JP2009079480A - Intake control device of internal combustion engine - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide an intake control device of an internal combustion engine which realizes further improvement in combustion under various operating states of the internal combustion engine. <P>SOLUTION: The intake control device 20 of the internal combustion engine is equipped with an intake passage 30 which feeds air 14 in a cylinder 8 of an engine 1, a combustor 9 which forms combustion gas fed to the intake passage 30, an exhaust pipe 10 which connects the combustor 9 with the intake passage 30 and feeds combustion gas to the intake passage 30, and a jetting port 11 which is provided to a wall surface 32 of the intake passage 30 and which jets combustion gas from the exhaust pipe 10 in a direction of the cylinder 8 along the wall surface 32 of the intake passage 30, wherein the combustion gas 15 jetted through the jetting port 11 flows in the intake passage 30 with a speed faster than air 14 and a swirl 16 is generated in the cylinder 8. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  The present invention relates to an intake control device for an internal combustion engine that generates a swirl flow such as a swirl flow or a tumble flow in a cylinder of the internal combustion engine.

  2. Description of the Related Art Conventionally, there is an apparatus in which an intake control valve is provided in an intake pipe of an internal combustion engine, and an auxiliary intake passage that bypasses the intake pipe from upstream of the intake control valve is provided (Patent Document 1). The auxiliary intake passage opens to an intake port that communicates with a cylinder of the internal combustion engine. The air passing through the auxiliary intake passage becomes a jet flow, flows into the cylinder through the intake port, and generates a swirl flow in the cylinder. The swirl flow promotes the mixing of air and fuel in the cylinder, and can improve the combustion of the internal combustion engine.

  There is also a device that provides an injection pipe that opens to an intake port that communicates with a cylinder of an internal combustion engine, and injects compressed air from the injection pipe to the intake port (Patent Document 2). Compressed air is created by the compressor and injected through the injection pipe into the intake port, creating a swirl flow in the cylinder.

Further, in an internal combustion engine equipped with a turbocharger, there is a device that provides an air supply passage that opens to an intake port that communicates with a cylinder and injects compressed air from the air supply passage to the intake port (Patent Document 3). Compressed air is supplied by an air tank, and is injected into the intake port through the air supply passage when a large amount of intake air is required, such as during rapid acceleration of the vehicle. The air in the air tank is maintained at a predetermined pressure by the compressor.
Japanese Patent No. 3422024 Japanese Utility Model Publication No.59-21030 JP 59-158324 A

  In the device described in Patent Document 1, since air flowing in the intake pipe passes through the auxiliary intake passage and is injected into the intake port, the pressure of the air injected into the intake port depends on the air pressure in the intake pipe and the auxiliary intake passage. Depends on the inner diameter etc. For this reason, the pressure of the air ejected to the intake port cannot be freely changed, and the strength of the swirl flow (vortex flow) generated in the cylinder cannot be freely controlled. Therefore, depending on the operating state of the internal combustion engine, the effect of the swirl flow may not be sufficiently obtained.

  In the device described in Patent Document 2, compressed air that is injected into the intake port is generated by a compressor. The compressor needs a certain amount of time (rise time) to generate the necessary pressure. For this reason, compressed air is not injected immediately after the start of operation of the compressor, and depending on the operation state of the internal combustion engine, there is a possibility that a required swirl flow (vortex flow) cannot be generated in the cylinder. Further, as described in Patent Document 3, a method of using a compressor and an air tank in combination is also conceivable, but the number of times that compressed air can be continuously injected is determined by the capacity and pressure accumulation capacity of the air tank. For this reason, depending on the operating state of the internal combustion engine, a required swirl flow (vortex flow) may not be generated in the cylinder.

  As described above, in the conventional apparatus, the control of the eddy current contributing to the combustion improvement is not sufficient, and there is room for further combustion improvement in various operating states of the internal combustion engine.

  Therefore, the present invention has been made in view of the above problems, and an object of the present invention is to provide an intake control device for an internal combustion engine that can further improve combustion in various operating states of the internal combustion engine.

  In order to solve the above-mentioned problems, the technical means taken in the present invention are, as claimed in claim 1, an intake passage for sending combustion air into a cylinder of an internal combustion engine, and a combustion sent to the intake passage. A combustor that generates gas, an exhaust pipe that communicates the combustor and the intake passage, and sends the combustion gas to the intake passage; and a wall surface of the intake passage, the combustion gas from the exhaust pipe An intake control device for an internal combustion engine, and a jet outlet that jets in the direction of the cylinder along the wall surface of the intake passage, and the combustion gas flows in the intake passage at a faster speed than the combustion air, In this configuration, a vortex flow is generated in the cylinder.

  Preferably, as described in claim 2, the intake passage communicates with the cylinder through two or more intake ports, and the ejection port is connected to only one of the two or more intake ports. Combustion gas should be ejected.

  Preferably, as described in claim 3, the jet port is provided on a side of the wall surface of the intake passage facing the cylinder side.

  Preferably, as described in claim 4, the ejection port may eject the combustion gas to the outside of a region located between the central axes of two or more intake ports.

  Preferably, as described in claim 5, the combustor is pulse jet combustion.

  According to the first aspect of the invention, the flow of the air (combustion air) in the cylinder can be biased by the ejection of the combustion gas, and a vortex is generated in the cylinder. Since the pressure of the combustion gas can be controlled by changing the amount of combustion in the combustor, the flow rate of the desired combustion gas ejected toward the cylinder becomes variable, and the strength of the vortex generated in the cylinder can be controlled by the internal combustion engine. It can be controlled more freely according to the driving state.

  Also, the combustor rise time is shorter than the compressor rise time, and the combustion gas can be generated continuously, so that the required vortex flow can be generated more suitably in the cylinder according to the operating state of the internal combustion engine.

  As described above, the apparatus according to the present invention further promotes mixing of air (combustion air) and fuel in the cylinder in various operating states of the internal combustion engine by generating a vortex flow in the cylinder by the combustion gas. It is possible to improve combustion in the internal combustion engine.

  According to the second aspect of the present invention, since a flow velocity difference of air is generated between the intake ports, a swirl flow is generated in the cylinder. Thereby, the combustion in a cylinder is accelerated | stimulated and the combustion improvement in an internal combustion engine can further be aimed at.

  According to the third aspect of the present invention, since a difference in air flow velocity occurs between the cylinder side and the opposite side in the intake passage, a tumble flow is generated in the cylinder. Thereby, the combustion in a cylinder is accelerated | stimulated and the combustion improvement in an internal combustion engine can further be aimed at.

  According to the fourth aspect of the present invention, since the combustion gas ejected from the ejection port causes a strong bias due to the air flow in the cylinder, a stronger swirl flow is generated in the cylinder. Thereby, the combustion in a cylinder is accelerated | stimulated and the combustion improvement in an internal combustion engine can further be aimed at.

  According to the invention described in claim 5, since higher pressure combustion gas is generated by pulse jet combustion, the flow velocity of the combustion gas injected toward the cylinder is higher than that in the case of continuous combustion, and a stronger vortex flow is generated in the cylinder. Generated within. Thereby, the combustion in a cylinder is accelerated | stimulated and the combustion improvement in an internal combustion engine can further be aimed at.

  Hereinafter, embodiments for carrying out the present invention will be described with reference to the drawings.

(First embodiment)
FIG. 1 is a schematic view of an engine 1 provided with an intake air control device 20 according to the present invention.

  The engine 1 (internal combustion engine) is a known four-cylinder engine having two valves per cylinder, and includes an intake pipe 2, a throttle body 3, an intake manifold 4, an injector 5, an intake port 6, an engine body 7, and the like. Prepare. The engine body 7 is provided with a cylinder 8. The air sucked into the intake pipe 2 is sent to the intake manifold 4 through the throttle body 3. The air (combustion air) sent to the intake manifold 4 is mixed with fuel injected from the injector 5 at the intake port 6 and sent to the cylinder 8. The intake pipe 2, the throttle body 3, the intake manifold 4, and the intake port 6 constitute an intake passage 30 in the present invention. In the first embodiment, the intake passage 30 communicates with the cylinder 8 through one intake port 6.

  The engine 1 further includes a combustor 9 and an exhaust pipe 10. The combustor 9 generates combustion gas by burning fuel. The exhaust pipe 10 communicates the combustor 9 with the intake passage 30 and sends the combustion gas generated in the combustor 9 to the intake passage 30.

  FIG. 2 is a diagram showing a main part of the intake control device 20. 3 is a cross-sectional view taken along line III-III in FIG. The intake control device 20 includes an intake passage 30, a combustor 9, an exhaust pipe 10, and an ejection port 11.

  The intake passage 30 includes a passage 31 and an intake port 6. The passage 31 is provided at the outlet 41 of the intake manifold 4. An outlet 41 of the intake manifold 4 is attached to the engine body 7. The intake port 6 is provided in the engine body 7 continuously with the passage 31 and communicates with the cylinder 8. The intake port 6 is opened and closed by an intake valve 71 provided in the engine body 7. The intake port 6 passes the air 14 (combustion air) sent to the intake manifold 4 (passage 31) through the intake pipe 2 and the throttle body 3 (see FIG. 1) together with the fuel 51 injected from the injector 5. It feeds into the cylinder 8.

  The combustor 9 generates combustion gas by burning fuel. As the combustor 9, for example, a pulse jet combustor that intermittently generates high-pressure combustion gas by pulse jet combustion can be used. Air used in the combustor 9 is supplied from the intake pipe 2 via the pump 12 and the pipe 13 (see FIG. 1). The fuel used in the combustor 9 may be the same as the fuel of the engine 1 or may be a dedicated fuel different from the fuel of the engine 1.

  The exhaust pipe 10 communicates the combustor 9 with the intake passage 30 and sends the combustion gas generated in the combustor 9 to the intake passage 30. The exhaust pipe 10 should be as short as possible to reduce the pressure loss of the combustion gas.

  The ejection port 11 is provided on the wall surface 32 of the intake passage 30 (passage 31). The spout 11 is provided not on the cylinder side 33 but on the side 34 facing the cylinder side of the wall surface 32 of the passage 31. The ejection port 11 ejects combustion gas from the exhaust pipe 10 in the direction of the cylinder 8 (toward the cylinder 8) along the wall surface 32 of the passage 31 and the wall surface 6 a of the intake port 6. The combustion gas 15 ejected from the ejection port 11 flows in the intake passage 30 (passage 31, intake port 6) at a speed faster than the air 14 (combustion air) sent into the cylinder 8, The flow is biased and a vortex 16 is generated in the cylinder 8.

  In addition, as shown in FIG. 4, the spiral groove | channel is formed in the internal peripheral surface of the jet nozzle 11, and the speed (flow velocity) at which the combustion gas 15 is jetted from the jet nozzle 11 can also be improved.

(Second Embodiment)
Next, a second embodiment of the intake control device 20 according to the present invention will be described with reference to FIGS. Detailed description of points common to the first embodiment will be omitted.

  FIG. 5 is a diagram illustrating a second embodiment of the intake air control device 20, and corresponds to FIG. 1 of the first embodiment.

  The engine 1 (internal combustion engine) is a known four-cylinder engine having four valves per cylinder. The air sucked into the intake pipe 2 is sent to the intake manifold 4 through the throttle body 3. The air (combustion air) sent to the intake manifold 4 is mixed with fuel injected from the injector 5 at the intake port 6 and sent to the cylinder 8. The intake pipe 2, the throttle body 3, the intake manifold 4, and the intake port 6 constitute an intake passage 30 in the present invention. In the second embodiment, the intake passage 30 communicates with the cylinder 8 via the two intake ports 6 and 6.

  The engine 1 further includes a combustor 9 and an exhaust pipe 10. The combustor 9 generates combustion gas by burning fuel. The exhaust pipe 10 communicates the combustor 9 with the intake passage 30 and sends the combustion gas generated in the combustor 9 to the intake passage 30.

  FIGS. 6 and 7 are views showing a second embodiment of the intake air control device 20 and corresponding to FIG. 3 of the first embodiment.

  The ejection port 11 ejects the combustion gas from the exhaust pipe 10 along the wall surface 6 a of the intake port 6 in the direction of the cylinder 8 (toward the cylinder 8). The ejection port 11 ejects combustion gas only to one of the two intake ports 6 and 6 (the left intake port 6 in FIGS. 6 and 7). The combustion gas ejected from the ejection port 11 flows in the intake port 6 at a faster speed than the air (combustion air) sent into the cylinder 8, causing the flow in the cylinder 8 to be biased, and in the cylinder 8. Generate eddy currents. In the example of FIG. 7, the ejection port 11 ejects combustion gas to the outside of the region 6 c located between the central axes 6 b and 6 b of the two intake ports 6 and 6.

  The intake control device 20 according to the present invention generates a vortex 16 in the cylinder 8 by ejecting the combustion gas generated in the combustor 9 into the intake port 6. Since the pressure of the combustion gas can be controlled by changing the strength of combustion in the combustor 9, the flow velocity of the combustion gas 15 ejected from the ejection port 11 is variable, and the strength of the vortex 16 generated in the cylinder 8 is increased. This can be controlled more freely according to the operating state of the engine 1.

  Further, the rise time of the combustor 9 (the time until the combustion gas is generated after the start of operation) is shorter than the rise time of the compressor, and the combustion gas can be continuously generated. The required vortex flow 16 can be generated more suitably in the cylinder 8.

  As described above, the intake control device 20 according to the present invention generates the vortex 16 in the cylinder 8 by the combustion gas, so that the air in the cylinder 8 (combustion air) in various operating states of the engine 1. And fuel can be further promoted, and combustion in the engine 1 can be further improved.

  Further, in the intake air control device 20 according to the present invention, since a high-temperature inert gas called combustion gas flows into the cylinder 8, NOx reduction (EGR effect), combustion improvement at cold start, and warm-up effect of the engine 1 Is obtained.

  Furthermore, as shown in FIG. 3, when the outlet 11 from which the combustion gas is ejected is provided on the side 34 facing the cylinder side of the wall surface 32 of the intake passage 30, Since a difference in air flow velocity occurs between the opposite sides, a tumble flow is generated in the cylinder 8. Thereby, combustion in the cylinder 8 is promoted, and combustion in the engine 1 can be further improved.

  Further, as shown in FIGS. 5 to 7, the intake passage 30 communicates with the cylinder 8 through the two intake ports 6, 6, and the ejection port 11 burns only in one of the two intake ports 6, 6. When gas is ejected, a flow velocity difference of air is generated between the two intake ports 6, 6, so that a swirl flow is generated in the cylinder 8. Thereby, combustion in the cylinder 8 is promoted, and combustion in the engine 1 can be further improved. If the ejection port 11 is arranged as shown in FIG. 7, the combustion gas ejected from the ejection port 11 causes a strong bias due to the air flow in the cylinder 8, so that a stronger swirl flow is generated in the cylinder 8. The

 Further, when the combustor 9 is a pulse jet combustor, higher-pressure combustion gas is generated by pulse jet combustion, and the flow velocity of the combustion gas 15 ejected toward the cylinder 8 is further increased. As a result, a stronger vortex 16 is generated in the cylinder 8, combustion in the cylinder 8 is promoted, and combustion in the engine 1 can be further improved.

1 is a schematic diagram of an engine 1 including an intake control device 20 according to the present invention. The figure which shows the principal part of the intake control apparatus. Sectional drawing which follows the III-III line in FIG. The figure which shows the modification of the jet nozzle 11. FIG. The figure which shows 2nd Embodiment of the intake control apparatus. The figure which shows 2nd Embodiment of the intake control apparatus. The figure which shows 2nd Embodiment of the intake control apparatus.

Explanation of symbols

1 engine (internal combustion engine)
6 Intake port 6b Center shaft 6c Region 8 Cylinder 9 Combustor 10 Exhaust pipe 11 Jet port 14 Air (combustion air)
15 Combustion gas 16 Swirl 20 Intake control device (intake device for internal combustion engine)
30 Intake passage 32 Wall surface 33 Cylinder side 34 The side opposite to the cylinder side

Claims (5)

An intake passage for sending combustion air into the cylinder of the internal combustion engine;
A combustor for generating combustion gas sent to the intake passage;
An exhaust pipe that communicates the combustor and the intake passage and sends the combustion gas to the intake passage;
A jet port provided on a wall surface of the intake passage, and jetting the combustion gas from the exhaust pipe along the wall surface of the intake passage in the direction of the cylinder,
The intake control apparatus for an internal combustion engine, wherein the combustion gas flows in the intake passage at a speed higher than that of the combustion air, and generates a vortex flow in the cylinder.   The intake passage communicates with the cylinder via two or more intake ports, and the jet port ejects the combustion gas only to one of the two or more intake ports. Item 2. An intake control device for an internal combustion engine according to Item 1.   2. The intake control device for an internal combustion engine according to claim 1, wherein the ejection port is provided on a side of the wall surface of the intake passage facing the cylinder side.   The intake control device for an internal combustion engine according to claim 2, wherein the ejection port ejects the combustion gas to the outside of a region located between the central axes of two or more intake ports.   The intake control device for an internal combustion engine according to any one of claims 1 to 4, wherein the combustor is pulse jet combustion.

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