CN113444543B

CN113444543B - Biological aviation kerosene component oil and preparation method thereof

Info

Publication number: CN113444543B
Application number: CN202010216151.6A
Authority: CN
Inventors: 闫瑞; 郭勇; 赵红; 王艳芹
Original assignee: Sinopec Research Institute of Petroleum Processing; China Petroleum and Chemical Corp; East China University of Science and Technology
Current assignee: Sinopec Research Institute of Petroleum Processing; China Petroleum and Chemical Corp; East China University of Science and Technology
Priority date: 2020-03-25
Filing date: 2020-03-25
Publication date: 2023-03-28
Anticipated expiration: 2040-03-25
Also published as: CN113444543A

Abstract

The invention provides biological aviation kerosene component oil and a preparation method thereof, wherein the preparation method comprises the following steps: performing aldol condensation reaction on lignocellulose-based furfural compound and carbonyl compound to obtain C ₈ ～C ₁₆ A long chain oxygen-containing compound; to C ₈ ～C ₁₆ Carrying out hydrogenation saturation on the long-chain oxygen-containing compound; hydrodeoxygenation of the hydrosaturated product to give C ₈ ～C ₁₆ Long-chain alkanes; and to C ₈ ～C ₁₆ And (4) isomerizing the long-chain alkane, and fractionating to obtain the biological aviation kerosene component oil. The method can realize catalytic conversion based on the biomass sugar platform compound to prepare the biological aviation kerosene component oil, is beneficial to comprehensive utilization of agricultural and forestry wastes, and realizes green sustainable development.

Description

Biological aviation kerosene component oil and preparation method thereof

Technical Field

The invention relates to the technical field of petrochemical industry, in particular to biological aviation kerosene component oil and a preparation method thereof.

Background

In the oil crisis and the greenhouse effect are increasingly seriousIn the background, biomass, the only renewable energy source containing a carbon source, is currently the most promising resource for producing hydrocarbon liquid fuels to replace petroleum. In order to continue the transition from fossil energy economy to carbohydrate economy and convert biomass into fuels and chemicals with high added values, the Dumesic working group uses lignocellulose hydrolysate furfural as a raw material, and firstly prolongs the carbon chain through aldol condensation reaction to obtain furylideneacetone [4- (2-furyl) -3-butene-2-one]And difurfurylideneacetone [1,5-bis- (2-furyl) -1,4-pentadien-3-one]Then hydrodeoxygenation to C ₈ Straight chain alkane and C ₁₃ Straight-chain alkanes are finally isomerized to obtain qualified jet fuel components, and high-efficiency utilization of biomass is realized (science, 2005,308, 1446-1450). As shown in formula I below:

however, since the difurfurylideneacetone generated by the condensation of furfural and acetone is solid, the direct entering of the reactor into a tubular reactor for continuous treatment is difficult. On the other hand, furfurylideneacetone, difurfurylideneacetone, and the like have a large conjugated structure with a furan ring and a C = C double bond, are unstable at high temperatures, and are liable to cause side reactions such as self-polymerization. In addition, hydrodeoxygenation (HDO) reactions, which allow higher calorific values and chemical stability of the lignocellulosic hydrolysates, are key steps in the preparation of liquid hydrocarbon fuels. However, the existing reports aiming at preparing liquid hydrocarbon fuel by catalyzing sugar platform compounds are not many, and most of the reports are direct hydrodeoxygenation conversion, and the mode has the problems of more side reactions, easy carbon deposition and inactivation of catalysts and the like.

It is noted that the information disclosed in the foregoing background section is only for enhancement of background understanding of the invention and therefore it may contain information that does not constitute prior art that is already known to a person of ordinary skill in the art.

Disclosure of Invention

The invention aims to overcome at least one defect of the prior art and provides a biological aviation kerosene component oil and a preparation method thereof, so as to solve the problems of more side reactions, easy inactivation of a catalyst and the like in the process of preparing hydrocarbon fuel by using the existing sugar platform compounds.

In order to achieve the purpose, the invention adopts the following technical scheme:

the invention provides a preparation method of biological aviation kerosene component oil, which comprises the following steps: subjecting lignocellulose-based furfural compound and carbonyl compound to aldol condensation reaction to obtain C ₈ ～C ₁₆ A long chain oxygen-containing compound; to C ₈ ～C ₁₆ Carrying out hydrogenation saturation on the long-chain oxygen-containing compound; hydrodeoxygenation of the hydrosaturated product to yield C ₈ ～C ₁₆ A long-chain alkane; and to C ₈ ～C ₁₆ Isomerizing long-chain alkane, and fractionating to obtain the biological aviation kerosene component oil.

According to one embodiment of the invention, the lignocellulose-based furfural compound is selected from one or more of furfural and 5-hydroxymethyl furfural, the carbonyl compound is an alpha-H carbonyl compound, the alpha-H carbonyl compound is selected from one or more of acetone and levulinic acid, and the molar ratio of the lignocellulose-based furfural compound to the carbonyl compound is 1:2-5:1.

According to one embodiment of the invention, the aldol condensation reaction is carried out under the action of a base catalyst, the base catalyst is an inorganic base, the inorganic base is one or more selected from sodium hydroxide, potassium hydroxide, ammonia water, sodium carbonate and potassium carbonate, and the molar concentration of the inorganic base is 0.05 mol/L-1 mol/L.

According to one embodiment of the invention, the hydrosaturation is carried out over a hydrosaturation catalyst comprising a composite of nickel and silica, wherein the silica is in an amorphous structure and the nickel is in a crystalline structure.

According to one embodiment of the invention, the compound has the formula Ni- (SiO) ₂ ) _a And a has a value of 0.1 to 40.

According to one embodiment of the invention, the hydrosaturation comprises: c is to be ₈ ～C ₁₆ Dissolving long-chain oxygen-containing compound in organic solvent, and hydrogenating saturation reaction of the solution in fixed bed reactor containing hydrogenating saturation catalystThe medium organic solvent is oxygen-containing solvent selected from one or more of methanol, ethanol and acetone, and C in the solution ₈ ～C ₁₆ The mass percentage of the long-chain oxygen-containing compound is 0.5-50%.

According to one embodiment of the invention, the hydrogenation saturation reaction temperature is 0-200 ℃, the reaction pressure is 0.5-15 MPa, and the mass space velocity is 0.1h ^-1 ～10h ^-1 The volume ratio of hydrogen to oil is 50-3000.

According to one embodiment of the present invention, the hydrodeoxygenation is performed under the action of a hydrodeoxygenation catalyst, which comprises a first support and a first active metal loaded on the first support, wherein the first active metal is one or more selected from nickel, molybdenum, tungsten, cobalt, palladium and platinum, and the first support is M- (SiO —) ₂ ) _X The composite oxide, M is selected from one or more of niobium oxide, cobalt oxide and cerium oxide, and x is 1-100.

According to one embodiment of the invention, M is Nb in an amorphous structure ₂ O ₅ X is 1 to 40; the first active metal is selected from one or more of palladium, nickel and platinum, and the loading amount of the first active metal is 0.05-30 wt%.

According to one embodiment of the invention, the first support is made of M and SiO ₂ Porous structure of aggregated oxide particle clusters, siO ₂ The carrier is an amorphous structure, the size of the cluster is 200 nm-2000 nm, and the specific surface area of the first carrier is 200m ² /g～700m ² (iii) a pore volume of 0.1cc/g to 0.9cc/g.

According to one embodiment of the invention, hydrodeoxygenation comprises: the hydrogenation saturated product is subjected to hydrogenation deoxidation reaction in a fixed bed reactor containing a hydrogenation deoxidation catalyst, wherein the reaction temperature is 100-400 ℃, the reaction pressure is 0.5-15 MPa, and the mass space velocity is 0.1h ^-1 ～10h ^-1 The volume ratio of hydrogen to oil is 50-3000.

According to one embodiment of the present invention, the isomerization is carried out over a hydroisomerization catalyst comprising a second support and a second active metal supported on the second support, wherein the second active metal is selected from one or more of nickel, molybdenum, tungsten, cobalt, palladium and platinum, and the second support is selected from one or more of ZSM5, ZSM12, ZSM22, ZSM23, ZSM35, ZSM48, SAPO11, beta and Y molecular sieves.

According to one embodiment of the invention, the isomerization process comprises: c ₈ ～C ₁₆ The long-chain alkane is subjected to isomerization treatment in a fixed bed reactor containing a hydroisomerization catalyst, wherein the reaction temperature is 100-450 ℃, the reaction pressure is 0.5-15 MPa, and the mass space velocity is 0.1h ^-1 ～10h ^-1 The volume ratio of hydrogen to oil is 50-3000.

The invention also provides biological aviation kerosene component oil prepared by the method.

According to the technical scheme, the invention has the beneficial effects that:

according to the preparation method of the biological aviation kerosene component oil, provided by the invention, through designing a synthesis route, hydrogenation saturation treatment is carried out before hydrodeoxygenation is carried out on a condensation product, and a proper specific catalyst is adopted in each step, so that the side reaction in the whole reaction process is less, the conversion rate and the yield are higher, and the preparation method has a good application prospect. The method can realize catalytic conversion based on the biomass sugar platform compound to prepare the biological aviation kerosene component oil, is beneficial to comprehensive utilization of agricultural and forestry wastes, and realizes green sustainable development.

Drawings

The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention.

FIG. 1 is a flow diagram of a process for the preparation of a biological aviation fuel component oil in accordance with one embodiment of the present invention;

FIG. 2 is an XRD spectrum of a hydrogenation saturation catalyst in preparation example 1;

FIG. 3 is an XRD spectrum of the hydrodeoxygenation catalyst of preparation 2;

FIG. 4 is a C-NMR spectrum of a condensation product of example 1;

FIG. 5 is an H-NMR spectrum of a condensation product of example 1;

FIG. 6 is an IR spectrum of the condensation product of example 1;

FIG. 7 is a process flow diagram of a hydrosaturation reaction in accordance with one embodiment of the present invention;

FIG. 8 is a process flow diagram of a hydrodeoxygenation reaction according to one embodiment of the present invention;

FIG. 9 is a dodecane MS spectrum of the hydrodeoxygenation product of example 21;

FIG. 10 is the MS spectrum of the hydrodeoxygenation product tridecane of example 21;

FIG. 11 is a process flow diagram of an isomerization reaction in accordance with one embodiment of the present invention.

Detailed Description

The following presents various embodiments, or examples, in order to enable one of ordinary skill in the art to practice the invention with reference to the description herein. These are, of course, merely examples and are not intended to limit the invention. The endpoints of the ranges and any values disclosed in the present application are not limited to the precise range or value, and such ranges or values should be understood to encompass values close to those ranges or values. For ranges of values, between the endpoints of each of the ranges and the individual points, and between the individual points may be combined with each other to yield one or more new ranges of values, which ranges of values should be considered as specifically disclosed herein.

Fig. 1 shows a flow chart of a process for preparing the biological aviation kerosene component oil according to an embodiment of the present invention, and as shown in fig. 1, the method for preparing the biological aviation kerosene component oil comprises the following steps:

s1: performing aldol condensation reaction on lignocellulose-based furfural compound and carbonyl compound to obtain C ₈ ～C ₁₆ A long chain oxygen-containing compound;

s2: to C ₈ ～C ₁₆ Carrying out hydrogenation saturation on the long-chain oxygen-containing compound;

s3: hydrodeoxygenation of the hydrosaturated product to give C ₈ ～C ₁₆ Long-chain alkanes;

s4: to C ₈ ～C ₁₆ And (4) isomerizing the long-chain alkane, and fractionating to obtain the biological aviation kerosene component oil.

According to the invention, the problems of more side reactions, easy inactivation of the catalyst and the like still exist in the process of preparing the hydrocarbon fuel by using the existing sugar platform compounds. According to the invention, a synthesis route is redesigned, firstly, a bio-friendly sugar platform compound is selected to perform carbon chain regulation through an aldol condensation reaction to obtain a proper long-chain oxygen-containing compound, then, the condensation product is subjected to hydrogenation saturation treatment to saturate double bonds of C = C and C = O and convert the double bonds into liquid dissolved in saturated alkane, and thus, the liquid can enter a continuous tubular reactor. Then, a specific catalyst is used for further carrying out hydrodeoxygenation reaction, so that oxygen atoms in the product can be removed in the form of water, and the lignocellulose hydrolysate has higher calorific value and chemical stability. Finally, the invention also reduces the freezing point of the hydrocarbon fuel through an isomerization treatment process, and finally fractionates to obtain the biological aviation kerosene component oil with high added value. The whole process is reasonable in design and less in side reaction, and the adopted hydrogenation catalyst has the characteristics of high activity, high stability, good reusability and the like, so that the reaction conversion rate and yield are further improved, and the method has a good application prospect.

The method for producing the biological aviation kerosene component oil will be described in detail below.

In step S1, an aldol condensation reaction is performed on lignocellulose-based furfural compounds and carbonyl compounds using an alkali catalyst. The lignocellulose-based furfural compound is selected from one or more of furfural and 5-hydroxymethyl furfural, the carbonyl compound is an alpha-H carbonyl compound, and the alpha-H carbonyl compound is selected from one or more of acetone and levulinic acid. In some embodiments, the molar ratio of lignocellulose-based furfural-based compound to carbonyl compound is 1:2 to 5:1, e.g., 1:2, 1:1, 3.5, 4:1, 5:1, etc..

In some embodiments, the base catalyst is an inorganic base selected from one or more of sodium hydroxide, potassium hydroxide, ammonia, sodium carbonate and potassium carbonate, and the molar concentration of the inorganic base is 0.05mol/L to 1mol/L.

In aldolizationIn the synthesis reaction, a batch tank reactor is generally used, and the reaction temperature is 0 ℃ to 100 ℃, for example, 0 ℃, 10 ℃, 25 ℃,40 ℃, 55 ℃, 70 ℃, 75 ℃, 80 ℃, 94 ℃, 100 ℃ and the like. The reaction time is 1h to 12h, such as 1h, 2h, 4h, 6h, 8h, 11h, 12h and the like; the reaction solvent is water, the molar concentration of the inorganic base in the reaction solution is 0.05mol/L to 1.00mol/L, such as 0.05mol/L, 0.15mol/L, 0.85mol/L, 0.13mol/L, 0.68mol/L, 0.93mol/L, 1mol/L and the like, and the mass fraction of the lignocellulose-based furfural-based compound in the reaction solution is 5% to 40%, such as 5%, 15%, 20%, 27%, 34%, 38%, 40% and the like. By selecting the above specific test conditions, especially by controlling the molar ratio of the raw materials, carbon chain regulation can be performed, thereby preparing C ₈ ～C ₁₆ A long chain oxygen-containing compound.

In step S2, after the aldol condensation reaction is completed, the resultant C is subjected to ₈ ～C ₁₆ And (4) hydrogenating and saturating the long-chain oxygen-containing compound. Taking the condensation reaction of furfural and acetone as an example, the generated difurfurylideneacetone is solid and is difficult to directly enter a tubular reactor for continuous treatment; in addition, for example, furfurylideneacetone, difurfurylideneacetone, and the like have a large conjugated structure having a furan ring and a C = C double bond, and are unstable at high temperatures and are liable to cause side reactions such as self-polymerization. Therefore, the hydrogenation pretreatment is firstly completed at a lower temperature, namely the hydrogenation saturation is carried out on the hydrogenation pretreatment, so that the side reaction in the subsequent hydrodeoxygenation process carried out at a higher temperature can be avoided; by simultaneously saturating the double bonds C = C and C = O, the solid product can be converted into a liquid dissolved in saturated alkane, and then can enter a continuous tubular reactor for subsequent reaction.

The hydrogenation saturation process mainly comprises the following steps: c is to be ₈ ～C ₁₆ The long-chain oxygen-containing compound is dissolved in an organic solvent, and the obtained solution is subjected to hydrogenation saturation reaction in a fixed bed reactor containing a hydrogenation saturation catalyst, so that a hydrogenation saturation product is obtained. Wherein the organic solvent is selected from one or more of oxygen-containing solvents such as methanol, ethanol, and acetone, and in some embodiments, C in solution ₈ ～C ₁₆ The mass percentage of the long-chain oxygen-containing compound is 0.5-50 percent, such as 0.5 percent, 1.7 percent, 3.8 percent, 12 percent and 24 percent32%, 40%, 47%, 50% etc.

The hydrogenation saturation catalyst comprises a composite of nickel and silica, wherein the nickel is in a crystal structure, and the silica is in an amorphous structure. Specifically, the chemical formula of the compound is Ni- (SiO) ₂ ) _a And a has a value of 0.1 to 40, for example, 2.1, 3, 3.2, 4.5, 5, 6.7, 6.8, 6.9, 7, 7.1, 10, 10.8, 11, 13.9, 14, etc. In some embodiments, preferably, a is 2.9 to 11.1. The structure of the composite is a porous structure formed by gathering nickel crystal grains and silicon dioxide oxide particle clusters, the particle clusters are distributed irregularly, the cluster size is 200 nm-500 nm, and the nickel crystal grain size is 0.5 nm-10 nm. The specific surface area of the hydrogenation saturation catalyst is 200m ² /g～500m ² A/g, preferably of 200m ² /g～380m ² G, e.g. 220m ² /g、240m ² /g、300m ² /g、320m ² (iv)/g, etc.; the pore volume is 0.2cc/g to 0.7cc/g, preferably 0.3cc/g to 0.6cc/g, for example, 0.37cc/g, 0.40cc/g, 0.42cc/g, 0.44cc/g, 0.45cc/g, etc. From the foregoing, it can be seen that the hydrogenation saturation catalyst has a specific porous cluster aggregation structure, which is beneficial to increasing the specific surface area of the catalyst in contact with reactants, and further improving the catalytic activity. In some embodiments, the hydrosaturation catalyst comprises nickel in an amount of 1wt% to 60wt% and silica in an amount of 40wt% to 99wt%. Preferably, the nickel content is 5wt% to 40wt%, and the silica content is 60wt% to 95wt%.

The hydrogenation saturation catalyst can be prepared by a precipitation method or a sol-gel method.

In some embodiments, the precipitation method comprises: adding alkali into the mixture of the nickel source and the silicon source for reaction to generate a precipitate; and drying, roasting and reducing the precipitate to obtain the hydrogenation saturation catalyst. Furthermore, the catalyst can be shaped during the preparation process of the hydrogenation saturation catalyst to improve the mechanical strength of the catalyst. Specifically, the method comprises the following steps: adding alkali into the mixture of the nickel source and the silicon source for reaction to generate a precipitate; drying the precipitate, adding an auxiliary agent, and carrying out molding treatment; and reducing the formed material to obtain the hydrogenation saturation catalyst. Wherein the forming process includes, but is not limited to, one or more of extruding, rolling, tabletting, and pelletizing.

In the process of precipitation reaction, firstly, the soluble nickel source and the soluble silicon source are mixed with water to prepare a mixed solution, then alkali liquor is added into the mixed solution, and the mixture is stirred to generate precipitate. Generally, the reaction temperature for generating the precipitate is 0 ℃ to 60 ℃, and the stirring time is 0h to 6h, i.e., the stirring may be carried out or not. Standing and aging for a period of time after the precipitate is generated, wherein the standing time is about 6-12 h, preferably 8-12 h; then, the precipitate after the standing aging is dried, and then, the molding treatment can be performed. The drying temperature is 100-130 ℃, and the drying time is 2-24 h. In some embodiments, the precipitate is dried and then is further roasted, wherein the roasting temperature is 300-700 ℃, and the roasting time is 2-6 h. Then, reducing the roasted product at 400-600 ℃ for 2-6 h. And reducing to obtain a compound of crystalline nickel and amorphous silicon dioxide, namely the hydrogenation saturation catalyst. By adopting the hydrogenation saturation catalyst, the preparation method is simple, pollution-free and low in cost, and the obtained catalyst is higher in activity and stability and easier to separate.

In some embodiments, the sol-gel process comprises: adding a hydrolytic agent and water into a mixture of a nickel source and a silicon source to carry out sol-gel reaction; and drying, roasting and reducing the product obtained after the sol-gel reaction to obtain the hydrogenation saturation catalyst. Furthermore, the catalyst can be shaped during the preparation process of the hydrogenation saturation catalyst to improve the mechanical strength of the catalyst. The method specifically comprises the following steps: adding a hydrolytic agent and water into a mixture of a nickel source and a silicon source to carry out sol-gel reaction; adding an auxiliary agent into the product after the sol-gel reaction for molding treatment; and reducing the formed material to obtain the hydrogenation saturation catalyst. Wherein the forming process includes, but is not limited to, one or more of extruding, rolling, tabletting, and pelletizing.

In the sol-gel reaction process, firstly mixing a nickel source, a silicon source and water to prepare a mixed solution, then adding a hydrolytic agent into the mixed solution, and stirring to generate sol; and standing and aging the obtained sol to obtain gel. In the sol-gel reaction process, the temperature of the standing and aging is generally 0 to 60 ℃, preferably 10 to 30 ℃, and the time of the standing and aging is 0 to 24 hours, preferably 2 to 12 hours. The hydrolytic agent is generally an acid or an alkali, and the concentration of the hydrolytic agent is 0.5mol/L to 2mol/L, such as 0.5mol/L, 1mol/L, 1.5mol/L, 2mol/L and the like. The acid is selected from one or more of hydrochloric acid, sulfuric acid, nitric acid, formic acid, acetic acid, oxalic acid and citric acid, and the base is selected from one or more of ammonia water, triethylamine, ethylenediamine and tetramethylethylenediamine. Drying and roasting the product after the sol-gel reaction, wherein the drying temperature is 60-120 ℃, preferably 100-120 ℃, the roasting temperature is 300-700 ℃, and the roasting time is 2-6 h. Then, reducing the roasted product at 400-600 deg.c for 2-6 hr. And reducing to obtain a compound of crystalline nickel and amorphous silicon dioxide, namely the hydrogenation saturation catalyst.

In some embodiments, the nickel source used in the aforementioned precipitation method or sol-gel method is a soluble nickel source, and may be one or more of basic nickel carbonate, nickel nitrate, nickel sulfate, nickel chloride and nickel acetate, and the silicon source is a soluble silicon source, and may be one or more of water glass, silica sol and ethyl orthosilicate; the alkali is one or more selected from sodium hydroxide, potassium hydroxide, ammonia water, sodium carbonate, potassium carbonate, sodium bicarbonate, potassium bicarbonate and ammonium carbonate. The molar ratio of the nickel source to the silicon source is 1 (0.1-40), for example, 1:3, 1. In one embodiment, the molar ratio of the nickel source to the silicon source is 1 (2-15).

The prepared hydrogenation saturation catalyst is used in the hydrogenation saturation reaction, wherein the hydrogenation saturation reaction temperature is 0-200 ℃, for example, 0 ℃,12 ℃, 35 ℃, 46 ℃, 58 ℃, 70 ℃, 75 ℃, 80 ℃, 94 ℃ and the like, and is generally lower than the hydrogenation deoxidation temperature. The reaction pressure is 0.5MPa to 15MPa, for example, 0.5MPa, 1.6MPa, 3MPa, 4.5MPa, 5MPa, 6.7MPa, 7.2MPa, 10MPa, 13MPa, etc. The mass space velocity is 0.1h ^-1 ～10h ^-1 For example, 0.7h ^-1 、1h ^-1 、3h ^-1 、5.5h ^-1 、7.2h ^-1 、10h ^-1 And so on. The hydrogen-oil volume ratio is 50 to 3000, and may be further 300 to 1000, for example, 500, 600, 800, or the like.

In step S3, the hydrodeoxygenation reaction of the hydrogenated saturated product includes: the hydrogenation saturated product is subjected to hydrodeoxygenation reaction in a fixed bed reactor containing a hydrodeoxygenation catalyst, and the reaction can be carried out under the condition of solvent or no solvent. Wherein the reaction temperature is 100 ℃ to 400 ℃, for example, 110 ℃, 220 ℃, 350 ℃, 380 ℃ and the like. The reaction pressure is 0.5MPa to 15MPa, for example, 0.5MPa, 1.6MPa, 3MPa, 4.5MPa, 5MPa, 6.7MPa, 7.2MPa, 10MPa, 13MPa, etc. The mass space velocity is 0.1h ^-1 ～10h ^-1 For example, 0.7h ^-1 、1h ^-1 、3h ^-1 、5.5h ^-1 、7.2h ^-1 、10h ^-1 And the like. The hydrogen-oil volume ratio is 50 to 3000, and may be further 300 to 1000, for example, 500, 600, 800, or the like.

The hydrodeoxygenation catalyst is a specific supported catalyst and comprises a first carrier and a first active metal loaded on the first carrier, wherein the first active metal is selected from one or more of nickel, molybdenum, tungsten, cobalt, palladium and platinum, and the first carrier is M- (SiO) ₂ ) _X The composite oxide, M is selected from one or more of niobium oxide, cobalt oxide and cerium oxide, x is 1-100, for example, x can be 4.4, 13, 20.6, 27.2, 31.4, 50.8, 56.6, 73.8, 79.4, 94.2, 99.6, etc. The metal-silicon composite oxide is prepared by a precipitation method or a sol-gel method to be used as a carrier, corresponding active metal is loaded on the carrier, the obtained material has good hydrodeoxygenation catalytic activity, and high stability and reusability, and the material has good effect when being used for catalyzing a condensation product of a sugar platform compound to carry out hydrodeoxygenation reaction to prepare liquid alkane.

In some embodiments, M is Nb in an amorphous structure ₂ O ₅ And x is 1 to 40. Nb of amorphous structure ₂ O ₅ Has good capability of activating carbon-oxygen bonds and promoting carbon in the hydrodeoxygenation processThe oxygen bond is broken, which is beneficial to the catalytic deoxidation reaction. The first active metal is selected from one or more of palladium, nickel and platinum, and the loading amount of the first active metal is 0.05wt% to 30wt%, for example, 0.2wt%,1.5wt%,2wt%,2.6wt%,8wt%,12wt%,15wt%,18wt%,20wt%, etc., preferably 0.1wt% to 25wt%, more preferably 0.2wt% to 20wt%. The load capacity is excessive, and the cost is too high; too little loading means that there are fewer metal hydrogenation centers, which is not favorable for exerting hydrogenation activity.

Specifically, with Nb ₂ O ₅ -SiO ₂ The composite oxide is taken as an example of a carrier, and the structure of the composite oxide is mainly Nb ₂ O ₅ And SiO ₂ The oxide particle clusters are in a porous structure formed by aggregating the oxide particle clusters, the particle clusters are distributed irregularly, and the cluster size is 200 nm-2000 nm, preferably 300 nm-600 nm. The specific surface area of the carrier was 200m ² /g～700m ² A ratio of 300 to 500 m/g ² G, e.g. 320m ² /g、360m ² /g、420m ² /g、480m ² And/g, etc. The pore volume is 0.1cc/g to 0.9cc/g, preferably 0.1cc/g to 0.5cc/g, more preferably 0.2cc/g to 0.4cc/g, for example, 0.21cc/g, 0.28cc/g, 0.32cc/g, 0.38cc/g, etc. Further, the foregoing SiO ₂ Is an amorphous structure. The cluster aggregation structure with specific porous holes is beneficial to loading of active metal, promotes diffusion of raw material molecules and improves catalytic activity.

The preparation method of the hydrodeoxygenation catalyst can adopt a coprecipitation method or a sol-gel method and an impregnation method, for example, a hydrolytic agent and water are added into a mixture of an M precursor and a silicon precursor to carry out sol-gel reaction, or alkali is added into the mixture of the M precursor and the silicon precursor to carry out coprecipitation reaction; then roasting the obtained product to obtain M- (SiO) ₂ ) _X A composite oxide; with the M- (SiO) ₂ ) _X And (3) taking the composite oxide as a carrier, preparing an active metal salt solution as an impregnation solution, and loading the active metal on the carrier by adopting an impregnation method to obtain the hydrodeoxygenation catalyst. Similar to the previously described hydrosaturation catalysts, it may also be carried out during the preparation of the hydrodeoxygenation catalystAnd (4) molding treatment to further improve the mechanical strength.

In some embodiments, the M precursor is selected from one or more of citrate, tartrate, malate, nitrate, hydrochloride, and sulfate salts of M, with M being niobium pentoxide (Nb) ₂ O ₅ ) For example, the M precursor may be one or more of niobium citrate, niobium tartrate and niobium malate, and the silicon precursor is one or more selected from water glass, silica sol and ethyl orthosilicate. The hydrolyzing agent in the sol-gel method is an acid or an alkali, and the concentration of the hydrolyzing agent is 0.5mol/L to 2mol/L, for example, 0.5mol/L, 1mol/L, 1.5mol/L, 2mol/L, or the like. The acid is selected from one or more of hydrochloric acid, sulfuric acid, nitric acid, formic acid, acetic acid, oxalic acid and citric acid, and the base is selected from one or more of ammonia water, triethylamine, ethylenediamine and tetramethylethylenediamine. The alkali in the coprecipitation method is one or more selected from sodium hydroxide, potassium hydroxide, ammonia water, sodium carbonate, potassium carbonate, sodium bicarbonate, potassium bicarbonate and ammonium carbonate.

The hydrodeoxygenation catalyst prepared by the method has a relatively larger specific surface area due to the special structure of the carrier, and the porous structure is beneficial to the diffusion of raw material molecules, so that the integral catalytic performance is improved. In addition, the catalyst has the characteristics of easy separation and good reusability, so that the catalyst is suitable for the method of the invention, and can further improve the overall reaction conversion rate and yield and ensure the subsequent reaction.

In step S4, C is obtained after hydrodeoxygenation ₈ ～C ₁₆ Long-chain alkanes. For C is to ₈ ～C ₁₆ The long-chain alkane is further subjected to isomerization treatment, comprising: c ₈ ～C ₁₆ The long-chain alkane is isomerized in a fixed bed reactor containing a hydroisomerization catalyst, and the reaction can be carried out under the condition of solvent or no solvent. Wherein the reaction temperature is 100 to 450 ℃, for example, 110 ℃, 220 ℃, 350 ℃, 380 ℃, 410 ℃, 440 ℃ and the like. The reaction pressure is 0.5MPa to 15MPa, for example, 0.5MPa, 1.6MPa, 3MPa, 4.5MPa, 5MPa, 6.7MPa, 7.2MPa, 10MPa, 13MPa, etc. The mass space velocity is 0.1h ^-1 ～10h ^-1 For example, 0.7h ^-1 、1h ^-1 、3h ^-1 、5.5h ^-1 、7.2h ^-1 、10h ^-1 And the like. The hydrogen-oil volume ratio is 50 to 3000, and may be further 300 to 1000, for example, 500, 600, 800, or the like.

The hydroisomerization catalyst comprises a second carrier and a second active metal loaded on the second carrier, wherein the second active metal is selected from one or more of nickel, molybdenum, tungsten, cobalt, palladium and platinum, and the second carrier is selected from one or more of ZSM5, ZSM12, ZSM22, ZSM23, ZSM35, ZSM48, SAPO11, beta and Y molecular sieves. The hydroisomerization catalyst can be prepared by adopting an impregnation method, wherein a second active metal precursor solution is added into a second carrier, the second carrier is kept stand for 2 to 12 hours, then the second carrier is roasted for 2 to 6 hours in a muffle furnace at the temperature of 300 to 600 ℃, and finally the second carrier is reduced for 2 to 6 hours by hydrogen at the temperature of 0 to 500 ℃.

The isomerization treatment process can be adopted to reduce the freezing point of the hydrocarbon fuel, and finally the biological aviation kerosene component oil with high added value is obtained by fractionation. The biological aviation kerosene component oil obtained through the process can fully realize catalytic conversion based on the biomass-based sugar platform compound, the yield of the biological aviation kerosene component oil is higher than 80%, the comprehensive utilization of agricultural and forestry wastes is facilitated, and the green sustainable development is realized. The obtained biological aviation kerosene component oil can be used for blending and preparing biological aviation kerosene, can also be used as a biological aviation kerosene additive, improves the physicochemical properties of aviation kerosene, and has wide application prospect.

The invention will be further illustrated by the following examples, but is not to be construed as being limited thereto.

The invention adopts a Fourier transform infrared spectrometer produced by German Bruker company to carry out infrared analysis (FT-IR), a sample absorbs infrared light with specific frequency, a detector detects that the intensity of interference light changes, interference light intensity signals under different moving distances of a movable mirror are obtained, then Fourier transform is carried out to obtain a curve of the change of the intensity of light along with the frequency, and the resolution is 4cm ^-1 Scanning 16 times;

the nuclear magnetic resonance hydrogen spectrum analysis (1H-NMR) of the product is carried out on a nuclear magnetic resonance spectrometer produced by Varian corporation in America, samples are scanned by changing the magnetic field intensity, a receiver displays a series of absorption signals which are characterized by gyromagnetic ratio, and related analysis is carried out in sequence, and the temperature control range is-150-180 ℃;

the hydrogenation product of the invention is respectively qualitatively and quantitatively analyzed on a mass spectrum detector and a hydrogen flame ion detector of an Agilent 5977A-7890B gas chromatograph-mass spectrometer.

The catalyst strength in the present invention refers to the radial (i.e., the direction passing through the axis line in the radial plane) strength of the strip catalyst; the strength was measured using a mechanical strength meter.

Preparation example 1

This preparation example is intended to illustrate the preparation process of the hydrosaturation catalyst of the present invention.

290g of Ni (NO) are weighed ₃ ) ₂ ·6H ₂ Dissolving O and 1600g of silica sol (with the solid content of 30%) in deionized water to prepare a solution a of 1.0mol/L calculated by Ni ions; preparing 1.0mol/L sodium hydroxide solution b; keeping the solution a in a stirring state, and slowly adding the solution b into the solution a until the pH value of the system is 10.5. After the dropwise addition, stirring is continued for 1h, then stirring is stopped, and standing and aging are carried out for 8h. The precipitate was then filtered, washed to neutrality, and the filter cake was dried in a forced air drying oven at 110 ℃ for 12h and then calcined in a muffle furnace at 500 ℃ for 3h.

Uniformly mixing 160.0g of roasted product, 140.0g of silica sol (with the solid content of 30 percent), 1.0g of citric acid, 10.0g of sesbania powder and 40.0g of water, repeatedly kneading, extruding into cylindrical thin strips with the diameter of 1.8mm by using a strip extruding machine, cutting into strips with the length of 3-5 mm, drying at 120 ℃ for 4h, and roasting at 500 ℃ for 4h; finally, hydrogen reduction was carried out at 400 ℃ for 3 hours to obtain a catalyst in the form of a strip having a mechanical strength of 18.9N/mm.

Fig. 2 shows an XRD spectrum of the hydrogenation saturation catalyst in preparation example 1. As seen from fig. 2: the catalyst has no obvious SiO ₂ Diffraction characteristic peak, indicating SiO ₂ Exist in an amorphous structure. In addition, the catalyst of preparation example 1 has a characteristic peak of Ni diffraction, which indicates that Ni is also present in a crystal structure.

Preparation example 2

This preparation example is intended to illustrate the preparation process of the hydrodeoxygenation catalyst of the invention.

Preparing 0.5mol/L niobium citrate solution a, weighing 14.6g of Tetraethoxysilane (TEOS) and placing the Tetraethoxysilane (TEOS) in 7.9mL of solution a to obtain mixed solution b, then adding citric acid (the weight ratio of the citric acid to the TEOS is 0.2. The gel was dried in a forced air oven at 100 ℃ for 12h and then calcined in a muffle furnace at 600 ℃ for 5h to give a white solid.

PdCl with Pd content of 5g/L ₂ Transferring 3mL of the solution c to prepare a maceration extract d, putting the solution d into 2g of the white solid by an isometric maceration method, uniformly stirring, standing for 12h, and drying in a forced air drying oven at 100 ℃ for 12h; and roasting the mixture for 4 hours at 500 ℃ in a muffle furnace to obtain yellow solid, and finally reducing the yellow solid for 2 hours at 200 ℃ in a hydrogen reduction furnace to obtain the hydrodeoxygenation catalyst.

FIG. 3 is an XRD pattern of the hydrodeoxygenation catalyst of preparation example 2, and from FIG. 3, it can be seen that SiO in the catalyst prepared by the sol-gel method ₂ Exist in an amorphous structure. Active centers Pd and Nb ₂ O ₅ No obvious diffraction peak is generated, which is because the load of Pd is low and the active center Pd is in a high dispersion state; and Nb with a high loading ₂ O ₅ Is an amorphous structure. In general, the better the active center dispersion, the higher the catalytic activity, which verifies the Pd/Nb ratio ₂ O ₅ -SiO ₂ The catalyst has good catalytic activity.

Preparation example 3

This preparation example is intended to illustrate the preparation of the hydroisomerization catalyst of the present invention.

Preparing Pt (NO) with the Pt content of 5g/L ₃ ) ₂ Transferring 3mL of the solution a to prepare a steeping liquor b, placing the solution b on a 2g ZSM22 carrier by adopting an isometric steeping method, uniformly stirring, standing for 12 hours, and then placing the solution b in a blast drying oven to dry for 12 hours at the temperature of 100 ℃; then roasting in a muffle furnace at 500 ℃ for 3h, finally reducing the roasted material in a hydrogen reduction furnace at 300 ℃ for 2h to obtain the hydrogenAn isomerization catalyst.

The following examples 1 to 11 are intended to illustrate the aldol condensation reaction in the process of preparing the bio-aviation fuel composition oil according to the present invention.

Example 1

600mL of 0.3mol/L NaOH aqueous solution is prepared, 115.4g of furfural and 34.9g of acetone are added, and then the mixture is stirred and reacted at 20 ℃ for 24 hours. After the reaction is finished, filtering, washing and drying are carried out to obtain yellow granular crystals, 122.9g of crystals C are weighed ₁₃ The mass yield of the oxygen-containing intermediate (difurfurylideneacetone) is 95.9 percent, and the purity is 99.1 percent. FIG. 4 shows the C-NMR spectrum of the condensation product of example 1, FIG. 5 shows the H-NMR spectrum of the condensation product of example 1, FIG. 6 shows the IR spectrum of the condensation product of example 1, and it can be seen that difurfurylideneacetone, a condensation product, was successfully obtained

The filtered waste lye is recycled for 6 times by repeating the steps, and the yield is as follows 1:

TABLE 1

Example 2

Preparing 0.3mol/L of Na ₂ CO ₃ 600mL of the aqueous solution was added 115.4g of furfural and 34.9g of acetone, followed by stirring at 20 ℃ for 6 hours. After the reaction is finished, yellow granular crystals are obtained by filtering, washing and drying, and 117.9g of the yellow granular crystals are weighed, the yield of the product is 92.0 percent, and the purity is 97.3 percent.

The filtered waste lye is recycled for 1 time by repeating the steps, and the yield is as follows 2:

TABLE 2

Example 3

600mL of 0.3mol/L ammonia water is prepared, 115.4g of furfural and 34.9g of acetone are added, and then the mixture is stirred and reacted at 10 ℃ for 6 hours. After the reaction is finished, the yellow granular crystal is obtained by filtering, washing and drying, and 120.1g is obtained by weighing, the yield of the product is 93.7 percent, and the purity is 97.9 percent.

The filtered waste lye is recycled for 3 times by repeating the steps, and the yield is as follows 3:

TABLE 3

Example 4

600mL of 0.3mol/L KOH aqueous solution is prepared, 115.4g of furfural and 34.9g of acetone are added, and then the mixture is stirred and reacted at 20 ℃ for 6 hours. After the reaction is finished, yellow granular crystals are obtained by filtering, washing and drying, and 119.7g of the yellow granular crystals are weighed, the product yield is 93.4 percent, and the purity is 99.2 percent.

The filtered waste alkali liquor is recycled for 6 times by repeating the steps, and the yield is shown in the following table 4:

TABLE 4

Example 5:

400mL of 0.3mol/L NaOH aqueous solution is prepared, 115.4g of furfural and 34.9g of acetone are added, and then the mixture is stirred and reacted at 20 ℃ for 12 hours. After the reaction is finished, yellow granular crystals are obtained by filtering, washing and drying, and 119.7g of the yellow granular crystals are weighed, the product yield is 93.4 percent, and the purity is 99.2 percent.

The filtered waste lye is recycled for 2 times by repeating the steps, and the yield is as follows 5:

TABLE 5

Example 6

800mL of 0.3mol/L KOH aqueous solution is prepared, 115.4g of furfural and 34.9g of acetone are added, and then the mixture is stirred and reacted at 20 ℃ for 4 hours. After the reaction is finished, filtering, washing and drying are carried out to obtain yellow granular crystals, and 126.9g of the yellow granular crystals are obtained by weighing, the yield of the product is 99.0 percent, and the purity is 99.2 percent.

The filtered waste alkali liquor is recycled for 6 times by repeating the steps, and the yield is as follows in the following table 6:

TABLE 6

Example 7

600mL of 0.5mol/L KOH aqueous solution is prepared, 115.4g of furfural and 34.9g of acetone are added, and then the reaction is stirred at 20 ℃ for 6h. After the reaction is finished, yellow granular crystals are obtained by filtering, washing and drying, 126.1g of the yellow granular crystals are obtained by weighing, the yield of the product is 98.2 percent, and the purity is 98.5 percent.

The filtered waste lye is recycled for 6 times by repeating the steps, and the yield is as follows 7:

TABLE 7

Example 8

600mL of 0.2mol/L NaOH aqueous solution is prepared, 57.7g of furfural and 34.9g of acetone are added, and then stirring reaction is carried out at 20 ℃ for 6 hours. After the reaction is finished, yellow granular crystals are obtained by filtering, washing and drying, 77.5g of yellow granular crystals are obtained by weighing, and the yield of the oxygen-containing intermediate product is 94.7 percent, wherein the oxygen-containing intermediate comprises C ₈ Oxygen-containing intermediate

And C ₁₃ Oxygen-containing intermediate (difurfurylideneacetone), C ₈ Oxygenated intermediates->

Selectivity 58.5%, C ₁₃ The selectivity of the oxygen-containing intermediate difurfurylideneacetone was 36.7%. Therefore, condensation products with different carbon chain lengths can be obtained in a targeted manner by regulating the proportion of the raw materials.

The filtered waste lye is recycled for 2 times by repeating the steps, and the yield is as follows:

TABLE 8

Example 9

600mL of 0.5mol/L NaOH aqueous solution is prepared, 115.4g of furfural and 17.4g of acetone are added, and then stirring reaction is carried out at 20 ℃ for 6 hours. After the reaction, the reaction mixture was filtered, washed with water and dried to obtain yellow granular crystals, and 10.5g of the yellow granular crystals were weighed. Due to the excess of furfural, most of the product dissolved in the reaction solution, resulting in a severe reduction in product yield. The alkali liquor can not be recycled.

Example 10

600mL of 0.5mol/L NaOH aqueous solution is prepared, 115.4g of furfural and 69.7g of levulinic acid are added, and then the mixture is stirred and reacted at 20 ℃ for 6 hours. After the reaction is finished, acid neutralization and separation are carried out to obtain

126.1g is weighed, the product yield is 98.2 percent, and the purity is 98.5 percent. The concentration of the alkali liquor is not enough to be continuously recycled for catalytic reaction due to the neutralization of the acid liquor.

Example 11

600mL of 0.5mol/L NaOH aqueous solution is prepared, 151.3g of 5-hydroxymethylfurfural and 34.9g of acetone are added, and then the mixture is stirred and reacted at the temperature of 20 ℃ for 6 hours. Separating after the reaction is finished to obtain the dimethylol furylideneacetone

Weighing 162.1g, yield 98.5% pure productThe degree is 98.1%.

The waste alkali liquor is recycled for 6 times by repeating the steps, and the yield is as follows in the following table 9:

TABLE 9

The following examples 12 to 20 are provided to illustrate the hydrogenation saturation reaction in the process of preparing bio-aviation kerosene component oil according to the present invention, wherein fig. 7 shows a process flow diagram of the hydrogenation saturation reaction according to an embodiment of the present invention.

Examples 12 to 20

As shown in fig. 7, the condensation product obtained after the aldol condensation reaction and the oxygen-containing solvent are placed in a mixer 1, stirred, dissolved, preheated by a heating furnace 2, and then enter a hydrogenation reactor 3 together with hydrogen, and react under the action of the hydrogenation saturation catalyst in preparation example 1, the reacted material is separated into gas-phase and liquid-phase material flows by a first separator 4, wherein the gas-phase material flow hydrogen is recycled after being pressurized. The liquid phase material flow enters a second separator 5, the second separator 5 is a normal pressure separation tower, the material flow at the top of the tower is condensed by a condenser 6 and then mixed with a new solvent to enter a mixer 1, and the tower bottom flows out of the device, wherein the operation conditions and the reaction results of the specific examples 12-20 are respectively shown in a table 10.

Watch 10

The following examples 21 to 28 are provided to illustrate the hydrodeoxygenation reaction in the process of preparing bio-aviation kerosene component oil according to the present invention, and fig. 6 shows a process flow diagram of the hydrodeoxygenation reaction according to an embodiment of the present invention.

Examples 21 to 28

As shown in fig. 8, the hydrogenation saturated product is placed in a mixing tank 21, preheated by a heating furnace 22, and then enters a hydrogenation reactor 23 together with hydrogen, and reacts under the action of the hydrodeoxygenation catalyst of preparation example 2, the reacted material is separated into a gas phase material flow and a liquid phase material flow by a first separator 24, wherein the gas phase material flow hydrogen is recycled after being pressurized. FIG. 9 and FIG. 10 show the dodecane and tridecane MS spectra of the hydrodeoxygenation product of example 21. Specific operating conditions and reaction results are shown in Table 11.

TABLE 11

The following examples 29 to 36 are provided to illustrate the isomerization reaction in the process of preparing bio-aviation kerosene component oil according to the present invention, wherein fig. 11 shows a process flow diagram of the isomerization reaction according to an embodiment of the present invention.

Examples 29 to 36

As shown in fig. 11, the hydrodeoxygenation product is placed in a mixing tank 31, preheated by a heating furnace 32, and then enters a hydrogenation reactor 33 together with hydrogen, and reacts under the action of the hydroisomerization catalyst of preparation example 3, and the reacted material is separated into a gas phase material and a liquid phase material by a first separator 34, wherein the gas phase material hydrogen is recycled after being pressurized. The liquid phase material enters a rectifying tower 35 and is fractionated to obtain the biological aviation kerosene component oil (150-350 ℃). Specific operating conditions and reaction results are shown in Table 12.

TABLE 12

Comparative example 1

The condensation product obtained in example 1 was directly subjected to hydrodeoxygenation, the test conditions and results of which are given in table 13 below.

Watch 13

	Comparative example 1
		Condensation products	Example 1
Mixer atmosphere/pressure, MPa	Nitrogen/0.5
		Preheating temperature of heating furnace,. Degree.C	220
Hydrogen pressure, MPa, of the reactor	3.0
		Reactor temperature,. Deg.C	240
Mass space velocity h ^-1	0.80
		Volume ratio of hydrogen to oil, v/v	1500
Condenser temperature,. Degree.C	20
		Conversion rate%	98
Hydrodeoxygenation product (C) ₈ ～C ₁₅ Alkane), yield/%	78% of yellow liquid

Comparative example 2

The condensation product of example 1 was subjected to the hydrogenation saturation reaction in the same manner as in example 12, and the obtained product was subjected to the hydrodeoxygenation reaction in the same manner as in example 21. Different from the prior art, the adopted catalysts are Raney Ni catalysts in the hydrogenation saturation reaction process, and the adopted catalysts are sulfuration state Ni-W/Al in the hydrogenation deoxidation reaction process ₂ O ₃ A catalyst. The conversion rate of the obtained hydrogenation saturated product is 95%, the conversion rate of the hydrogenation deoxidation product is 91% and the yield is 75% through calculation.

Therefore, compared with the traditional hydrogenation catalyst, the hydrogenation saturation catalyst and the hydrogenation deoxidation catalyst have better catalytic activity. It can be seen from the above examples 1-36 and comparative examples 1-2 that the bio-aviation kerosene component oils prepared by the method of the present invention have the characteristics of high conversion rate and high yield, and compared with the method in which the condensation product is directly subjected to hydrodeoxygenation, the method of the present invention first performs hydrogenation pretreatment, i.e., hydrogenation saturation treatment, on the condensation product, so that the product can obtain higher calorific value and chemical stability, side reactions are reduced, and the conversion rate and yield are both improved.

In summary, the preparation method of the biological aviation kerosene component oil provided by the invention has the advantages that the synthesis route is redesigned, the hydrogenation saturation treatment is carried out before the hydrodeoxygenation is carried out on the condensation product, and the proper specific catalyst is adopted in each step, so that the side reaction in the whole reaction process is less, the conversion rate and the yield are higher, the production cost is reduced, and the preparation method has a good application prospect. The method can realize catalytic conversion based on the biomass sugar platform compound to prepare the biological aviation kerosene component oil, is beneficial to comprehensive utilization of agricultural and forestry wastes, and realizes green sustainable development.

It should be noted by those skilled in the art that the described embodiments of the present invention are merely exemplary and that various other substitutions, alterations, and modifications may be made within the scope of the present invention. Accordingly, the present invention is not limited to the above-described embodiments, but is only limited by the claims.

Claims

1. A preparation method of biological aviation kerosene component oil is characterized by comprising the following steps:

performing aldol condensation reaction on lignocellulose-based furfural compound and carbonyl compound to obtain C ₈ ～C ₁₆ A long chain oxygen-containing compound;

for the C ₈ ～C ₁₆ Carrying out hydrogenation saturation on the long-chain oxygen-containing compound;

hydrodeoxygenation of the hydrosaturated product to yield C ₈ ～C ₁₆ Long-chain alkanes; and

for the C ₈ ～C ₁₆ Isomerizing long-chain alkane, and fractionating to obtain the biological aviation kerosene component oil;

the aldol condensation reaction is carried out under the action of a base catalyst;

the hydrogenation saturation is carried out under the action of a hydrogenation saturation catalyst, and the hydrogenation saturation catalyst comprises a compound of nickel and silicon dioxide, wherein the silicon dioxide is in an amorphous structure, and the nickel is in a crystal structure;

the hydrodeoxygenation is carried out under the action of a hydrodeoxygenation catalyst, the hydrodeoxygenation catalyst comprises a first carrier and a first active metal loaded on the first carrier, wherein the first active metal is selected from one or more of nickel, molybdenum, tungsten, cobalt, palladium and platinum, and the first carrier is M- (SiO) ₂ ) _X A composite oxide of M selected from the group consisting of niobium oxide, cobalt oxide and cerium oxideX is 1 to 100;

the isomerization treatment is carried out under the action of a hydroisomerization catalyst, wherein the hydroisomerization catalyst comprises a second carrier and a second active metal loaded on the second carrier, the second active metal is selected from one or more of nickel, molybdenum, tungsten, cobalt, palladium and platinum, and the second carrier is selected from one or more of ZSM5, ZSM12, ZSM22, ZSM23, ZSM35, ZSM48, SAPO11, beta and Y molecular sieves.

2. The preparation method according to claim 1, wherein the lignocellulose-based furfural compound is one or more selected from furfural and 5-hydroxymethylfurfural, the carbonyl compound is an alpha-H carbonyl compound, the alpha-H carbonyl compound is one or more selected from acetone and levulinic acid, and the molar ratio of the lignocellulose-based furfural compound to the carbonyl compound is 1:2-5:1.

3. The preparation method of claim 1, wherein the base catalyst is an inorganic base selected from one or more of sodium hydroxide, potassium hydroxide, ammonia water, sodium carbonate and potassium carbonate, and the molar concentration of the inorganic base is 0.05mol/L to 1mol/L.

4. The method of claim 1, wherein the compound has a chemical formula of Ni- (SiO) ₂ ) _a And a has a value of 0.1 to 40.

5. The method of claim 1, wherein the hydrosaturating comprises: subjecting said C to ₈ ～C ₁₆ Dissolving a long-chain oxygen-containing compound in an organic solvent, and carrying out hydrogenation saturation reaction on the obtained solution in a fixed bed reactor containing the hydrogenation saturation catalyst, wherein the organic solvent is an oxygen-containing solvent, the oxygen-containing solvent is selected from one or more of methanol, ethanol and acetone, and C in the solution ₈ ～C ₁₆ The mass percent of the long-chain oxygen-containing compound is 0.5 percent～50％。

6. The preparation method of claim 1, wherein the hydrogenation saturation reaction temperature is 0-200 ℃, the reaction pressure is 0.5-15 MPa, and the mass space velocity is 0.1h ^-1 ～10h ^-1 The volume ratio of hydrogen to oil is 50-3000.

7. The method according to claim 1, wherein M is Nb in an amorphous structure ₂ O ₅ X is 1 to 40; the first active metal is selected from one or more of palladium, nickel and platinum, and the loading amount of the first active metal is 0.05-30 wt%.

8. The method according to claim 1, wherein the first carrier is composed of M and SiO ₂ Porous structure of cluster-aggregated oxide particles, siO ₂ The carrier is an amorphous structure, the size of the cluster is 200 nm-2000 nm, and the specific surface area of the first carrier is 200m ² /g～700m ² (iii) a pore volume of 0.1cc/g to 0.9cc/g.

9. The method of claim 1, wherein the hydrodeoxygenation comprises: the hydrogenation saturated product is subjected to hydrogenation deoxidation reaction in a fixed bed reactor containing the hydrogenation deoxidation catalyst, wherein the reaction temperature is 100-400 ℃, the reaction pressure is 0.5-15 MPa, and the mass space velocity is 0.1h ^-1 ～10h ^-1 The volume ratio of hydrogen to oil is 50-3000.

10. The method according to claim 1, wherein the isomerization treatment comprises: said C is ₈ ～C ₁₆ The long-chain alkane is subjected to isomerization treatment in a fixed bed reactor containing the hydroisomerization catalyst, wherein the reaction temperature is 100-450 ℃, the reaction pressure is 0.5-15 MPa, and the mass space velocity is 0.1h ^-1 ～10h ^-1 The volume ratio of hydrogen to oil is 50-3000.

11. A biological aviation kerosene component oil prepared by the method of any one of claims 1 to 10.