METHOD OF FORMING A FUEL-AIR MIXTURE FOR INTERNAL COMBUSTION ENGINE
20170306875 · 2017-10-26
Inventors
Cpc classification
Y02T10/30
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02M31/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M31/205
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M21/0227
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D19/0671
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02D41/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M31/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M25/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M27/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M31/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method of serially phased, phase forming a fuel-air mixture for internal combustion engine is disclosed. The technical result increases the compression ratio of the engine, resulting in economical fuel burning and improved environmental characteristics. The method includes a serially-staged, serially-phased formation of the fuel-air mixture for the engine, which includes the following steps: fuel evaporation; obtaining hydrogen-gas fuel by cleavage of the fuel; cooling and optimization of fuel temperature; preparation of air parallel to the preparation of the fuel; direct formation of the fuel-air mixture; mixing of the fuel, containing hydrocarbon gases with air, with an excess air coefficient Kea≧3; enrichment of the desired air-fuel ratio to the excess air coefficient Kea=from 1.0 to 2.8; a mixture enrichment correction; obtaining control conditions of an idling engine power mode by changing the excess air coefficient, as well as by changing the value of the cylinder filling coefficient.
Claims
1. A method of formation of a fuel-air mixture for internal combustion engine, comprising: evaporating fuel; decomposing the fuel; obtaining the hydrogen-containing gases from the fuel; cooling and optimization of the temperature of the fuel; preparation of air for mixture with the fuel; mixing the fuel and air to form a fuel-air mixture; and re-enrichment of the air-fuel mixture to the desired excess air coefficient.
2. The method of claim 1, further comprising correcting the mixture enrichment.
3. The method of claim 1, wherein the air preparation occurs in parallel with the fuel preparation.
4. The method of claim 1, wherein the mixing of the fuel containing hydrocarbon gases, with air with the excess air coefficient Kea≧[[4]]3.
5. The method of claim 1, wherein the excess air coefficient Kea=from 1.0 to 2.8.
6. The method of claim 1, wherein the preparation of the air is selected from the group consisting of humidification, ozonization, treatment with magnetic fields, and chemical treatment.
7. The method of claim 1, further comprising obtaining control conditions of an idling engine power mode by changing the excess air coefficient, as well as by changing the value of a cylinder filling coefficient.
8. The method of claim 1, wherein the step of evaporating the fuel comprises applying heat to the fuel.
9. A method of formation of a fuel-air mixture for internal combustion engine, comprising: evaporating fuel through heating of the fuel; obtaining the hydrogen-containing gases from the fuel; cooling and optimization of the temperature of the fuel; preparation of air for mixture in parallel with the fuel; mixing the fuel and air to form a fuel-air mixture; and re-enrichment of the air-fuel mixture to the desired excess air coefficient; and correcting the mixture enrichment.
10. The method of claim 9, wherein the mixing of the fuel containing hydrocarbon gases, with air with the excess air coefficient Kea≧[[4]]3.
11. The method of claim 9, wherein the excess air coefficient Kea=from 1.0 to 2.8.
12. The method of claim 9, wherein the preparation of the air is selected from the group consisting of humidification, ozonization, treatment with magnetic fields, and chemical treatment.
13. The method of claim 9, further comprising obtaining control conditions of an idling engine power mode by changing the excess air coefficient, as well as by changing the value of a cylinder filling coefficient.
Description
DETAILED DESCRIPTIOPN OF THE PREFERRED EMBODIMENTS
[0014] In the proposed method, the fuel-air mixture is formed gradually and in several stages.
[0015] In the first stage of the fuel preparation, the fuel is fed into the evaporator, where it expands during evaporation, which eliminates the use of additional aids for the movement of the fuel in the system. In the evaporator, heat can be used from either the exhaust gases, or from other sources, for example, the heat from the onboard electric-power supply.
[0016] In the second stage, fuel vapors enter into a special device, where they are exposed to factors capable of decomposition/separating the fuel. As a result, the hydrogen-containing gases are formed: H.sub.2—hydrogen, CH.sub.4—methane, C.sub.2H.sub.6—ethane, C.sub.2H.sub.4—ethylene, C.sub.2H.sub.2—acetylene, C.sub.3H.sub.8—propane, C.sub.3H.sub.6—propylene, i-C.sub.4H.sub.10-isobutene, n-C.sub.4N.sub.10-n/-butane and other derivatives of gaseous and liquid hydrocarbons in the percentage, contained in the fuel.
[0017] These factors include: thermal, dynamic, chemical, piezoelectric, of crown-discharged, electro-arced; it also includes diffuse plasma, ultrasound, cavitation, catalytic, and even nuclear—ways of fuel decomposition.
[0018] Selection of the above listed factors and their amounts depends on: [0019] 1. engine type: gasoline piston, gasoline rotary, diesel, gas turbine for aviation, gas turbine for land use, reactive, and others. [0020] 2. tasks performed by the engines: work in difficult urban environments, sports race, work in Arctic conditions, and others.
[0021] Selection of the factors affect: [0022] 1. -% formation and fractional composition of the hydrogen-containing gases. [0023] 2. the final octane number of the resulting mixture (the octane number is the degree of formation of the peroxide groups, which are the cause of the detonation. Reducing the magnitude of detonation, ultimately, increases the compression ratio.) [0024] 3. elimination of undesirable phenomena, such as formation of polymer compounds, coke and deposition of both polymer compounds and coke on the walls of the construction system [0025] 4. the rate of combustion of the mixture (the rate of flame propagation) [0026] 5. the completeness of fuel combustion [0027] 6. reducing the formation of harmful compounds such as CO, NO.sub.3, and others, without the use of special filters—the exhaust gas neutralizers [0028] 7. the ability to support all of the above properties of the fuel under extremely low air temperatures and in a wide range of values of excess air coefficient Kea=from 1.0 to 2.80, which are important for aircraft engines. [0029] 8. possibility of using different types of liquid fuel and their mixtures (multifuel) [0030] 9. the elimination of differences between the requirements for the use of special fuels—summer-fuel, winter-fuel, arctic-fuel, on the basis of alcohol, etc.,
[0031] Because these effects are highly desirable and are one of the goals to achieve in this development, the proposed method involves the use of up to several factors capable of decomposing the fuel, acting on the fuel at the same time (parallel) or sequentially.
[0032] The next step in fuel preparation is cooling and temperature adjustment to avoid unintentional ignition when connecting with the air, as well as to create a stable and optimum temperatures of air-fuel mixture.
[0033] In parallel with the fuel preparation, air can be prepared, just like the fuel, in stages or simultaneously. The preparation of the air may include steps such as humidification, ozonation (ozone treatment), an air treatment with magnetic fields, such as HFC (high frequency current), the introduction of chemicals, such as oxidizing agents, or others—in the presence of which combustion processes give the best environmental effect.
[0034] After the completion of the preparation of the fuel and air, the first phase of the formation of direct air-fuel mixture (the fuel mixing) comes into action, with the content of hydrogen-containing gases, and the air with excess air coefficient Kea≧3.
[0035] The second phase is the re-enrichment of the fuel-air mixture to the desired excess air coefficient Kea. The desired excess air coefficient Kea depends on the regime of engine load at a particular time and is determined by the electronic system of the engine.
[0036] Since the resulting fuel mixture has high anti-knock properties and is able to burn well in a fairly wide range of excess air coefficient values Kea, the observed method regulates the load on the engine using not only the fullness of the cylinder, but also by changing the excess air coefficient of Kea in the broad range from 1.0 to 2.8.
[0037] In connection with this, the proposed method provides another phase, or more additional phases—which correct and re-enrich the mixture.
[0038] It would be appreciated by those skilled in the art that various changes and modifications can be made to the illustrated embodiments without departing from the spirit of the present invention. All such modifications and changes are intended to be within the scope of the present invention except as limited by the scope of the appended claims.