KR200431166Y1 - Reduction of exhaust gas fuel economy system for an internal combustion engine - Google Patents

Abstract

The present invention relates to an exhaust gas reducing fuel reducer for an internal combustion engine, and more particularly, is installed on the fuel supply line of an internal combustion engine to pressurize and diffuse fuel and at the same time atomize molecules to achieve complete combustion of fuel. An inlet housing, one end of which is connected to the fuel pipe side of the fuel tank, and a discharge side housing, of which the engine side fuel pipe is connected to the other end thereof, and a ring magnet and a diffuser are sequentially installed at the inner end of each housing. In the center, a sleeve having a spherical sleeve ball in the fuel cylinder hole can be retracted, a cap is provided with a plurality of discharge holes and coupled to the fuel cylinder hole on the sleeve, a plurality of ring magnets are embedded in the fuel cylinder hole overlapping the lower portion of the sleeve A fuel saver provided with an assembly of a sleeve body coupled to the inside of the discharge port housing The wall at the side end is curved to diffusely reflect the fuel, and between each ring magnet superimposed inside the sleeve body and a washer of a size corresponding to the ring magnet is disposed at the outermost side, and the ring magnet and the washer An internal combustion engine exhaust gas reduction fuel saver is disclosed, characterized in that a concave-convex surface is formed in the inner surface, a jaw is formed in one end portion, and a cylindrical bushing in which the bushing ball is retractable is inserted therein.

Description

Reduction of exhaust gas fuel economy system for an internal combustion engine

1 is an exploded perspective view of a fuel saver according to an embodiment of the present invention.

Figure 2 is a longitudinal cross-sectional view showing the assembled state of the fuel saver according to an embodiment of the present invention, a state without stepping on the accelerator.

Figure 3 is a longitudinal sectional view showing an assembled state of the fuel saver according to an embodiment of the present invention, a state stepped on the accelerator.

4 to 7 is a view showing the emissions of smoke before and after mounting the product of the present invention according to Example 2

<Description of Symbols for Main Parts of Drawings>

10 discharge side housing 12 reflecting surface

20: ring magnet 21: washer

30, 31: diffuser

40: cap 41: discharge hole

50: sleeve ball 51: bushing ball

60: sleeve 61, 81, 92: fuel hole

70: bushing 71: uneven surface

72: jaw 80: sleeve body

90: inlet side housing

The present invention relates to an exhaust gas reducing fuel reducer for an internal combustion engine, and more particularly, is installed on a fuel supply line of an internal combustion engine to pressurize and diffuse fuel, and at the same time, atomize molecules to achieve complete combustion of fuel. TECHNICAL FIELD The present invention relates to an engine exhaust fuel saving fuel reducer.

In general, a mixer supplied to an engine such as an internal combustion engine used in an automobile or a ship requires very precise control to simultaneously satisfy reduction of exhaust gas, reduction of fuel consumption, and output improvement.

The fuel injection device applied to the internal combustion engine electrically detects the intake air amount and injects the fuel according to the detected air intake to suit the operating conditions of the engine. The fuel injection device includes a control unit.

The injector is a component that injects fuel into the intake manifold of each cylinder in response to a signal from the controller.It consists of a solenoid coil plunger and a needle valve, and when the current flows through the solenoid coil, the plunger is sucked and formed integrally with the plunger. By opening the injection port by pulling the needle valve which is present serves to inject the fuel.

In the above operation, the injection amount of fuel is determined by the time when the needle valve is opened, that is, the time when the solenoid coil is energized.

The electric circuit for operating such an injector is roughly divided into a voltage control type and a current control type. The voltage control type and the current control type are determined by the use of a resistor (register).

On the other hand, the fuel inlet is installed on the inlet side connected to the engine to cause a swirl flow of the fuel injected from the injector, this fuel saver is known in various forms, as an example the present inventors Fuel savings such as 2004-0005552 have been proposed.

The prior art is an inlet-side housing to which the fuel pipe on the fuel tank side is connected, a first permanent magnet fixed to the inside of the inlet-side housing, and coupled to the inlet-side housing by coupling means, one end of the engine-side fuel tube The discharge side housing to be connected, the second permanent magnet fixed to face the same polarity as the first permanent magnet in the discharge side housing, and installed in the middle portion of the housing to partition the interior of the housing, the fuel passage hole in the center A formed diaphragm, a third permanent magnet installed on the fuel inlet side of the diaphragm, a fourth permanent magnet installed on the fuel discharge side of the diaphragm and provided with a first ball retractable in the through hole, and installed on one side of the diaphragm. And a sleeve having a fuel passage hole formed at the center thereof, and installed on the fuel passage hole of the sleeve to open and close the fuel passage hole by the magnetic force of the fourth permanent magnet. A second ball for miniaturizing the fuel, a cap provided on one side of the sleeve, and a plurality of fuel supply holes formed so that the fuel is supplied to the combustion chamber side as the second ball opens the fuel passage hole of the sleeve by pressing the activator; And a first diffuser plate provided in the inlet-side housing to diffuse fuel primarily, and a second diffuser plate installed in the discharge-side housing to secondary diffuse and refine the fuel.

However, the prior art has the disadvantage that the surface coating layer of the permanent magnet is continuously exposed to the fuel, such as oxidation and corrosion, and the magnet flows due to the gap between the magnets or the minute vibration is repeated, the magnetic force is sharply reduced or the magnet There was a problem of weak durability, such as a problem such as cracking.

In addition, since there is not enough space between the first ball and the fourth permanent magnet provided to be able to move in and out of the fourth permanent magnet, when fine debris accumulates in the fuel, the fuel does not pass and is blocked. Since the position is determined depending on the Gaussian size of the permanent magnet and the third permanent magnet, it is necessary to measure and assemble the Gaussian of each magnet one by one. There was a problem that the durability and stability are not good, such as the ball retreating up to the third permanent magnet to go out with the first diffusion plate to damage the diffusion wing.

Accordingly, the present invention devised to solve the above problems is to atomize while spreading the fuel several times in the process of supplying fuel by a pair of diffuser plate, a plurality of permanent magnets (ring magnet), and a metal ball. It is possible to achieve complete combustion, to reduce exhaust gas due to the complete combustion of fuel, and to improve the durability and stability of the fuel saver for realizing this, while increasing the output power by increasing the explosive power according to the complete combustion. The purpose is to provide an exhaust gas reducing fuel saver for an internal combustion engine.

The present invention for achieving the above object is a housing coupled to the inlet-side housing is connected to the fuel pipe side of the fuel tank at one end and the discharge-side housing is connected to the engine side fuel pipe at the other end, ring magnets and The diffuser is mounted in sequence, the inner center of the housing, the sleeve is provided so that the spherical sleeve ball in the fuel cylinder hole can be retracted, a plurality of discharge holes are provided, the cap coupled to the fuel cylinder hole on the sleeve, the plurality of fuel cylinder holes A ring magnet overlaps and constitutes an exhaust gas reducing fuel saver for an internal combustion engine having a combination of a sleeve body coupled to the bottom of the sleeve, wherein the wall of the inner end of the outlet housing is curved to diffuse the fuel. Corresponding to each of the ring magnets superimposed within the sleeve body and on the outermost side respectively. Characterized in that a washer is interposed in the size of the ring magnet and the interior of the washer has a convex surface on the inner surface being formed with a projection formed on one end of the ball bushing is moved forward and backward can be provided in the cylindrical inner bushing within the

Hereinafter, preferred embodiments of the present invention will be described in more detail with reference to FIGS. 1 to 3.

1 is an exploded perspective view of a fuel saver according to an embodiment of the present invention, Figure 2 is a longitudinal cross-sectional view showing the assembled state of the fuel saver according to an embodiment of the present invention, the fuel saver of the present invention with reference to Figs. The configuration is as follows.

One end of the discharge-side housing 10 is provided with a discharge nipple 11 so that the engine-side fuel pipe is fitted, and the fuel tank is located on the other side of the inlet-side housing 90 coupled with the discharge-side housing 10 by a conventional screwing means. Inlet nipple 91 is provided to be coupled to the fuel pipe connected with.

At each inner end of the discharge side housing 10 and the inlet side housing 90, a ring-shaped ring magnet 20 and a washer 21 having a size corresponding to the ring magnet 20, as shown in FIG. 2. And diffusers 30 and 31 formed of a plurality of blades are provided in symmetry with each other.

At this time, the inner surface of the discharge-side housing 10 is preferably curved so that the cross section is curved so that the inner diameter is gradually reduced toward the discharge nipple (11) side as shown in the curved form in FIG.

The prior art proposed by the inventors of the present invention, while the shape is a straight form, when manufactured in a curved shape as in the present invention, the fuel diffused and discharged through the discharge-side diffuser 30 hits the reflecting surface 12, causing diffuse reflection Fuel can be efficiently distributed over a large area.

Meanwhile, a cap 40, a sleeve 60, and a sleeve body are formed in each of the diffusion plates 30 and 31 of the housings 10 and 90 in which the discharge side housing 10 and the inlet side housing 90 are coupled. An assembly in which 80 is coupled to each other is incorporated.

First, the sleeve 60, the sleeve body 80 is coupled to the bottom, as a medium means for coupling the cap 40 to the top, that is, the spherical sleeve ball 50 in the fuel cylinder hole 61 is advanced It is provided to be possible, the lower portion of the fuel cylinder hole 61 is formed with a protruding nozzle portion 62 so that the sleeve ball 50 does not retreat any more, the lower portion of the nozzle portion 62 is curved inclined portion 63 On the other hand, the cap 40 having a plurality of discharge holes 41 is screwed to the outer circumferential surface of the fuel cylinder 61, the cap 40 is a sleeve ball 50 in the fuel cylinder 61 It has a structure to prevent the departure.

Here, the curved inclined portion 63 also, when the fuel that passes through the inside of the bushing 70 to be described later, like the curved portion 12 formed in the discharge side housing 10 is reflected while hitting the curved inclined portion 63, the fuel The fuel is further activated by the magnetic force of the ring magnet 20, while dispersing it efficiently over a large area.

The sleeve body 80 which is screwed under the sleeve 60 is alternately embedded in the inner fuel hole 81 with a plurality of ring magnets 20 and washers 21 as shown, wherein each ring The partition wall 82 protruding from the sleeve body 80 may be formed between the magnet 20 and the washer 21 so that these gaps may be defined by the partition wall 82. It is also possible to prevent the gap or flow of (21). Of course, the arrangement of the washer 21 and the magnet 21 is not limited to the order of the illustrated example.

The cylindrical bushing 70 is interpolated inside the magnetic material in which the plurality of ring magnets 20 and the washers 21 are alternately stacked.

The bushing 70 is provided with a spherical bushing ball 51 therein so that the bushing ball 51 can be moved in and out of the bushing 70, and the bushing ball 51 has the sleeve ( Retraction is prevented by the curved inclined portion 63 formed at 60, and retraction is prevented by the jaw 72 protruding inwardly from the other end of the bushing 70 at the time of retreat.

Therefore, the inner diameter of the bushing 70 is somewhat larger than the outer diameter of the bushing ball 51, the inner diameter of the jaw 72 is preferably smaller than the outer diameter of the bushing ball 51, where the bushing ( 70) The gap between the uneven surface 71 formed in the longitudinal direction on the inner surface and the bushing ball 51 can be appropriately designed depending on the type of internal combustion engine within the range of 0.05 to 0.2 mm.

At this time, the uneven surface 71 formed in the longitudinal direction of the bushing 70 allows the fuel blocked by the bushing ball 51 to pass through the uneven portion of the uneven surface 71. 71 is formed on the entire inner circumferential surface of the bushing 70. In the illustrated embodiment, unevenness is formed in the longitudinal direction of the bushing 70, but it is possible to form a vortex while extending the residence time of the fuel further. In order to ensure that the irregularities can be manufactured in the form of a spiral like a female thread.

The height of the unevenness is different depending on the type and displacement of the internal combustion engine, but it is preferable to be within the range of 0.1mm to 1.0mm. If the height of the unevenness is too low, the amount of fuel is supplied so that the fuel pump is overloaded. The fuel pump may be burned out. On the contrary, if the fuel pump is too high, there is a limit to atomizing the fuel, which is not suitable because the effect of the fuel saver is inferior.

When configured in this way, the number of the Gaussian of the ring magnets 20 according to the position or do not need to separately manage, assembling the size of the Gaussian, it is advantageous than the conditions of the prior art in terms of assembly and management.

On the other hand, the ring magnet 20 is generally treated with a metal coating such as nickel plating on the surface to improve the durability of the magnet, the metal coating layer is easily peeled off when exposed to fuel for a long time.

Thus, if the side surface of the ring magnet 20 is assembled using the washer 21 having the same size as the ring magnet 20, the metal coating layer is not directly exposed to the fuel by the washer 21, so durability Is improved.

2 is a state diagram without stepping on the accelerator, Figure 3 is a longitudinal cross-sectional view showing the assembled state of the fuel saver according to an embodiment of the present invention, is a state diagram stepped on the accelerator.

2 and 3, the operation of the present invention will be described.

First, when the fuel saver of the present invention is installed on the fuel supply line of the vehicle, the sleeve ball 50 is retracted by the magnetic force of the ring magnet 20 formed inside the sleeve body 80 to close the nozzle 62. do.

In this state, when the fuel pump is driven by driving the engine, fuel is introduced into the inlet housing 90 by the pumping force of the fuel pump, and the fuel introduced into the inlet housing 90 is a ring magnet. The bushing ball 51 formed in the inner surface of the bushing 70 after passing through the washer 21 and spreading and spreading primarily inside the inlet-side housing 90 through the inlet-side diffuser 31. It passes through between the concave and concave surface 71, and at this time, since the concave and convex surface 71 is formed over the entire inner circumferential surface of the bushing 70, the fuel is dispersed over the entire surface, and the fuel is also bushing ( 70) It is further activated by the magnetic force of the ring magnet 20 provided on the outer circumferential surface of the bushing 70 while passing through the inside.

When the dispersed and activated fuel reaches the nozzle part 62 of the sleeve 60, the bushing ball 51 opens the nozzle part 62 by the pumping pressure of the fuel, and the fuel is nozzle part 62. And atomized again while passing between the bushing ball 51 and supplied to the discharge side housing 10 through the plurality of discharge holes 41 formed in the cap 40, and then inside the discharge side housing 10, the discharge side diffuser 30. By diffusing again, it is possible to realize complete combustion of fuel in the combustion chamber.

What has been described so far is the idle state without the driver stepping on the accelerator.

However, when the driver steps on the accelerator for driving, a pressure difference is generated by the pressure of the fuel pump so that the bushing ball 51 moves in the fuel supply direction and the sleeve ball 50 also opens the nozzle part 62.

At this time, while the sleeve ball 50 closes a part of the discharge hole 61 formed in the cap 40 to reduce the fuel passage cross-sectional area, the pumping pressure of the fuel is further increased, and eventually, the discharge hole 61 of the cap 40. After passing through), fuel is quickly supplied to the combustion chamber. That is, more fuel is supplied to the combustion chamber side during the same time.

As described above, after the fuel refined by the bushing 70 passes through the discharge hole 61 of the cap 40, the diffuser 30 and the reflective surface 12 provided in the discharge side housing 10 are described. By the fuel is diffused and activated again by the fuel, it is possible to realize the complete combustion of the fuel in the combustion chamber (not shown).

Example 1

After fueling the fuel saving device of the present invention in the old Sonata (exhaust rate 1800cc, gasoline) vehicle with and without the fuel saving device of the present invention three times each, 64 liters of gasoline was calculated, and the average mileage was calculated. The 64 liter average mileage of the car was 400 km, while the average mileage of the car was 480 km, resulting in an average of 80 km (20.0% increase).

After fueling 50 liters of diesel fuel in seven times with and without the fuel saver of the present invention in an old Vesta (exhaust 2700cc, transmission, diesel) vehicle, the average mileage was calculated and The 50-liter average mileage was 440 km, and the average mileage when mounted was 550 km, resulting in an average of 110 km (20.2% increase).

       Example 2

The experiment was conducted in the Department of Automotive Engineering, Inha Technical College, Incheon, Korea under the following conditions.

Car Name: Carnival II Diesel

Engine type: 2.9L, dohc, turbo-intercooler, AT4

Fuel system: mechanical injection system

Mileage: 130,000 Km

Meter and type

Chasiss Dynamometer: 100kw DC morter, twin roll

Driving mode: CVS-75 mode (hot test)

Smoke measurement: In-line full flow light transmission opacimeter (OPC-130)

PM measuring instrument: CVS method, PM measuring instrument using weighing chamber

CO ₂ Analyzer: Mexa-554 JK (Horiba)

<Measurement result>

Smoke emissions

As shown in FIG. 4 to FIG. 7, the smoke measurement result was measured by an in-line full flow type opecimeter, and the product of the present invention was marked with (a) and before mounting (b), where acceleration ( 4), constant speed (FIG. 5), deceleration (FIG. 6), no load (FIG. 7) region can be seen that the smoke is reduced in the vehicle after mounting the product of the present invention.

Winners of PM (Unit: mg)

TABLE 1

   Before mounting (b)     After mounting (a)       a-b    Reduction Conduct 1    88.76     89.12       0.36    7.7% Conduct 2    89.17     89.62       0.45    21.1 Conduct 3    88.3     88.73       0.39    18.7

As a result of measuring the prize winner material (PM) using the Weighing Chamber in <Table 1>, it can be seen that the CVS-75 mode is reduced by 7.7 in practice 1, 21.1% in practice 2 and 18.7% in practice 3.

CO ₂ emissions by constant speed test (unit: mg)

TABLE 2

100 Km / h 80 Km / h 60 Km / h 40 Km / h  Idle  Comparative example CO2 (% vol) 4.52 4.02 3.20 2.34 2.02  Example CO2 (% vol 4.34 3.78 3.05 2.26 1.90 CO ₂ reduction rate 4.0% 6.0% 3.8% 3.4% 5.9%

In Table 2, the results of the constant speed test showed that CO ₂ emissions were reduced by 3.4% to 5.9% depending on the speed.

Example 3

Military Mobile Equipment Test Results

 TABLE 3

 Car type Mileage fuel efficiency per liter  Fuel consumption  Remarks  Before mounting  After mounting  Reduction 500 km Before mounting After mounting Reduction 1/4 (K-131) 8.7 Km 10.56 Km +1.86 Km 57.5 ℓ 47.3 ℓ 10.2 ℓ  17.73% 1 1/4 (K-311) 4 Km 5 Km +1 Km 125 ℓ 100 ℓ 25 ℓ  20% 2 1/2 (K-511) 2.5 Km 3.14 Km +0.64 Km 200 ℓ 161.29 ℓ 87.7 ℓ  19.3% Armored Car (K-200) 0.72 Km 0.82 Km +0.1 Km 690 ℓ 610 ℓ 80 ℓ  12%

       According to <Table 3>, the fuel consumption per ℓ can be reduced from + 0.1Km to + 1.86Km, depending on the type of maneuvering equipment before and after the product of the present invention. You can see up to 20% savings.

According to the exhaust gas reduction fuel reducer for an internal combustion engine of the present invention, in addition to the effects of the prior art, the reflection surface is formed in a curved surface so that the fuel can be diffused in a more uniform distribution, thereby increasing the combustion efficiency of the fuel. In addition to improving the output of the internal combustion engine, it is possible to further minimize the generation of exhaust gas.

Furthermore, the magnet's flow prevention structure, the magnet's coating layer damage prevention structure and the uneven surface and jaw's bushing and bushing ball retracting structure improve the durability of the magnet and the durability of the diffuser, as well as the overload of the fuel pump. Since it is not caught, it has the effect of extending the life of the fuel saver without affecting the life of the existing parts of the vehicle.

Claims (9)

An inlet-side housing to which the fuel pipe on the fuel tank side is connected at one end; A housing to which the discharge side housing to which the engine side fuel pipe is connected is coupled; Each housing inner end is equipped with a ring magnet and a diffuser in turn, and the inner central portion of the housing is provided with a sleeve for retracting the spherical sleeve ball from the fuel hole, and a plurality of discharge holes and coupled to the fuel hole on the sleeve. Cap, a combination of the sleeve body which is embedded in the plurality of ring magnets in the fuel hole overlapping and coupled to the lower sleeve, In the ring magnet embedded in the sleeve body, an uneven surface is formed on the inner surface, a jaw is formed at one end, and a cylindrical bushing in which the bushing ball is retracted from the inside is interpolated. . The method of claim 1, The inner diameter of the bushing is somewhat larger than the outer diameter of the bushing ball, the inner diameter of the jaw is configured to be smaller than the outer diameter of the bushing ball, the gap between the uneven surface and the bushing ball is characterized in that 0.05mm to 0.2mm range Emissions reduction fuel savings for internal combustion engines The method of claim 1, The unevenness (배기) is an exhaust gas reducing fuel saver for an internal combustion engine, characterized in that formed in the same straight or spiral form as the bushing longitudinal direction. The method of claim 3, The height of the uneven (배기) is an exhaust gas reducing fuel saver for an internal combustion engine, characterized in that the range of 0.1mm to 1.0mm. The method of claim 1, The inner surface of the sleeve is an exhaust gas reduction fuel saver for an internal combustion engine, characterized in that the curved inclined portion is formed. The method according to any one of claims 1 to 5, And a washer having a size corresponding to the ring magnet is disposed between each ring magnet and the outermost side overlapping the inside of the sleeve body, respectively. The method of claim 6, And a washer having a size corresponding to the ring magnet is mounted on each outer surface of the ring magnet formed at the inner end of each housing. The method according to any one of claims 1 to 5, And an inner wall of the discharge port housing has a curved surface. The method according to any one of claims 1 to 5, And the diffuser has a shape in which a plurality of diffuser blades having a propeller shape are divided into the openings of the ring magnets mounted in the respective housings.

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