阅读说明：本技术 烷烃组合物、含该烷烃组合物的100号无铅航空汽油组合物及其生产方法 (Alkane composition, No. 100 unleaded aviation gasoline composition containing alkane composition and production method thereof ) 是由 杜文莉 隆建 钱锋 钟伟民 杨明磊 于 2021-10-12 设计创作，主要内容包括：本发明提供一种烷烃组合物、含该烷烃组合物的100号无铅航空汽油组合物及其生产方法,所述烷烃组合物含有C4烷烃、C5烷烃、C6烷烃、C7烷烃、C8烷烃和C9烷烃,所述航空汽油组合物含有基础油和添加剂,所述基础油包括作为调合组分A的所述烷烃组合物、调合组分B、调合组分C和调合组分D,所述添加剂包括甲基环戊二烯三羰基锰。本发明的航空汽油组合物在满足抗爆性、蒸发性及安定性等各项指标要求的同时,不含有四乙基铅,可以降低燃烧时产生的污染,对环境友好,能满足人们环保的需求。本发明的航空汽油组合物辛烷值在99.6到103之间,蒸气压和馏程均满足要求,成本低,原料简单易得,制备方法简单。(The invention provides an alkane composition, a No. 100 unleaded aviation gasoline composition containing the alkane composition and a production method thereof, wherein the alkane composition contains C4 alkane, C5 alkane, C6 alkane, C7 alkane, C8 alkane and C9 alkane, the aviation gasoline composition contains base oil and an additive, the base oil comprises the alkane composition serving as a blending component A, a blending component B, a blending component C and a blending component D, and the additive comprises methylcyclopentadienyl manganese tricarbonyl. The aviation gasoline composition disclosed by the invention meets the requirements of various indexes such as antiknock property, evaporability and stability, does not contain tetraethyl lead, can reduce pollution generated during combustion, is environment-friendly, and can meet the requirements of people on environmental protection. The aviation gasoline composition has the octane number of 99.6-103, the vapor pressure and the distillation range meeting the requirements, the cost is low, the raw materials are simple and easy to obtain, and the preparation method is simple.)

1. An alkane composition comprising, based on the total weight of the alkane composition, 3 to 9 wt% of a C4 alkane, 2 to 7 wt% of a C5 alkane, 4 to 9 wt% of a C6 alkane, 21 to 30 wt% of a C7 alkane, 56 to 70 wt% of a C8 alkane, and 0.51 to 2.4 wt% of a C9 alkane.

2. The alkane composition of claim 1,

the alkane composition comprises 3.76 to 7.38 weight percent of C4 alkane, 2.61 to 4.78 weight percent of C5 alkane, 4.46 to 8.91 weight percent of C6 alkane, 22.37 to 28.67 weight percent of C7 alkane, 56.53 to 68.67 weight percent of C8 alkane, and 0.54 to 2.31 weight percent of C9 alkane, based on the total weight of the alkane composition; and/or

The initial boiling point of the alkane composition is 21-45 ℃, and the final boiling point is 140-153 ℃; preferably, the alkane composition has an initial boiling point of 40-45 ℃ and an end point of 145-153 ℃.

3. A process for preparing the alkane composition of claim 1 or 2, characterized in that the process comprises: distilling the alkylation reaction product of C4 olefin and isobutane to obtain a component with an initial boiling point of 21-45 ℃ and an end boiling point of 140-153 ℃ as the alkane composition;

preferably, the alkylation reaction temperature is 4-10 ℃, the pressure is 0.4-0.45MPa, and the molar ratio of isobutane to C4 olefin is 8-12: 1.

4. The process according to claim 3, wherein the alkylation reaction product of C4 olefin and isobutane is distilled using a distillation column having a bottom temperature of 136-145 ℃, a bottom pressure of 0.43-0.52MPa, an overhead temperature of 51-56 ℃ and an overhead pressure of 0.41-0.53 MPa;

preferably, the components with the initial boiling point of 21-45 ℃ and the end boiling point of 140-153 ℃ are extracted from the side line of the distillation tower, or the components with the initial boiling point of 21-45 ℃ and the end boiling point of 140-153 ℃ are cut from the bottom oil of the distillation tower.

5. An aviation gasoline composition, which is characterized by comprising base oil and an additive, wherein the base oil comprises a blending component A, a blending component B, a blending component C and a blending component D; wherein the blending component a is the alkane composition of claim 1 or 2; the base oil comprises 60-80 wt% of blending component A, 5-20 wt% of blending component B, 5-20 wt% of blending component C and 10-20 wt% of blending component D based on the total weight of the base oil; the additive comprises methylcyclopentadienyl manganese tricarbonyl;

wherein the blending component B contains more than 95 wt% of C7 aromatic hydrocarbon based on the total weight of the blending component B;

the blending component C is selected from one or more of paraxylene, metaxylene, mesitylene and cumene;

the blend component D contains 0.3 to 5.1 weight percent of C4 alkane, 41 to 75 weight percent of C5 alkane, 25 to 50 weight percent of C6 alkane and 0.05 to 0.7 weight percent of C7 alkane based on the total weight of the blend component D.

6. The aviation gasoline composition of claim 5 wherein said aviation gasoline composition has one or more of the following characteristics:

the base oil comprises 60-75 wt% of blending component A, 8-18 wt% of blending component B, 7-15 wt% of blending component C and 10-15 wt% of blending component D based on the total weight of the base oil;

the blending component B also contains C8 aromatic hydrocarbon, and the total content of the C7 aromatic hydrocarbon and the C8 aromatic hydrocarbon is more than 98 weight percent based on the total weight of the blending component B;

the initial distillation point of the blending component B is 107-112 ℃, and the final distillation point is 110-113 ℃;

based on the total weight of the blending component D, the blending component D contains 3-5.1 wt% of C4 alkane, 60-70 wt% of C5 alkane, 25-35 wt% of C6 alkane and 0.1-0.7 wt% of C7 alkane;

the initial boiling point of the blending component D is 26-30 ℃, and the final boiling point is 60-64 ℃;

based on the total volume of the base oil, the content of the methylcyclopentadienyl manganese tricarbonyl is 100-200 mg/L;

the aviation gasoline composition is free of tetraethyl lead;

the aviation gasoline composition does not contain aromatic amine compounds and methyl tertiary butyl ether.

7. The aviation gasoline composition of claim 5 further comprising one or more selected from the group consisting of an antioxidant, an anti-icing agent, an anti-static agent, an anti-corrosion agent, and a dye.

8. The aviation gasoline composition of claim 5 wherein said aviation gasoline composition has a motor octane number of not less than 99.6;

preferably, the aviation gasoline composition has a motor octane number of 100-103.

9. A process for preparing the aviation gasoline composition of any one of claims 5 to 8 comprising the step of mixing the components of the aviation gasoline composition.

10. Use of the alkane composition of claim 1 or 2 or obtained by the process of claim 3 or 4 for the preparation of aviation gasoline; preferably, the aviation gasoline is No. 100 unleaded aviation gasoline.

Technical Field

The invention belongs to the technical field of aviation fuels, and particularly relates to an alkane composition, a No. 100 unleaded aviation gasoline composition containing the alkane composition and a production method of the composition.

Background

Aviation gasoline is a high octane fuel for aircraft and is an important component of aviation fuel. Octane Number (Octane Number) is an indicator of the resistance of the fuel used by the vehicle to knock. As the compression ratio of the aviation engine is gradually increased, the requirement of the engine on the octane number of the used fuel is continuously improved. In order to ensure that the engine obtains the maximum power under the non-knock condition and consumes less fuel, an additive capable of improving the anti-knock property of the fuel is required to be added into the aviation gasoline. Tetraethyl lead is a common anti-knock agent and can improve the octane number of fuel and prevent knocking in an engine. However, tetraethyl lead is a highly toxic substance, is harmful to human health, and can cause environmental pollution. Tetraethyl lead is an important atmospheric pollutant and is the main source of lead in air. Therefore, with the increasing awareness of environmental protection, the production of unleaded gasoline with high octane number is a necessary trend for the development of aviation gasoline in the future.

CN 103965974B proposes a lead-free aviation gasoline and a preparation method thereof, and proposes the components of the lead-free aviation gasoline as follows: 20-100% of alkane, 0-86% of aromatic hydrocarbon, 0-10% of olefin, 0-20% of nitrogen-containing organic compound and 0-20% of organic oxygen-containing compound, wherein the organic oxygen-containing compound is methyl tertiary butyl ether. Methyl tert-butyl ether is easy to enter an underground drinking water system, has stable property, is difficult to decompose, and can cause certain harm to the intestines and stomach, the liver, the nervous system and the ecology of people. And the octane number is not obviously improved due to the limitation of oxygen content and the general addition amount of the catalyst is within 10 percent.

CN 106398783B proposes a lead-free aviation gasoline and a preparation method thereof, and proposes the components of the lead-free aviation gasoline as follows: 10-18% of industrial isopentane, 1-11% of light alkylate, 45-55% of industrial isooctane, 15-22% of toluene, 0-4% of m-xylene, 5-11% of cumene, 1.5-5.5% of aniline, 0.55-3.5% of N-methylaniline and 0-3% of m-toluidine by volume. The aromatic amine compound in the patent is relatively rich, and the nitrogen-containing compound fuel forms nitrogen oxide during combustion, which is one of the main pollution sources causing air pollution. The emission of nitrogen oxides is easy to form acid rain, and causes pollution to the environment.

In summary, the existing unleaded aviation gasoline generally contains oxygen-containing/nitrogen-containing compounds which cause environmental pollution, such as methyl tertiary butyl ether, arylamine compounds and the like, and can not meet the requirements of environmental protection.

Disclosure of Invention

In order to overcome the problems of the prior art, the invention provides an alkane composition, a No. 100 unleaded aviation gasoline composition containing the alkane composition and a production method thereof. The aviation gasoline composition provided by the invention meets the requirements of 100LL aviation gasoline on various indexes such as anti-knock property, evaporation property and stability in ASTM-D910 and GB1787-2018 standards, does not contain tetraethyl lead, can reduce pollution generated during combustion, is environment-friendly, and can meet the requirements of people on environmental protection. The aviation gasoline composition of the invention has the advantages of low fixed investment, low production cost, convenient modification and easy implementation, especially for oil refining enterprises.

Specifically, one aspect of the invention provides an alkane composition useful as an aviation gasoline blending component comprising, based on the total weight of the alkane composition, from 3 to 9 weight percent of a C4 alkane, from 2 to 7 weight percent of a C5 alkane, from 4 to 9 weight percent of a C6 alkane, from 21 to 30 weight percent of a C7 alkane, from 56 to 70 weight percent of a C8 alkane, and from 0.51 to 2.4 weight percent of a C9 alkane.

In one or more embodiments, the alkane composition has an initial boiling point of 21 ℃ to 45 ℃ and an end point of 140 ℃ to 153 ℃.

In one or more embodiments, the alkane composition comprises 3.76 to 7.38 weight percent of a C4 alkane, 2.61 to 4.78 weight percent of a C5 alkane, 4.46 to 8.91 weight percent of a C6 alkane, 22.37 to 28.67 weight percent of a C7 alkane, 56.53 to 68.67 weight percent of a C8 alkane, and 0.54 to 2.31 weight percent of a C9 alkane, based on the total weight of the alkane composition.

In one or more embodiments, the alkane composition has an initial boiling point of 40 to 45 ℃ and an end point of 145-153 ℃.

Another aspect of the invention provides a method of making an alkane composition according to any of the embodiments herein, the method comprising: distilling the alkylation reaction product of C4 olefin and isobutane to obtain a component with an initial boiling point of 21-45 ℃ and an end boiling point of 140-153 ℃ or a component with an initial boiling point of 40-45 ℃ and an end boiling point of 145-153 ℃ as the alkane composition.

In one or more embodiments, the alkylation reaction is at a temperature of 4 to 10 ℃, a pressure of 0.4 to 0.45MPa, and a molar ratio of isobutane to C4 olefin of 8 to 12: 1.

In one or more embodiments, the distillation is carried out using a distillation column having a bottom temperature of 136-145 deg.C, a bottom pressure of 0.43-0.52MPa, an overhead temperature of 51-56 deg.C, and an overhead pressure of 0.41-0.53 MPa.

In one or more embodiments, the components having an initial boiling point of 21-45 ℃, an end point of 140-.

The present invention also provides an alkane composition prepared by the method of preparing an alkane composition according to any one of the embodiments herein.

The present invention also provides the use of a paraffinic hydrocarbon composition as described in any of the embodiments herein in the preparation of an aviation gasoline, preferably an unleaded aviation gasoline, such as unleaded aviation gasoline No. 100.

One aspect of the invention provides an aviation gasoline composition comprising a base oil and an additive, the base oil comprising as blending component a the paraffinic hydrocarbon composition of any of the embodiments herein, blending component B, blending component C and blending component D; the base oil comprises 60-80 wt% of blending component A, 5-20 wt% of blending component B, 5-20 wt% of blending component C and 10-20 wt% of blending component D based on the total weight of the base oil; the additive comprises methylcyclopentadienyl manganese tricarbonyl;

wherein the blending component A contains 3-9 wt% of C4 alkane, 2-7 wt% of C5 alkane, 4-9 wt% of C6 alkane, 21-30 wt% of C7 alkane, 56-70 wt% of C8 alkane and 0.51-2.4 wt% of C9 alkane based on the total weight of the blending component A;

the blending component B contains more than 95 weight percent of C7 aromatic hydrocarbon based on the total weight of the blending component B;

the blending component C is selected from one or more of paraxylene, metaxylene, mesitylene or cumene;

the blend component D contains 0.3 to 5.1 weight percent of C4 alkane, 41 to 75 weight percent of C5 alkane, 25 to 50 weight percent of C6 alkane and 0.05 to 0.7 weight percent of C7 alkane based on the total weight of the blend component D.

In one or more embodiments, the base oil includes 60 to 75 weight percent of blend component A, 8 to 18 weight percent of blend component B, 7 to 15 weight percent of blend component C, and 10 to 15 weight percent of blend component D, based on the total weight of the base oil.

In one or more embodiments, the blend component a contains 3.76 to 7.38 weight percent C4 alkanes, 2.61 to 4.78 weight percent C5 alkanes, 4.46 to 8.91 weight percent C6 alkanes, 22.37 to 28.67 weight percent C7 alkanes, 56.53 to 68.67 weight percent C8 alkanes, and 0.54 to 2.31 weight percent C9 alkanes, based on the total weight of the blend component a.

In one or more embodiments, the initial boiling point of blend component A is from 21 ℃ to 45 ℃ and the end point is 140 ℃ to 153 ℃.

In one or more embodiments, the initial boiling point of blend component A is from 40 to 45 ℃ and the end point is 145-153 ℃.

In one or more embodiments, the blend component B also contains C8 aromatics and the total content of C7 aromatics and C8 aromatics is 98 wt.% or greater, based on the total weight of the blend component B.

In one or more embodiments, the initial boiling point of the blending component B is 107-112 ℃ and the final boiling point is 110-113 ℃.

In one or more embodiments, the blend component D contains 3 to 5.1 weight percent C4 alkanes, 60 to 70 weight percent C5 alkanes, 25 to 35 weight percent C6 alkanes, and 0.1 to 0.7 weight percent C7 alkanes, based on the total weight of the blend component D.

In one or more embodiments, the initial boiling point of blend component D is from 26 to 30 ℃ and the final boiling point is from 60 to 64 ℃.

In one or more embodiments, the methylcyclopentadienyl manganese tricarbonyl is in an amount of 100-200mg/L based on the total volume of the base oil.

In one or more embodiments, the aviation gasoline composition is free of tetraethyl lead.

In one or more embodiments, the aviation gasoline composition is free of aromatic amine antiknock agents.

In one or more embodiments, the aviation gasoline composition is free of aromatic amine compounds.

In one or more embodiments, the aviation gasoline composition is free of methyl tertiary butyl ether.

In one or more embodiments, the aviation gasoline composition is free of alkyl ether based antiknock agents.

In one or more embodiments, the aviation gasoline composition further comprises one or more selected from the group consisting of antioxidants, anti-icing agents, anti-static agents, anti-corrosion agents, and dyes.

In one or more embodiments, the aviation gasoline composition has a motor octane number of not less than 99.6.

In one or more embodiments, the aviation gasoline composition has a motor octane number of 100-.

Another aspect of the invention provides a method of making an aviation gasoline composition according to any one of the embodiments herein, the method comprising the step of mixing the components of the aviation gasoline composition.

In one or more embodiments, the method comprises: distilling the alkylation reaction product of C4 olefin and isobutane to obtain a component with an initial boiling point of 21-45 ℃ and an end boiling point of 140-153 ℃ or a component with an initial boiling point of 40-45 ℃ and an end boiling point of 145-153 ℃ as a blending component A.

In one or more embodiments, the alkylation reaction is at a temperature of 4 to 10 ℃, a pressure of 0.4 to 0.45MPa, and a molar ratio of isobutane to C4 olefin of 8 to 12: 1.

In one or more embodiments, the distillation is carried out using a distillation column having a bottom temperature of 136-145 deg.C, a bottom pressure of 0.43-0.52MPa, an overhead temperature of 51-56 deg.C, and an overhead pressure of 0.41-0.53 MPa.

In one or more embodiments, the component having an initial boiling point of 21-45 ℃ and an end point of 140-153 ℃ or the component having an initial boiling point of 40-45 ℃ and an end point of 145-153 ℃ is withdrawn from the side line of the distillation column as the blending component A, or the component having an initial boiling point of 21-45 ℃ and an end point of 140-153 ℃ or the component having an initial boiling point of 40-45 ℃ and an end point of 145-153 ℃ is cut from the bottom oil of the distillation column as the blending component A.

The present invention also provides an aviation gasoline composition prepared by the method of preparing an aviation gasoline composition as described in any one of the embodiments herein.

Detailed Description

To make the features and effects of the present invention comprehensible to those skilled in the art, general description and definitions are made below with reference to terms and expressions mentioned in the specification and claims. 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 this invention belongs.

The theory or mechanism described and disclosed herein, whether correct or incorrect, should not limit the scope of the present invention in any way, i.e., the present disclosure may be practiced without limitation to any particular theory or mechanism.

The terms "comprising," "including," "containing," "having," and the like, herein, encompass the meanings of "consisting essentially of … …" and "consisting of … …," e.g., when "a comprises B and C" is disclosed herein, "a consists of B and C" should be considered to have been disclosed herein.

All features defined herein as numerical ranges or percentage ranges, such as numbers, amounts, levels and concentrations, are for brevity and convenience only. Accordingly, the description of numerical ranges or percentage ranges should be considered to cover and specifically disclose all possible subranges and individual numerical values (including integers and fractions) within the range.

Herein, when embodiments or examples are described, it is to be understood that they are not intended to limit the invention to these embodiments or examples. On the contrary, all alternatives, modifications, and equivalents of the methods and materials described herein are intended to be included within the scope of the invention as defined by the appended claims.

In this context, for the sake of brevity, not all possible combinations of features in the various embodiments or examples are described. Therefore, the respective features in the respective embodiments or examples may be arbitrarily combined as long as there is no contradiction between the combinations of the features, and all the possible combinations should be considered as the scope of the present specification.

In the present invention, alkylation refers to a process in which an alkyl group is transferred from one molecule to another, and is a reaction in which an alkyl group is introduced into a molecule of a compound.

In the present invention, the "C + number" previously indicated for a compound indicates the number of carbon atoms contained in the compound, for example, C4 alkane indicates an alkane containing four carbon atoms, C4 alkene indicates an alkene containing four carbon atoms, C7 arene indicates an arene containing seven carbon atoms, and so on.

In the invention, the method for measuring the motor octane number is carried out according to the measurement of the GB _ T503-2016 gasoline octane number.

The aviation gasoline composition of the invention contains base oil and additives. It is to be understood that in the present invention, base oil refers to the hydrocarbon material in the aviation gasoline composition.

The inventor of the invention finds that the alkane composition with the initial boiling point of 21-45 ℃ and the final boiling point of 140-153 ℃ obtained by distilling the alkylation reaction product not only removes high carbon compounds with the boiling range of more than 160 ℃, but also reserves 56-70 wt% of C8 alkane which can contribute higher octane number, and simultaneously contains lighter components such as C4, C5 and the like, and the octane number, the boiling range and the saturated vapor pressure data of the alkane composition are close to the related index requirements in the aviation gasoline standard ASTM-D910, and the alkane composition is suitable for being used as the main component of aviation gasoline, in particular No. 100 lead-free aviation gasoline. Accordingly, the present invention includes a paraffinic hydrocarbon composition useful as a blending component for aviation gasolines, preferably comprising more than 60% by weight of a paraffinic hydrocarbon composition of the invention, for example comprising 70%, 75%, 80% by weight of a paraffinic hydrocarbon composition of the invention, and its use in the preparation of aviation gasolines, particularly unleaded aviation gasoline No. 100.

The alkane composition of the present invention comprises or consists of 3 to 9 wt% of C4 alkane, 2 to 7 wt% of C5 alkane, 4 to 9 wt% of C6 alkane, 21 to 30 wt% of C7 alkane, 56 to 70 wt% of C8 alkane, and 0.51 to 2.4 wt% of C9 alkane. It is to be understood that in the present invention, for compositions containing two or more components, the sum of the weight percentages of all components in the composition should equal 100 weight percent. Preferably, the alkane composition of the present invention comprises or consists of 3.76 to 7.38 wt% of C4 alkane, 2.61 to 4.78 wt% of C5 alkane, 4.46 to 8.91 wt% of C6 alkane, 22.37 to 28.67 wt% of C7 alkane, 56.53 to 68.67 wt% of C8 alkane and 0.54 to 2.31 wt% of C9 alkane. For example, in the alkane composition of the present invention, the C4 alkane may be present in an amount of 3.76%, 5%, 5.4%, 5.43%, 5.86%, 5.98%, 6.90%, 7.31%, or 7.38% by weight, the C5 alkane may be present in an amount of 2.61%, 3%, 3.21%, 3.22%, 3.98%, 4.28%, or 4.78% by weight, the C6 alkane may be present in an amount of 4.46%, 4.53%, 5.98%, 6.24%, 6.42%, 6.73%, or 8.91% by weight, the C7 alkane may be present in an amount of 22.37%, 23.01%, 23.17%, 24.08%, 25.1%, 25.32%, or 28.67% by weight, the C8 alkane may be present in an amount of 56.53%, 56.8%, 58.8%, 7.17%, 68.67%, 54%, or 8%, and the C8 alkane may be present in an amount of 8625.8%, 58.8%, 7%, 7.8%, 7%, 7.31%, 7%, 3, 7.53%, or 8%, 7.91%, 3% by weight, 0.67 wt%, 1.52 wt%, 1.7 wt%, 1.93 wt%, or 2.31 wt%.

The alkane composition has an initial boiling point of 21-45 ℃ and an end boiling point of 140-153 ℃. Preferably, the alkane compositions of the present invention have an initial boiling point in the range of from 24 to 45 deg.C, more preferably from 40 to 45 deg.C. Preferably, the alkane compositions of the present invention have an end point of 145-153 ℃. For example, the alkane composition of the present invention may have an initial boiling point of 42.61 ℃, 42.70 ℃, 43.17 ℃, 44.02 ℃ or 44.26 ℃ and an end boiling point of 146.31 ℃, 147.89 ℃, 148.56 ℃, 150.56 ℃ or 152.02 ℃. In the present invention, the "distillation range of a certain component is A-B ℃ C" means that the initial boiling point of the component is A ℃ C and the final boiling point is B ℃ C. The alkane composition of the invention may have a 10% distillation temperature of 68-78 deg.C, such as 70-75 deg.C, a 50% distillation temperature of 98-108 deg.C, such as 101-105 deg.C, a 90% distillation temperature of 110-120 deg.C, such as 114-117 deg.C.

The alkane compositions of the present invention are fractions having target initial and end points obtained by distilling the alkylation reaction product. The alkylation reaction product may be an alkylation reaction product of isobutane and a C4 olefin. The pressure of alkylation reaction can be 0.4-0.45MPa, the mole ratio of isobutane to C4 olefin (alkane-alkene ratio) can be 8-12:1, and the temperature can be 4-10 ℃. The alkylation reaction is carried out in the presence of a catalyst. The catalyst for the alkylation reaction may be an acid such as sulfonic acid, hydrofluoric acid, concentrated sulfuric acid, and the like. The molar ratio of catalyst to C4 olefin (acid to olefin ratio) may be 1-1.2: 1. In some embodiments, the alkylation reaction is at a temperature of about 7.3 ℃, a pressure of about 0.42MPa, the catalyst is hydrofluoric acid, and the alkane to alkene ratio is about 10.2: 1. The alkylation reaction product may be distilled in a distillation column. The conditions of the distillation may be: the temperature of the top of the distillation tower is 51-56 ℃, the pressure of the top of the distillation tower is 0.41-0.53MPa, the temperature of the bottom of the distillation tower is 136-145 ℃, and the pressure of the bottom of the distillation tower is 0.43-0.52 MPa. In some embodiments, the distillation column overhead temperature is about 53 ℃, the overhead pressure is about 0.44MPa, the bottoms temperature is about 142 ℃, and the bottoms pressure is about 0.47 MPa. The manner of obtaining the fraction having the target initial boiling point and end point is not particularly limited, and for example, the fraction having the target initial boiling point and end point may be drawn out from a side line of the distillation column, or the fraction having the target initial boiling point and end point may be cut out from the bottom of the distillation column. Extraction and cutting may be performed using methods conventional in the art.

The base oil of the aviation gasoline composition of the present invention comprises as blending component a the paraffinic hydrocarbon composition of the present invention. Blending component A makes up 60 to 80 wt%, preferably 60 to 75 wt%, for example 60 to 70 wt%, 65 wt% of the base oil.

In the invention, the base oil also comprises a blending component B, a blending component C and a blending component D so as to further adjust the distillation range and the saturated vapor pressure of the aviation gasoline and enable the aviation gasoline to meet the requirements of relevant indexes in the aviation gasoline standard ASTM-D910. The blending combination B has higher octane number and distillation range and low saturated vapor pressure, and the addition amount of the component has larger influence on the improvement range of the base oil octane number. The blending component C has high octane value and distillation range and low saturated vapor pressure, and the addition of the component has great influence on the improvement range of the base oil octane value. The blending component D has low octane number and distillation range and high vapor pressure and is mainly used for adjusting the saturated vapor pressure and distillation range of the base oil so as to ensure that the base oil meets the standard.

The blending component B contains more than 95 wt% of C7 aromatic hydrocarbon, and the balance of a small amount of C8 aromatic hydrocarbon, C7 by-products, benzene and the like. Preferably, the blending component B has an initial boiling point of 107-112 ℃ and an end point of 110-113 ℃. Preferably, blend component B contains 95 to 99 wt.%, e.g., 96 to 99 wt.%, C7 aromatics. Preferably, the total content of C7 aromatics and C8 aromatics in blend component B is greater than 98 wt.%. In some embodiments, blend component B contains 95 wt.% or more, such as 95 to 99 wt.%, 96 to 99 wt.% C7 aromatics, and 5 wt.% or less, such as 1 to 5 wt.%, 1 to 3 wt.% C8 aromatics.

Blending component B is either commercially available or is a product of various conventional processes in the art, provided that the above requirements are met. Preferably, blend component B is a C7 aromatics blend component produced by an aromatics extraction unit. The C7 aromatic hydrocarbon blending component produced by the aromatic hydrocarbon extraction device refers to a C7 fraction separated from a reformed mixed product obtained by reforming straight-run naphtha by adopting a sulfolane liquid-liquid extraction process.

The octane number of the base oil can be improved by adding a proper amount of the blending component B. In the aviation gasoline composition of the present invention, blending component B makes up from 5 to 20% by weight, preferably from 8 to 18% by weight, for example 8%, 10%, 12%, 15% by weight of the base oil.

The blending component C is selected from one or more of paraxylene, metaxylene, mesitylene or cumene.

Blending component C is either commercially available or is a product of various conventional processes in the art, provided that the above requirements are met. Preferably, blending component C is mesitylene. It will be appreciated that blending component C may contain minor amounts, for example, less than 5% by weight, of impurities.

The distillation range, the saturated vapor pressure and the octane number of the base oil can be further adjusted by adding a proper amount of the blending component C. In the aviation gasoline composition of the present invention, blending component C makes up 5 to 20 wt%, preferably 7 to 15 wt%, for example 9 wt%, 10 wt%, 15 wt% of the base oil.

Blending component D contains or consists of 0.3 to 5.1 weight percent of C4 alkane, 41 to 75 weight percent of C5 alkane, 25 to 50 weight percent of C6 alkane and 0.05 to 0.7 weight percent of C7 alkane. Preferably, blend component D contains 3 to 5.1 weight percent C4 alkane, 60 to 70 weight percent C5 alkane, 25 to 35 weight percent C6 alkane, and 0.1 to 0.7 weight percent C7 alkane. For example, in blend component D, C4 alkane may be present in an amount of 3.5 wt%, 3.8 wt%, 4.3 wt%, 4.7 wt%, 4.8 wt%, 4.9 wt% or 5 wt%, C5 alkane may be present in an amount of 62 wt%, 62.9 wt%, 63.8 wt%, 64.3 wt%, 66.7 wt%, 67.8 wt% or 70 wt%, C6 alkane may be present in an amount of 26 wt%, 26.9 wt%, 29.3 wt%, 30.6 wt%, 31.2 wt%, 31.9 wt% or 35 wt%, C7 alkane may be present in an amount of 0.1 wt%, 0.2 wt%, 0.4 wt%, 0.6 wt% or 0.7 wt%, preferably blend component D has an initial boiling point of 26 to 30 ℃ and an end boiling point of 60 to 64 ℃.

Blending component D is either commercially available or is a product of various conventional processes in the art, provided that the above requirements are met. Blending component D may be derived from various processes commonly used in the art for the preparation of light naphtha, for example, light naphtha produced by a hydrocracking unit, an atmospheric and vacuum initial overhead oil produced by an atmospheric and vacuum distillation unit, and an atmospheric and vacuum overhead oil produced by an atmospheric and vacuum distillation unit. The light naphtha produced by the hydrocracking device is an oil product which is prepared by the hydrocracking reaction of a heavy raw material in the presence of a catalyst and hydrogen. The atmospheric and vacuum distillation device produces atmospheric and vacuum primary top oil, which is an oil product obtained by feeding raw oil in the atmospheric and vacuum distillation device into an electric desalting tank through primary heat exchange, feeding the raw oil into a primary distillation tower through secondary heat exchange, and separating the raw oil from the tower top. The atmospheric and vacuum distillation device produces atmospheric and vacuum overhead oil which is an oil product entering an atmospheric fractionating tower from a primary distillation tower in the atmospheric and vacuum distillation device and distilled from the top of the tower after rectification. In some embodiments, blending component D is a light naphtha produced by a hydrocracking unit.

The distillation range of the aviation gasoline can be further adjusted by adding a proper amount of the blending component D. In the aviation gasoline composition of the present invention, blending component D makes up 10 to 20 wt%, preferably 10 to 15 wt%, for example 12 wt%, 14 wt% of the base oil.

In the aviation gasoline composition, the base oil comprises or consists of 60-80 wt% of blending component A, 5-20 wt% of blending component B, 5-20 wt% of blending component C and 10-20 wt% of blending component D; preferably, the base oil comprises or consists of 60 to 75 wt.% of blend component A, 8 to 18 wt.% of blend component B, 7 to 15 wt.% of blend component C and 10 to 15 wt.% of blend component D.

In some embodiments, the base oil of the aviation gasoline composition of the present invention comprises, based on the total weight of the base oil: 3.8-5.6 wt.%, preferably 4-5.4 wt.% C4 alkane, 8.9-12.8 wt.%, preferably 9.1-12.6 wt.% C5 alkane, 6.4-8.9 wt.%, preferably 6.6-8.7 wt.% C6 alkane, 14.8-17.1 wt.%, preferably 15-16.9 wt.% C7 alkane, 33.5-42 wt.%, preferably 33.7-41.8 wt.%, more preferably 33.9-41.6 wt.% C8 alkane, 0.2-1.6 wt.%, preferably 0.4-1.4 wt.% C9 alkane, 7.5-15 wt.%, preferably 7.7-14.8 wt.% C7 aromatics in total, 8.7-15.2 wt.%, preferably 8.9-15 wt.% C8 and C9 aromatics, and possibly impurities. Preferably, the major constituent of the C8 aromatics and C9 aromatics in the base oil of the aviation gasoline composition of the present invention is one or more selected from the group consisting of para-xylene, meta-xylene, mesitylene, and cumene, for example, 80 wt% or more, 90 wt% or more, or 95 wt% or more of the C8 aromatics and C9 aromatics is one or more selected from the group consisting of para-xylene, meta-xylene, mesitylene, and cumene.

The additive in the aviation gasoline composition of the invention comprises methylcyclopentadienyl manganese tricarbonyl. The methyl cyclopentadienyl manganese tricarbonyl is decomposed into manganese oxide particles under the combustion condition, and can participate in the flame front reaction of hydrocarbon, i.e. the active center of the chain reaction can be acted to make it be changed into oxidation intermediate product with small activity, so that the peroxide concentration can be reduced, the length and branch of chain can be reduced, at the same time the speed for releasing energy also can be reduced, so that the induction period of fire can be prolonged, and the antiknock property of fuel can be raised. The invention discovers that the Motor Octane Number (MON) of the aviation gasoline can be effectively improved by a very small amount of the methylcyclopentadienyl manganese tricarbonyl when the additive is matched with the aviation gasoline base oil. In the present invention, the amount of methylcyclopentadienyl manganese tricarbonyl added is not more than 200mg/L, and may be 100-200mg/L, such as 150mg/L, 160mg/L, 180mg/L, based on the total volume of the base oil. The composition of the aviation gasoline has low methylcyclopentadienyl manganese tricarbonyl content, can obviously improve the octane number of the aviation gasoline, and is more environment-friendly compared with the prior lead-containing aviation gasoline.

The additive in the aviation gasoline composition of the present invention may optionally or preferably further comprise other additives commonly used in the art to meet and improve aviation gasoline performance, such as one or more selected from antistatic agents, dyes, anti-icing agents, anti-corrosion agents, antioxidants, and the like.

The corrosion inhibitors suitable for use in the present invention may be any of a variety of corrosion inhibitors conventional in the art, and may be added to the aviation gasoline composition in amounts conventional in the art. Examples of the preservative include DCI-4A (Innospec Co.). At one endIn some embodiments, the preservative is added in an amount of 10 to 30mg/m based on the total volume of the base oil³E.g. 20mg/m³。

Antistatic agents suitable for use in the present invention can be any of a variety of antistatic agents conventional in the art, such as, for example, Stadis 450, a commercially available product (Octel America Inc, Newark, DE 19702). The amount of the antistatic agent added is generally not more than 3mg/L, for example, 2mg/L, based on the total volume of the base oil, but when the conductivity of the fuel decreases and further addition of the antistatic agent is required, the addition may be continued, but the cumulative total amount cannot exceed 5 mg/L.

The antioxidant suitable for use in the present invention may be various antioxidants conventional in the art, and may be, for example, one or more selected from the group consisting of 2, 6-di-t-butyl-4-cresol, 2, 4-dimethyl-6-t-butylphenol, 2, 6-di-t-butylphenol, N '-dipropyl-p-phenylenediamine and N, N' -di-sec-butyl-p-phenylenediamine. In some embodiments, the antioxidant is 2, 6-di-tert-butyl-4-methylphenol. The content of the antioxidant is not more than 12mg/L, preferably 10-12mg/L based on the total volume of the base oil.

The anti-icing agent suitable for the present invention may be various anti-icing agents conventional in the art, and for example, may be selected from one or more of isopropyl alcohol, diethylene glycol monomethyl ether, and the like. In some embodiments, the anti-icing agent is diethylene glycol monomethyl ether. The amount of the anti-icing agent added to the aviation gasoline composition may be an amount conventionally added in the art. In some embodiments, the anti-icing agent is added in an amount of 0.1 to 0.15 volume percent, for example 0.12 volume percent, based on the total volume of the base oil.

The aviation gasoline composition of the present invention may be prepared by mixing the aforementioned blending components of the aviation gasoline composition. The invention includes a process for preparing the aviation gasoline composition of the invention comprising the step of mixing the various blending components of the aviation gasoline composition. Wherein the blending components and the content of the aviation gasoline composition are required to be as described in the specification.

In preparing the aviation gasoline composition of the present invention, the components may be mixed together in any order of mixing as long as they are sufficiently mixed, and there is no particular limitation. For example, the base oil may be mixed first and then the additive may be added to the base oil, a part of the base oil and the additive may be mixed first and then the remaining part of the base oil may be added, or the base oil and the additive may be added simultaneously and mixed uniformly. In the present invention, preferably, the base oil is mixed uniformly, and then the additive is added and mixed uniformly.

The preparation method of the aviation gasoline composition can also comprise the step of distilling the alkylation reaction product of C4 olefin and isobutane to obtain the fraction with the initial boiling point of 21-45 ℃ and the final boiling point of 140-153 ℃ as the blending component A. Preferably, the initial boiling point of the obtained component is 40-45 ℃. Preferably, the final cut point of the components obtained is 145-153 ℃. The composition and distillation range of the component obtained by the above process meet the requirements for blending component A as described hereinbefore. The alkylation reaction is carried out in the presence of a catalyst. The catalyst for the alkylation reaction may be an acid, and may be selected from one or more of sulphonic acid, hydrofluoric acid, concentrated sulphuric acid, for example. The molar ratio of catalyst to C4 olefin (acid to olefin ratio) may be 1-1.2: 1. The temperature of the alkylation reaction can be 4-10 ℃, the pressure can be 0.4-0.45MPa, and the alkane-alkene ratio can be 8-12: 1. The distillation may be carried out in a distillation column. The conditions of the distillation may be: the temperature of the top of the distillation tower is 51-56 ℃, the pressure of the top of the distillation tower is 0.41-0.53MPa, the temperature of the bottom of the distillation tower is 136-145 ℃, and the pressure of the bottom of the distillation tower is 0.43-0.52 MPa. The manner of obtaining the fraction having the target initial boiling point and end point is not particularly limited, and for example, the fraction having the target initial boiling point and end point may be drawn out from a side line of the distillation column, or the fraction having the target initial boiling point and end point may be cut out from the bottom of the distillation column. Extraction and cutting may be performed using methods conventional in the art.

The aviation gasoline composition of the present invention can be used directly as aviation gasoline, such as unleaded aviation gasoline No. 100. The aviation gasoline composition has high octane number, good anti-knock performance and high safety coefficient, and can meet the requirement of aviation piston engine fuel on the octane number. The motor octane number of the aviation gasoline composition is not less than 99.6. To further improve the safety performance of the aviation gasoline composition, preferably, the motor octane number of the aviation gasoline composition of the present invention is 100-103.

In some embodiments, the aviation gasoline composition of the present invention has an initial boiling point of 45 to 55 deg.C, such as 46 to 53.5 deg.C, and an end point of 140 deg.C and 165 deg.C, such as 143 to 161.5 deg.C. In some embodiments, the aviation gasoline composition of the present invention has a net heating value of 43MJ/kg or greater, such as 43.5MJ/kg or greater. In some embodiments, the aviation gasoline composition of the present invention has a copper flake corrosion (2h, 100 ℃, ASTM-D910) of about 1. In some embodiments, the aviation gasoline composition of the present invention has a density of 705-725kg/m³. In some embodiments, the aviation gasoline composition of the present invention has a freeze point of about-58 ℃. In some embodiments, the aviation gasoline compositions of the present invention have a sulfur content of 0.003% or less, such as 0.0026% or less. In some embodiments, the aviation gasoline composition of the present invention has a water reaction volume of about 0.7 mL.

The aviation gasoline composition provided by the invention has various parameters meeting the standards of ASTM-D910 and GB1787-2018 for aviation gasoline of No. 100 LL. The potential colloid of the aviation gasoline composition is not more than 6mg/100mL, obviously lead precipitation is not more than 3mg/100mL, and the stability requirement is met. The motor octane number of the aviation gasoline composition is not less than 99.6, and the requirement of antiknock property is met. The Reid vapor pressure of the aviation gasoline composition is between 38 and 49kPa, and the requirement of evaporability is met.

The aviation gasoline composition of the invention has the advantages of low fixed investment, low production cost, convenient modification and easy implementation, especially for oil refining enterprises.

The aviation gasoline composition disclosed by the invention is low in aromatic hydrocarbon content, does not contain or basically does not contain tetraethyl lead, is low in methylcyclopentadienyl manganese tricarbonyl content, and is green and environment-friendly. In some embodiments, the aviation gasoline composition of the present invention comprises no or substantially no methyl tertiary butyl ether. In some embodiments, the aviation gasoline composition of the present invention comprises no or substantially no alkyl ether antiknock agent. Examples of alkyl ether antiknock agents include methyl tert-butyl ether, ethyl tert-butyl ether, methyl tert-amyl ether, and diisopropyl ether. In some embodiments, the aviation gasoline composition of the present invention does not comprise, or is substantially free of, aromatic amine antiknock agents. Examples of the aromatic amine antiknock agent include aniline, N-methylaniline and m-toluidine. In some embodiments, the aviation gasoline composition of the present invention does not comprise or substantially does not comprise an aromatic amine compound. The aviation gasoline containing the aromatic amine compound can not only cause the emission of nitrogen-containing compounds in the using process, but also cause the swelling problem to the rubber of a piston engine, and the quality of the aviation gasoline containing the aromatic amine compound is a certain distance away from the currently implemented aviation gasoline standard. As used herein, "substantially free" means that the material is not intentionally or specifically added to an aviation gasoline composition.

Compared with the existing aviation gasoline, the aviation gasoline disclosed by the invention has the following characteristics:

although the methylcyclopentadienyl manganese tricarbonyl is used as an automobile gasoline antiknock agent to improve Research Octane Number (RON) of the automobile gasoline, the antiknock performance of the methylcyclopentadienyl manganese tricarbonyl is different for different base oils, and the use of the methylcyclopentadienyl manganese tricarbonyl on a piston type aviation gasoline engine has the defect of metal deposit formation on a spark plug, and the addition amount of the methylcyclopentadienyl manganese tricarbonyl needs to be carefully considered, so that the conventional lead-free aviation gasoline does not use the methylcyclopentadienyl manganese tricarbonyl as the antiknock agent. Based on the action relationship between the selected components of the aviation gasoline base oil and the methylcyclopentadienyl manganese tricarbonyl, after a mechanism that the motor octane number of the base oil is improved by the methylcyclopentadienyl manganese tricarbonyl is deeply researched, the composition of the aviation gasoline base oil is properly matched with the methylcyclopentadienyl manganese tricarbonyl, the method that the methylcyclopentadienyl manganese tricarbonyl is mixed with the aviation gasoline base oil is provided, the Motor Octane Number (MON) of the aviation gasoline is effectively improved under the condition of a very small amount of the methylcyclopentadienyl manganese tricarbonyl, the components are in a complex interaction and synergistic improvement relationship, and corresponding benefits can be achieved by simply mixing none of the components. In the invention, the addition of the methylcyclopentadienyl manganese tricarbonyl antiknock agent effectively improves the MON of the base oil under the condition of not bringing obvious adverse factors to the base oil.

The aviation gasoline provided by the invention is an oil product directly produced by a refinery, does not need to be purified, is convenient to blend for a refinery and has low production cost.

Compared with the aviation gasoline containing tetraethyl lead, the aviation gasoline disclosed by the invention is less harmful and more environment-friendly, and compared with the aviation gasoline added with the arylamine compound and methyl tertiary butyl ether, the aviation gasoline disclosed by the invention has the property of meeting the standard requirements of the existing aviation gasoline.

The present invention will be illustrated below by way of specific examples. It should be understood that these examples are illustrative only and are not intended to limit the scope of the present invention. The methods, reagents and materials used in the examples are, unless otherwise indicated, conventional in the art. The starting materials in the examples, unless otherwise stated, are commercially available.

In the following examples, the parameters were measured according to ASTM-D910.

In the following examples, antistatic agents Stadis 450 are available from Octel America Inc, Newark, DE 19702; preservative DCI-4A was purchased from Innospec.

In the following examples, the aromatic hydrocarbon blending component of the aromatic hydrocarbon extraction device is a C7 fraction separated from a reformed mixed product obtained by reforming straight-run naphtha by a sulfolane liquid-liquid extraction process.

In the following examples, the light naphtha of the hydrocracking apparatus is a light naphtha obtained by subjecting a heavy feedstock and hydrogen to a hydrocracking reaction in the presence of a catalyst.

In the following examples, the atmospheric and vacuum overhead oil is an oil product which enters an atmospheric fractionating tower from a primary distillation tower in an atmospheric and vacuum device and is distilled from the top of the tower after being rectified.

In the following examples, the atmospheric and vacuum primary top oil is an oil product distilled from the top of a primary distillation tower after the primary heat exchange of the crude oil in an atmospheric and vacuum device, the crude oil enters an electric desalting tank and enters a primary distillation tower for separation through the secondary heat exchange.

Preparation example

C4 olefin and isobutane with an alkane-olefin ratio of 10.2:1 were alkylated at 7.3 ℃ under 0.42MPa in the presence of a catalyst, hydrofluoric acid. The alkylation reaction product of C4 olefin and isobutane was distilled in a distillation column at a top temperature of 53 deg.C, a top pressure of 0.44MPa, a bottom temperature of 142 deg.C, and a bottom pressure of 0.47MPa, and components having distillation ranges of 42.61-148.56 deg.C, 44.26-146.31 deg.C, 43.17-150.56 deg.C, 44.02-147.89 deg.C, 42.70-152.02 deg.C, and 42.70-152.02 deg.C were obtained from the side draw of the distillation column, as side draw oils of the fractionation column of the alkylation plant used in examples 1-5 and comparative example 1, respectively.

Example 1

Mixing 60 mass percent of side draw oil of a fractionating tower of an alkylation device (the property of the side draw oil is shown in a table 1-1), 15 mass percent of light naphtha of a hydrocracking device (the property of the side draw oil is shown in a table 1-2), 15 mass percent of aromatic hydrocarbon blending components of an aromatic hydrocarbon extraction device (the property of the aromatic hydrocarbon blending components is shown in a table 1-3) and 10 mass percent of mesitylene (the property of the mesitylene is shown in a table 1-4), adding 160mg/L of methylcyclopentadienyl manganese tricarbonyl, adding other additives according to a table 1-5, and uniformly blending to obtain the aviation gasoline, wherein the property of the aviation gasoline is shown in a table 1-6.

TABLE 1-1

Tables 1 to 2

Tables 1 to 3

Tables 1 to 4

Tables 1 to 5

Additive agent	2, 6-di-tert-butyl-4-methylphenol	Diethylene glycol monomethyl ether	Stadis 450	DCI-4A
					Adding amount of	10mg/L	0.12% by volume	2mg/L	20mg/m3

Tables 1 to 6

Example 2

Mixing 65 mass percent of side draw oil of a fractionating tower of an alkylation device (the property of the side draw oil is shown in a table 2-1), 15 mass percent of light naphtha of a hydrocracking device (the property of the side draw oil is shown in a table 2-2), 10 mass percent of aromatic hydrocarbon blending component of an aromatic hydrocarbon extraction device (the property of the aromatic hydrocarbon blending component is shown in a table 2-3) and 10 mass percent of meta-xylene (the property of the meta-xylene is shown in a table 2-4), adding 180mg/L of methylcyclopentadienyl manganese tricarbonyl, adding other additives according to the table 1-5, and uniformly blending to obtain the aviation gasoline, wherein the property of the aviation gasoline is shown in a table 2-5.

TABLE 2-1

Tables 2 to 2

Tables 2 to 3

Tables 2 to 4

Tables 2 to 5

Example 3

Mixing 70 mass percent of side draw oil of a fractionating tower of an alkylation device (the property of the side draw oil is shown in a table 3-1), 12 mass percent of atmospheric and vacuum overhead oil (the property of the side draw oil is shown in a table 3-2), 8 mass percent of aromatic hydrocarbon blending component of an aromatic hydrocarbon extraction device (the property of the aromatic hydrocarbon blending component is shown in a table 3-3) and 10 mass percent of meta-xylene (the property of the meta-xylene is shown in a table 3-4), adding 160mg/L of methylcyclopentadienyl manganese tricarbonyl, adding other additives according to the table 1-5, and uniformly blending to obtain the aviation gasoline, wherein the property of the aviation gasoline is shown in a table 3-5.

TABLE 3-1

TABLE 3-2

Tables 3 to 3

Tables 3 to 4

Tables 3 to 5

Example 4

Mixing 60 mass percent of side draw oil of a fractionating tower of an alkylation device (the property of the side draw oil is shown in a table 4-1), 10 mass percent of atmospheric and vacuum top oil (the property of the side draw oil is shown in a table 4-2), 15 mass percent of aromatic hydrocarbon blending component of an aromatic hydrocarbon extraction device (the property of the aromatic hydrocarbon blending component is shown in a table 4-3) and 15 mass percent of isopropyl benzene (the property of the isopropyl benzene is shown in a table 4-4), adding 180mg/L of methylcyclopentadienyl manganese tricarbonyl, adding other additives according to the table 1-5, and uniformly blending to obtain the aviation gasoline, wherein the property of the aviation gasoline is shown in a table 4-5.

TABLE 4-1

TABLE 4-2

Tables 4 to 3

Tables 4 to 4

Tables 4 to 5

Example 5

Mixing 65 mass percent of side draw oil of a fractionating tower of an alkylation device (the property of the side draw oil is shown in a table 5-1), 14 mass percent of atmospheric and vacuum top oil (the property of the side draw oil is shown in a table 5-2), 12 mass percent of aromatic hydrocarbon blending component of an aromatic hydrocarbon extraction device (the property of the aromatic hydrocarbon blending component is shown in a table 5-3) and 9 mass percent of isopropyl benzene (the property of the isopropyl benzene is shown in a table 5-4), adding 150mg/L of methylcyclopentadienyl manganese tricarbonyl, adding other additives according to the table 1-5, and uniformly blending to obtain the aviation gasoline, wherein the property of the aviation gasoline is shown in a table 5-5.

TABLE 5-1

TABLE 5-2

Tables 5 to 3

Tables 5 to 4

Tables 5 to 5

Comparative example 1

Mixing 65 mass percent of side draw oil of a fractionating tower of an alkylation device (the property of the side draw oil is shown in a table 6-1), 14 mass percent of atmospheric and vacuum initial top oil (the property of the side draw oil is shown in a table 6-2), 12 mass percent of aromatic hydrocarbon blending component of an aromatic hydrocarbon extraction device (the property of the aromatic hydrocarbon blending component is shown in a table 6-3) and 9 mass percent of isopropyl benzene (the property of the isopropyl benzene is shown in a table 6-4), adding other additives according to the table 1-5, and uniformly blending to obtain the aviation gasoline, wherein the property of the aviation gasoline is shown in a table 6-5.

TABLE 6-1

TABLE 6-2

Tables 6 to 3

Tables 6 to 4

Tables 6 to 5

It can be seen from the above results of the examples that the blending can be successfully and successfully carried out by uniformly mixing various easily available components in the field, such as alkylate modified oil, light naphtha (hydrocracking unit light naphtha, atmospheric and vacuum overhead oil or atmospheric and vacuum initial overhead oil), aromatic hydrocarbon blending component of aromatic hydrocarbon extraction unit, high-octane number aromatic hydrocarbon blending component, etc., and then adding a small amount of additives, such as methylcyclopentadienyl manganese tricarbonyl, anti-icing agent, preservative, etc. The blended aviation gasoline does not contain tetraethyl lead, and meets the requirements of environmental protection, no toxicity and no pollution. Although methylcyclopentadienyl trihydroxymanganese is a known antiknock agent, its antiknock properties in aviation gasoline have not been documented. From example 5 and comparative example 1, it can be seen that methylcyclopentadienyl manganese tricarbonyl can significantly improve the antiknock properties of aviation gasoline.

The preferred embodiments of the present invention have been described above in detail, but the present invention is not limited thereto. Within the scope of the technical idea of the invention, many simple modifications can be made to the technical solution of the invention, including combinations of various technical features in any other suitable way, and these simple modifications and combinations should also be regarded as the disclosure of the invention, and all fall within the scope of the invention.