WO2012154070A1 - Process for achieving total combustion with the help of injectors and injectors - Google Patents
Process for achieving total combustion with the help of injectors and injectors Download PDFInfo
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- WO2012154070A1 WO2012154070A1 PCT/RO2012/000006 RO2012000006W WO2012154070A1 WO 2012154070 A1 WO2012154070 A1 WO 2012154070A1 RO 2012000006 W RO2012000006 W RO 2012000006W WO 2012154070 A1 WO2012154070 A1 WO 2012154070A1
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- Prior art keywords
- pipe
- compressed air
- injector
- total combustion
- tap
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
- F23L5/00—Blast-producing apparatus before the fire
- F23L5/04—Blast-producing apparatus before the fire by induction of air for combustion, e.g. using steam jet
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M67/00—Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type
- F02M67/02—Apparatus in which fuel-injection is effected by means of high-pressure gas, the gas carrying the fuel into working cylinders of the engine, e.g. air-injection type the gas being compressed air, e.g. compressed in pumps
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F25/00—Flow mixers; Mixers for falling materials, e.g. solid particles
- B01F25/30—Injector mixers
- B01F25/31—Injector mixers in conduits or tubes through which the main component flows
- B01F25/313—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced in the centre of the conduit
- B01F25/3131—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced in the centre of the conduit with additional mixing means other than injector mixers, e.g. screens, baffles or rotating elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F25/00—Flow mixers; Mixers for falling materials, e.g. solid particles
- B01F25/30—Injector mixers
- B01F25/31—Injector mixers in conduits or tubes through which the main component flows
- B01F25/313—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced in the centre of the conduit
- B01F25/3132—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced in the centre of the conduit by using two or more injector devices
- B01F25/31322—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced in the centre of the conduit by using two or more injector devices used simultaneously
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F25/00—Flow mixers; Mixers for falling materials, e.g. solid particles
- B01F25/40—Static mixers
- B01F25/42—Static mixers in which the mixing is affected by moving the components jointly in changing directions, e.g. in tubes provided with baffles or obstructions
- B01F25/43—Mixing tubes, e.g. wherein the material is moved in a radial or partly reversed direction
- B01F25/433—Mixing tubes wherein the shape of the tube influences the mixing, e.g. mixing tubes with varying cross-section or provided with inwardly extending profiles
- B01F25/4335—Mixers with a converging-diverging cross-section
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M21/00—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
- F02M21/02—Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
- F02M21/0218—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
- F02M21/0287—Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers characterised by the transition from liquid to gaseous phase ; Injection in liquid phase; Cooling and low temperature storage
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
- F02M25/022—Adding fuel and water emulsion, water or steam
- F02M25/032—Producing and adding steam
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M31/00—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture
- F02M31/02—Apparatus for thermally treating combustion-air, fuel, or fuel-air mixture for heating
- F02M31/16—Other apparatus for heating fuel
- F02M31/18—Other apparatus for heating fuel to vaporise fuel
- F02M31/186—Other apparatus for heating fuel to vaporise fuel with simultaneous mixing of secondary air
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M51/00—Fuel-injection apparatus characterised by being operated electrically
- F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
- F02M51/061—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C99/00—Subject-matter not provided for in other groups of this subclass
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/48—Nozzles
- F23D14/52—Nozzles for torches; for blow-pipes
- F23D14/54—Nozzles for torches; for blow-pipes for cutting or welding metal
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/62—Mixing devices; Mixing tubes
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M5/00—Casings; Linings; Walls
- F23M5/02—Casings; Linings; Walls characterised by the shape of the bricks or blocks used
- F23M5/025—Casings; Linings; Walls characterised by the shape of the bricks or blocks used specially adapted for burner openings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B2275/00—Other engines, components or details, not provided for in other groups of this subclass
- F02B2275/14—Direct injection into combustion chamber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24H—FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING HEAT-GENERATING MEANS, e.g. HEAT PUMPS, IN GENERAL
- F24H1/00—Water heaters, e.g. boilers, continuous-flow heaters or water-storage heaters
- F24H1/10—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium
- F24H1/12—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium
- F24H1/14—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium by tubes, e.g. bent in serpentine form
- F24H1/16—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium by tubes, e.g. bent in serpentine form helically or spirally coiled
- F24H1/165—Continuous-flow heaters, i.e. heaters in which heat is generated only while the water is flowing, e.g. with direct contact of the water with the heating medium in which the water is kept separate from the heating medium by tubes, e.g. bent in serpentine form helically or spirally coiled using fluid fuel
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- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/30—Use of alternative fuels, e.g. biofuels
Definitions
- This invention relates to a process of achieving a total combustion at fuels, with help of at injectors, that would reduce total emissions of pollutants in the atmosphere will be solved, in large part crisis climatic, will stop the greenhouse effect and global warming with which is facing civilization.
- the invention's field of use is very wide, e.g.; engines at the cars and trucks, engines of propulsion, engines for aircraft, engines of at vessels and of all transport facilities and burning for heat and electricity devices. All types of fuels used until now have been burned without control, through a burning incomplete, in itself, which has led uncontrolled pollution into the atmosphere This has led to global warming, and the greenhouse effect. The total burning of fuels, including wood, can stop global warming and the greenhouse effect.
- the books of specialty show a total combustion of methane CH4 with oxygen.
- the first principle of the THERMOCHIJVnSTRY 1 shows that the engines are produced by manufacturers at a fuel equivalent ratio ⁇ >1 and through combustion, it produces only oxide of carbon CO, and oxide of hydrogen HO, plus fuel.
- the fuels which not are total combusted, are those that have contributed at the greenhouse effect and at the global warming. Practically the gases which have caused global warming and greenhouse effect, are oxides: CO, HO, NO, SiO, SO, and methane; these are more slight than air.
- the technical problem which my invention proposes to solve is a process which achieves a total combustion of fuels, a process which is capable to endowed, with the necessary amount of air, fuels in order to achieve a total combustion.
- My invention solves this problem by using injectors with compressed air into the pipe of air, which has in centre a pipe for fuels.
- the compressed air will absorb the quantity of fuel used at combustion, achieving a total combustion of fuels through firing.
- the total combustion presented in the books of specialists we reached at the conclusion that you must built an injector which inject into the burning air space molecule by molecule of fuel, because only in this way these a molecule of fuel will be surrounded by the molecules of air needed for achieved a total combustion of fuels.
- the chemical stoichiometric equation for a total combustion of hydrocarbons with air is.
- Column 1 contains several hydrocarbons and theirs chemical formula.
- Column 3 contains the number of air compressed molecules stoichiometricaly needed for total combustion at one molecule of hydrocarbons.
- the pipe for compressed air will be with 90 mm longer than the pipe for fuel. This length of 90mm creates a zone of rapid mixing on basis of the pressure and diffusion.
- - Fig. 1 injector for total combustion with mixture between compressed air, fuel and coal.
- injector for engines with propulsion used in place of the combustion chamber.
- injector used for distribution of methane gas.
- injector with compressed air which supplies engines with a mixture of compressed air and fuel.
- - Fig. 8 cylinder's geometry with piston.
- - Fig. 9 reactor with closed system to produce steam or hot water in a turbine.
- - Fig. 1 1 reactor with closed system for producing warming and hot water in private houses.
- This example refers to an injector (Fig 1) for a total combustion with a mixture between compressed air, fuel (crude oil) and coal.
- the injector is made of three different concentric pipes with diameters chosen from Table 1.
- the pipe 1 for crude oil is fitted with the tap 2
- both pipes are mounted in the center at the pipe 3 for air compressed at 5 to 150 ATM.
- which is fitted with the tap 4 a flange 11.
- the mixing of total combustion is achieved in the area 7, which continues with angle 8 for speed, here the mixing is total, the mixture leaving the injector through the angle 9 in the shape of a cone 10 of injection (Fig, 1).
- the taps 2, 4, and 6 are opened of the pipes 1, 3, 5.
- This injector is easily to be manufactured in large memori. Similarly, all installation of combustion for coal, can be equipped with such injector in a year or two. The injector will reduce fuel consumption with 50 %.
- the diameter of pipe 3 between the angles 8 and 9, is 3 mm and this depends on the size aof the injector.
- the pipe with compressed air is with 90 mm longer which form zone 7.
- the diameters at the pipes mentioned above are calculated in accordance with the Column 4 from Table 1, for fuel selected from the Column 1 from Table 1.
- This examples refers to an injector for total combustion with mixture between compressed air and fuel (crude oil), intended for all fuels mentioned in Table 1.
- the injector consists of two concentric pipes, pipe 1 with crude oil is fitted with a tap 2 (Solenoid), the pipe 1 is mounted in center of pipe 3 for air compressed at 10 at 250 ATM, or more, and fitted with solenoid 4, the mixture for a total combustion is achieved in zone 7, which finishes with angle 8 for speed; this is the region where the mixture is totally mixed, the mixture will be injected through angle 9 in the shape of a cone 10, a flange 11 (Fig. 2).
- a molecule of crude oil needs 107,40 molecules of air for total combustion according to Table 1
- the pipe 3 with compressed air is 90 mm, longer than the pipe 1 of crude oil, and creates zone 7.
- the resulting products are H 2 0 + C0 2 + N 2 + energy
- solenoids When the injector begins to work, at the same time, solenoids must open the taps 2 and 4 at the pipes 1, 3.
- the air having the pressure of 10 to 250 ATM or more, will transport 107.40 molecules.
- 107, 40 molecules of compressed air reach the zone 7 of homogenized mixture, on basis of the vacuum created in front of the pipe 1 for crude oil, will absorbe, at the same time, o molecule of crude oil from pipe 1.
- This mixture reaches the angle 8 of 60° for speed, then passes in the angle 9 of 90° and will be injected in reactor in the shape of the cone 10.
- This example refers to an injector for total combustion for engines with propulsion, which will replace the combustion chamber known so far.
- the injector is composed of a pipe 3 for compressed air, four pipes 1 for the fuel isooctane, arranged at 90° one of the other, fitted with a particular tap 2, the angle 8 of speed and the angle 9 for injection in the shape of a cone 10.
- the mixture of combustion is realized in zone 7 finished with theangle 8 for speed, the mixture leaving the injector through the angle 9 (Fig 3).
- the engines with propulsion will be designed in accordance with Table 1.
- the compressor at engine with propulsion must ensure air at a minimum of 5 ATM pressure.
- the tap 2 fitted with the pipe 1 for isooctane regulates the flow which is absorbed with a rotation of 360° for the total combustion,.
- isooctane must flow easy in the injector.
- the reservoir with isooctane must be set up above engine in case of an airplane.
- the angle 8 is 50° for the mixture prepared in zone 7 and the mixture is totall homogenized.
- the mixture is than injected through the angle 9 of 30°, than the mixture is ignited to create propulsion of the engine.
- - PI is the pressure (5 at 150 ATM or more) of the compressed air and it is selected.
- - P2 is the atmospheric pressure in the pipe for fuel .
- an injector is fitted up on the pipe of distribution (Fig 4).
- the pipe 3 for compressed air in the injector has a diameter D A which is the same with the diameter of pipe for distribution.
- one molecule of the methane gas needs 10, 52 molecules of air (Table 1, Column 3) for a total combustion.
- the air is compressed at a pressure between 5 at 150 ATM.
- This injector will be fitted up on the pipe for the distribution of methane.
- This example refers to a total combustion process in the case of welding with acetylene (Fig. 5).
- - P I is the pressure at compressed air and it is 5 at 150 ATM or more (selected).
- - P2 is the atmospheric pressure in the pipe for fuel.
- - ⁇ is the viscosity of the fuel (acetylene) or air.
- the acetylene which is absorbed by the compressed air in its mass will be diffused rapidly among molecules of air.
- the pipe of compressed air will be with 90 mm longer than the pipe for acetylene. This length creates a zone 7 of quick diffusion and total mixing. When the molecules of compressed air at pressure of minimum 5 ATM reach in front of the pipe for acetylene this is absorbed in the mass with formula 6 and ensure a total combustion.
- a tap 4 is fitted with the end in the shape of a beak 12 for speed; the injector also has an angle 8 of 14°, an exit hole 13 of 0, 9 mm.
- a pipe 3 is concentricaly fitted up in the pipe 1 of acetylene, fitted with a tap 2.
- the injector also has a zone 7 with the length of 90 mm for creating the mixture between air and acetylene and a shape of a cone 10 for the flame of welding (Fig. 5).
- This example refers to a process of total combustion at the welding with propane (Fig. 6).
- - P I is the pressure of the compressed air (5 at 1 50 ATM or more) and it is selected.
- - P2 is the atmospheric pressure in the pipe for fuel .
- the propane which is absorbed by the compressed air will rapidly diffuse among the molecules of air.
- the pipe 3 for compressed air will be with 90 mm longer than the pipe 1 for propane. This length of 90 mm creates a zone 7 of diffusion for a total mixing.
- molecules of air are compressed at a pressure of minimum 5 ATM in the front of the pipe for propane and these will absorb propane in the mass of air according to formula 6, ensuring a total combustion.
- the resulting products of the total combustion of propane are: H 2 0 + C0 2 + N 2 + energy.
- the welding is achieved with the help of some different tipes of nozzles with dimensions known and available on the market, which will use compressed air of at 5 at 150 ATM.
- the pipe 3 for compressed air, fitted with a tap 4 has at end the shape of a beak 12 for increasing speed, with an angle 8 of 14° and with the exit hole 13 of 0, 9 mm.
- the compressed air pipe 3 is concentricaly fitted with a pipe 1 for propane, fitted with a tap 2; the injector also has a zone 7 with the length of 90 mm for realizing the mixture between air and propane and the flame of welding 10 has the shape of a cone (Fig. 6).
- the tap 4 fitted on the pipe 3 for compressed air is first opened and then tap 2 fitted on the pipe 1 for propane is opened at maximum.
- This example refers to a solution for total combustion of fuel, which uses an injector intended to work for delivering the mixture of compressed air and the fuel at engines in two and four-stroke; the solution can use all types of fuels presented in Table 1.
- the injector will inject the mixture of compressed air and fuel, of e.g. gasoline, in the cylinder of the engine at the same time, with the proportion
- the injector is fitted up on the cylinder head of the engine instead of the admission valves.
- Each cylinder of the engine will be equipped with such an injector.
- the injector body 16 is fitted on the cylinder head 14 with the screws 15.
- the pipe 3 for compressed air is uniting with pipe 27 for compressed air
- the pipe 1 for gasoline is fitted with the tap 2
- the gasoline flow is regulated with the special tap 17.
- the injector also has an solenoid 18 which commands the needle (19) of the injector, provided with a channel 20 of 1 mm in the middle, the needle also having four holes 21 at the top.
- the solenoid 18 raises and lets down the needle, which closes and opens at the same time the entrance of the mixture between compressed air and gasoline in the cylinder 28 of the engine.
- the mixture of compressed air and gasoline is injected in the cylinder 28 through a spout 29 when the needle opens with the help of the solenoid 18 (Fig. 7).
- the needle 19 of the injector has a conical shape at the top.
- the pipe 27 has a cone 30. The needle closes and opens at the same time the entrance of mixture between compressed air and gasoline in the cylinder of the engine.
- the pipe 3 for compressed air has a volume equal with 2* (Vc + VD) (Fig: 8).
- the diameter D A of the pipe for compressed air must be selected from Column 4 of the
- the solenoid 18 raises and lets down the needle 19 of the injector, when it is electricaly powered.
- the needle 19 of the injector has a conical shape 30 at the top.
- the conical angle 30 of the pipe 27 is the same as the conical top of the needle 18 of the injector.
- the quantity of fuel which will be absorbed by compressed air in the mass of the air, for a total combustion, will be calculated with
- - PI is the pressure of the compressed air (5 at 150 ATM or more) and it is selected.
- - P2 is the atmospheric pressure in the fuel pipe.
- crank offset, 40 s the pistons ' position.
- the solenoid liberates the needle.
- One spiral arc presses the needle down on the the cone of the pipe 27 which closes both compressed air and gasoline.
- the spiral arch spiral is supported by a security (safety) ring. Therefore, this high pressure along with diffusion achieves the mixture between compressed air and fuel in the cylinder of the engine. This is why the mixture is 200 times better homogenized than at the known engines.
- this high pressure at compressed air absorbs fuel through the holes of the needle and the mixture is injected through the spout in the cylinder, it creates a high turbulence, which is 200 times higher than at the known engines.
- a tap is fitted and then linked with a device at the accelerator of the vehicle.
- the tap is opened for a ⁇ ⁇ 0, 40 and this coresponds to a minimum rotation.
- the new engines which will use my invention do not need a catalyst for that they do not release oxides such as CO, HO, NO; these engines release only H 2 0 + C0 2 + N 2 +energy, through a total combustion of all types of hydrocarbons.
- oxides such as CO, HO, NO
- these engines release only H 2 0 + C0 2 + N 2 +energy, through a total combustion of all types of hydrocarbons.
- hydrogen the result of the combustion is only H 2 0 + energy.
- the water which is obtained can be recover and used in the battery, laboratories and in pharmacies.
- the injectors will be manufactured using the current technology.
- the injector can be manufactured .in big series, and in 10 years all new and old engines can be equipped with these injectors.
- This example refers to a reactor with a closed system without emissions released into the atmosphere, for producing steam or hot water in turbines, respective to produce usually hot water for apartments, villas or private homes and alse ⁇ 3 ⁇ 4y r ⁇ heating them.
- Fig 2 The results of the total combustion (Fig 2) are: 3 ⁇ 40 + C0 2 + N 2 + energy, and these are dissolved in water in the closed system.
- These reactors are used in closed system and will produce steam or hot water with temperature of 100° C or more, at a pressure of 200 ATM or more. The water is heated in direct contact with the flames of the fire created by the injector.
- These reactors can be used for total combustion in closed system at all types of hydrocarbons from Table 1, using an injector as presented Fig 2.
- the reactors are manufactured with double walls and the water from the closed system is also used for cooling down them.
- the reactor presented in Fig 9 is used to produce steam at the pressure of 200 ATM or hot water at pressure of 200 ATM for turbines.
- the reactor has a radius e.g. of 2 m and the double walls have the length of 7 m.
- the reactor will utilize an injector as in example 2 (Fig 2) which works at the pressure of 250 ATM in order to produce hot water or steam at pressure of 200 ATM.
- the reactor presented in Fig 10 also utilizes an injector as in example 2 (Fig 2) which works at the pressure of 15 ATM for heating apartments and institutions and for producing hot usual water.
- Fig 11 also utilizes an injector as in example 2 (Fig 2) which works at pressure of 5 ATM for heating and to producing hot usual water for villas or private homes.
- the injector will inject a flame with the pressure of 250 ATM inside the reactor. Over this flame, water is inject using a compressor with 210 ATM, through a sprayer. The water takes over the entire heating of the flame, and will turn the water into steam or hot water. Inside the reactor temperature and pressure grows because combustion is total and continue.
- the reactor contains a pipe which leads hot water or steam under pressure into the turbines. The pipe is fitted with a valve which is opened at a pressure of 200 ATM, thus the injector works with 50 ATM , and the compressor will pressed water at 10 ATM. In the turbine, water is conducted for cooling, and will reach the compressor and, so, the system is closed.
- the spiral pipe for heating the daily consumed water is located in the storage room.
- URSUT IOSIF CAMPEAN AURORA The reactors presented in Fig 9, 10 and 1 1 have the form of a cylinder with double walls 41 and 42. At the ends, two oval deadlightsl are mounted through welding. At the upper end there is a pipe for feeding with water, for closed system, through the space between the walls of the reactor and water water is the cooling agent. The pipe has a tap which is closed when the system is filled with water.
- the water fills the space between the walls 41 and 42.
- the pipe comes out from the reactor at the bottom part through a special pulverizer 43 with angle of 150 °, having a tap 44 that opens in case of a damage.
- the water at pressure of 210, 10 and 5 ATM, through a pulveriser 43 is pulverized over flames of the injector 45.
- the flames which burn inside the reactors 9, 10 and 11 have different pressures: 250, 15 and 7 ATM.
- the water pulverized over flames will take all the heat of at flames and will create a pressure in the storage room 46 that has a volume of approximate 25 m 3 .
- the evacuation valve 48 opens; this valve is fitted on the transport pipe 50 toward the turbine, apartments, villas or private homes.
- the pipe is fitted with a damage tap 49. This pipe, in case of reactor 9 transports water at 200 ATM to the turbine which will be put in function.
- the pipe 50 transport the water for heating the villas or private homes.
- the tap 56 on the water pipe 55 fills the closed system. Besides the double walls, the water pipe 55 also feeds the compressorclosing the system.
- the storage room 46 of the reactors 9, 10 and 11 a spiral pipe 47 with the diameter of 100 mm, 100 mm, and 10 mm for heating usual water.
- the water enters the compressor which will press the water up to 210, 10 and 5 ATM.
- the water flows in the spiral pipe 47 located in the feeding pipe 63 having an opened damage tap 64, and then goes to the pump 62 which presses the water through the spiral pipe 47 spiral and leads the water to the distribution pipe 61 toward the apartments, institution and villas; the water comes back through the return pipe into the pump 62.
- the evacuation valve 48 opens at 200, 7, or 3 ATM.
- the surplus of water will be taken out from the closed system in the reservoir 54 which is coupled at valve 53 mounted on the return pipe 52.
- the product from the reservoir 54 can be used to irrigated plants which through photosynthesis can produce oxygen 0 2 .
- the reactor 9 (Fig 9) has a cylindrical form and contains 16 injectors 45 grouped on two or more rows for a total combustion of hydrocarbons. The number of rows with injectors depends on the size of the flames.
- the evacuation valve 48 opens at the pressure of 200 ATM.
- the damage tap 49 on the supply pipe 50 opens and lesds the steam to turbine 51: The dimension of the supply pipe 50 is calculated on the basis of neccessary water or steam for the turbine.
- the reactor also contains the return pipe 52, a valve 53 connected to the reservoir with a capacity of 25 liters 54 that collects H2C03 +N2, a filling pipe 55 with the tap 56 which is opened.
- the reactor also contains a shower bath 43 with the angle of 150°, one compressor 57 for 210 ATM.
- the double walls 41 and 42 are fitted with the water pipe 55 having the tap 56 opened, which will fill the closed system of the reactor with water.
- the tap 56 will be closed after the system is filled with water.
- the reactor also consists of a storage room 46 which has 25 m 3 or more.
- the reactor from Fig 9 is used to produce steam under pressure of 200 ATM or hot water and must be calculated to resist at a pressure of 260 ATM.
- the reactor from Fig 10 is used for heating apartments and institution and to produce usual hot water; it must be calculated to resist at a pressure of 40 ATM. With my invention only one litre of fuel oil is needed for heating a quantity of 120 litres of water at 100° C (in direct contact with the flames). Consuming 720 litres of combustible crude oil in the reactor acoording to my invention (Fig 9, 10) under a total combustion, in 24 hours, the reactor can warm 86400 litres of water at 100°C. In addition, 2400 litres of H2C03+N2 are produced through a total combustion of crude oil.
- the reactor in Fig 11 is used for daily heat and hot water in villas and private homes and must be calculated to resist at a pressure of 10 ATM.
- the reactor consumes two litres of crude oil, e.g., in 24 hours and will heat up 240 litres of water in private homes.
- the dioxide of carbon C0 2 is a gas more difficult than air and when dissolved in water it results: H2CO3 + N 2 which is a natural fertilizer for plants and forests.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Dispersion Chemistry (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- General Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Feeding And Controlling Fuel (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2835482A CA2835482A1 (en) | 2011-05-09 | 2012-03-12 | Process for achieving total combustion with the help of injectors and injectors |
US14/116,661 US20140057216A1 (en) | 2011-05-09 | 2012-03-12 | Process for achieving total combustion with the help of injectors and injectors |
EP12735961.0A EP2707595A1 (en) | 2011-05-09 | 2012-03-12 | Process for achieving total combustion with the help of injectors and injectors |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ROA201100442 | 2011-05-09 | ||
ROA201100442A RO127544A0 (en) | 2011-05-09 | 2011-05-09 | Process for achieving total combustion by using injectors and injectors |
Publications (1)
Publication Number | Publication Date |
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WO2012154070A1 true WO2012154070A1 (en) | 2012-11-15 |
Family
ID=46319322
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/RO2012/000006 WO2012154070A1 (en) | 2011-05-09 | 2012-03-12 | Process for achieving total combustion with the help of injectors and injectors |
Country Status (5)
Country | Link |
---|---|
US (1) | US20140057216A1 (en) |
EP (1) | EP2707595A1 (en) |
CA (1) | CA2835482A1 (en) |
RO (1) | RO127544A0 (en) |
WO (1) | WO2012154070A1 (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
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CN104154539B (en) * | 2014-08-15 | 2016-06-15 | 四川旭虹光电科技有限公司 | A kind of oxygen-enriched burning device |
CN104338633B (en) * | 2014-11-04 | 2017-02-22 | 佛山市阳光陶瓷有限公司 | Energy-saving spray gun device for kiln |
CN104611066B (en) * | 2015-02-28 | 2017-06-30 | 中国神华能源股份有限公司 | Gasifier nozzle |
CN106050471B (en) * | 2016-06-13 | 2017-09-15 | 南京理工大学 | A kind of advance atomization igniter for Liquid fuel ramjet engine |
CN110939507B (en) * | 2019-12-12 | 2021-03-23 | 湖南姜姐生态农业科技发展有限公司 | Biogas power generation system |
CN112226585A (en) * | 2020-09-17 | 2021-01-15 | 孙红秀 | Steel rail welding seam heating device |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4057021A (en) * | 1975-06-20 | 1977-11-08 | Fritz Schoppe | Combustion of pulverized coal |
US4823756A (en) * | 1988-03-24 | 1989-04-25 | North Dakota State University Of Agriculture And Applied Science | Nozzle system for engines |
WO1989007898A1 (en) * | 1988-02-29 | 1989-09-08 | Braun Aktiengesellschaft | Gas-operated appliance for personal use |
US4895136A (en) * | 1988-09-02 | 1990-01-23 | Kemco Systems, Inc. | High-temperature heaters, methods and apparatus |
EP1605204A2 (en) * | 2004-06-09 | 2005-12-14 | Delavan Inc | Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
WO2009121384A1 (en) * | 2008-03-31 | 2009-10-08 | Campean, Romulus | Combustion process with full control over all of the purified fules that are submitted to high compressed air |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8308477B2 (en) * | 2006-03-01 | 2012-11-13 | Honeywell International Inc. | Industrial burner |
-
2011
- 2011-05-09 RO ROA201100442A patent/RO127544A0/en unknown
-
2012
- 2012-03-12 US US14/116,661 patent/US20140057216A1/en not_active Abandoned
- 2012-03-12 CA CA2835482A patent/CA2835482A1/en not_active Abandoned
- 2012-03-12 EP EP12735961.0A patent/EP2707595A1/en not_active Withdrawn
- 2012-03-12 WO PCT/RO2012/000006 patent/WO2012154070A1/en active Application Filing
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4057021A (en) * | 1975-06-20 | 1977-11-08 | Fritz Schoppe | Combustion of pulverized coal |
WO1989007898A1 (en) * | 1988-02-29 | 1989-09-08 | Braun Aktiengesellschaft | Gas-operated appliance for personal use |
US4823756A (en) * | 1988-03-24 | 1989-04-25 | North Dakota State University Of Agriculture And Applied Science | Nozzle system for engines |
US4895136A (en) * | 1988-09-02 | 1990-01-23 | Kemco Systems, Inc. | High-temperature heaters, methods and apparatus |
EP1605204A2 (en) * | 2004-06-09 | 2005-12-14 | Delavan Inc | Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
WO2009121384A1 (en) * | 2008-03-31 | 2009-10-08 | Campean, Romulus | Combustion process with full control over all of the purified fules that are submitted to high compressed air |
WO2009121473A2 (en) * | 2008-03-31 | 2009-10-08 | Iosif Ursut | New combustion process |
Also Published As
Publication number | Publication date |
---|---|
EP2707595A1 (en) | 2014-03-19 |
RO127544A0 (en) | 2012-06-29 |
CA2835482A1 (en) | 2012-11-15 |
US20140057216A1 (en) | 2014-02-27 |
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