WO2017222124A1 - Energy efficiency increasing apparatus for internal combustion engine for exhaust - Google Patents
Energy efficiency increasing apparatus for internal combustion engine for exhaust Download PDFInfo
- Publication number
- WO2017222124A1 WO2017222124A1 PCT/KR2016/014036 KR2016014036W WO2017222124A1 WO 2017222124 A1 WO2017222124 A1 WO 2017222124A1 KR 2016014036 W KR2016014036 W KR 2016014036W WO 2017222124 A1 WO2017222124 A1 WO 2017222124A1
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- WIPO (PCT)
- Prior art keywords
- hollow tube
- air
- amplifying
- wing
- exhaust
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
- F01N3/2892—Exhaust flow directors or the like, e.g. upstream of catalytic device
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
- F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
- F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
- F01N3/28—Construction of catalytic reactors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/08—Other arrangements or adaptations of exhaust conduits
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2240/00—Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being
- F01N2240/20—Combination or association of two or more different exhaust treating devices, or of at least one such device with an auxiliary device, not covered by indexing codes F01N2230/00 or F01N2250/00, one of the devices being a flow director or deflector
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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
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A50/00—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE in human health protection, e.g. against extreme weather
- Y02A50/20—Air quality improvement or preservation, e.g. vehicle emission control or emission reduction by using catalytic converters
Definitions
- the present invention relates to an apparatus for increasing energy efficiency of an internal combustion engine for exhaust gas. More specifically, the amplification wing and protrusion are increased together with the sequential wind speed increase in the hollow tube using the first and second rotary coupling protrusions spaced apart from each other. In addition to reducing the wind speed outside the hollow tube, it prevents air from passing through the inside and the outside of the hollow tube, and improves the wind speed through the induction of the air, thereby preventing backflow of the air as well as maintaining a constant exhaust velocity. It is possible to increase energy efficiency by maintaining the energy efficiency, and to reduce the emission of pollutants through rapid auxiliary combustion using wire mesh, and to reduce the generation of loads at high speeds as well as medium and low speeds. It relates to an energy efficiency increasing device of.
- Automobile engines use gasoline, diesel, and the like as main fuels by appropriately mixing fuel and air to flow into the cylinder of the engine and igniting the mixed air to obtain power.
- the vortex phenomenon may be better mixed gas on the intake manifold from the air purifier to the intake valve, but the cylinder pressure is reduced because the air is sucked by the reciprocating of the cylinder piston It is not possible to increase it further, and when the same amount of air passes through the vortex device, the cross-sectional area by the vortex device is reduced, so the flow rate in the area with the smaller cross-sectional area becomes faster, so the flow rate through the part becomes the same as the previous speed. Considering the friction energy of the device, the amount of air flowing into the cylinder cannot be increased.
- the fuel pedal system needs to deeply press the accelerator pedal to increase the supply of fuel. Therefore, when the explosion is not completely burned, a lot of combustion gas is emitted, which pollutes the atmosphere.
- a turbocharger which is an intake forced pressure method using a rotary blade rotational force by exhaust pressure, has been developed as an engine output improving device using forced suction force. It is used only at high speed or high speed.
- the electric motors installed in these air intake control devices have a rotational speed of less than 1,000 to 10,000 rpm, so the rotor blades (impellers) of the electric motor interfere with the engine suction input at the engine speed of 3,000 rpm or more.
- the vehicle loses the engine power such as pulling the car behind at 80 km / h.
- the method of directly injecting fuel into the cylinder has been developed to make the injection while forming a vortex inside the fuel injector only for some products, but the vortex angle and rotation range of the injected fuel is not wide to achieve the desired purpose.
- the vortex angle and rotation range of the injected fuel is not wide to achieve the desired purpose.
- the present inventor has proposed an "air amplification device" such as Patent Publication No. 10-1578833 in order to increase the output of the automobile engine and reduce the fuel.
- the above-described conventional air amplification device is connected to the intake pipe of the air cleaner to improve the passage speed of the air, the amplification groove formed in the entire area of the inner and outer circumference of the amplification pipe, that is, the amplification groove formed to the outlet of the amplification pipe.
- turbulence occurs in the exit direction by the amplification wing, and the velocity of the discharged air is lowered due to the reverse flow of the counter-air due to such turbulence.
- the amplification groove and the amplification wing are formed from the inlet of the amplification tube, there is a problem that a collision occurs in the process of splitting the supplied air at the inlet of the amplifying tube. In addition to the delay of the passage speed, the backflow phenomenon of the air caused by the turbulent flow was increased.
- the present applicant can not only make the flow of air discharged through the backflow prevention of the air constant, but also increase the energy efficiency of the internal combustion engine for exhaust gas that can reduce the emission of pollutants by making the exhaust gas completely burned. Led to develop.
- the present invention provides an energy efficiency increasing apparatus for an internal combustion engine for exhaust gas that can increase energy efficiency by maintaining a constant speed of exhaust air by preventing a backflow phenomenon due to turbulence.
- the present invention can not only reduce the collision of air generated when the air supplied through the first space formed between the hollow tube and the exhaust pipe is separated at the inlet of the hollow tube, but also the air rotated by the amplifying wing Due to the fact that forced rotation is suppressed in the course of passing through the second space, it is possible to prevent a collision phenomenon in which air passing through each of the inside and the outside of the hollow tube collides with each other, thereby preventing backflow of air, and slowly moving the outside of the hollow tube slowly. It is an object of the present invention to provide an energy efficiency increasing device of an internal combustion engine for exhaust gas, in which an air flow is smoothed and energy efficiency is increased by allowing the air passing through to be guided by the air passing quickly through the inside of the hollow tube.
- the present invention can achieve a secondary combustion of the exhaust gas not completely burned due to the heat generated by the wire mesh installed in close contact with the inner circumferential surface of the hollow tube to reduce the emission of pollutants such as fine dust or nitrogen compounds It is an object of the present invention to provide an energy efficiency increasing apparatus of an internal combustion engine for exhaust gas.
- the present invention can reduce the amount of air wound by the round formed in the amplification wing in the inlet direction of the hollow tube, and the amount of air drawn in the outlet direction of the hollow tube can be gradually increased. It is an object of the present invention to provide a device for increasing energy efficiency of an internal combustion engine for exhaust gas, which can increase the combustion efficiency by reducing load generation at high speeds as well as at low and medium speeds.
- the present invention for achieving the above object consists of a hollow tube, a plurality of first coupling holes penetrating in the inlet direction of the hollow tube, and a plurality of second coupling holes penetrating in the outlet direction of the hollow tube Amplification tube section;
- a wire mesh attached to the inner circumferential surface of the amplifying pipe part by sputtering so as to combust the exhaust gas passing through the inside of the hollow tube by heating with high temperature exhaust gas;
- a plurality of amplifying wings forming one space, and forming a second space between the exhaust pipe and the hollow tube and between the outlet of the hollow tube at an outlet side end of the amplifying wing;
- the first rotary coupling protrusion
- the second rotary coupling protrusion is formed in a spiral shape is integrally formed in the lower portion of the amplifying wing, corresponding to the second coupling hole formed in the exit direction of the hollow tube and protrudes into the hollow tube through the second coupling hole.
- the sequential wind speed increases in the hollow tube using the first and second rotary coupling protrusions spaced apart from each other, and the hollow tube outside using the amplification blades and the protrusions.
- the present invention can not only reduce the collision of air generated when the air supplied through the first space formed between the hollow tube and the exhaust pipe is separated at the inlet of the hollow tube, but also the air rotated by the amplifying wing Due to the fact that forced rotation is suppressed in the course of passing through the second space, it is possible to prevent a collision phenomenon in which air passing through each of the inside and the outside of the hollow tube collides with each other, thereby preventing backflow of air, and slowly moving the outside of the hollow tube slowly. Since the passing air is guided by the air passing through the inside of the hollow tube quickly, the air flows smoothly, which increases the energy efficiency.
- the present invention can achieve a secondary combustion of the exhaust gas not completely burned due to the heat generated by the wire mesh installed in close contact with the inner circumferential surface of the hollow tube to reduce the emission of pollutants such as fine dust or nitrogen compounds There is an advantage.
- the present invention can reduce the amount of air wound by the round formed in the amplification wing in the inlet direction of the hollow tube, and the amount of air drawn in the outlet direction of the hollow tube can be gradually increased. It is a useful invention that can increase the combustion efficiency by reducing the load generation at high speed as well as medium and low speed.
- FIG. 1 is a cross-sectional view showing a state in which an energy efficiency increasing apparatus of an exhaust internal combustion engine of the present invention is installed in an exhaust pipe.
- Figure 2 is an exploded perspective view showing the energy efficiency increasing apparatus of the internal combustion engine for exhaust of the present invention.
- Figure 3 is a perspective view showing an energy efficiency increasing apparatus of the internal combustion engine for exhaust of the present invention.
- the present invention relates to an energy efficiency increasing apparatus 100 of an internal combustion engine for exhaust gas which is installed in an exhaust pipe 1 of an automobile to increase energy efficiency, as shown in FIGS. 1 to 3.
- Amplifying pipe section comprising a plurality of first coupling holes 13 formed in the inlet direction of the hollow tube 11 and a plurality of second coupling holes 15 formed in the outlet direction of the hollow tube 11.
- the air passing through the exhaust pipe 1 through the lowering of the wind speed and strong rotation of the air between the exhaust pipe 1 and the hollow tube 11 using the amplification wing 30 It is possible to increase the combustion efficiency compared to the amount of air supplied by preventing the reverse flow of the, characterized in that it is possible to reduce the pollutants contained in the exhaust gas discharged through the combustion of the heated wire mesh 20.
- the internal combustion engine for exhaust of the present invention comprising an amplifying pipe part 10, a wire mesh 20, an amplifying wing 30, a first rotary coupling protrusion 40, and a second rotary coupling protrusion 50. It will be described in more detail with respect to the energy efficiency increasing apparatus 100.
- the amplifying tube part 10 is configured to amplify the speed or rotation of the air passing through, and constitutes a hollow tube 11 formed in a hollow shape so that the inlet and the outlet communicate with each other.
- the hollow tube 11 is configured to penetrate first and second coupling holes 13 and 15 for coupling the first and second rotary coupling protrusions 40 and 50 integrally formed with the amplifying wing 30.
- the first and second coupling holes 13 and 15 are formed in plural numbers so that a plurality of amplification wings 30 may be installed on the outer circumferential surface of the hollow tube 11.
- the first and second coupling holes 13 and 15 are formed to be spaced apart from each other so as to minimize rotation of air through the air passing through the inside of the hollow tube 11.
- a plurality of first coupling holes 13 are spaced at equal intervals in the inlet direction of the hollow tube 11, and the second coupling holes 15 are spaced at equal intervals in the outlet direction of the hollow tube 11. It is characterized by being formed.
- the wire mesh 20 is configured for the complete combustion of the exhaust gas contained in the air passing through the hollow tube 11 of the amplifying tube part 10 by being heated by a high temperature exhaust gas quickly, the conventional sputtering It is attached to the inner circumferential surface of the hollow tube 11 through close installation.
- the exhaust gas passing through the inside of the hollow tube 11 is completely combusted by the wire mesh 20 which is rapidly heated to 900 ⁇ 1200 °C, such as fine dust and nitrogen compounds, the present invention is installed Pollutants emitted from cars are reduced, making it environmentally friendly.
- the wire mesh 20 is manufactured in a cylindrical shape, but may be attached to the inner circumferential surface of the hollow tube 11 by sputtering by rolling round a plate shape instead of a cylinder. .
- the amplifying wing 30 is a conventional configuration that is spirally bonded to the outer circumference of the hollow tube 11 formed in the amplifying tube portion 10, in the present invention to mitigate the impact generated when the air is dispersed At the same time, it is characterized in that it is possible to block the formation of turbulence due to a collision in the process of the air passing through each of the inside, the outside of the hollow tube 11 meet each other.
- the amplification wing 30 is installed at the inlet and the outlet of the hollow tube 11, respectively, between the exhaust pipe (1) and the hollow tube (11) and at the inlet side end of the amplified wing (30) 11) a first space 31 is formed between the inlets, and a second space is formed between the exhaust pipe 1 and the hollow tube 11 and between the outlet of the hollow tube 11 at the outlet side end of the amplifying wing 30. (32) is formed.
- the generated shock is alleviated to facilitate separation of the air and at the same time
- a smooth flow of the air is continuously maintained, and the air discharged while being rotated through the amplification wing 30 through the exhaust pipe 1 and the hollow tube 11 is diffused and supplied to the second space 32.
- forced rotation is suppressed, collision of air passing through each inside and outside of the hollow tube 11 is prevented from colliding with each other, thereby preventing backflow of air due to turbulence.
- the air passing through the outside of the hollow tube 11 is freely diffused by the second space 32, the air moves in a smooth flow, so that the air passing through the inside of the hollow tube 11 quickly passes through the hollow tube 11.
- the action of inducing the outside air of the air flow through the present invention can be quickly exhausted to a certain state, thereby, the air flow is smoothly has the advantage that the energy efficiency is increased.
- the width of the first and second spaces (31, 32) formed by the amplification wing 30 is preferably formed in a ratio relative to the length of the amplification wing (30) in order to reduce shock and prevent the backflow of air.
- the first space 31 is formed in a direction parallel to the longitudinal direction of the medium width wings 30 in a width corresponding to 0.1 ⁇ 0.15 times the length of the hollow tube 11, the second space 32
- the hollow tube 11 is characterized in that it is formed in a direction parallel to the longitudinal direction of the amplification wing 30 in a width corresponding to 0.2 ⁇ 0.3 times the length.
- the reason why the first and second spaces 31 and 32 are formed at the same ratio is that the energy efficiency increase is maximized when the first and second spaces 31 and 32 are manufactured at the above ratio. to be. That is, when the first space 31 is not 0.1 to 0.15 times larger than the length of the hollow tube 11, it does not smoothly cushion the shock of the supplied air or sufficiently rotate the air by the amplification wing 30. When the second space 32 is not 0.2 to 0.3 times the length of the hollow tube 11, the free flow of air forcedly rotated by the amplifying wing 30 may not be smoothly performed. This is because backflow phenomenon occurs.
- the length ratio of the length of the first space 31 and the length of the second space 32 is more preferably formed in a ratio of 1: 2, which is an energy increase efficiency when manufactured by the above ratio as a result of its own experiment. Because this was the best.
- a round (R) is formed to wind and attract air, but the amount of air drawn through the amplifying wing (30) is attracted in the inlet direction, and the round (R) is inlet and outlet so that a lot occurs in the outlet direction. It is characterized in that it is formed in a direction opposite to each other in the direction.
- the round (R) formed in the opposite direction as described above is characterized in that the connection is formed integrally along the spiral shape of the amplification wing (30).
- the round R is formed in the opposite direction, so that the load is reduced by reducing the amount of air drawn through the amplifying vanes 30 and attracting the air.
- the round (R) is formed to be formed in the forward direction to increase the amount of air drawn through the amplification wing (30) to prevent backflow of the counterweight and to improve energy efficiency. As a result, even when the vehicle is driving at a high speed, the load on the amplified wing is minimized.
- the flow rate of the air passing between the exhaust pipe 1 and the hollow pipe 11 of the amplifying pipe part 10 is further slowed, and the rotational force of the air passing through is increased, thereby preventing the backflow of air. It is desirable to achieve efficiently, such a configuration is to form a resistance surface by forming a plurality of protrusions 60 on the outer circumferential surface of the hollow tube 11 and the outer surface of the amplification wing 30, that is, the surface. It can be achieved easily.
- the load is applied to the air passing between the exhaust pipe 1 and the hollow tube 11, so that the air drawn through the amplification wing 30
- the flow velocity is reduced, as well as the effect of increasing the rotational force of the air it is possible to more smoothly prevent the phenomenon of the air flow back.
- the first rotary coupling protrusion 40 is formed in a spiral shape to be integrally formed at the lower portion of the amplification wing 30, respectively, as described above the first coupling hole configured in the inlet direction of the hollow tube 11 ( 13 is formed to correspond to the inner side of the hollow tube by protruding into the hollow tube 11 through the first coupling hole 13.
- the air supplied into the hollow tube 11 is first rotated by the first rotary coupling protrusion 40 which is composed of a plurality of air, and the passage speed of the air by the centripetal force according to the rotation. Is slightly increased.
- the second rotary coupling protrusion 50 is formed in a spiral shape is integrally formed in the lower portion of the amplification wing 30, so as to be spaced apart from the first rotary coupling protrusion, in the exit direction of the hollow tube 11 It is formed to correspond to the configured second coupling hole 15 and protrudes to the inside of the hollow tube 11 through the second coupling hole 15 is disposed on the inner outlet side of the hollow tube (11).
- the secondary air is accelerated by the second rotary coupling protrusion 50 to the first rotated air supplied to the inside of the hollow tube 1, and the passage speed of air is increased by the centripetal force according to the rotational force. It is further increased.
- the protrusion heights of the first and second rotary coupling protrusions are different from each other in order to maximize the passage speed due to the rotation. Do.
- the first rotary coupling protrusion 40 located in the inlet direction of the hollow tube 11 is formed to protrude to a height corresponding to 0.2 times the height of the amplification wing 30 to the inlet of the hollow tube 11. It is configured to apply a first rotation without generating a large resistance to the supplied air, the second rotary coupling protrusion 50 located in the inner exit direction of the hollow tube 11 corresponds to 0.25 times the height of the amplified wing 30 It is formed to protrude to a height that is characterized in that to increase the speed of the air passing through the hollow tube 11 by walking the secondary rotation more than the first rotation to the air discharged to the outlet of the hollow tube 11 do.
- the air passing through the hollow tube 11 inside the amplification pipe part 10 may achieve complete combustion of the exhaust gas included in the air by the wire mesh 20 heated to 900 to 1200 ° C. Contaminants contained in the action is reduced.
- the air passing through the inside of the hollow tube 11 is the first rotary coupling protrusion 40 in the state that the first rotation is made without a large resistance through the first rotary coupling protrusion 40 protruding to a relatively low height.
- the hollow tube can be increased, and the air passing through the inside of the hollow tube 11 quickly attracts the air passing through the outside of the hollow tube 11 to improve the speed at which the air passes. Air passing through the (11) is safely controlled at a constant speed in an accelerated state has the advantage of improving the ride comfort of the vehicle.
- the reverse flow of the generated air can be achieved by blocking the air supplied by the strong rotation between the exhaust pipe (1) and the hollow tube (11), and thus, it is possible to keep the flow of air smoothly and energy efficiency It will be able to bring an increase.
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- Chemical Kinetics & Catalysis (AREA)
- Combustion & Propulsion (AREA)
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Abstract
The present invention relates to an energy efficiency increasing apparatus for an internal combustion engine for an exhaust which is installed in an exhaust pipe of a motor vehicle to increase energy efficiency. The apparatus comprises: a hollow tube; a plurality of first engagement holes formed to penetrate in an inlet direction of the hollow tube; an amplifying tube part; a wire mesh; an amplifying blade; a first rotational coupling protrusion; and a second rotational coupling protrusion. Accordingly, it is possible to provide an energy efficiency increasing apparatus, which can gradually increase an air velocity inside the hollow tube of the amplifying tube part using the first and second rotational coupling protrusions spaced apart from each other, can prevent a decrease in the air velocity between the exhaust tube and the hollow tube and the backflow of air passing through the exhaust tube through a strong rotation by using the amplifying blade, thereby increasing a combustion efficiency relative to the amount of supplied air, and reducing the pollutants contained in a discharged exhaust gas by means of the burning of a heated wire mesh.
Description
본 발명은 배기용 내연기관의 에너지 효율 증대장치에 관한 것으로, 보다 구체적으로는, 서로 이격배치된 제1, 2회전결합돌부를 이용한 중공관 내부에서의 순차적인 풍속 증가와 더불어 증폭날개 및 돌기를 이용한 중공관 외부에서의 풍속 저하를 이룸과 동시에, 중공관의 내외부를 통과하는 공기의 충돌현상을 방지시키고, 공기의 유도작용을 통해 풍속을 향상시킴으로써 공기의 역류를 방지함은 물론, 일정한 배기속도를 유지시켜 에너지 효율의 증대를 이룰 수 있으며, 와이어매쉬를 이용한 신속한 보조연소를 통해 공해물질의 배출을 저감할 수 있고, 중·저속 뿐만 아니라 고속주행시에도 부하 발생을 감소시킬 수 있는 배기용 내연기관의 에너지 효율 증대장치에 관한 것이다.The present invention relates to an apparatus for increasing energy efficiency of an internal combustion engine for exhaust gas. More specifically, the amplification wing and protrusion are increased together with the sequential wind speed increase in the hollow tube using the first and second rotary coupling protrusions spaced apart from each other. In addition to reducing the wind speed outside the hollow tube, it prevents air from passing through the inside and the outside of the hollow tube, and improves the wind speed through the induction of the air, thereby preventing backflow of the air as well as maintaining a constant exhaust velocity. It is possible to increase energy efficiency by maintaining the energy efficiency, and to reduce the emission of pollutants through rapid auxiliary combustion using wire mesh, and to reduce the generation of loads at high speeds as well as medium and low speeds. It relates to an energy efficiency increasing device of.
자동차 엔진은 연료와 공기를 적절히 혼합하여 엔진의 실린더 내부로 유입시키고, 유입된 혼합공기를 점화시켜서 동력을 얻는 것으로 가솔린이나 경유 등을 주 연료로 사용하고 있다.Automobile engines use gasoline, diesel, and the like as main fuels by appropriately mixing fuel and air to flow into the cylinder of the engine and igniting the mixed air to obtain power.
일반적으로 잘 알려진 바와 같이 자동차 엔진은 분사되는 연료가 가솔린이나 경유이든 간에 연료가 원활히 연소할 수 있도록 공기여과기에서 흡입된 공기를 필터로 정화한 후, 기화기나 분사기로 분사되는 연료와 자연 혼합하여 폭발시켜서 자동차가 움직일 수 있는 동력을 얻도록 하고 있다.As is well known, automobile engines explode by filtering the air sucked in the air filter with a filter so that the fuel can be burned smoothly, whether gasoline or diesel, and then naturally mixed with the fuel injected by the carburetor or injector. The car is getting power to move.
그러나 자동차 엔진의 출력은 엔진의 회전수와 배기량 및 실린더속의 혼합기체 압력에 비례하는 것이어서 배기량과 엔진의 회전수가 정해진 상태에서 출력을 향상시키기 위해서는 혼합기체의 압력을 높여야 하며, 혼합기체의 압력을 높이기 위해서 공기흡입도를 증가시켜야 하는 것이므로 이미 상용화되어서 널리 알려져 있는 기술 구성이다.However, the output of an automobile engine is proportional to the engine speed and displacement, and the pressure of the gas mixture in the cylinder. Therefore, the pressure of the gas mixture must be increased and the pressure of the gas mixture must be increased in order to improve the output in a fixed state. In order to increase the air intake in order to be commercially known technology configuration has already been commercialized.
그리고 기존의 개발된 엔진들은 연료의 원활한 연소를 위하여 연료와 공기의 완전한 혼합이 이루어지지 못하는 단점이 있었고, 아울러 엔진의 산소공급량이 부족하여 분사연료의 불완전 연소가 발생하고, 나아가서 엔진의 수명을 단축 시키거나 연료의 과소비와 매연이 다량 발생하여 대기를 오염시키는 등 여러 가지 문제점이 있었다.In addition, existing engines have a disadvantage in that complete mixing of fuel and air is not performed for smooth combustion of fuel, and incomplete combustion of injection fuel occurs due to insufficient oxygen supply of the engine, thereby shortening engine life. There are various problems such as polluting the air due to excessive consumption of fuel and soot.
그러므로 위와 같은 문제점을 해결하기 위하여 종래와 같은 엔진의 출력을 향상시키기 위한 장치로서, 흡입 및 배기메니홀드의 입구에 공기와류장치를 설치하여서 에어크리너에 복수개의 후렉시블한 안내판을 중앙부에서 외측의 방사상으로 형성한 엔진의 흡기 및 배기와류장치가 개발되어 있다.Therefore, in order to solve the above problems, as a device for improving the output of the engine as in the prior art, by installing an air vortex device at the inlet of the inlet and exhaust manifold, a plurality of flexible guide plates on the air cleaner from the center to the outside radially The intake and exhaust vortex devices of the formed engine have been developed.
그러나 위와 같은 구조는, 엔진의 흡기 및 배기의 와류장치에서 와류현상은 공기정화기에서 흡입밸브까지 흡기메니홀드 상에서 혼합가스가 더 잘 혼합될 수 있으나 실린더 피스톤의 왕복에 의하여 공기가 흡입되므로 실린더압력은 더 높일 수 없으며, 같은 량의 공기가 와류장치를 통과할 때 와류장치에 의한 단면적이 적어져 있으므로 단면적이 적어진 부분에서의 유속은 빨라지게 되므로 그 부분을 통과한 유속은 이전속도와 같게 되어서 와류장치의 마찰에너지를 감안하면 실린더 속으로 유입되는 공기량은 증가할 수 없는 것이다.However, in the above structure, in the vortex of the engine intake and exhaust, the vortex phenomenon may be better mixed gas on the intake manifold from the air purifier to the intake valve, but the cylinder pressure is reduced because the air is sucked by the reciprocating of the cylinder piston It is not possible to increase it further, and when the same amount of air passes through the vortex device, the cross-sectional area by the vortex device is reduced, so the flow rate in the area with the smaller cross-sectional area becomes faster, so the flow rate through the part becomes the same as the previous speed. Considering the friction energy of the device, the amount of air flowing into the cylinder cannot be increased.
그리고 또 다른 종래 기술의 일례로서, 엔진의 흡기에 있어서 엔진의 부압에 의하여 흡입되는 공기가 안내부재에 부딪쳐서 와류되게 하면 단위시간의 이송속도가 증가하면서 엔진의 실린더 내로 공기가 공급되어 연소효율을 향상시켜 엔진의 출력을 높이기 위한 과급장치들의 선행기술로 미국특허 제2,017,043호, 제3,877,907호, 제4,962,642호와, 일본 공개특허 공고번호 소58-13122호, 국내실용신안공보 공고번호 76-1369호, 국내공개실용신안 공개번호 제85-1789호, 국내 공개실용신안 공개번호 제85-5029호 등이 알려져 있다.As another example of the related art, when the air sucked by the negative pressure of the engine in the intake of the engine hits the guide member and vortexes, air is supplied into the cylinder of the engine to increase the combustion efficiency while increasing the feed rate in unit time. As a prior art of the superchargers to increase the output of the engine, US Patent Nos. 2,017,043, 3,877,907, 4,962,642, Japanese Patent Application Publication No. So 58-13122, Korean Utility Model Publication No. 76-1369, Korean Utility Model Publication No. 85-1789 and Domestic Utility Model Publication No. 85-5029 are known.
그러나 이러한 과급장치들은 엔진 시동 시 자연적으로 흡입되는 공기량 이외에는 대기의 공기를 더 많이 실린더 내로 강제 흡입하는 강제 흡입력이 없어서 엔진의 출력이 현저하게 증대되는 효과를 기대할 수 없었다.However, these superchargers do not have the forced suction force to forcibly draw more atmospheric air into the cylinder except for the amount of air naturally sucked at engine start-up, so the output of the engine could not be remarkably increased.
그리고 엔진에서는 차량의 출발 및 가속 시 큰 힘이 필요하기 때문에 연료공급을 많이 하기 위해서는 연료공급계통의 가속페달을 깊게 밟아 연료의 공급을 높이도록 하고 있으나, 그에 따라 연소공기가 비례적으로 충분히 공급되지 못하여서 폭발 시 완전연소되지 않은 상태로 연소가스가 많이 방출되므로 대기를 오염시키는 것이다.In addition, since the engine requires a large force when starting and accelerating the vehicle, in order to supply a lot of fuel, the fuel pedal system needs to deeply press the accelerator pedal to increase the supply of fuel. Therefore, when the explosion is not completely burned, a lot of combustion gas is emitted, which pollutes the atmosphere.
또한, 강제 흡입력을 이용한 엔진출력향상장치로서, 배기압에 의한 회전날개 회전력을 이용한 흡기 강제압력방식인 터보차저(Turbo-charger)가 개발되어 있으나 엔진의 회전이 중, 저속에서는 오히려 출력을 저하시키는 작용을 하므로 고속주행이나 고속회전시에만 사용하고 있는 것이다.In addition, a turbocharger, which is an intake forced pressure method using a rotary blade rotational force by exhaust pressure, has been developed as an engine output improving device using forced suction force. It is used only at high speed or high speed.
통상의 엔진이 1분당 3,000 ~ 6,000rpm으로 회전할 때 흡, 배기식 과급장치의 1분당 회전속도는 60,000 ~ 120,000rpm으로 동작하여 회전 관성에 의한 자연공기 강제압축으로 고속영역에서만 출력을 얻을 수 있었다.When the normal engine rotates at 3,000 to 6,000 rpm per minute, the rotational speed per minute of the intake / exhaust type supercharger operates at 60,000 to 120,000 rpm, and the output is obtained only in the high speed region by forced air compression by rotational inertia. .
그리고 전동모터를 이용한 자연공기 압축방식으로서, 일본 공개실용신안공보 소58-124656호와, 국내 특허공보등록특허 10-1578840, 공고번호 제94-3524호와, 제94-6055호 등의 내연기관용 공기흡입량조절장치가 개발되어 있으나 상기의 장치들은 공기여과기로 유입되는 관통구멍들 즉, 흡기계통을 모두 막아서 전동모터를 형성함으로써, 저속에서는 엔진출력향상에 기여한 바가 있으나 중, 고속에서는 오히려 엔진출력이 저하되는 등의 문제점이 있었다.And as a natural air compression method using an electric motor, for internal combustion engines such as Japanese Utility Model Publication No. 58-124656, Korean Patent Publication No. 10-1578840, Publication No. 94-3524, 94-6055 The air intake control device has been developed, but the above devices contribute to the improvement of engine output at low speed by forming the electric motor by blocking all the through-holes that enter the air filter, that is, the intake pipe. There was a problem such as deterioration.
그리고 이들 공기흡입량 조절장치에 설치된 전동모터는 분당회전수가 고작 1,000 ~ 10,000rpm 미만이므로 엔진의 분당회전수 3,000rpm 이상에서는 전동 모터의 회전날개(임페라)가 엔진흡입력을 방해하므로 오히려 중, 고속에서의 엔진출력이 원래상태보다 현저하게 떨어져 자동차의 경우 시속 80Km/h에서는 뒤에서 자동차를 당기는 것과 같은 엔진출력을 잃어버리는 경우가 발생한다.In addition, the electric motors installed in these air intake control devices have a rotational speed of less than 1,000 to 10,000 rpm, so the rotor blades (impellers) of the electric motor interfere with the engine suction input at the engine speed of 3,000 rpm or more. When the engine power is significantly lower than the original state, the vehicle loses the engine power such as pulling the car behind at 80 km / h.
또한, 연료를 실린더 내부로 직접 분사하는 방식은 일부 제품에 한해서 연료 인젝터 내부에서 와류를 형성하면서 분사되도록 하는 기술이 개발되어 있으나 분사되는 연료의 와류 각도와 회전범위가 넓지 못하여서 소기의 목적을 달성할 수 없었다.In addition, the method of directly injecting fuel into the cylinder has been developed to make the injection while forming a vortex inside the fuel injector only for some products, but the vortex angle and rotation range of the injected fuel is not wide to achieve the desired purpose. Could not.
한편, 본 발명자는 자동차 엔진의 출력 증진과 연료의 절감을 위하여 등록특허공보 제10-1578833호와 같은 "에어 증폭장치"를 제안한 바 있다.On the other hand, the present inventor has proposed an "air amplification device" such as Patent Publication No. 10-1578833 in order to increase the output of the automobile engine and reduce the fuel.
그러나, 전술한 종래의 에어 증폭장치는 에어클리너의 흡기관에 연결설치되어 공기의 통과 속도를 개선시키는 구성으로, 증폭관의 내, 외주 전체면적에 형성 즉, 증폭관의 출구까지 형성된 증폭홈 및 증폭날개에 의해 출구 방향에서 난류가 발생하는 문제가 있었으며, 이와 같은 난류에 의한 역기의 역류로 인해 토출되는 공기의 속도가 저하됨 물론, 진동 및 충격파가 크게 발생하여 효율이 떨어지는 문제점이 있었다.However, the above-described conventional air amplification device is connected to the intake pipe of the air cleaner to improve the passage speed of the air, the amplification groove formed in the entire area of the inner and outer circumference of the amplification pipe, that is, the amplification groove formed to the outlet of the amplification pipe There was a problem that turbulence occurs in the exit direction by the amplification wing, and the velocity of the discharged air is lowered due to the reverse flow of the counter-air due to such turbulence.
또한, 상기 증폭홈 및 증폭날개가 증폭관의 입구에서부터 형성되어 있기 때문에 공급되는 공기가 증폭관의 입구에서 분할되는 과정에서 충돌이 발생하는 문제가 있었으며, 이와 같은 충격으로 인해 충격파가 발생하여 공기의 통과속도 지연은 물론, 난류에 의한 공기의 역류 현상이 증대되는 원인이 되었다.In addition, since the amplification groove and the amplification wing are formed from the inlet of the amplification tube, there is a problem that a collision occurs in the process of splitting the supplied air at the inlet of the amplifying tube. In addition to the delay of the passage speed, the backflow phenomenon of the air caused by the turbulent flow was increased.
아울러, 완전연소되지 않은 배기가스를 처리하기 위한 구성이 구비되어 있지 아니하여 미세먼지나 질소화합물과 같은 공해물질의 배출을 저감시킬 수 없는 문제점도 있었다.In addition, there is a problem that can not reduce the emission of pollutants such as fine dust and nitrogen compounds because it is not provided with a configuration for treating the exhaust gas not completely burned.
그리하여, 본 출원인은 공기의 역류방지를 통해 배출되는 공기의 흐름을 일정하게 할 수 있을 뿐만 아니라, 배기가스의 완전연소를 이루어 공해물질의 배출을 저감시킬 수 있는 배기용 내연기관의 에너지 효율 증대장치를 개발하기에 이르렀다.Therefore, the present applicant can not only make the flow of air discharged through the backflow prevention of the air constant, but also increase the energy efficiency of the internal combustion engine for exhaust gas that can reduce the emission of pollutants by making the exhaust gas completely burned. Led to develop.
본 발명의 목적은 서로 이격배치된 제1, 2회전결합돌부를 이용한 중공관 내부에서의 순차적인 풍속 증가와 더불어, 증폭날개 및 돌기를 이용한 중공관 외부에서의 풍속 저하를 통해, 통과하는 공기의 난류에 의한 역류 현상을 방지시킴으로써 배기공기의 속도를 일정하게 유지하여 에너지 효율을 증대시킬 수 있는 배기용 내연기관의 에너지 효율 증대장치를 제공하는데 있다.It is an object of the present invention to sequentially increase the wind speed inside the hollow tube using the first and second rotary coupling protrusions spaced apart from each other, and to reduce the wind speed outside the hollow tube using the amplification wings and protrusions. The present invention provides an energy efficiency increasing apparatus for an internal combustion engine for exhaust gas that can increase energy efficiency by maintaining a constant speed of exhaust air by preventing a backflow phenomenon due to turbulence.
또한, 본 발명은 중공관과 배기관 사이에 형성되는 제1공간을 통해 공급되는 공기가 중공관의 입구에서 분리될 때에 발생하는 공기의 충돌을 완화시킬 수 있을 뿐만 아니라, 증폭날개에 의해 회전하는 공기가 제2공간을 거치는 과정에서 강제 회전이 억제되는 것으로 인해 중공관 내, 외부를 각각 통과하는 공기가 서로 부딪치는 충돌현상을 방지하여 공기의 역류 현상을 막을 수 있고, 상기 중공관의 외부를 천천히 통과하는 공기가 중공관의 내부를 빠르게 통과하는 공기에 의해 유도되는 작용이 이루어지도록 함으로써 공기의 흐름이 원활해져 에너지 효율이 증대되는 배기용 내연기관의 에너지 효율 증대장치를 제공하는데 목적이 있다.In addition, the present invention can not only reduce the collision of air generated when the air supplied through the first space formed between the hollow tube and the exhaust pipe is separated at the inlet of the hollow tube, but also the air rotated by the amplifying wing Due to the fact that forced rotation is suppressed in the course of passing through the second space, it is possible to prevent a collision phenomenon in which air passing through each of the inside and the outside of the hollow tube collides with each other, thereby preventing backflow of air, and slowly moving the outside of the hollow tube slowly. It is an object of the present invention to provide an energy efficiency increasing device of an internal combustion engine for exhaust gas, in which an air flow is smoothed and energy efficiency is increased by allowing the air passing through to be guided by the air passing quickly through the inside of the hollow tube.
아울러, 본 발명은 중공관의 내주면에 밀착설치되어 있는 와이어매쉬에 의한 발열로 인해 완전연소되지 않은 배기가스의 보조적인 연소를 빠르게 이룰 수 있어 미세먼지나 질소화합물과 같은 공해물질의 배출이 저감되는 배기용 내연기관의 에너지 효율 증대장치를 제공하는데 목적이 있다.In addition, the present invention can achieve a secondary combustion of the exhaust gas not completely burned due to the heat generated by the wire mesh installed in close contact with the inner circumferential surface of the hollow tube to reduce the emission of pollutants such as fine dust or nitrogen compounds It is an object of the present invention to provide an energy efficiency increasing apparatus of an internal combustion engine for exhaust gas.
더불어, 본 발명은 증폭날개에 형성된 라운드에 의해 중공관의 입구방향에서 감아서 유인되는 공기의 양을 적게 하고, 상기 중공관의 출구방향에서 감아서 유인되는 공기의 양은 점차적으로 많아지도록 할 수 있어 중·저속 뿐만 아니라 고속주행시에도 부하 발생을 감소시켜 연소효율의 증대를 이룰 수 있는 배기용 내연기관의 에너지 효율 증대장치를 제공하는데 목적이 있다.In addition, the present invention can reduce the amount of air wound by the round formed in the amplification wing in the inlet direction of the hollow tube, and the amount of air drawn in the outlet direction of the hollow tube can be gradually increased. It is an object of the present invention to provide a device for increasing energy efficiency of an internal combustion engine for exhaust gas, which can increase the combustion efficiency by reducing load generation at high speeds as well as at low and medium speeds.
상기와 같은 목적을 달성하기 위한 본 발명은 중공관과, 상기 중공관의 입구방향에 관통형성되는 복수 개의 제1결합홀과, 상기 중공관의 출구방향에 관통형성되는 복수 개의 제2결합홀로 구성된 증폭관부; 상기 증폭관부의 내주면에 밀착설치되도록 스퍼터링으로 부착되어 중공관의 내부를 통과하는 배기가스를 고온의 배기가스에 의한 가열로 연소시키는 와이어매쉬; 상기 증폭관부에 구성된 중공관의 외주에 나선형상으로 접합되되, 상기 중공관의 입구와 출구에서 각각 이격설치되어, 상기 배기관과 중공관 사이 및 증폭날개의 입구측 단부에서 중공관의 입구 사이에 제1공간을 형성시키고, 상기 배기관과 중공관 사이 및 증폭날개의 출구측 단부에서 중공관의 출구 사이에는 제2공간을 형성시키는 복수 개의 증폭날개; 나선형상으로 형성되어 증폭날개의 하부에 일체로 구성되되, 중공관의 입구방향에 구성된 제1결합홀에 대응되게 형성되어 상기 제1결합홀을 통해 중공관의 내측으로 돌출되는 제1회전결합돌부; 나선형상으로 형성되어 증폭날개의 하부에 일체로 구성되되, 중공관의 출구방향에 구성된 제2결합홀에 대응되게 형성되어 상기 제2결합홀을 통해 중공관의 내측으로 돌출되는 제2회전결합돌부;로 이루어져, 서로 이격배치된 제1, 2회전결합돌부를 이용한 중폭관부의 중공관 내부에서의 공기의 순차적인 풍속 증가와 더불어, 증폭날개를 이용한 배기관과 중공관 사이에서의 공기의 풍속 저하 및 강한 회전을 통해 배기관을 통과하는 공기의 역류를 방지하여 공급된 공기량 대비 연소효율을 증대시킬 수 있고, 배출되는 배기가스에 포함된 공해물질을 가열된 와이어매쉬의 연소를 통해 저감시킬 수 있는 것을 특징으로 하는 배기용 내연기관의 에너지 효율 증대장치를 제공한다.The present invention for achieving the above object consists of a hollow tube, a plurality of first coupling holes penetrating in the inlet direction of the hollow tube, and a plurality of second coupling holes penetrating in the outlet direction of the hollow tube Amplification tube section; A wire mesh attached to the inner circumferential surface of the amplifying pipe part by sputtering so as to combust the exhaust gas passing through the inside of the hollow tube by heating with high temperature exhaust gas; Spirally bonded to the outer periphery of the hollow tube configured in the amplification pipe portion, and are respectively spaced apart from the inlet and outlet of the hollow tube, between the exhaust pipe and the hollow tube and between the inlet of the hollow tube at the inlet side end of the amplification wing A plurality of amplifying wings forming one space, and forming a second space between the exhaust pipe and the hollow tube and between the outlet of the hollow tube at an outlet side end of the amplifying wing; The first rotary coupling protrusion is formed in a spiral shape is integrally formed on the lower portion of the amplification wing, and is formed to correspond to the first coupling hole formed in the inlet direction of the hollow tube and protrudes into the hollow tube through the first coupling hole. ; The second rotary coupling protrusion is formed in a spiral shape is integrally formed in the lower portion of the amplifying wing, corresponding to the second coupling hole formed in the exit direction of the hollow tube and protrudes into the hollow tube through the second coupling hole. And sequential wind speed increase of the air inside the hollow tube of the medium width pipe portion using the first and second rotary coupling protrusions spaced apart from each other, and decrease of the wind speed of the air between the exhaust pipe and the hollow tube using the amplifying wing and It is possible to increase the combustion efficiency compared to the amount of air supplied by preventing the reverse flow of air through the exhaust pipe through the strong rotation, and to reduce the pollutants contained in the exhaust gas by burning the heated wire mesh. Provided is an energy efficiency increasing apparatus for an internal combustion engine for exhaust gas.
본 발명의 배기용 내연기관의 에너지 효율 증대장치를 이용하면, 서로 이격배치된 제1, 2회전결합돌부를 이용한 중공관 내부에서의 순차적인 풍속 증가와 더불어, 증폭날개 및 돌기를 이용한 중공관 외부에서의 풍속 저하를 통해, 통과하는 공기의 난류에 의한 역류 현상을 방지시킬 수 있으므로 배기공기의 일정속도가 유지되어 에너지 효율이 증대되는 장점이 있다.When the energy efficiency increasing apparatus of the internal combustion engine for exhaust gas of the present invention is used, the sequential wind speed increases in the hollow tube using the first and second rotary coupling protrusions spaced apart from each other, and the hollow tube outside using the amplification blades and the protrusions. By lowering the wind speed at, it is possible to prevent the reverse flow due to turbulent flow of air passing through it has the advantage that the constant speed of the exhaust air is maintained to increase the energy efficiency.
또한, 본 발명은 중공관과 배기관 사이에 형성되는 제1공간을 통해 공급되는 공기가 중공관의 입구에서 분리될 때에 발생하는 공기의 충돌을 완화시킬 수 있을 뿐만 아니라, 증폭날개에 의해 회전하는 공기가 제2공간을 거치는 과정에서 강제 회전이 억제되는 것으로 인해 중공관 내, 외부를 각각 통과하는 공기가 서로 부딪치는 충돌현상을 방지하여 공기의 역류 현상을 막을 수 있고, 상기 중공관의 외부를 천천히 통과하는 공기가 중공관의 내부를 빠르게 통과하는 공기에 의해 유도되는 작용이 이루어지므로 공기의 흐름이 원활해져 에너지 효율이 증대되는 장점이 있다.In addition, the present invention can not only reduce the collision of air generated when the air supplied through the first space formed between the hollow tube and the exhaust pipe is separated at the inlet of the hollow tube, but also the air rotated by the amplifying wing Due to the fact that forced rotation is suppressed in the course of passing through the second space, it is possible to prevent a collision phenomenon in which air passing through each of the inside and the outside of the hollow tube collides with each other, thereby preventing backflow of air, and slowly moving the outside of the hollow tube slowly. Since the passing air is guided by the air passing through the inside of the hollow tube quickly, the air flows smoothly, which increases the energy efficiency.
아울러, 본 발명은 중공관의 내주면에 밀착설치되어 있는 와이어매쉬에 의한 발열로 인해 완전연소되지 않은 배기가스의 보조적인 연소를 빠르게 이룰 수 있어 미세먼지나 질소화합물과 같은 공해물질의 배출이 저감되는 장점이 있다.In addition, the present invention can achieve a secondary combustion of the exhaust gas not completely burned due to the heat generated by the wire mesh installed in close contact with the inner circumferential surface of the hollow tube to reduce the emission of pollutants such as fine dust or nitrogen compounds There is an advantage.
더불어, 본 발명은 증폭날개에 형성된 라운드에 의해 중공관의 입구방향에서 감아서 유인되는 공기의 양을 적게 하고, 상기 중공관의 출구방향에서 감아서 유인되는 공기의 양은 점차적으로 많아지도록 할 수 있어 중·저속 뿐만 아니라 고속주행시에도 부하 발생을 감소시켜 연소효율의 증대를 이룰 수 있는 유용한 발명이다.In addition, the present invention can reduce the amount of air wound by the round formed in the amplification wing in the inlet direction of the hollow tube, and the amount of air drawn in the outlet direction of the hollow tube can be gradually increased. It is a useful invention that can increase the combustion efficiency by reducing the load generation at high speed as well as medium and low speed.
도 1은 본 발명의 배기용 내연기관의 에너지 효율 증대장치가 배기관에 설치된 상태를 도시한 단면도.1 is a cross-sectional view showing a state in which an energy efficiency increasing apparatus of an exhaust internal combustion engine of the present invention is installed in an exhaust pipe.
도 2는 본 발명의 배기용 내연기관의 에너지 효율 증대장치를 분해하여 도시한 사시도.Figure 2 is an exploded perspective view showing the energy efficiency increasing apparatus of the internal combustion engine for exhaust of the present invention.
도 3은 본 발명의 배기용 내연기관의 에너지 효율 증대장치를 도시한 사시도.Figure 3 is a perspective view showing an energy efficiency increasing apparatus of the internal combustion engine for exhaust of the present invention.
* 부호의 설명 ** Explanation of Codes *
1 : 배기관1: exhaust pipe
10 : 증폭관부 11 : 중공관 13, 15 : 제1, 2결합홀10: amplification tube portion 11: hollow tube 13, 15: the first and second coupling holes
20 : 와이어매쉬20: wire mesh
30 : 증폭날개 31, 32 : 제1, 2공간 R : 라운드30: amplification wing 31, 32: 1st, 2nd space R: round
40, 50 : 제1, 2회전결합돌부 60 : 돌기40, 50: the first and second rotation coupling protrusion 60: protrusion
100 : 배기용 내연기관의 에너지 효율 증대장치100: device for increasing energy efficiency of exhaust internal combustion engine
상기와 같은 문제점을 해결하기 위한 본 발명의 구성을 살펴보면 다음과 같다.Looking at the configuration of the present invention for solving the above problems are as follows.
본 발명은 도 1 내지 도 3에 도시된 바와 같이 자동차의 배기관(1)에 설치되어 에너지 효율을 증대시키는 배기용 내연기관의 에너지 효율 증대장치(100)에 관한 것으로, 중공관(11)과, 상기 중공관(11)의 입구방향에 관통형성되는 복수 개의 제1결합홀(13)과, 상기 중공관(11)의 출구방향에 관통형성되는 복수 개의 제2결합홀(15)로 구성된 증폭관부(10); 상기 증폭관부(10)의 내주면에 밀착설치되도록 스퍼터링으로 부착되어 중공관(11)의 내부를 통과하는 배기가스를 고온의 배기가스에 의한 가열로 연소시키는 와이어매쉬(20); 상기 증폭관부(10)에 구성된 중공관(11)의 외주에 나선형상으로 접합되되, 상기 중공관(11)의 입구와 출구에서 각각 이격설치되어, 상기 배기관(1)과 중공관(11) 사이 및 증폭날개(30)의 입구측 단부에서 중공관(11)의 입구 사이에 제1공간(31)을 형성시키고, 상기 배기관(1)과 중공관(11) 사이 및 증폭날개(30)의 출구측 단부에서 중공관(11)의 출구 사이에는 제2공간(32)을 형성시키는 복수 개의 증폭날개(30); 나선형상으로 형성되어 증폭날개(30)의 하부에 일체로 구성되되, 중공관(11)의 입구방향에 구성된 제1결합홀(13)에 대응되게 형성되어 상기 제1결합홀(13)을 통해 중공관(11)의 내측으로 돌출되는 제1회전결합돌부(40); 나선형상으로 형성되어 증폭날개(30)의 하부에 일체로 구성되되, 중공관(11)의 출구방향에 구성된 제2결합홀(15)에 대응되게 형성되어 상기 제2결합홀(15)을 통해 중공관(11)의 내측으로 돌출되는 제2회전결합돌부(50);로 이루어져, 서로 이격배치된 제1, 2회전결합돌부(40, 50)를 이용한 중폭관부(10)의 중공관(11) 내부에서의 공기의 순차적인 풍속 증가와 더불어, 증폭날개(30)를 이용한 배기관(1)과 중공관(11) 사이에서의 공기의 풍속 저하 및 강한 회전을 통해 배기관(1)을 통과하는 공기의 역류를 방지하여 공급된 공기량 대비 연소효율을 증대시킬 수 있고, 배출되는 배기가스에 포함된 공해물질을 가열된 와이어매쉬(20)의 연소를 통해 저감시킬 수 있는 것을 특징으로 한다.The present invention relates to an energy efficiency increasing apparatus 100 of an internal combustion engine for exhaust gas which is installed in an exhaust pipe 1 of an automobile to increase energy efficiency, as shown in FIGS. 1 to 3. Amplifying pipe section comprising a plurality of first coupling holes 13 formed in the inlet direction of the hollow tube 11 and a plurality of second coupling holes 15 formed in the outlet direction of the hollow tube 11. 10; A wire mesh (20) attached to the inner circumferential surface of the amplifying pipe part (10) by sputtering to combust the exhaust gas passing through the inside of the hollow tube (11) by heating with high temperature exhaust gas; Spirally bonded to the outer periphery of the hollow tube 11 formed in the amplifying pipe part 10, and are respectively installed at the inlet and outlet of the hollow tube 11, between the exhaust pipe (1) and the hollow tube (11) And a first space 31 is formed between the inlet of the hollow tube 11 at the inlet side end of the amplifying wing 30, between the exhaust pipe 1 and the hollow tube 11 and the outlet of the amplifying wing 30. A plurality of amplifying vanes 30 forming a second space 32 between the outlets of the hollow tubes 11 at the side ends; Is formed in a spiral shape is integrally formed in the lower portion of the amplification wing 30, formed corresponding to the first coupling hole 13 formed in the inlet direction of the hollow tube 11 through the first coupling hole (13) A first rotary coupling protrusion 40 protruding inward of the hollow tube 11; Is formed in a spiral shape is integrally formed in the lower portion of the amplification wing 30, formed corresponding to the second coupling hole 15 formed in the outlet direction of the hollow tube 11 through the second coupling hole (15) A second rotary coupling protrusion 50 protruding inwardly of the hollow tube 11; consisting of the first and second rotary coupling protrusions 40 and 50 spaced apart from each other using the hollow tube 11 of the medium width pipe portion 10. In addition to the sequential increase of air velocity inside the air, the air passing through the exhaust pipe 1 through the lowering of the wind speed and strong rotation of the air between the exhaust pipe 1 and the hollow tube 11 using the amplification wing 30. It is possible to increase the combustion efficiency compared to the amount of air supplied by preventing the reverse flow of the, characterized in that it is possible to reduce the pollutants contained in the exhaust gas discharged through the combustion of the heated wire mesh 20.
이하에서는 증폭관부(10)와, 와이어매쉬(20)와, 증폭날개(30)와, 제1회전결합돌부(40)와, 제2회전결합돌부(50)로 이루어진 본 발명의 배기용 내연기관의 에너지 효율 증대장치(100)에 대해 보다 상세히 설명한다.Hereinafter, the internal combustion engine for exhaust of the present invention comprising an amplifying pipe part 10, a wire mesh 20, an amplifying wing 30, a first rotary coupling protrusion 40, and a second rotary coupling protrusion 50. It will be described in more detail with respect to the energy efficiency increasing apparatus 100.
첫째, 증폭관부(10)는 통과되는 공기의 속도 또는 회전을 증폭시키기 위한 구성으로, 입구와 출구가 연통되도록 중공형상으로 형성되는 중공관(11)을 구성한다.First, the amplifying tube part 10 is configured to amplify the speed or rotation of the air passing through, and constitutes a hollow tube 11 formed in a hollow shape so that the inlet and the outlet communicate with each other.
아울러, 상기 중공관(11)에는 증폭날개(30)에 일체로 구성되는 제1, 2회전결합돌부(40, 50)를 결합하기 위한 제1, 2결합홀(13, 15)이 관통 구성되는데, 상기 제1, 2결합홀(13, 15)은 중공관(11)의 외주면에 증폭날개(30)를 복수 개로 설치할 수 있도록 각각 복수 개로 관통 형성된다.In addition, the hollow tube 11 is configured to penetrate first and second coupling holes 13 and 15 for coupling the first and second rotary coupling protrusions 40 and 50 integrally formed with the amplifying wing 30. In addition, the first and second coupling holes 13 and 15 are formed in plural numbers so that a plurality of amplification wings 30 may be installed on the outer circumferential surface of the hollow tube 11.
그리고, 상기 제1, 2결합홀(13, 15)은 중공관(11)의 내부를 통과하는 공기에 순차적으로 회전을 주어 부하가 생기는 것이 최소화될 수 있도록 서로 이격되어 형성되는데, 이를 위하여, 상기 제1결합홀(13)은 중공관(11)의 입구방향에 등 간격으로 이격되어 복수 형성되고, 상기 제2결합홀(15)은 중공관(11)의 출구방향에 등 간격으로 이격되어 복수 형성되는 것을 특징으로 한다.The first and second coupling holes 13 and 15 are formed to be spaced apart from each other so as to minimize rotation of air through the air passing through the inside of the hollow tube 11. A plurality of first coupling holes 13 are spaced at equal intervals in the inlet direction of the hollow tube 11, and the second coupling holes 15 are spaced at equal intervals in the outlet direction of the hollow tube 11. It is characterized by being formed.
둘째, 와이어매쉬(20)는 고온의 배기가스에 의해 빠르게 가열됨으로써 상기 증폭관부(10)의 중공관(11)을 통과하는 공기에 포함된 배기가스의 완전연소를 위한 구성으로, 통상의 스퍼터링을 통해 중공관(11)의 내주면에 부착되어 밀착설치된다.Second, the wire mesh 20 is configured for the complete combustion of the exhaust gas contained in the air passing through the hollow tube 11 of the amplifying tube part 10 by being heated by a high temperature exhaust gas quickly, the conventional sputtering It is attached to the inner circumferential surface of the hollow tube 11 through close installation.
따라서, 중공관(11)의 내부를 통과하는 배기가스는 900 ~ 1200℃까지 신속하게 가열되는 와이어매쉬(20)에 의해 미세먼지 및 질소화합물과 같은 공해물질이 완전히 연소되어 지므로, 본 발명이 설치된 자동차에서 배출되는 공해물질이 저감되어 친환경적으로 사용할 수 있게 된다.Therefore, the exhaust gas passing through the inside of the hollow tube 11 is completely combusted by the wire mesh 20 which is rapidly heated to 900 ~ 1200 ℃, such as fine dust and nitrogen compounds, the present invention is installed Pollutants emitted from cars are reduced, making it environmentally friendly.
그리고, 첨부한 도면에서는 상기 와이어매쉬(20)가 원통형상으로 제작되는 구성으로 도시하였으나, 원통이 아닌 판 형상으로 제작한 후, 둥글게 말아서 스퍼터링하여 중공관(11)의 내주면에 부착시킬 수도 있을 것이다.In the accompanying drawings, the wire mesh 20 is manufactured in a cylindrical shape, but may be attached to the inner circumferential surface of the hollow tube 11 by sputtering by rolling round a plate shape instead of a cylinder. .
셋째, 증폭날개(30)는 상기 증폭관부(10)에 구성된 중공관(11)의 외주에 나선형상으로 접합되는 통상의 구성으로, 본 발명에서는 공기가 분산될 때에 발생될 때에 발생하는 충격을 완화시킬 수 있음과 동시에, 중공관(11)의 내, 외부를 각각 통과하는 공기가 서로 만나는 과정에서 충돌에 의한 난류가 형성되는 것을 차단할 수 있도록 하는 것을 특징으로 한다.Third, the amplifying wing 30 is a conventional configuration that is spirally bonded to the outer circumference of the hollow tube 11 formed in the amplifying tube portion 10, in the present invention to mitigate the impact generated when the air is dispersed At the same time, it is characterized in that it is possible to block the formation of turbulence due to a collision in the process of the air passing through each of the inside, the outside of the hollow tube 11 meet each other.
따라서, 상기 증폭날개(30)는 중공관(11)의 입구와 출구에서 각각 이격설치되어, 상기 배기관(1)과 중공관(11) 사이 및 증폭날개(30)의 입구측 단부에서 중공관(11) 입구 사이에 제1공간(31)을 형성시키고, 상기 배기관(1)과 중공관(11) 사이 및 증폭날개(30)의 출구측 단부에서 중공관(11)의 출구 사이에는 제2공간(32)을 형성시킨다.Therefore, the amplification wing 30 is installed at the inlet and the outlet of the hollow tube 11, respectively, between the exhaust pipe (1) and the hollow tube (11) and at the inlet side end of the amplified wing (30) 11) a first space 31 is formed between the inlets, and a second space is formed between the exhaust pipe 1 and the hollow tube 11 and between the outlet of the hollow tube 11 at the outlet side end of the amplifying wing 30. (32) is formed.
이에 따르면, 중공관(11)으로 공급되는 공기가 제1공간(31)으로 확산 수용된 후, 증폭날개(30)를 통해 회전되므로, 발생하는 충격이 완화되어 공기의 용이한 분리가 이루어짐과 동시에 공기의 원활할 흐름이 지속적으로 유지되고, 상기 배기관(1)과 중공관(11) 사이를 통과하여 증폭날개(30)를 통해 회전되는 상태로 배출되는 공기가 제2공간(32)으로 확산 공급되는 것에 의해 강제회전이 억제되므로 상기 중공관(11)의 내, 외부에서 각각 회전하는 상태로 통과되는 공기가 서로 부딪치는 충돌현상이 방지되어 난류에 의한 공기의 역류가 발생하지 않게 된다 According to this, since the air supplied to the hollow tube 11 is diffused and accommodated in the first space 31, and then rotated through the amplification wing 30, the generated shock is alleviated to facilitate separation of the air and at the same time A smooth flow of the air is continuously maintained, and the air discharged while being rotated through the amplification wing 30 through the exhaust pipe 1 and the hollow tube 11 is diffused and supplied to the second space 32. As a result, forced rotation is suppressed, collision of air passing through each inside and outside of the hollow tube 11 is prevented from colliding with each other, thereby preventing backflow of air due to turbulence.
또한, 중공관(11)의 외부을 통과하는 공기가 제2공간(32)에 의해 자유롭게 확산되는 것에 의해 부드러운 흐름으로 이동되므로, 중공관(11)의 내부를 빠르게 통과하는 공기가 중공관(11)의 외부공기를 유도하는 작용이 이루어져 본 발명을 통과하는 공기의 흐름을 일정한 상태로 신속하게 배기시킬 수 있으며, 이로 인해, 공기의 흐름이 원활해져 에너지 효율이 증대되는 장점을 가진다.In addition, since the air passing through the outside of the hollow tube 11 is freely diffused by the second space 32, the air moves in a smooth flow, so that the air passing through the inside of the hollow tube 11 quickly passes through the hollow tube 11. The action of inducing the outside air of the air flow through the present invention can be quickly exhausted to a certain state, thereby, the air flow is smoothly has the advantage that the energy efficiency is increased.
한편, 상기 증폭날개(30)에 의해 형성되는 제1, 2공간(31, 32)의 폭은 충격완화와 더불어 공기의 역류방지를 위하여 증폭날개(30)의 길이 대비 일정 비율로 형성되는 것이 바람직한데, 본 발명에서는 상기 제1공간(31)이 중공관(11) 길이의 0.1 ~ 0.15배에 해당되는 폭으로 중폭날개(30)의 길이방향과 나란한 방향으로 형성되고, 제2공간(32)은 중공관(11) 길이의 0.2 ~ 0.3배에 해당되는 폭으로 증폭날개(30)의 길이방향과 나란한 방향으로 형성되는 것을 특징으로 한다.On the other hand, the width of the first and second spaces (31, 32) formed by the amplification wing 30 is preferably formed in a ratio relative to the length of the amplification wing (30) in order to reduce shock and prevent the backflow of air. However, in the present invention, the first space 31 is formed in a direction parallel to the longitudinal direction of the medium width wings 30 in a width corresponding to 0.1 ~ 0.15 times the length of the hollow tube 11, the second space 32 The hollow tube 11 is characterized in that it is formed in a direction parallel to the longitudinal direction of the amplification wing 30 in a width corresponding to 0.2 ~ 0.3 times the length.
여기서, 상기 제1, 2공간(31, 32)이 상기와 같은 비율로 형성되는 이유는 상기 제1, 2공간(31, 32)이 위 비율로 제작되었을 때에 에너지 효율 증대가 최대치로 이루어지기 때문이다. 즉, 중공관(11)의 길이 대비 제1공간(31)이 0.1 ~ 0.15배로 형성되지 않았을 때에는 공급되는 공기의 충격 완충을 원활하게 시키지 못하거나 증폭날개(30)에 의한 공기의 회전을 충분히 이루지 못하는 문제점이 있었고, 중공관(11)의 길이 대비 제2공간(32)이 0.2 ~ 0.3배로 형성되지 않았을 때에는 증폭날개(30)에 의해 강제회전되는 공기의 자유 흐름이 원활하게 이루어지지 못하여 난류에 의한 역류현상이 발생하기 때문이다.The reason why the first and second spaces 31 and 32 are formed at the same ratio is that the energy efficiency increase is maximized when the first and second spaces 31 and 32 are manufactured at the above ratio. to be. That is, when the first space 31 is not 0.1 to 0.15 times larger than the length of the hollow tube 11, it does not smoothly cushion the shock of the supplied air or sufficiently rotate the air by the amplification wing 30. When the second space 32 is not 0.2 to 0.3 times the length of the hollow tube 11, the free flow of air forcedly rotated by the amplifying wing 30 may not be smoothly performed. This is because backflow phenomenon occurs.
그리고, 상기 제1공간(31)의 길이와 제2공간(32)의 길이 비율은 1 : 2의 비율로 형성되는 것이 더욱 바람직하는데, 이는, 자체 실험결과, 위 비율로 제작되었을 때에 에너지 증대 효율이 가장 우수하였기 때문이다.In addition, the length ratio of the length of the first space 31 and the length of the second space 32 is more preferably formed in a ratio of 1: 2, which is an energy increase efficiency when manufactured by the above ratio as a result of its own experiment. Because this was the best.
또한, 본 발명에서는 자동차의 중·저속 주행뿐만 아니라, 고속주행시에도 증폭날개(30)를 통과하는 공기로 인한 부하발생이 크게 생기지 않도록 하는 것이 바람직한데, 이와 같은 구성은 상기 증폭날개(30)에 공기를 감아서 유인하기 위한 라운드(R)를 형성시키되, 증폭날개(30)를 통해 감아서 유인되는 공기의 양이 입구방향에서는 적고, 출구방향에서는 많이 발생하도록 상기 라운드(R)가 입구와 출구방향에서 서로 반대방향으로 형성되는 것을 특징으로 한다.In addition, in the present invention, it is preferable not to generate a load due to air passing through the amplifying vanes 30 even at high speeds as well as at low and medium speeds of automobiles. Such a configuration is applied to the amplifying vanes 30. A round (R) is formed to wind and attract air, but the amount of air drawn through the amplifying wing (30) is attracted in the inlet direction, and the round (R) is inlet and outlet so that a lot occurs in the outlet direction. It is characterized in that it is formed in a direction opposite to each other in the direction.
아울러, 상기와 같이 서로 반대방향으로 형성되는 라운드(R)는 상기 증폭날개(30)의 나선형상을 따라 일체로 연결형성되는 것을 특징으로 한다.In addition, the round (R) formed in the opposite direction as described above is characterized in that the connection is formed integrally along the spiral shape of the amplification wing (30).
즉, 공기가 유입되는 중공관(11)의 입구 측에서는 라운드(R)가 반대방향으로 형성되도록 함으로써 증폭날개(30)를 통해 감아서 유인되는 공기의 양을 적게 하여 부하가 적게 걸리도록 하고, 공기가 배출되는 출구 측에서는 라운드(R)가 정방향으로 형성되도록 함으로써 증폭날개(30)를 통해 감아서 유인되는 공기의 양을 많게 하여 역기의 역류 방지 및 에너지 효율의 증진을 이룰 수 있게 하는 것이며, 이에 따르면, 자동차의 고속주행시에도 증폭날개에서 부하가 걸리는 것이 최소화되는 작용효과가 있게 된다.That is, at the inlet side of the hollow tube 11 through which air is introduced, the round R is formed in the opposite direction, so that the load is reduced by reducing the amount of air drawn through the amplifying vanes 30 and attracting the air. At the exit side of the discharge, the round (R) is formed to be formed in the forward direction to increase the amount of air drawn through the amplification wing (30) to prevent backflow of the counterweight and to improve energy efficiency. As a result, even when the vehicle is driving at a high speed, the load on the amplified wing is minimized.
또한, 본 발명에서는 배기관(1)과 증폭관부(10)의 중공관(11) 사이를 통과하는 공기의 유속을 더욱 느리게 함과 동시에, 통과하는 공기의 회전력을 증대시킴으로써, 공기의 역류 방지를 더욱 효율적으로 이루게 하는 것이 바람직하는데, 이와 같은 구성은 상기 중공관(11)의 외주면 및 증폭날개(30)의 외측면 즉, 표면에 다수의 돌기(60)를 형성하는 것을 통해 저항면을 형성시키는 것으로 용이하게 이룰 수 있다.In the present invention, the flow rate of the air passing between the exhaust pipe 1 and the hollow pipe 11 of the amplifying pipe part 10 is further slowed, and the rotational force of the air passing through is increased, thereby preventing the backflow of air. It is desirable to achieve efficiently, such a configuration is to form a resistance surface by forming a plurality of protrusions 60 on the outer circumferential surface of the hollow tube 11 and the outer surface of the amplification wing 30, that is, the surface. It can be achieved easily.
그리고, 이와 같은 다수의 돌기(60)에 의한 저항면에 따르면, 상기 배기관(1)과 중공관(11) 사이를 통과하는 공기에 부하가 걸리게 되므로, 증폭날개(30)를 통해 유인되는 공기의 유속저하는 물론, 공기의 회전력이 증가되는 작용효과가 있어 공기가 역류하는 현상을 보다 원활하게 방지할 수 있게 된다.And, according to the resistance surface by the plurality of protrusions 60, the load is applied to the air passing between the exhaust pipe 1 and the hollow tube 11, so that the air drawn through the amplification wing 30 The flow velocity is reduced, as well as the effect of increasing the rotational force of the air it is possible to more smoothly prevent the phenomenon of the air flow back.
한편, 배기관(1)과 중공관(11) 사이를 통과하는 공기에 회전력을 증가시키는 것은, 증폭날개(30)의 나선 피치를 변경하여 회전각을 크게 하는 것으로도 이룰 수 있으나, 상기와 같이 증폭날개(30)의 나선 피치 변경을 통한 공기의 회전력 증진 시에는, 엔진의 고속제어에서 심각한 부하가 걸리는 문제점이 있어, 본 발명에서는 중공관과 증폭날개의 표면에 돌기(60)를 각각 추가구성하여 저항면을 형성시키는 것으로 공기의 회전력 증진을 이루었으며, 이와 같은 돌기(60)에 의한 저항면에 따르면, 엔진의 중·저속제어는 물론, 고속제어에서도 부하가 걸리는 것이 최소화되어 안정적인 차량운행을 이룰 수 있게 된다.On the other hand, increasing the rotational force in the air passing between the exhaust pipe (1) and the hollow tube 11 can be achieved by changing the helix pitch of the amplification wing (30) to increase the rotation angle, amplification as described above When improving the rotational force of the air by changing the spiral pitch of the wing 30, there is a problem that a serious load is applied in the high-speed control of the engine, in the present invention by additionally configuring the projections 60 on the surface of the hollow tube and the amplification wing By forming a resistance surface to improve the rotational force of the air, according to the resistance surface by the projection (60), the load is minimized in the medium and low speed control, as well as high speed control of the engine to achieve a stable vehicle operation It becomes possible.
넷째, 제1회전결합돌부(40)는 나선형상으로 형성되어 증폭날개(30)의 하부에 각각 일체로 구성되는 것으로, 전술한 바와 같이 중공관(11)의 입구방향에 구성된 제1결합홀(13)에 대응되게 형성되어 상기 제1결합홀(13)을 통해 중공관(11)의 내측으로 돌출됨으로써 상기 중공관의 내부 입구 측에 배치된다.Fourth, the first rotary coupling protrusion 40 is formed in a spiral shape to be integrally formed at the lower portion of the amplification wing 30, respectively, as described above the first coupling hole configured in the inlet direction of the hollow tube 11 ( 13 is formed to correspond to the inner side of the hollow tube by protruding into the hollow tube 11 through the first coupling hole 13.
따라서, 상기 중공관(11)의 내부로 공급되는 공기는 다수로 구성되는 제1회전결합돌부(40)에 의해 1차 회전하는 작동이 이루어지며, 이와 같은 회전에 따른 구심력에 의해 공기의 통과 속도가 소폭 증가된다.Therefore, the air supplied into the hollow tube 11 is first rotated by the first rotary coupling protrusion 40 which is composed of a plurality of air, and the passage speed of the air by the centripetal force according to the rotation. Is slightly increased.
다섯째, 제2회전결합돌부(50)는 나선형상으로 형성되어 증폭날개(30)의 하부에 일체로 구성되는 것으로, 제1회전결합돌부와 이격되어 배치되도록, 중공관(11)의 출구방향에 구성된 제2결합홀(15)에 대응되게 형성되어 상기 제2결합홀(15)을 통해 중공관(11)의 내측으로 돌출됨으로써 중공관(11)의 내부 출구 측에 배치된다.Fifth, the second rotary coupling protrusion 50 is formed in a spiral shape is integrally formed in the lower portion of the amplification wing 30, so as to be spaced apart from the first rotary coupling protrusion, in the exit direction of the hollow tube 11 It is formed to correspond to the configured second coupling hole 15 and protrudes to the inside of the hollow tube 11 through the second coupling hole 15 is disposed on the inner outlet side of the hollow tube (11).
따라서, 상기 중공관(1)의 내부로 공급되어 1차 회전된 공기는 제2회전결합돌부(50)에 의해 2차 회전이 가속되어 지며, 이와 같은 회전력에 따른 구심력에 의해 공기의 통과 속도가 더욱 증대되어 진다.Therefore, the secondary air is accelerated by the second rotary coupling protrusion 50 to the first rotated air supplied to the inside of the hollow tube 1, and the passage speed of air is increased by the centripetal force according to the rotational force. It is further increased.
또한, 본 발명에서는 중공관의 내부로 공급되는 공기에 의한 저항을 최소화 할 수 있음과 더불어, 회전에 의한 통과 속도의 최대화를 위하여 제1, 2회전결합돌부의 돌출높이가 서로 다르게 형성되는 것이 바람직하다.In addition, in the present invention, in addition to minimizing the resistance by the air supplied into the hollow tube, it is preferable that the protrusion heights of the first and second rotary coupling protrusions are different from each other in order to maximize the passage speed due to the rotation. Do.
이를 위하여, 상기 중공관(11)의 내측 입구방향에 위치되는 제1회전결합돌부(40)는 증폭날개(30) 높이의 0.2배에 해당되는 높이로 돌출형성되어 중공관(11)의 입구로 공급되는 공기에 큰 저항 발생 없이 1차 회전을 걸어주도록 구성되고, 상기 중공관(11)의 내측 출구방향에 위치되는 제2회전결합돌부(50)는 증폭날개(30) 높이의 0.25배에 해당되는 높이로 돌출형성되어 중공관(11)의 출구로 배출되는 공기에 2차 회전을 1차 회전보다 많이 걸어줌으로써 상기 중공관(11)을 통과하는 공기의 속도를 증대시킬 수 있게 하는 것을 특징으로 한다.To this end, the first rotary coupling protrusion 40 located in the inlet direction of the hollow tube 11 is formed to protrude to a height corresponding to 0.2 times the height of the amplification wing 30 to the inlet of the hollow tube 11. It is configured to apply a first rotation without generating a large resistance to the supplied air, the second rotary coupling protrusion 50 located in the inner exit direction of the hollow tube 11 corresponds to 0.25 times the height of the amplified wing 30 It is formed to protrude to a height that is characterized in that to increase the speed of the air passing through the hollow tube 11 by walking the secondary rotation more than the first rotation to the air discharged to the outlet of the hollow tube 11 do.
이하에서는 본 발명의 바람직한 실시 예에 따른 작용을 설명한다.Hereinafter will be described the operation according to a preferred embodiment of the present invention.
먼저, 운전자가 자동자의 가속장치인 액셀을 밟으면, 흡기관을 통과하여 폭발 행정을 거친 배기가스가 포함된 공기가 배기관(1)을 통과한 후, 자동차의 외부로 배출되는데, 본 발명의 배기용 내연기관의 에너지 효율 증대장치(100)는 배기관(1)에 장착되어 있으므로, 상기 배기관(1)을 통과하는 공기의 연소 효율 증대가 이루어진다.First, when the driver steps on an accelerator, which is an accelerator of the automobile, air containing exhaust gas passing through the intake pipe and undergoing an explosion stroke passes through the exhaust pipe 1, and then is discharged to the outside of the vehicle. Since the energy efficiency increasing apparatus 100 of the internal combustion engine is mounted on the exhaust pipe 1, the combustion efficiency of air passing through the exhaust pipe 1 is increased.
그리고, 증폭관부(10)의 중공관(11) 내부를 통과하는 공기는 900 ~ 1200℃로 가열되는 와이어매쉬(20)에 의해 공기에 포함되어 있는 배기가스의 완전연소를 이룰 수 있어 배출되는 공기에 포함된 오염물질이 저감되는 작용이 이루어진다.In addition, the air passing through the hollow tube 11 inside the amplification pipe part 10 may achieve complete combustion of the exhaust gas included in the air by the wire mesh 20 heated to 900 to 1200 ° C. Contaminants contained in the action is reduced.
또한, 상기 중공관(11) 내부를 통과하는 공기는 비교적 낮은 높이로 돌출되어 있는 제1회전결합돌부(40)를 통해 큰 저항 없이 1차 회전이 이루어진 상태에서, 상기 제1회전결합돌부(40)와 이격배치된 제2회전결합돌부(50)에 의해 2차 회전이 보다 강하게 이루어지도록 되어 있으므로, 중·저속제어는 물론, 고속제어에서도 공기가 충돌하는 저항을 저감시킬 수 있음과 동시에 회전력을 증대시킬 수 있으며, 상기 중공관(11)의 내부를 빠르게 통과하는 공기가 중공관(11)의 외부를 통과하는 공기를 유인하는 작용을 하여 상기 공기가 통과되는 속도를 향상시킬 수 있으므로 상기 중공관(11)을 통과하는 공기가 가속된 상태로 일정한 속도로 안전하게 제어되어 차량의 승차감을 좋게 하는 장점을 가진다.In addition, the air passing through the inside of the hollow tube 11 is the first rotary coupling protrusion 40 in the state that the first rotation is made without a large resistance through the first rotary coupling protrusion 40 protruding to a relatively low height. And the second rotation coupling protrusion 50 spaced apart from each other, so that the secondary rotation is made stronger, the resistance to the collision of air can be reduced and the rotational force at the same time as well as the medium and low speed control. The hollow tube can be increased, and the air passing through the inside of the hollow tube 11 quickly attracts the air passing through the outside of the hollow tube 11 to improve the speed at which the air passes. Air passing through the (11) is safely controlled at a constant speed in an accelerated state has the advantage of improving the ride comfort of the vehicle.
아울러, 배기관(1)과 중공관(11) 사이를 통과하는 공기는 제1공간(31)에 의해 큰 충돌 없이 확산되어 지므로, 분할되는 공기에 의한 충격이 발생하지 않아 공기의 원활한 흐름이 지속적으로 이루어지고, 이 후, 증폭날개(30)에 의한 회전 및 중공관(11)과 증폭날개(30)에 각각 형성된 돌기(60)에 의한 저항을 통해 과도한 부하 없이도 회전력의 증가를 크게 이룰 수 있어 난류에 의한 공기의 역류 현상을 차단시킬 수 있는 장점도 있다.In addition, since the air passing between the exhaust pipe 1 and the hollow tube 11 is diffused without a great collision by the first space 31, the impact of the divided air does not occur, so that the smooth flow of air is continuously performed. After this, through the rotation by the amplification wing 30 and the resistance by the projections 60 formed in the hollow tube 11 and the amplification wing 30, respectively, it is possible to achieve a large increase in the rotational force without excessive load turbulent flow There is also an advantage that can block the backflow phenomenon of air by.
이는, 상기 중공관(11)의 내, 외부를 각각 통과하는 공기의 속도 차를 이용한 것으로, 중공관(11) 내부를 공기가 빠르게 통과하는 과정에서 배기관(1)과 중공관(11)의 사이로 발생되는 공기의 역류 현상을 상기 배기관(1)과 중공관(11) 사이에서 강한 회전으로 공급되는 공기로 막는 것을 통해 이룰 수 있으며, 이로 인해, 공기의 흐름을 원활하게 유지시킬 수 있어 에너지의 효율 증대를 가져올 수 있게 되는 것이다.This is to use the speed difference of the air passing through the inside and the outside of the hollow tube 11, respectively, between the exhaust pipe 1 and the hollow tube 11 in the process of rapidly passing air through the inside of the hollow tube 11 The reverse flow of the generated air can be achieved by blocking the air supplied by the strong rotation between the exhaust pipe (1) and the hollow tube (11), and thus, it is possible to keep the flow of air smoothly and energy efficiency It will be able to bring an increase.
이상에서 설명한 바와 같이, 본 발명은 한정된 실시 예와 도면으로 설명하였으나, 이에 한정되지 않으며, 본 발명의 기술적인 사상에서 벗어나지 않는 범위 내에서 다양한 형태로 변경하여 실시할 수도 있을 것이다.As described above, the present invention has been described with limited embodiments and drawings, but the present invention is not limited thereto and may be implemented in various forms without departing from the technical spirit of the present invention.
Claims (5)
- 자동차의 배기관(1)에 설치되는 에너지의 효율을 증대시키는 장치에 있어서,In the device for increasing the efficiency of the energy installed in the exhaust pipe (1) of the vehicle,중공관(11)과, 상기 중공관(11)의 입구방향에 관통형성되는 복수 개의 제1결합홀(13)과, 상기 중공관(11)의 출구방향에 관통형성되는 복수 개의 제2결합홀(15)로 구성된 증폭관부(10);The hollow tube 11, a plurality of first coupling holes 13 formed in the inlet direction of the hollow tube 11, and a plurality of second coupling holes formed in the outlet direction of the hollow tube 11. An amplifier tube section (10) consisting of (15);상기 증폭관부(10)의 내주면에 밀착설치되도록 스퍼터링으로 부착되어 중공관(11)의 내부를 통과하는 배기가스를 고온의 배기가스에 의한 가열로 연소시키는 와이어매쉬(20);A wire mesh (20) attached to the inner circumferential surface of the amplifying pipe part (10) by sputtering to combust the exhaust gas passing through the inside of the hollow tube (11) by heating with high temperature exhaust gas;상기 증폭관부(10)에 구성된 중공관(11)의 외주에 나선형상으로 접합되되, 상기 중공관(11)의 입구와 출구에서 각각 이격설치되어, 상기 배기관(1)과 중공관(11) 사이 및 증폭날개(30)의 입구측 단부에서 중공관(11)의 입구 사이에 제1공간(31)을 형성시키고, 상기 배기관(1)과 중공관(11) 사이 및 증폭날개(30)의 출구측 단부에서 중공관(11)의 출구 사이에는 제2공간(32)을 형성시키는 복수 개의 증폭날개(30);Spirally bonded to the outer periphery of the hollow tube 11 formed in the amplifying pipe part 10, and are respectively installed at the inlet and outlet of the hollow tube 11, between the exhaust pipe (1) and the hollow tube (11) And a first space 31 is formed between the inlet of the hollow tube 11 at the inlet side end of the amplifying wing 30, between the exhaust pipe 1 and the hollow tube 11 and the outlet of the amplifying wing 30. A plurality of amplifying vanes 30 forming a second space 32 between the outlets of the hollow tubes 11 at the side ends;나선형상으로 형성되어 증폭날개(30)의 하부에 일체로 구성되되, 중공관(11)의 입구방향에 구성된 제1결합홀(13)에 대응되게 형성되어 상기 제1결합홀(13)을 통해 중공관(11)의 내측으로 돌출되는 제1회전결합돌부(40);Is formed in a spiral shape is integrally formed in the lower portion of the amplification wing 30, formed corresponding to the first coupling hole 13 formed in the inlet direction of the hollow tube 11 through the first coupling hole (13) A first rotary coupling protrusion 40 protruding inward of the hollow tube 11;나선형상으로 형성되어 증폭날개(30)의 하부에 일체로 구성되되, 중공관(11)의 출구방향에 구성된 제2결합홀(15)에 대응되게 형성되어 상기 제2결합홀(15)을 통해 중공관(11)의 내측으로 돌출되는 제2회전결합돌부(50);로 이루어져,Is formed in a spiral shape is integrally formed in the lower portion of the amplification wing 30, formed corresponding to the second coupling hole 15 formed in the outlet direction of the hollow tube 11 through the second coupling hole (15) Consisting of the second rotary coupling protrusion 50 protruding inwardly of the hollow tube 11,서로 이격배치된 제1, 2회전결합돌부(40, 50)를 이용한 중폭관부(10)의 중공관(11) 내부에서의 공기의 순차적인 풍속 증가와 더불어, 증폭날개(30)를 이용한 배기관(1)과 중공관(11) 사이에서의 공기의 풍속 저하 및 강한 회전을 통해 배기관(1)을 통과하는 공기의 역류를 방지하여 공급된 공기량 대비 연소효율을 증대시킬 수 있고, 배출되는 배기가스에 포함된 공해물질을 가열된 와이어매쉬(20)의 연소를 통해 저감시킬 수 있는 것을 특징으로 하는 배기용 내연기관의 에너지 효율 증대장치.In addition to the sequential increase in air velocity of the air inside the hollow tube 11 of the medium width pipe part 10 using the first and second rotary coupling protrusions 40 and 50 spaced apart from each other, the exhaust pipe using the amplification wing 30 ( It is possible to increase the combustion efficiency compared to the amount of supplied air by preventing the reverse flow of air passing through the exhaust pipe 1 through the decrease in the wind speed and strong rotation of the air between 1) and the hollow tube 11, Energy efficiency increasing apparatus of the internal combustion engine for exhaust, characterized in that the pollutant contained can be reduced through the combustion of the heated wire mesh (20).
- 제 1항에 있어서, 상기 증폭날개(30)에 의해 형성되는 제1공간(31)은 중공관(11) 길이의 0.1 ~ 0.15배에 해당되는 폭으로 형성되어, 입구방향으로 공급되는 공기가 증폭관부(10) 및 증폭날개(30)에 의해 분리되는 충격을 완화시키는 작용을 하고,The method of claim 1, wherein the first space 31 formed by the amplification wing 30 is formed in a width corresponding to 0.1 ~ 0.15 times the length of the hollow tube 11, the air supplied in the inlet direction is amplified It acts to mitigate the impact that is separated by the tube portion 10 and the amplification wing 30,상기 증폭날개(30)에 의해 형성되는 제2공간(32)은 중공관(11) 길이의 0.2 ~ 0.3배에 해당되는 폭으로 형성되어 배기되는 공기의 역류 방지를 이루는 작용을 하되,The second space 32 formed by the amplifying wing 30 is formed to a width corresponding to 0.2 ~ 0.3 times the length of the hollow tube 11 serves to prevent the backflow of the exhaust air,상기 제1공간(31)의 길이와 제2공간(32)의 길이는 1 : 2의 비율로 형성되는 것을 특징으로 하는 배기용 내연기관의 에너지 효율 증대장치.The length of the first space (31) and the length of the second space (32) is an energy efficiency increasing apparatus of the internal combustion engine for exhaust, characterized in that formed in a ratio of 1: 2.
- 제 1항에 있어서, 상기 증폭날개(30)에는 흡기되는 공기를 회전시킴과 동시에, 회전하는 공기를 감아서 유인하기 위한 라운드(R)가 형성되되,The method of claim 1, wherein the amplifying wing 30 is formed at the same time as rotating the intake air, at the same time the round (R) for winding and attracting the rotating air,상기 라운드(R)는 증폭날개(30)를 통해 감아서 유인되는 공기의 양이 입구방향에서는 적고, 출구방향에서는 많이 발생되도록 서로 반대반향으로 형성되며,The round (R) is formed in the opposite direction so that the amount of air wound through the amplification wing 30 is attracted to the inlet direction is less, a lot in the outlet direction,서로 반대방향으로 형성되는 라운드(R)는 상기 증폭날개(30)의 나선형상을 따라 일체로 연결형성되는 것을 특징으로 하는 배기용 내연기관의 에너지 효율 증대장치.Round (R) is formed in the opposite direction to each other, the energy efficiency of the internal combustion engine for exhaust gas, characterized in that integrally formed along the spiral shape of the amplification wing (30).
- 제 1항에 있어서, 상기 증폭관부(10)에 구성된 중공관(11)의 외주면과 증폭날개(30)의 외측면에는, 배기관(1)과 증폭관부(10) 사이를 통과하는 공기에 부하를 걸어 공기의 회전력을 증대시킬 수 있도록, 돌기(60)가 다수로 돌출구성되어 저항면을 형성하는 것을 특징으로 하는 배기용 내연기관의 에너지 효율 증대장치.The load is applied to the air passing between the exhaust pipe 1 and the amplifying pipe section 10 on the outer circumferential surface of the hollow tube 11 and the amplifying wing section 30 formed in the amplifying pipe section 10. Energy efficiency increasing apparatus of the internal combustion engine for exhaust gas, characterized in that the projection (60) is formed of a plurality so as to increase the rotational force of the air to form a resistance surface.
- 제 1항에 있어서, 상기 중공관(11)의 내측 입구방향에 위치되는 제1회전결합돌부(40)는 증폭날개(30) 높이의 0.2배에 해당되는 높이로 돌출형성되어 중공관(11)의 입구로 공급되는 공기에 1차 회전을 걸어주고,The hollow rotary tube 11 of claim 1, wherein the first rotary coupling protrusion 40 positioned in the inner inlet direction of the hollow tube 11 protrudes to a height corresponding to 0.2 times the height of the amplifying wing 30. The first turn on the air supplied to the inlet of the상기 중공관(11)의 내측 출구방향에 위치되는 제2회전결합돌부(50)는 증폭날개(30) 높이의 0.25배에 해당되는 높이로 돌출형성되어 중공관(11)의 출구로 배출되는 공기에 2차 회전을 걸어주도록 된 것을 특징으로 하는 배기용 내연기관의 에너지 효율 증대장치.The second rotary coupling protrusion 50 positioned in the inner exit direction of the hollow tube 11 is formed to protrude to a height corresponding to 0.25 times the height of the amplifying wing 30 and is discharged to the outlet of the hollow tube 11. Energy efficiency increasing device of the internal combustion engine for exhaust, characterized in that the second rotation to give.
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WO2019203438A1 (en) * | 2018-04-17 | 2019-10-24 | 주식회사 아스티즈 | Noise reduction-type exhaust device for enhancing output of internal combustion engine |
KR101933494B1 (en) * | 2018-04-17 | 2018-12-31 | 이재욱 | Noise reduction type exhaust device for enhancing output of internal combustion engine |
KR102137023B1 (en) * | 2019-03-06 | 2020-07-24 | 김기락 | Air eddy apparatus for internal combustion engine |
KR102346303B1 (en) * | 2020-11-13 | 2022-01-03 | 피에스테크 주식회사 | Amplifying pipe unit and amplifying pipe |
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KR20150118463A (en) * | 2014-04-14 | 2015-10-22 | 박상호 | An augmentation device having improved air flow |
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