2 Scheme 1 1500 ppm 1500 ppm 3000 ppm 1500 ppm 1500 ppm 9000 ppm Scheme 2 1500 ppm 1500 ppm 3000 ppm 1500 ppm 1500 ppm 10% Cycle period = 2, 4, 10, 20 min, duty cycle = 50%, T = 330 C.
[0149]
[0150] It should be emphasized that the above-described embodiments of the present disclosure are merely possible examples of implementations set forth for a clear understanding of the principles of the disclosure. Many variations and modifications may be made to the above-described embodiment(s) without departing substantially from the spirit and principles of the disclosure. All such modifications and variations are intended to be included herein within the scope of this disclosure and protected by the following claims.
REFERENCES
[0151] 1. Becker, T. et al. 2021. Decentralized Modular Production to Increase Supply Chain Efficiency in Chemical Markets: An Example of Polymer Production. Journal of Business Economics 91 (6): 867-95. [0152] 2. Brazdil, J. F. 2018. Designing Multifunctionality into Single Phase and Multiphase Metal-Oxide-Selective Propylene Ammoxidation Catalysts. Catalysts 8 (3): 103. [0153] 3. Callahan, J.L. et al. 1970. Oxidation and Ammoxidation of Propylene over Bismuth Molybdate Catalyst. Industrial and Engineering Chemistry Product Research and Development 9 (2): 134-42. [0154] 4. Chang, T.S. et al. 2000. Catalytic Behavior of BiPO4 in the Multicomponent Bismuth Phosphate System on the Propylene Ammoxidation. Catalysis Letters 68 (3-4): 229-34. [0155] 5. Fouladvand, S. et al. 2016. Unsteady-State Operation of Supported Platinum Catalysts for High Conversion of Methane. Chemical Engineering Journal 292: 321-25. [0156] 6. Grasselli, R.K. 2011. Chapter 5. Ammoxidation of Propylene and Propane to Acrylonitrile. In Nanostructured Catalysts: Selective Oxidations, 96-140. The Royal Society of Chemistry. [0157] 7. Huang, X. F., et al. 2001. Investigation of the Unsteady-State Oxidation of n-Butane to Maleic Anhydride in Fixed-Bed Reactors. Industrial and Engineering Chemistry Research 40 (3): 768-73. [0158] 8. Jain, A K, et al. 1983. Influence of Forced Feed Composition Cycling on the Rate of Ammonia Synthesis over an Industrial Iron Catalyst Part IEffect of Cycling Parameters and Mean Composition. The Canadian Journal of Chemical Engineering 61 (6): 824-32. [0159] 9. Lang, X. et al. 1989. Maleic Anhydride Formation from 1, 3-butadiene Oxidation over a Vanadia Molybdate Catalyst. The Canadian Journal of Chemical Engineering 67 (3): 423-31. [0160] 10. Licht, R.B. et al. 2016. The Mechanism and Kinetics of Propene Ammoxidation over -Bismuth Molybdate. Journal of Catalysis 339: 228-41. [0161] 11. Silveston, P.L., et al. 2007. Periodic Operation of Reactors. Cyclic Separating Reactors. doi.org/10.1002/9780470988688.ch2. [0162] 12. Idol, Jr., J.D. 1959. U.S. Pat. No. 2,904,580. [0163] 13. Suresh, D.D. et al. 1992. U.S. Pat. No. 5,093,299. [0164] 14. Guan, X. et al. 2003. U.S. Pat. No. 6,596,897. [0165] 15. Paparizos, C. et al., 2006, U.S. Pat. No. 7,071,140. [0166] 16. Brazdil, J.F. et al., 2020, U.S. Pat. No. 10,780,427.