140 results about "Jet fuel" patented technology

The present invention relates to a process for producing a jet fuel composition (12), the process comprising: a) Processing an oxygenate stream (1) in an Oxygenate-to-Olefin (OtO) unit (2) to produce an olefin stream (3); b) Separating the olefin stream (3) in a fractionation unit (4) into at least a C2-olefin-rich stream (5), a C3-olefin-rich stream (6) and a C4+-olefin-rich stream (7); c) Dimerizing at least a portion of ethylene contained in the C2-olefin-rich stream (5) to C4-olefins in a dimerization unit (20), thereby producing a dimerized product stream (21); d) Processing an oligomerization feed (8) comprising at least a portion of the C4+-olefin-rich stream (7) and at least a portion of the dimerized product stream (21) in an oligomerization unit (9) to produce an oligomerized olefin stream (10); e) Hydrogenating at least a portion of the oligomerized olefin stream (10).

The present invention relates to a process for producing a jet fuel composition (12), the process comprising: a) Processing an oxygenate stream (1) in an Oxygenate-to-Olefin (OtO) unit (2) to produce an olefin stream (3); b) Processing an oligomerization feed (8) comprising at least a portion of the olefin stream (3) in an oligomerization unit (9) to produce an oligomerized olefin stream (10); c) Hydrogenating at least a portion of the oligomerized olefin stream (10); wherein a fraction of the oligomerized olefin stream (10) is withdrawn as a recycle stream (40a, 40b) and passed to a steamcracking unit (41) to produce a steamcracking product stream (42), wherein at least a portion of the steamcracking product stream (42) is included in the oligomerization feed (8).

The present invention relates to a process for producing a jet fuel composition (12), the process comprising: a) Processing an oxygenate stream (1) in an Oxygenate-to-Olefin (OtO) unit (2) to produce an olefin stream (3); b) Providing an oligomerization feed (8) comprising at least a portion of the olefin stream (3) and at least a portion of an external C4+-olefin stream (30) comprising C4+-olefins; c) Processing the oligomerization feed (8) in an oligomerization unit (9) to produce an oligomerized olefin stream (10); d) Hydrogenating at least a portion of the oligomerized olefin stream (10).

A process for the production of sustainable aviation fuel (SAF) with low carbon intensity. The jet fuel is produced from the reaction of hydrogen from the electrolysis of water with captured carbon dioxide. The hydrogen and carbon dioxide are reacted to product a stream comprising carbon monoxide. Hydrogen and carbon monoxide are reacted to produce n-alkanes. Alkanes are hydroisomerized to produce sustainable aviation fuel with low carbon intensity.

A process for oligomerizing olefins to distillate fuels in the presence of a diluent for absorbing the exotherm. Oligomerization may comprise oligomerizing a charge olefin stream in a first-stage oligomerization reactor which is oligomerized in a second-stage oligomerization reactor to provide an oligomerate stream. The oligomers are hydrogenated and stripped to provide a stripped distillate stream. The diluent may be taken from the stripped distillate stream.

Systems and methods are provided for co-processing plastic waste in a coker as part of an integrated refinery environment that produces kerosene, jet fuel, and / or jet fuel blending components as a product. The co-processing can be performed in a fluidized coker, a delayed coker, or a combination of fluidized cokers and delayed cokers. After coking, hydroprocessing can be performed on one or more portions of the coker effluent that contribute to formation of the kerosene, jet fuel, and / or jet fuel blending component product(s). The hydroprocessing can be used to reduce or minimize the presence of unexpected nitrogen contaminants in the resulting kerosene, jet fuel, and / or jet fuel blending component product(s).

This application discloses a process for making jet fuel including: (1) oligomerizing an olefin stream to an oligomer stream; (2) hydrogenating said oligomer stream to provide a paraffin stream; (3) separating said paraffin stream to provide a jet fuel stream and a reformer feed stream; and (4) reforming said reformer feed stream to provide a reformed stream with an increased concentration of aromatics.

The invention discloses a method for synthesizing sustainable aviation kerosene through CO2 hydrogenation in biogas. The method comprises the following steps: taking Fe / Mn-CaO as a CO2 adsorption separating agent, taking NiMoGa ternary liquid metal as a catalyst for methane decarbonization hydrogen production, and taking a metal oxide-molecular sieve as a catalyst for synthesizing aryl aviation kerosene through CO2 hydrogenation. According to the metal oxide-molecular sieve catalyst for synthesizing the aromatic sustainable aviation kerosene through CO2 hydrogenation, a metal oxide (ABO3) with a perovskite structure is synthesized through a sol-gel method, and the metal oxide (ABO3) is physically mixed with a molecular sieve; a in ABO3 is lanthanum, and a B element comprises iron, chromium, cobalt or nickel; the molecular sieve contains ZSM-5 (Zeolite Socony Mobil-5), ZSM-11 (Zeolite Socony According to the oxide catalyst disclosed by the invention, a polydentate chelate is formed by metal nitrate and citric acid, and a special perovskite structure can be formed through simple drying and roasting, so that the oxide catalyst has excellent carburization resistance, and a formed oxygen-containing intermediate is diffused into a zeolite molecular sieve to form aromatic aviation kerosene; the preparation of aryl aviation kerosene from bio-based CO2 hydrogenation is realized.

The invention provides an ammonia fuel cell power generation dual-fuel scramjet engine capable of achieving energy gradient utilization, belongs to the technical field of aircraft thermal protection and power generation, and solves the problems that a traditional airborne power generation system is difficult to use due to the high incoming flow Mach number in hypersonic flight, and coking is caused in a regeneration cooling channel of a fuel decomposition gas turbine. Ammonia and aviation kerosene generate high-temperature fuel gas in a combustion chamber of the scramjet engine to push the engine to generate thrust; high-temperature waste heat of the combustion chamber is recycled through the regeneration cooling channel, fuel is heated, a part of ammonia is decomposed, and decomposed gas drives a turbine generator to generate electric energy. According to the power generation system for gradient utilization of energy, factors such as actual use temperature and pressure are fully considered, the energy utilization efficiency is effectively improved, energy waste is reduced, and reasonable adaptation of energy is achieved, so that the power generation efficiency of the whole system is improved, and the electric energy requirement of a hypersonic aircraft is greatly met.

The present invention relates to a process for producing a jet fuel composition (12), the process comprising: a) Processing an oxygenate stream (1) in an Oxygenate-to-Olefin (OtO) unit (2) to produce an olefin stream (3); b) Separating the olefin stream (3) in a fractionation unit (4) into at least a C2-olefin-rich stream (5), a C3-olefin-rich stream (6) and a C4+-olefin-rich stream (7); c) Processing an oligomerization feed comprising a first oligomerization feed stream (8a) containing at least a portion of the C3-olefin-rich stream (6) and a second oligomerization feed stream (8b) containing at least a portion of the C4+-olefin-rich stream (7) in an oligomerization unit (9) to produce an oligomerized olefin stream (10); d) Hydrogenating at least a portion of the oligomerized olefin stream (10); wherein the oligomerization unit (9) comprises at least a first reaction zone (9a), and a second reaction zone (9b) downstream of the first reaction zone (9a); wherein the first oligomerization feed stream (8a) is introduced into the oligomerization unit (9) at a position upstream of the first reaction zone (9a), and the second oligomerization feed stream (8b) is introduced into the oligomerization unit (9) at a position downstream of the first reaction zone (9a) and upstream of the second reaction zone (9b).

Disclosed is a process for producing a jet fuel, comprising a step of converting an alcohol stream in a fluidized bed, a jet fuel and a plant associated with said process. The process involves the following steps:(a) converting a C1 to C6 alcohol stream to produce a mixture containing paraffins, olefins, aromatics, and water;(b) separating water from the mixture;(c) oligomerizing olefins; and(d) alkylating aromatics from the mixture;(e) forming a stream of hydrocarbons to be hydrogenated;(f) hydrogenating the stream of hydrocarbons to be hydrogenated;(g) recovering at least one jet fuel fraction from the hydrogenated hydrocarbon stream.Conversion step (a) is carried out in a reaction zone comprising at least one fluidized catalytic bed.In the mixture of paraffins, olefins, aromatics and water produced in conversion step (a), the ratio of the mass of C3+ olefins to the total mass of olefins is greater than or equal to 0.8.

This invention discloses an automated system and method for determining the trace total acid value of jet fuel. The system includes a sample moving unit, a titration unit, a nitrogen control unit, and a jet fuel total acid value determination unit. The sample moving unit moves the titration cup containing the sample below the titration unit. The nitrogen control unit maintains a nitrogen atmosphere inside the titration cup. The titration unit includes a porous burette, a burette tube, a photometric electrode, and a temperature electrode. The porous burette seals the titration cup. The titration unit injects titrant, mixed solvent, and mixed titration solvent into the titration cup, and determines the titration endpoint using the photometric and temperature electrodes. The jet fuel total acid value determination unit integrates the data from the titration unit to calculate the jet fuel total acid value. This invention eliminates endpoint errors that may result from subjective human judgment using manual indicators, and overcomes the need for machine vision technology, which requires the construction and intelligent training of a dataset of titration endpoint color images, in specialized instrument methods.

The application relates to a method for producing jet fuel from oil and fat raw materials, wherein the oil and fat raw materials are reacted with a hydrotreating catalyst in a hydrotreating reaction zone, the obtained liquid hydrocarbons are introduced into a first hydroisomerization reaction zone, an optional second hydroisomerization reaction zone is arranged, the obtained diesel oil fraction is recycled into the first hydroisomerization reaction zone or introduced into the second hydroisomerization reaction zone for reaction, and the reaction effluent is separated to obtain jet fuel. The application can produce high-quality biological jet fuel at a high yield.

Disclosed are systems and methods for producing renewable alcohols by fermentative processes using cell lysate or a combination of cell lysate and whole cells, as well as the cell lysate itself. The disclosure also provides processes and systems for converting renewable alcohols to transportation fuels, such as, gasoline, jet fuel, and diesel fuels.

A process for producing a jet fuel fraction (41), said process comprising steps of feeding at least one of a biogas stream (1), a carbon dioxide stream (2), or a methane stream (3), and at least a fraction of a tail gas recycle stream (32), to a reformer section (10) to provide a synthesis gas stream (11); feeding said synthesis gas stream (11, 22) to a synthesis section (30) to provide a stabilized condensate stream (31), a liquid wax stream (38), the tail gas recycle stream (32) and a concentrated oxygenate recycle stream (36); refining at said stabilized condensate stream (31) and liquid wax stream (38) in a refinery section (40) to provide a jet fuel fraction stream (41); and recycling said concentrated oxygenate recycle stream (36) to a biogas plant, and a plant for carrying out the process.

The utility model relates to an automatic tester for the total acid value of jet fuel, which comprises a machine table, a titration device, an aeration device, a light source, a reflecting mirror, a camera and a controller, and a test station and a collection station are arranged on the machine table; the aeration device comprises an aeration pipe, a gas supply control element, a moving mechanism and a cleaning mechanism, the moving mechanism drives the aeration pipe to move, and the aeration pipe is communicated with a nitrogen source through the gas supply control element; the cleaning mechanism comprises an inner flushing assembly for flushing the inner wall of the aeration pipe and an outer flushing assembly for flushing the outer wall of the aeration pipe. After the test sample is measured, the moving mechanism controls the aeration pipe to lift and move to the collecting station, and then controls the inner flushing assembly and the outer flushing assembly to start, so that the inside and the outside of the aeration pipe can be flushed, and flushing wastewater is collected at the collecting station. And the flushed aeration pipe is translated to the test station again to wait for starting the next measurement. Moving and cleaning of the aeration pipe are controlled by the controller, automatic execution can be achieved, and labor is saved.

The invention belongs to the field of stoichiometry, and relates to a preparation method of a standard substance, in particular to a jet fuel water separation index standard substance and a preparation method thereof, a plurality of emulsifiers are screened out and are used for preparing the water separation index standard substance, so that the quantity value stability of the standard substance is greatly improved, and the stability of the standard substance is remarkably prolonged; when in use, the water separation index tester does not need to be prepared and used immediately, is convenient to operate, and improves the simplicity, accuracy and stability of verification and calibration of the water separation index tester.

Provided are an apparatus and a method for producing a synthetic fuel with which it is possible to obtain a hydrocarbon having a high selectivity of jet fuel components and to produce a jet fuel at a high yield. A synthetic fuel production device (1) for producing a predetermined synthetic fuel by a direct FT synthesis reaction using a raw material gas containing hydrogen gas and carbon dioxide, the synthetic fuel production device (1) being provided with: a reactor (9) having a cylindrical reactor main body section (9a) filled with a predetermined FT catalyst (20) for generating a direct FT synthesis reaction; a raw material gas flow rate adjustment unit (7) and / or composition adjustment units (5a, 5b) for adjusting the flow rate of the raw material gas supplied to the reactor (9); and a control device (3) that controls the linear velocity, which is the flow rate of the raw material gas per unit cross-sectional area of the reactor main body section (9a), by controlling the raw material gas flow rate adjustment section (7) and / or the composition adjustment sections (5a, 5b), and that controls the linear velocity to 0.2 m / sec to 4.0 m / sec when a given synthetic fuel is a jet fuel.

The utility model discloses distillation equipment for biological aviation kerosene production, which relates to the technical field of distillation equipment and comprises an equipment main body, an electric push rod is fixedly connected to the outer wall of the equipment main body, and one end of the electric push rod is fixedly connected with a lifting plate slidably connected with the outer wall of the equipment main body. The outer wall of the lifting plate is rotationally connected with a pulling rod, and one end of the pulling rod is rotationally connected with a connecting rod. By arranging the pull rod, when auxiliary aviation kerosene production is carried out through distillation equipment, in order to improve the synchronous protection effect on a distillation head and the shielding protection effect on the top of a collecting box under the condition that an oil drum is switched for use, the lifting plate ascends through rotation of the pull rod; and a connecting rod fixedly connected with a limiting rod is driven to slide, so that a first protection plate moves to the position below the distillation head, a second protection plate moves to the top of a collection box, the situation that kerosene leaks and is wasted is reduced, and the aviation kerosene production efficiency of the distillation equipment is improved.

The present invention discloses a method for synthesizing polycyclic alkanes from phenols derived from lignin via a one-pot two-step process. 1) In the first step of the reaction, the phenolic compound derived from lignin is first converted into a ketone compound under the action of a hydrogenation catalyst, and then the ketone compound rapidly undergoes aldol condensation under the action of a solid acid to generate a jet fuel precursor; 2) In the second step of the reaction, the product of the first step is not separated, but the reaction conditions are directly strengthened. The jet fuel precursor is directly subjected to complete hydrodeoxygenation to generate polycyclic alkanes under the action of the hydrogenation catalyst and the solid acid in the first step; the phenolic compound derived from lignin is synthesized into polycyclic jet fuel by changing the reaction conditions in a single reaction vessel. Compared with traditional chain-like jet fuel, it has a higher density and a higher calorific value and can be used as a substitute for traditional aviation fuel. The catalyst and raw materials used in the present invention are abundant in source, low in price, and easy to separate; the entire production process is simple to operate.

An aviation fuel composition is disclosed, containing 50-95 vol-% of petroleum-derived jet fuel component, and 5-50 vol-% of renewable middle distillate component. The fuel composition has a viscosity of 12 mm2 / s or below at −40° C., 10 mm2 / s or below at −30° C., and 8 mm2 / s or below at −20° C., as measured in accordance with an EN ISO 3104 (1996) standard. A method for producing the aviation fuel composition is also disclosed. The method containing mixing the petroleum derived jet fuel component and the renewable middle distillate component to obtain the aviation fuel composition, such that the petroleum-derived jet fuel component and the renewable middle distillate component are mixed together in an amount containing 5-50 vol-% of renewable middle distillate component and about 50-95 vol-% of petroleum-derived jet fuel component.

The invention relates to a process for producing a jet fuel from a mixture to be treated, comprising, in particular, a mixture of phenolic compounds, preferably a lignin oil, the process comprising a step of hydrotreating the mixture to be treated, wherein the mixture to be treated has specific properties. The present invention also relates to a mixture of hydrocarbons and to a jet fuel obtained using this process.

The present invention provides a method and system for hydrocracking of high-nitrogen raw materials. The hydrocracking system includes a hydrogenation reaction unit, a separation unit, and a second fractionation tower; wherein the hydrogenation reaction unit includes a hydrofining reaction zone and a hydrocracking reaction zone; and the separation unit includes a gas-liquid separator and a first fractionation tower. The method for hydrocracking of high-nitrogen raw materials includes the following steps: high-nitrogen raw oil and hydrogen are mixed and sequentially enter the hydrofining reaction zone and the hydrocracking reaction zone for reaction, and the hydrocracking product oil obtained after the reaction is separated to obtain gas, light naphtha, heavy naphtha, jet fuel, diesel, and tail oil. The method of the present invention not only improves the yield of intermediate distillate oil but also solves the problem of substandard quality of the jet fuel fraction generated by processing high-nitrogen raw materials, providing favorable technical support for the stable and efficient production of enterprises.

Internal combustion engine (110), powered by ducted jet direct fuel injection, having a cylinder head (130) and at least one piston (140) to form a combustion chamber (150), in which the cylinder head (130) is provided with: - a channel (20) inside which an injector (170) is positioned in line with the channel (20), - a plurality of ducts (30) that branch off from the channel (20) and connect the channel (20) to the combustion chamber (150), - a plurality of features designed to promote airflow within the ducts (30). Methodology for identifying any maximum acceptable misalignments between fuel jets and ducts (30).

PROCESS FOR PRODUCING A JET FUEL FROM FEEDSTOCKS OF RENEWABLE ORIGIN The invention relates to a process for producing a jet fuel comprising at least the steps of: a) providing fatty acid ethyl esters from the reaction of animal fats and / or waste oils with methanol in a transesterification reactor, b) providing hydrocarbons of fossil origin, c) preparing a hydrocarbon feedstock containing the hydrocarbons of fossil origin provided by step b) and the fatty acid ethyl esters provided by step a) in a content of at most 5% by volume relative to the hydrocarbon feedstock, d) subjecting the hydrocarbon feedstock prepared in step c) to hydrotreatment and obtaining a treated hydrocarbon feedstock, e) fractionating the treated hydrocarbon feedstock obtained in step d) and recovering a kerosene fraction as jet fuel. Figure 1

This invention discloses a hydrorefining catalyst for the production of rocket jet fuel rich in cyclohexane-substituted compounds and a method for producing rocket jet fuel rich in cyclohexane-substituted compounds using the catalyst. According to the method of this invention, hydrocarbons with different ring numbers are refined, so the rocket kerosene fuel obtained has a high content of cyclohexane-substituted compounds and an extremely low content of easily coking substances, which reduces the carbon deposition rate of the engine and can effectively extend the service life of the engine.

Plant and process for converting a gaseous hydrocarbon feed to methanol, optionally to a transportation range fuel such as any of a gasoline product, a jet fuel product, and a diesel product; the plant including a synthesis gas section, a methanol synthesis section, optionally and a transportation range fuel synthesis section. The plant also includes diverting and supplying a purge gas from the methanol synthesis section to a water gas shift (WGS) section, CO2-removal section, and a first hydrogen purification section. In an embodiment, the first hydrogen purification section provides a first H2-rich gas, a second H2-rich gas, and a first hydrogen purification section off-gas. One or more fired heaters are suitably arranged to receive at least a portion of the second H2-rich gas.

An aircraft propulsion system includes a compressor section, a combustor section, and a fuel system assembly. The compressor section includes a plurality of inlet guide vanes, an inlet guide vane actuator (IGVA), and an IGVA servo. The IGVA is operably coupled with the plurality of inlet guide vanes. The IGVA servo is connected in fluid communication with the IGVA. The combustor section includes a combustor. The fuel system assembly includes a jet fuel system and a hydrogen fuel system. The jet fuel system is connected in fluid communication with the combustor. The hydrogen fuel system is connected in fluid communication with the combustor and the IGVA servo. The hydrogen fuel system is configured to direct the hydrogen fuel to the IGVA servo to control a position of the IGVA.

A process for oligomerizing olefins to distillate fuels in the presence of a diluent for absorbing the exotherm. Oligomerization may comprise oligomerizing a charge olefin stream in a first-stage oligomerization reactor which is oligomerized in a second-stage oligomerization reactor to provide an oligomerate stream. The oligomers are hydrogenated and stripped to provide a stripped distillate stream. The diluent may be taken from the stripped distillate stream.

A process for dimerizing and oligomerizing olefins to distillate fuels in which the oligomerized product is subjected to hydrocracking and hydroisomerization in a single reactor to convert heavier oligomers to jet fuel range oligomers. A jet fuel product stream is removed from the side of a stripping tower and a heavy drag stream is produced from the bottom of the stripping tower to ensure that the end boiling point specification is met.