US20090126668A1

US20090126668A1 - Internal combustion engine electric discharge structure

Info

Publication number: US20090126668A1
Application number: US12/269,948
Authority: US
Inventors: Taisuke Shiraishi; Eiji Takahashi; Tomonori Urushihara
Original assignee: Nissan Motor Co Ltd
Current assignee: Nissan Motor Co Ltd
Priority date: 2007-11-16
Filing date: 2008-11-13
Publication date: 2009-05-21
Also published as: EP2060780B1; EP2060780A3; JP2009121406A; EP2060780A2; JP5228450B2

Abstract

An internal combustion engine electric discharge structure is provided which comprises a first electrode and a dielectric material. The first electrode includes a first voltage receiving end and a second engine attachment end with a long thin conductive material that discharges non-equilibrium plasma. The dielectric material covers the first electrode.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims priority to Japanese Patent Application No. 2007-298294, filed on Nov. 16, 2007. The entire disclosure of Japanese Patent Application No. 2007-298294 is hereby incorporated herein by reference.

BACKGROUND OF THE INVENTION

1. Field of the Invention
The present invention generally relates to an internal combustion engine electric discharge structure. More specifically, the present invention relates to an electric discharge structure which discharges non-equilibrium plasma in order to increase a number of radicals and thereby improve autoignition properties of the internal combustion engine.
2. Background Information
An electric discharge device has been proposed for an internal combustion engine in which the air-fuel mixture is ignited in an assisted manner by a sparkplug. In this electric discharge device radicals are generated in a cylinder and the autoignition properties of the air-fuel mixture are improved (see, Japanese Laid-Open Patent Application No. 2001-20842). The radicals tend to induce oxidation reactions (i.e., combustion), and the oxidation reactions (combustion) tend to become chain reactions. Therefore, when radicals are generated in the cylinder, the autoignition properties of the air-fuel mixture are improved.
In view of the above, it will be apparent to those skilled in the art from this disclosure that there exists a need for an improved internal combustion engine electric discharge structure. This invention addresses this need in the art as well as other needs, which will become apparent to those skilled in the art from this disclosure.

SUMMARY OF THE INVENTION

As mentioned above, it has been discovered that, in order to improve the autoignition properties of the air-fuel mixture, a sparkplug can be used to generate radicals in the cylinder. However, since spark ignition is a thermal plasma discharge, the efficiency of radical generation is low even if spark ignition is induced by a sparkplug as in the conventional apparatus previously described. Moreover, in this conventional apparatus the amount of radicals generated is limited. It is therefore believed that the effects of improving the autoignition properties are small.
The present invention was designed in view of such conventional problems. One object of the present invention is to provide an electric discharge structure which is used in an internal combustion engine and which can improve the autoignition properties of an air-fuel mixture beyond that of conventional practice, and to provide a method for controlling the operation of the internal combustion engine.
In accordance with a first aspect, an internal combustion engine electric discharge structure is provided which basically comprises a first electrode and a dielectric material. The first electrode includes a first voltage receiving end and a second engine attachment end with a long thin conductive material that discharges non-equilibrium plasma. The dielectric material covers the first electrode.
These and other objects, features, aspects and advantages of the present invention will become apparent to those skilled in the art from the following detailed description, which, taken in conjunction with the annexed drawings, discloses preferred embodiments of the present invention.

BRIEF DESCRIPTION OF THE DRAWINGS

Referring now to the attached drawings which form a part of this original disclosure:

FIG. 1 is a simplified schematic cross-sectional view of a portion of a multi-link engine that is part of an electric discharge structure in accordance with a first embodiment;

FIG. 2A is a partial cross-sectional view of the electric discharge structure of the engine shown in FIG. 1;

FIG. 2B is a cross-sectional view of the electric discharge structure illustrated in FIG. 2A, taken along section line 2B-2B of FIG. 2A;

FIG. 3A is a diagram showing the electric discharges obtained when an AC voltage (electric potential) is applied to a spark ignition discharge mechanism in accordance with a comparative example of a conventional discharge mechanism;

FIG. 3B is a diagram showing the electric discharges obtained when an AC voltage (electric potential) is applied to the electric discharge structure in accordance with the first illustrated embodiment;

FIG. 4 is a diagram showing various methods for increasing the discharge energy of the electric discharge structure;

FIG. 5 is a graph showing the problems with forming non-equilibrium plasma by the application of short pulses in accordance with a comparative example of a conventional discharge mechanism;

FIG. 6A is a simple link diagram showing the arrangement of a multi-link variable compression ratio mechanism at a high compression ratio;

FIG. 6B is a simple link diagram showing the arrangement of the multi-link variable compression ratio mechanism at a low compression ratio;

FIG. 6C is a simple link diagram showing the method for varying the compression ratio using the multi-link variable compression ratio mechanism;

FIG. 7 is a perspective view of a variable valve timing mechanism for adjusting the opening and closing timing of a valve;

FIG. 8A is a simplified elevational view of the variable valve timing mechanism when valves are in a closed state;

FIG. 8B is a simplified elevational view of the variable valve timing mechanism when the valves are in a state of maximum lift;

FIG. 8C is a simplified elevational view showing the variable valve timing mechanism when the stroke amount of cam followers is minimized, cam noses are at the highest position, and the valves are in a closed state;

FIG. 8D is a simplified elevational view of the variable valve timing mechanism when the stroke amount of cam followers is minimized, the cam noses are at the lowest position, and the valves are in a closed state;

FIG. 9 is a graph showing the valve lift amount and the opening and closing timings in the variable valve timing mechanism;

FIG. 10A is a graph showing the relationship of an air-fuel ratio to various operational states of the engine having the electric discharge structure in accordance with the first embodiment;

FIG. 10B is a graph showing the relationship of a barrier discharge start timing to various operational states of the engine having the electric discharge structure in accordance with the first embodiment;

FIG. 10C is a graph showing the relationship of discharge energy to various operational states of the engine having the electric discharge structure in accordance with the first embodiment;

FIG. 10D is a graph showing the relationship of an intake valve close timing to various operational states of the engine having the electric discharge structure in accordance with the first embodiment;

FIG. 10E is a graph showing the relationship of a mechanical compression ratio to various operational states of the engine having the electric discharge structure in accordance with the first embodiment;

FIG. 11 is a graph showing the variation in the heat generation rate depending on if and when the barrier discharge start timing begins;

FIG. 12A is a drawing schematically depicting the state in which radicals are distributed within the cylinder when barrier discharge does not occur;

FIG. 12B is a drawing schematically depicting the state in which radicals are distributed within the cylinder when barrier discharge is initiated during compression stroke;

FIG. 12C is a drawing schematically depicting the state in which radicals are distributed within the cylinder when barrier discharge is initiated during intake stroke;

FIG. 13 is a graph showing the relationship between the barrier discharge start timing and the crank angle at which the mass combustion ratio is 50%;

FIG. 14 is a graph showing the piston behavior in a multi-link variable compression ratio mechanism;

FIG. 15 is a graph showing the relationship between the air-fuel ratio and combustion stability;

FIG. 16 is a graph showing the problems due to the heat generation rate suddenly increasing to an excessive degree, and the effects of the illustrated embodiment;

FIG. 17A is a graph showing the correlation between an air-fuel ratio and a fluctuation rate of the depicted average effective pressure;

FIG. 17B is a graph showing that a fuel consumption rate can be reduced if a lean combustion limit is expanded;

FIG. 18 is a simplified schematic cross-sectional view of a portion of an engine that is part of an electric discharge structure in accordance with a second embodiment;

FIG. 19 is a simplified schematic cross-sectional view of a portion of the engine showing the manner in which fuel is injected into the engine in accordance with the second embodiment;

FIG. 20A is a graph showing the relationship of an air-fuel ratio to various operational states of the engine having the electric discharge structure in accordance with the second embodiment;

FIG. 20B is a graph showing the relationship of a barrier discharge start timing to various operational states of the engine having the electric discharge structure in accordance with the second embodiment;

FIG. 20C is a graph showing the relationship of discharge energy to various operational states of the engine having an electric discharge structure in accordance with the second embodiment;

FIG. 20D is a graph showing the relationship of an intake valve close timing to various operational states of the engine having an electric discharge structure in accordance with the second embodiment;

FIG. 20E is a graph showing the relationship of a mechanical compression ratio to various operational states of the engine having an electric discharge structure in accordance with the second embodiment;

FIG. 21 is a partial cross-sectional view showing the operational configuration of the engine having an electric discharge structure in accordance with a third embodiment;

FIG. 22A is a partial cross-sectional view showing the operational configuration of the engine having an electric discharge structure in accordance with a fourth embodiment where a barrier discharge is formed within a combustion chamber;

FIG. 22B is a partial cross-sectional view showing the operational configuration of the engine having an electric discharge structure in accordance with a fourth embodiment where a barrier discharge is formed within a concave part of a top surface of a piston;

FIG. 23A is a partial cross-sectional view showing the operational configuration of the engine having an electric discharge structure in accordance with a fifth embodiment where a barrier discharge is formed within a combustion chamber;

FIG. 23B is a partial cross-sectional view showing the operational configuration of the engine having an electric discharge structure in accordance with a fifth embodiment where a barrier discharge is formed within a concave part of a top surface of a piston;

FIG. 24A is a diagram showing a waveform of an alternating current as a sine curve applied to the electric discharge structure; and

FIG. 24B is a diagram showing a waveform of an alternating current as a bipolar multiple pulse applied to the electric discharge structure.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

Selected embodiments of the present invention will now be explained with reference to the drawings. It will be apparent to those skilled in the art from this disclosure that the following descriptions of the embodiments of the present invention are provided for illustration only and not for the purpose of limiting the invention as defined by the appended claims and their equivalents.
First, the essential technological ideas relating to the internal combustion engine electric discharge structure will be described.
As described above, an engine has been proposed in which spark ignition generates radicals (chemically active species which are in a state wherein molecular dissociation is induced by the collision of high-energy electrons with fuel or air molecules, and which promote ignition of an air-fuel mixture) in a cylinder and in which the autoignition properties (compression ignition properties) of the air-fuel mixture are improved.
However, the effects of improving ignition properties in such an engine have been small. Specifically, spark ignition involves a thermal plasma discharge. In a thermal plasma discharge, kinetic energy is adequately exchanged among electrons, ions, and molecules. The result is an establishment of a state of thermal equilibrium in which the electron energy, the ion energy, and the neutral particle energy are in equilibrium with each other. Radicals are chemically active species which are in a state wherein molecular dissociation is induced by collisions of high-energy electrons with fuel or air molecules, and which promote ignition of the air-fuel mixture. In spark ignition, energy is also imparted to ions and molecules which do not contribute to the generation of radicals, and the efficiency of conversion of input energy to electron energy is low. When the input energy is increased in order to increase the amount of radicals, there is a possibility that the electrodes will melt. Therefore, it is difficult to increase the amount of radicals.
In view of this, a non-equilibrium plasma discharge is preferred. In a non-equilibrium plasma discharge, a thermally non-equilibrium state is achieved in which the electron temperature (electron energy) alone is extremely high (specifically, electron energy is much higher than ion energy and ion energy is equal to neutral particle energy), and the efficiency of converting input energy to electron energy is high. Heat loss is small in a non-equilibrium plasma discharge because the gas temperature is not increased. The danger that the electrodes will melt is also small.
Because of such reasons, radicals can be generated comparatively easily if a non-equilibrium plasma discharge is used. In view of this, a non-equilibrium plasma discharge mechanism for an engine is proposed herein. To conduct a non-equilibrium plasma discharge, possibilities include methods using a barrier discharge and methods using short pulse application. It has been discovered that of these methods, a barrier discharge is particularly preferable.
Now referring to FIG. 1, a simplified schematic cross-sectional view of a portion of a multi-link engine 1 is illustrated that forms a part of an electric discharge structure in accordance with a first embodiment. As explained hereinafter, the multi-link engine 1 utilizes a non-equilibrium plasma discharge function, preferably barrier discharge, to improve the autoignition properties of the multi-link engine 1.
The engine 1 is provided with a barrier discharge device 70. The barrier discharge device 70 is provided between an intake port 60 a and an exhaust port 60 b, substantially in the center of a combustion chamber of a cylinder head. The barrier discharge device 70 generates radicals through barrier discharge, which is a non-equilibrium plasma discharge. The barrier discharge device 70 is also capable of igniting an air-fuel mixture through barrier discharge at a comparatively high load (when the air-to-fuel ratio of the air-fuel mixture is comparatively rich). The detailed structure of the barrier discharge device 70 will be described hereinafter with reference to an enlarged view (FIG. 2).
The engine 1 having a barrier discharge function according to the present embodiment has a variable compression ratio mechanism (hereinafter referred to as a “multi-link variable compression ratio mechanism”), which uses a multi-link mechanism for connecting a piston 32 to a crankshaft 33 by two links. The multi-link variable compression ratio mechanism connects the piston 32 to the crankshaft 33 by an upper (first) link 11 and a lower (second) link 12. The multi-link variable compression ratio mechanism also controls the lower link 12 by using a control (third) link 13 to vary the mechanical compression ratio.
The upper link 11 is connected at the top end to the piston 32 via a piston pin 21. The upper link 11 is connected at the bottom end to one end of the lower link 12 via a connecting pin 22. The piston 32 receives combustion pressure that moves the piston 32 within a cylinder 31 a of a cylinder block 31 back and forth.
The lower link 12 is connected at one end to the upper link 11 via the connecting pin 22. The lower link 12 is connected at the other end to the control link 13 via a connecting pin 23. The lower link 12 also has a substantially central connecting hole in which crank pins 33 b of the crankshaft 33 are disposed. Thus, the lower link 12 oscillates around the crank pins 33 b as a center axis. The lower link 12 is divided into two left and right members. The crankshaft 33 comprises a plurality of crank journals 33 a and a plurality of crank pins 33 b for each cylinder. The journals 33 a are rotatably supported by the cylinder block 31 and a ladder frame 34. The crank pins 33 b are eccentric relative to the crank journals 33 a by a predetermined amount, and the lower link 12 is oscillatably connected thereto.
The control link 13 is connected to the lower link 12 via the connecting pin 23. The control link 13 is also connected at the other end to a control shaft 25 via a connecting pin 24. The control link 13 oscillates or rocks around the connecting pin 24. A gear is formed on the control shaft 25, and this gear meshes with a pinion 53 provided to a rotating axle 52 of an actuator 51. The control shaft 25 is rotated by the actuator 51 to move the connecting pin 24.
Various sensors are provided for sensing the operating state of the engine, including the engine rotation speed and the engine load. The signals of various sensors are inputted to a controller 90. The controller 90 controls the actuator 51 to rotate the control shaft 25 and vary the compression ratio. The controller 90 also controls a high-voltage high-frequency generator 80 so that the AC voltage value, the application duration, the AC frequency, the application timing, and other parameters corresponding to the operating state of the engine are applied. Thus, the controller 90 may be considered to constitute a non-equilibrium plasma discharge control unit. In addition, the high-voltage high-frequency generator 80 constitutes a voltage application device. Furthermore, the controller 90 controls the fuel injection of a fuel injection valve 65 provided to the intake port 60 a. An intake valve 61 is capable of varying the opening and closing timings thereof, as is described hereinafter. The controller 90 determines the engine load and performs control according to the load. The controller 90 is configured from a microcomputer comprising a central processing unit (CPU), a read-only memory (ROM), a random access memory (RAM), and an input/output interface (I/O interface). The controller 90 can also be configured from a plurality of microcomputers.
FIGS. 2A and 2B contain enlarged cross-sectional views of the barrier discharge device 70. The barrier discharge device 70 of the illustrated embodiment discharges non-equilibrium plasma by using a barrier discharge. Non-equilibrium plasma can also be formed by applying a short pulse instead of forming a barrier discharge, but barrier discharge is preferred in the illustrated embodiment. The reasons for this are described hereinafter.
The barrier discharge device 70 comprises a central electrode 71 and a tubular electrode 72. The central electrode 71 is a rod-shaped electrical conductor. The entire periphery of the central electrode 71 is covered by a dielectric material (insulating material) 73. The central electrode 71 is connected to the high-voltage high-frequency generator 80 via a terminal 71 a. An AC voltage is applied to the central electrode 71 upon being generated by the high-voltage high-frequency generator 80. The value, application duration, AC frequency, application timing, and other characteristics of the AC voltage are controlled (set) according to the operating state of the engine 1,
The tubular electrode 72 is a tubular electrical conductor. The tubular electrode 72 is attached to the cylinder head. The inner periphery side of the tubular electrode 72 is a discharge chamber 72 a. The central electrode 71 protrudes into the discharge chamber 72 a. The central electrode 71 is provided on the top side of the substantial center of the fuel chamber. The center of the central electrode is substantially parallel to a line extending through the center of the fuel chamber. The distance from the central electrode 71 to the dielectric material and the distance from the dielectric material to the tubular electrode 72 are set to be substantially the same.
When an AC voltage is applied to the central electrode 71 from the high-voltage high-frequency generator 80, streamers S are generated between the tubular electrode 72 and the dielectric material 73 as shown in FIG. 2A. A plurality of streamers S is generated in the vertical direction as shown in FIG. 2A. The streamers are branched into thin streaks, and FIG. 2A shows a state in which six streamers are generated on both the right and left sides of the dielectric material 73. The streamers are also formed in a radial pattern about the dielectric material 73, as shown in FIG. 2B. FIG. 2B shows a state in which twelve streamers are formed in a radial pattern about the dielectric material 73. The barrier discharge device 70 can generate a large amount of radicals in the discharge chamber 72 a by forming a plurality of streamers S. It is also possible for multipoint simultaneous ignition, i.e., a volumetric ignition (hereinafter referred to as “volume ignition”), to occur within the discharge chamber.
The barrier discharge device 70 can perform multiple electric discharges within a predetermined time, whereby a large amount of radicals can be generated in the discharge chamber 72 a. This will be described with reference to FIGS. 3A and 3B. FIGS. 3A and 3B contain views showing the electric discharge obtained when an AC voltage (electric potential) is applied. FIG. 3A is a diagram showing the electric discharges obtained when an AC voltage (electric potential) is applied by a spark ignition discharge mechanism in accordance with a comparative example of a conventional discharge mechanism. FIG. 3B is a view showing the electric discharges obtained when an AC voltage (electric potential) is applied by the electric discharge structure in accordance with the illustrated embodiment.
First, as a comparison, a case will be described in which an AC voltage is applied to the spark ignition discharge mechanism of a conventional sparkplug. In cases in which an AC voltage is applied to the sparkplug, an arc discharge occurs between the electrodes when the absolute value of an electric potential V₀formed between the electrodes by the applied voltage reaches a discharge voltage (insulation breakdown electric potential) Va, as shown in FIG. 3A. Arc discharge similarly occurs when the polarity is inverted. With this sparkplug, four arc discharges occur within the discharge time t as shown in FIG. 3A. A discharge takes place in one location, and the form of the discharge is either point or linear.
In the barrier discharge device 70, the dielectric material (insulating material) 73 covers the central electrode 71. The dielectric material 73 acts as a capacitor. After a barrier discharge (non-equilibrium plasma discharge) has occurred, an electric charge is accumulated on the surface of the dielectric material 73. The barrier discharge (non-equilibrium plasma discharge) occurs between the dielectric material 73 and the tubular electrode 72 when the absolute value of the difference between the electric potential V₀created by the applied voltage and the electric potential Vw created by the surface electric charge of the dielectric material 73 reaches a discharge voltage Vd, as shown in FIG. 3B. Therefore, streamers S are formed at a plurality of locations in the discharge chamber 72 a in the barrier discharge device 70, and eight barrier discharges (non-equilibrium plasma discharges) occur within the discharge time t, as shown in FIG. 3B.
Thus, the barrier discharge device 70 can increase the number of discharges in the same time (discharge time t) to a greater level than that obtained with a sparkplug in a conventional method.
Though not shown in the drawings, increasing the voltage value of the AC voltage in the barrier discharge device 70 also makes more likely that the absolute value of the difference between the electric potential V₀created by the applied voltage and the electric potential Vw created by the surface electric charge of the dielectric material 73 will reach the discharge voltage Vd, and makes it possible to increase the number of discharges.
FIG. 4 is a diagram showing various methods for increasing the discharge energy of the electric discharge structure.
The discharge energy of the barrier discharge device 70 is controlled by the voltage value, application duration, and AC frequency of the AC voltage from the high-voltage high-frequency generator 80. One possibility for increasing the discharge energy of the barrier discharge device 70 is a method for increasing the voltage value of the AC voltage in the manner shown in plot (B-1) of FIG. 4 relative to the waveform of a reference AC applied voltage (plot (A) of FIG. 4). The discharge energy of the barrier discharge part can also be increased by increasing the frequency of the AC voltage, the applied duration as in plot (B-2) of FIG. 4, or the AC frequency as in plot (B-3) of FIG. 4.
As described above, another method for forming non-equilibrium plasma aside from initiating a barrier discharge is a method for forming non-equilibrium plasma by applying a short pulse between the electrodes and blocking the electric potential before the transition to an arc discharge. However, a barrier discharge is preferred in the illustrated embodiment. The reasons for this are described with reference to FIG. 5 which is a graph showing the problems with forming non-equilibrium plasma by the application of short pulses in accordance with a comparative example of a conventional discharge mechanism.
To form non-equilibrium plasma by the application of short pulses, the required voltage (electric potential) corresponding to the discharge location (density, air-fuel mixture composition, and the like) must be applied. Non-equilibrium plasma is generated if the voltage V1 is applied at a pressure P0, but when the voltage V2 is applied, thermal plasma is generated, as shown in FIG. 5. Thus, non-equilibrium plasma or thermal plasma is generated merely by slight variations in the applied voltage, and the discharge lacks robustness with short pulse application.
By contrast, with a barrier discharge, the electrodes are originally covered on one side with a dielectric material, and the voltage is kept substantially within a range that extends from the discharge start voltage (lower limit of voltage) to a voltage at which the withstand-voltage properties of the dielectric material can be ensured (upper limit of voltage), whereby non-equilibrium plasma can always be maintained regardless of the voltage. An arc transition does not take place because the electrodes are covered by a dielectric material. Thus, discharge robustness is high. In an internal combustion engine, the potential required for a discharge varies extensively, and it is difficult to form non-equilibrium plasma by the application of short pulses. Therefore, non-equilibrium plasma based on a barrier discharge is preferable for application in an internal combustion engine.
FIGS. 6A-6C are simple link diagrams showing the arrangement of a multi-link variable compression ratio mechanism. With a multi-link variable compression ratio mechanism, the mechanical compression ratio can be varied by rotating the control shaft 25 and varying the position of the connecting pin 24. For example, if the connecting pin 24 is at position A as shown in FIG. 6C, the top dead center (TDC) is at a high level, resulting in a high compression ratio. If the connecting pin 24 is at position B as shown in FIGS. 6B and 6C, the control link 13 is pushed upward, and the position of the connecting pin 23 rises. The lower link 12 is thereby rotated counterclockwise around the crank pins 33 b, the connecting pin 22 moves down, and the piston 32 in the piston top dead center (TDC) moves to a lower position. Therefore, the compression ratio is low.
FIG. 7 is a perspective view showing a variable valve timing mechanism for adjusting the opening and closing timing of a valve. The engine 1 having a barrier discharge function comprises a variable valve timing mechanism 200. The mechanism disclosed, for example, in Japanese Laid-Open Patent Application No. 11-107725 can be used as the variable valve timing mechanism 200. This is described with reference to the drawings.
The variable valve timing mechanism 200 comprises a camshaft 210, a link arm 220, a valve lift control shaft 230, a rocker arm 240, a link member 250, and oscillating cams 260. Cam followers 63 are pushed by the oscillation of the oscillating cams 260, thus opening and closing valves (intake valves) 61.
The camshaft 210 is rotatably supported at the top part of the cylinder head along the longitudinal direction of the engine. One end of the camshaft 210 is inserted through a cam sprocket 270. The cam sprocket 270 is rotated by the transmission of torque from a crank axle of the engine. The camshaft 210 rotates together with the cam sprocket 270. The camshaft 210 can rotate relative to the cam sprocket 270 by hydraulic pressure, and the phase of the camshaft 210 relative to the cam sprocket 270 can be varied. This type of structure makes it possible to vary the rotational phase of the camshaft 210 relative to the crank axle. A cam 211 is fixed to the camshaft 210. The cam 211 rotates integrally with the camshaft 210. The pair of oscillating cams 260 connected by pipes is inserted through the camshaft 210. The oscillating cams 260 oscillate around the camshaft 210 as a rotational center, and the cam followers 63 perform a stroke.
The link arm 220 is supported by the insertion of the cam 211. The valve lift control shaft 230 is disposed parallel to the camshaft 210. A cam 231 is formed integrally on the valve lift control shaft 230. The valve lift control shaft 230 is controlled by an actuator 280 so as to rotate within a predetermined range of rotational angles.
The rocker arm 240 is supported by the insertion of the cam 231 and is connected to the link arm 220. The link member 250 is connected to the rocker arm 240.
The camshaft 210 is inserted through the oscillating cams 260, which can oscillate around the camshaft 210. The oscillating cams 260 are connected to the link member 250. The oscillating cams 260 move up and down, pushing down on the cam followers 63 and opening and closing the valves 61.
Next, the action of the variable valve timing mechanism 200 will be described with reference to FIGS. 8A-8D.
FIGS. 8A and 8B are views showing the manner in which the stroke amount of the cam followers 63 is maximized to maximize the lift amount of the valves 61. FIG. 8A shows the manner in which cam noses 262 are at their highest positions, and the oscillation direction of the oscillating cams 260 is inverted. At this time, the cam followers 63 are at top end positions, and the valves 61 are in a closed state. FIG. 8B shows the manner in which the cam noses 262 are at their lowest positions, and the oscillation direction of the oscillating cams 260 is inverted. At this time, the cam followers 63 are at bottom end positions, and the valves 61 are in a state of maximum lift.
FIGS. 8C and 8D are views showing the manner in which the stroke amount of the cam followers 63 is minimized. FIG. 8C shows the manner in which the cam noses 262 are at their highest positions and the oscillating direction of the oscillating cams 260 is inverted. FIG. 8D shows the manner in which the cam noses 262 are at their lowest positions and the oscillation direction of the oscillating cams 260 is inverted. In the present embodiment, the stroke amount of the cam followers 63 is zero, and the lift amount of the valves 61 is also zero. Therefore, in FIGS. 8C and 8D, the valves 61 are always in a closed state regardless of the action of the oscillating cams 260.
To increase the stroke amount of the cam followers 63 and the lift amount of the valves 61, the valve lift control shaft 230 is rotated to lower the position of the cam 231 and to set the axial center P1 below the axial center P2, as shown in FIGS. 8A and 8B. The entire rocker arm 240 is thereby moved downward.
When the camshaft 210 is rotatably driven in this state, the drive force is transmitted first to the link arm 220 and then to the rocker arm 240, the link member 250, and the oscillating cams 260.
When the cam 211 is to the left of the camshaft 210, as shown in FIG. 8A, the base-circle parts 261 of the oscillating cams 260 are in contact with the cam followers 63, at which time the cam followers 63 are at the top end position and the valves 61 are in a state of maximum lift.
When the cam 211 is to the right of the camshaft 210, as shown in FIG. 8B, the cam noses 262 of the oscillating cams 260 are in contact with the cam followers 63, at which time the cam followers 63 are at the bottom end positions and the valves 61 are in an opened state.
To reduce the stroke amount of the cam followers 63 and the lift amount of the valves 61, the valve lift control shaft 230 is rotated to raise the position of the cam 231, and the axial center P1 is set above and to the right of the axial center P2, as shown in FIGS. 8C and 8D. The entire rocker arm 240 is thereby moved upward. When the camshaft 210 is rotatably driven in this state, the drive force is transmitted first to the link arm 220 and then to the rocker arm 240, the link member 250, and the oscillating cams 260. When the cam 211 is to the left of the camshaft 210, as shown in FIG. 8C, the base-circle parts 261 of the oscillating cams 260 are in contact with the cam followers 63. When the cam 211 is to the right of the camshaft 210, as shown in FIG. 8D, the base-circle parts 261 of the oscillating cams 260 are still in contact with the cam followers 63.
Thus, in cases in which the valve lift control shaft 230 is rotated, the position of the cam 231 is raised, and the axial center P1 is set above and to the right of the axial center P2, the cam followers 63 do not perform a stroke and the valves 61 remain closed, even though the camshaft 210 rotates and the oscillating cams oscillate.
FIG. 9 is a graph showing the valve lift amount and the opening and closing timings in the variable valve timing mechanism 200. The solid lines indicate the lift amount and the opening and closing timings of the valves 61 when the valve lift control shaft 230 is rotated. The dashed lines indicate the opening and closing timings of the valves 61 when the phase of the camshaft 210 is varied relative to the cam sprocket 270.
According to the structure of the variable valve timing mechanism 200 described above, the lift amount and operating angle of the valves 61 can be continually varied. Thus, the lift amount and operating angle of the valves 61 can be continually and freely varied by varying the angle of the valve lift control shaft 230 and the phase of the camshaft 210 relative to the cam sprocket 270.
FIGS. 10A-10E are graphs showing an example of an operation map of the engine having a barrier discharge function. The range of extremely low load (for example, engine is an idol state) will now be discussed. When the load is in a range of extremely low load, the air-fuel ratio A/F is set to a constant value (FIG. 10A). Also, the barrier discharge start timing is set to a constant timing of the intake stroke (FIG. 10B). The constant timing is a timing in which the setting is made near the most advanced angle within the low load range described hereinafter. The discharge energy is set to a level that increases the lower the load is (FIG. 10C). The intake valve close timing (IVC) is set to be nearer to the advance angle than the bottom dead center (BDC), and the operation proceeds according to the Miller cycle. This timing is set to an angle that is more advanced the lower the load is (FIG. 10D). The mechanical compression ratio is set to a high level (FIG. 10E).
The range of low load will now be discussed. In a low load range in which the load is greater than in the extremely low load range, the air-fuel ratio A/F is set to decrease (i.e., become richer) as the load increases (FIG. 10A). The barrier discharge start timing is set to the intake stroke when the load is low, is set to approach the retard angle as the load increases, and is set to the compression stroke when the load is high (FIG. 10B). The reasons for these settings are described hereinafter. The discharge energy is set to a constant value (FIG. 10C). The intake valve close timing (IVC) is set to a constant value nearer the retard angle than the bottom dead center (BDC) (FIG. 10D). The mechanical compression ratio is set to a high level (FIG. 10E).
The range of low to moderate load will now be discussed. In a low-to-moderate load range in which the load is greater than in the low load range, the air-fuel ratio A/F is set to decrease (i.e., become richer) as the load increases (FIG. 10A). The barrier discharge start timing is set to lag much more than in the low load range, and is also set to approach the retard angle as the load increases (FIG. 10B). The discharge energy is set to a constant value (FIG. 10C). The intake valve close timing (IVC) is set to a constant value nearer to the lag angle than the bottom dead center (BDC) (FIG. 10D). The mechanical compression ratio is set to be much less than in the extremely low load range or the low load range, and is also set to decrease as the load increases (FIG. 10E).
The range of moderate to high load will now be discussed. In a moderate-to-high load range in which the load is greater than in the low-to-moderate load range, the air-fuel ratio A/F is set to decrease (i.e., become richer) as the load increases (FIG. 10A). The barrier discharge start timing is set to approach the retard angle as the load increases (FIG. 10B). The discharge energy is set to a constant value (FIG. 10C). The intake valve close timing (IVC) is set to a constant value nearer to the retard angle than the bottom dead center (BDC) (FIG. 10D). The mechanical compression ratio is set to be even less than in the low-to-moderate load range, and is also set to decrease as the load increases (FIG. 10E).
The reasons for setting the control map in the above manner will be described herein. In the low load range, the barrier discharge start timing is set to the intake stroke when the load is low, is set to approach the retard angle as the load increases, and is set to the compression stroke when the load is high (FIG. 10B). The reasons for these settings will be explained with reference to FIG. 11.
FIG. 11 is a graph showing the variation in the heat generation rate outside of the barrier discharge start timing. Line A in the diagram is shown as a comparative example, and is a line indicating variation in the heat generation rate when a barrier discharge is not performed (i.e., radicals are not generated). It can be seen from line A that the peak of the heat generation rate is suppressed at the crank angle θa. The heat generation rate is substantially symmetrical before and after this peak, and the crank angle MBθ50% (discussed below) at which the mass combustion ratio is 50% substantially coincides with θa.
Line B in the diagram is a line indicating variation in the heat generation rate when a barrier discharge is initiated during the compression stroke (for example, 135 deg BTDC). It can be seen from line B that the peak of the heat generation rate is suppressed at the crank angle θb nearer to the advance angle than when the barrier discharge was not performed (line A), and the heat generation rate rises more rapidly than when the barrier discharge was not performed (line A). The heat generation rate is substantially symmetrical before and after this peak, and the crank angle MBθ 50%, at which the mass combustion ratio is 50%, substantially coincides with θb.
Line C in the diagram is a line indicating variation in the heat generation rate when a barrier discharge is initiated during the intake stroke (for example, 270 deg BTCD). It can be seen from line C that the peak of the heat generation rate is suppressed at the crank angle θc even nearer to the advance angle than when the barrier discharge was initiated during the compression stroke (line B), and the variation is steep. The heat generation rate is substantially symmetrical before and after this peak, and the crank angle MBθ 50%, at which the mass combustion ratio is 50%, substantially coincides with θc.
FIGS. 12A-C contain drawings schematically depicting the state in which radicals are distributed within the cylinder, which is the result of analyzing the reasons that bring about a state such as in FIG. 11. The radicals are schematically depicted by the dots in the drawings. Research has shown that differences in the variation in the heat generation rate brought about by the barrier discharge start timing are caused by the state in which radicals are distributed within the cylinder, as shown in FIG. 11.
When a barrier discharge is not performed (i.e., when radicals are not generated), there is naturally no distribution of radicals in the cylinder 31 a (FIG. 12A). When the air-fuel mixture undergoes compression ignition while no radicals are distributed, the heat generation rate varies comparatively slowly, as shown by line A in FIG. 11.
In cases in which a barrier discharge is initiated during the intake stroke, it can be seen that radicals are distributed throughout substantially the entire cylinder 31 a immediately before ignition, as shown in FIG. 12C. This is because there is a long timing from the time when the barrier discharge device 70 performs a barrier discharge to generate radicals until the time of ignition, and the radicals are therefore carried by the intake flow to be widely dispersed throughout the cylinder 31 a. When compression ignition takes place in the state in which the radicals are widely distributed, the air-fuel mixture combusts substantially all at once throughout the entire cylinder 31 a. The radicals are in a state in which molecular dissociation is induced by collisions of high-energy electrons with fuel or air molecules. Such radicals have the characteristic of readily inducing oxidation reactions (i.e., combustion) and creating chain oxidation reactions. The radicals undergo combustion substantially all at once throughout the entire cylinder 31 a when the pressure in the cylinder increases while radicals having such characteristics are dispersed throughout the entire cylinder 31 a. Research has shown that the heat generation rate also rises suddenly because a combustion reaction takes place in this manner throughout the entire cylinder 31 a.
Initiating a barrier discharge during the compression stroke brings about an intermediate state in the cylinder 31 a immediately before ignition, that is, a state between the case of no barrier discharge (FIG. 12A) and the case in which a barrier discharge is initiated during the intake stroke (FIG. 12C). In the intermediate state, fewer radicals are distributed in the vicinity of the barrier discharge device 70 (FIG. 12B). This is because there is a short timing from the time when the barrier discharge device 70 performs a barrier discharge to generate radicals until the time of ignition, and the radicals are therefore unable to widely disperse. When compression ignition takes place in the state in which the radicals are dispersed in the vicinity of the barrier discharge device 70, the combustion process first involves the radicals and then spreads to the surrounding radical-free air-fuel mixture. It is because of this type of mechanism that line B is an intermediate line between line A and line C.
FIG. 13 is a graph showing the relationship between the barrier discharge start timing and the crank angle at which the mass combustion ratio is 50%.
As described above, varying the barrier discharge start timing causes a change in the crank angle MBθ 50% at which the mass combustion ratio is 50%. In other words, the autoignition properties change. This relationship is plotted in FIG. 13. Up until the barrier discharge start timing reaches approximately 270 deg BTDC, the crank angle MBθ 50% at which the mass combustion ratio is 50% advances as the barrier discharge start timing is advanced. In other words, autoignition properties are improved. When the barrier discharge start timing is advanced to 270 deg BTDC or greater, the crank angle MBθ 50% at which the mass combustion ratio is 50% lags behind as the barrier discharge start timing is advanced.
The following are thought to be the reasons that the crank angle MBθ 50% at which the mass combustion ratio is 50% advances the farthest (i.e., autoignition properties are best) when the barrier discharge start timing is approximately 270 deg BTDC. Specifically, there is an overlap between timings in which the intake valve and exhaust valve of the engine are normally opened and closed. It is believed that initiating a barrier discharge after the exhaust valve has closed causes the air-fuel mixture drawn in through the intake valve to scatter more readily and autoignition properties to improve in comparison with a case in which a barrier discharge is initiated during the timing in which the exhaust valve has not yet closed. It is also believed that the air-fuel mixture readily scatters and autoignition properties improve because the rate of air intake is higher during the latter half of the downward movement of the piston than the first half. The barrier discharge part continuously performs a barrier discharge for a predetermined time (predetermined crank angle timing) following discharge initiation. The air flow rate decreases after the intake valve is closed. When a non-equilibrium plasma discharge is performed while the air flow rate has decreased, the radicals do not disperse as readily as when the air flow rate is high. Therefore, to efficiently disperse radicals within the cylinder, the end timing of the non-equilibrium plasma discharge is preferably before the closing of the intake valve.
As can be seen from FIG. 13, the heat generation timing (the crank angle MBθ 50% at which the mass combustion ratio is 50%) can be controlled by adjusting the barrier discharge start timing. In other words, the autoignition properties of the air-fuel mixture can be controlled by adjusting the barrier discharge start timing. As the autoignition properties improve, the operability at a lean air-fuel ratio improves as well. However, if the autoignition properties improve excessively when the air-fuel ratio is not particularly lean, there is a danger that knocking will occur. In view of this, the barrier discharge start timing is preferably adjusted according to the air-fuel ratio (load).
As a comparative example, FIG. 13 also shows a case in which radicals are generated by a sparkplug. It is clear from the diagram that even if radicals are generated by a sparkplug, there is little difference from cases in which radicals are not generated.
Based on the above knowledge, an electric discharge structure is provided which causes a barrier discharge to be initiated during the intake stroke so that radicals are widely distributed within the cylinder when the air-fuel ratio corresponds to an extremely diluted (lean) condition.
Depending on the operating state, there is a danger that the autoignition properties will be improved to an excess and that knocking will occur if the amount of radicals generated within the cylinder is too great or the radicals are too widely distributed. In view of this, the autoignition properties are adjusted by delaying the barrier discharge start timing as the load increases (as the amount of fuel increases and the air-fuel ratio corresponds to a richer mixture). The above factors are the reasons that the barrier discharge start timing is set to occur during the intake stroke when the load is low, is set to approach a retard angle as the load increases, and is set to occur during the compression stroke when the load is high (FIG. 10B).
The mechanical compression ratio is set to a high level in a load range at or below a low load (FIG. 10E). The reasons for these settings will now be described.
An engine having a multi-link variable compression ratio mechanism has the characteristic of having a longer timing in which the piston stays in proximity to the top dead center in comparison with a common engine in which the compression ratio is constant (hereinafter referred to as a “normal engine”). Due to this characteristic, an engine having a multi-link variable compression ratio mechanism, even at a high compression ratio, is less susceptible to knocking than a common engine is, comparatively high combustion energy can be obtained even with ultra-lean combustion, and stable combustion can be maintained.
This aspect is described with reference to FIG. 14. FIG. 14 contains a graph showing the piston behavior in a multi-link variable compression ratio mechanism, wherein the upper portion of FIG. 14 is an enlarged view of the dotted line portion of the lower portion of the figure. In FIG. 14, the thin solid lines indicate the piston behavior in the multi-link variable compression ratio mechanism engine having the same compression ratio as a normal engine.
If the time in which the piston is within a predetermined distance from the top dead center is defined as the timing in which the piston is in proximity to the top dead center, it is clear from FIG. 14 that the multi-link variable compression ratio mechanism engine has a longer timing in which the piston is in proximity to the top dead center than does a normal engine having the same compression ratio. Specifically, in the multi-link variable compression ratio mechanism engine, the timing L1 in which the piston is in proximity to the top dead center at a high compression ratio is longer than the timing L2 in which the piston is in proximity to the top dead center at a low compression ratio. In other words, the inequality L1>L2 is true in FIG. 14.
Thus, the multi-link variable compression ratio mechanism engine has a longer timing in which the piston is in proximity to the top dead center than does a normal engine. Furthermore, the timing in which the piston is in proximity to the top dead center is longer than that observed at a high compression ratio. The fact that the piston is in proximity to the top dead center for a long time means that a high compression state is maintained for a long time during combustion. When a high compression state is maintained for a long time, knocking does not readily occur, and combustion is stable because comparatively high combustion energy can be obtained even during ultra-lean combustion.
Because of such characteristics, the multi-link variable compression ratio mechanism engine has the characteristics shown in FIG. 15. FIG. 15 is a graph showing the relationship between the air-fuel ratio and combustion stability. The thin line in the diagram denotes a normal engine, and the thick line denotes a multi-link variable compression ratio mechanism engine.
As can be seen from FIG. 15, in a normal engine (compression ratio: about 8 to 12), the air-fuel ratio which can ensure combustion stability is about 22.
According to the multi-link variable compression ratio mechanism engine, the combustion stability limit is not compromised because the piston remains in proximity to the top dead center for a long time. Increasing the compression ratio (e.g., to about 18) makes it possible to obtain stable combustion even at an air-fuel ratio A/F of about 30. The above are the reasons the mechanical compression ratio is set to a high level in a load range at or below a low load (FIG. 10E). The map load range in FIG. 10 was set based on this knowledge.
Next, the reasons for selecting the settings in the extremely low load range in the control map will be described. In the extremely low load range, as described above, the intake valve close timing (IVC) is set nearer to the advance angle than in the bottom dead center (BDC), and the operation proceeds according to the Miller cycle. The timing is set nearer to the advance angle at lower loads (FIG. 10D). The filling efficiency of intake air is thereby reduced, the effective compression ratio is lowered, and pump loss is reduced. Since the combustion amount decreases with decreased load (the air-fuel ratio is substantially constant because the air intake amount also decreases), the air-fuel mixture loses autoignition properties. In view of this, the discharge energy is greatly increased at lower loads (FIG. 10C). The map of the extremely low load range in FIG. 10 was set based on the above knowledge. As shown, operation is possible even at extremely low load ranges.
Next, the reasons for the settings in the low-to-moderate load range of the control map will be described. In the low-to-moderate load range, as described above, the barrier discharge start timing lags to a considerably greater extent than in the low load range (FIG. 10B). The mechanical compression ratio is set to be much lower than in the extremely low and low load ranges (FIG. 10E).
In cases in which radicals are generated and combustion takes place by compression ignition, the air-fuel mixture has better autoignition properties. Therefore, when the load is greater and the amount of combustion increases, there is a possibility that the heat generation rate will suddenly increase to an excessive degree, as shown by line A in FIG. 16. When the heat generation rate suddenly increases to an excessive degree in this manner, there is a danger that knocking will occur.
In view of this, in the present embodiment, when the load increases to within a low-to-moderate load range, the compression ratio is reduced so that the air-fuel mixture does not undergo compression ignition. It is designed so that volumetric ignition is performed by the barrier discharge part during the compression stroke. The fuel in the vicinity of the barrier discharge part thereby undergoes flame propagation. The remaining unburned air-fuel mixture is adiabatically compressed by the burned air-fuel mixture and is made to undergo autoignition. As a result, the heat generation rate varies as shown by line B in FIG. 16 and does not suddenly increase to an excessive degree, and knocking does not occur. The map of the low-to-moderate load range in FIG. 10 is set based on the above. Operation is thereby made possible even in a low-to-moderate load range.
Spark ignition is performed by the barrier discharge part at a moderate-to-high load or greater, whereby operation is possible even in a moderate-to-high load range.
FIGS. 17A and 17B contain graphs showing various effects of the present embodiment. In the present embodiment, it is possible to greatly expand the lean combustion limit because the barrier discharge start timing is appropriately controlled according to the operating state as described above.
In FIG. 17A, plotting the correlation between the air-fuel ratio A/F (horizontal axis) and the fluctuation rate CPi (vertical axis) of the depicted average effective pressure results in line A in normal combustion by compression ignition. The lean combustion limit is the air-fuel ratio AFa.
Line B depicts cases in which radicals are generated by a sparkplug, and combustion occurs by compression ignition. The lean combustion limit is the air-fuel ratio of AFb, and is somewhat leaner than the air-fuel ratio AFa of the lean combustion limit in normal cases.
Line C depicts cases in which radicals are generated by the barrier discharge part, and combustion occurs by compression ignition. The lean combustion limit is the air-fuel ratio of AFc. The lean combustion limit can be greatly expanded in comparison with the air-fuel ratio AFa of the lean combustion limit in normal cases and in comparison with the air-fuel ratio AFb of the lean combustion limit in generation of radicals by a sparkplug and combustion by compression ignition. As described above, the operation shown by the dashed lines can be arbitrarily selected because it is possible to control the crank angle MBθ 50% at which the mass combustion ratio is 50% by adjusting the barrier discharge start timing. If the lean combustion limit is expanded, the fuel consumption rate ISFC can be reduced as shown in FIG. 17B. The present embodiment makes it possible to reduce the fuel consumption rate regardless of the load, and to improve fuel consumption.
In the present embodiment, the first electrode composed of a long thin conductive material and the dielectric material for covering the first electrode allow a barrier discharge to be performed in which non-equilibrium plasma is discharged and radicals can be generated within a cylinder. Therefore, the autoignition properties of an air-fuel mixture during the compression stroke can be improved, the fuel consumption rate can consequently be reduced regardless of the load, and fuel consumption can also be improved.

Second Embodiment

Referring now to FIG. 18, an internal combustion engine electric discharge structure in accordance with a second embodiment will now be explained. Basically, in this second embodiment, the internal combustion engine electric discharge structure of the first embodiment is replaced in FIG. 1 with a modified structure as discussed below. In view of the similarity between the first and second embodiments, the parts of the second embodiment that are identical to the parts of the first embodiment will be given the same reference numerals as the parts of the first embodiment. Moreover, the descriptions of the parts of the second embodiment that are identical to the parts of the first embodiment can be omitted for the sake of brevity.
FIG. 18 is a simplified schematic cross-sectional view showing the operational configuration of the engine having an electric discharge structure in accordance with a second embodiment. The engine 1 having a barrier discharge function of the first embodiment was a so-called port-injection engine in which the fuel injection valve 65 was provided to the intake port, but the electric discharge structure can also be applied to a direct fuel-injection engine such as the one shown in FIG. 18, in which fuel is directly injected into the cylinder.
In this type of direct fuel-injection engine, the air-fuel mixture is stratified only in the vicinity of the barrier discharge device 70 as shown in FIG. 19 to make operation possible even with a lean air-fuel ratio. Generating radicals in this type of lean air-fuel mixture allows the lean combustion limit to be expanded, the fuel consumption rate to be reduced, and fuel consumption to be improved.
An example of an operation map for the engine having such a barrier discharge function is shown in FIGS. 20A-20E. An interval in which a barrier discharge is not performed is provided in the vicinity of a comparatively high load within the low load range (FIGS. 20A and 20B). In the low load range, a high compression ratio is set by the variable compression ratio mechanism, and knocking does not readily occur. Therefore, there is an operation range in which lean combustion is possible even though a barrier discharge is not performed. When a barrier discharge is performed in such an operating range, there is a danger that autoignition properties will improve excessively and that knocking will occur. In view of this, a barrier discharge is not performed in the vicinity of comparatively high loads within the low load range.
In an extremely low load range in which the load is lower than in the low load range, a stratified operation is performed (FIG. 20D) and the air-fuel ratio A/F is made leaner (sparser) according to the load (FIG. 20A). A barrier discharge is performed because the autoignition properties must be improved along with the increase in sparseness. The barrier discharge start timing is set to occur during the intake stroke, wherein the effects of autoignition properties improvement are high (FIG. 20B). The autoignition properties are improved by increasing the discharge energy along with the increase in sparseness (FIG. 20C).
By using the present embodiment, the invention can be carried out even with a direct fuel-injection engine, the fuel consumption rate can be reduced regardless of the load, and fuel consumption can be improved.

Third Embodiment

Referring now to FIG. 21, an internal combustion engine electric discharge structure in accordance with a third embodiment will now be explained. Basically, in this third embodiment, the internal combustion engine electric discharge structure of the first embodiment is replaced in FIG. 1 with a modified structure as discussed below. In view of the similarity between the first and second embodiments, the parts of the third embodiment that are identical to the parts of the first embodiment will be given the same reference numerals as the parts of the first embodiment. Moreover, the descriptions of the parts of the third embodiment that are identical to the parts of the first embodiment can be omitted for the sake of brevity.
FIG. 21 is a simplified schematic cross-sectional view showing the third embodiment of an engine having a barrier discharge function. In the barrier discharge device 70 of the present embodiment, a dielectric layer (insulating layer) 73 is formed on the inner periphery of the tubular electrode 72, and the central electrode 71 is exposed. The distal end of the dielectric layer (insulating layer) 73 preferably protrudes farther toward the combustion chamber than does the distal end of the tubular electrode 72 or the distal end of the central electrode 71. This is because such a configuration makes it possible to suppress the occurrence of a thermal plasma discharge between the distal end of the tubular electrode 72 and the distal end of the central electrode 71, even in cases in which the discharge energy of a non-equilibrium plasma discharge has been increased. The dielectric layer 73 acts as a capacitor in the configuration of the present embodiment as well, and the same effects as in the first embodiment are obtained.

Fourth Embodiment

Referring now to FIGS. 22A and 22B, an internal combustion engine electric discharge structure in accordance with a fourth embodiment will now be explained. Basically, in this fourth embodiment, the internal combustion engine electric discharge structure of the first embodiment is replaced in FIG. 1 with a modified structure as discussed below. In view of the similarity between the first and fourth embodiments, the parts of the fourth embodiment that are identical to the parts of the first embodiment will be given the same reference numerals as the parts of the first embodiment. Moreover, the descriptions of the parts of the fourth embodiment that are identical to the parts of the first embodiment can be omitted for the sake of brevity.
FIGS. 22A and 22B contain simplified schematic cross-sectional views showing the fourth embodiment of the engine having a barrier discharge function. In the barrier discharge device 70 of the present embodiment, in contrast to the first embodiment, the central electrode 71 protrudes into the combustion chamber.
Thus, the barrier discharge device 70 forms a barrier discharge within the combustion chamber as shown in FIG. 22A. In the present embodiment, the top surface of the piston 32 or the inside wall surface of the cylinder head functions as an electrode. Specifically, in the present embodiment, a barrier discharge is performed and radicals are generated in the area A between the top surface of the piston 32 and the dielectric layer (insulating layer) 73 of the central electrode 71, or in the area B between the inside wall surface of the cylinder head and the dielectric layer (insulating layer) 73. Whether the barrier discharge is performed in area A or B is determined by the position of the piston 32 when an AC voltage is applied to the barrier discharge device 70. In view of this, the discharge area of barrier discharge can be selected by controlling the application timing of the AC voltage applied to the barrier discharge device 70.
A concave part can be formed in the top surface of the piston 32 as shown in FIG. 22B, and the configuration can be designed so that barrier discharge is performed between the concave part and the distal end of the dielectric material (insulating material) 73 of the central electrode 71.

Fifth Embodiment

Referring now to FIGS. 23A and 23B, an internal combustion engine electric discharge structure in accordance with a fifth embodiment will now be explained. Basically, in this fifth embodiment, the internal combustion engine electric discharge structure of the first embodiment is replaced in FIG. 1 with a modified structure as discussed below. In view of the similarity between the first and fifth embodiments, the parts of the fifth embodiment that are identical to the parts of the first embodiment will be given the same reference numerals as the parts of the first embodiment. Moreover, the descriptions of the parts of the fifth embodiment that are identical to the parts of the first embodiment can be omitted for the sake of brevity.
FIGS. 23A and 23B contain simplified schematic cross-sectional views showing the fifth embodiment of the engine having a barrier discharge function. In the barrier discharge device 70 of the present embodiment, the dielectric material (insulating material) 73 is shorter in comparison with the fourth embodiment, and the central electrode 71 is exposed within the combustion chamber. A dielectric layer (insulating layer) 32 a is also formed on the top surface of the piston 32.
Thus, the barrier discharge device 70 performs a barrier discharge within the combustion chamber as shown in FIG. 23A. Specifically, a barrier discharge is performed and radicals are generated in the area A between the distal end of the central electrode 71 and the dielectric layer (insulating layer) 32 a on the top surface of the piston 32.
If a concave part is formed in the top surface of the piston 32, and the dielectric layer (insulating layer) 32 a is formed in the inner periphery of the concave part as shown in FIG. 23B, a barrier discharge is performed between the dielectric layer (insulating layer) 32 a and the distal end of the central electrode 71.
Although alternating current corresponding to the operating state of the engine is applied to the barrier discharge device 70, but the alternating current is not limited to a sine curve (FIG. 24A). A bipolar multiple pulse power source can also be used, such as is shown in FIG. 24B.
Also in the above descriptions, a multi-link mechanism was exemplified as the variable compression ratio mechanism, but other possible examples include, e.g., a mechanism in which a hydraulic device is incorporated into the piston as such to adjust the height of the top surface of the piston, a mechanism in which the distance between the cylinder head and the cylinder block can be adjusted, and a mechanism in which the piston height can be adjusted by offsetting the center of the crankshaft.
Furthermore, the mechanism for adjusting the valve timing of the intake valve can also be, e.g., an oscillating cam which uses a link (Japanese Laid-Open Patent Application No. 2000-213314), a mechanism in which the cam is twisted in the manner of a vane-type variable valve timing system (Japanese Laid-Open Patent Application No. 9-60508), a system in which a switch is made between two types of cams having different timings in the manner of a direct variable valve timing system (Japanese Laid-Open Patent Application No. 4-17706), or the like.

GENERAL INTERPRETATION OF TERMS

In understanding the scope of the present invention, the term “comprising” and its derivatives, as used herein, are intended to be open ended terms that specify the presence of the stated features, elements, components, groups, integers, and/or steps, but do not exclude the presence of other unstated features, elements, components, groups, integers and/or steps. The foregoing also applies to words having similar meanings such as the terms, “including”, “having” and their derivatives. Also, the terms “part,” “section,” “portion,” “member” or “element” when used in the singular can have the dual meaning of a single part or a plurality of parts. The terms of degree such as “substantially”, “about” and “approximately” as used herein mean a reasonable amount of deviation of the modified term such that the end result is not significantly changed.
While only selected embodiments have been chosen to illustrate the present invention, it will be apparent to those skilled in the art from this disclosure that various changes and modifications can be made herein without departing from the scope of the invention as defined in the appended claims. For example, the size, shape, location or orientation of the various components can be changed as needed and/or desired. Components that are shown directly connected or contacting each other can have intermediate structures disposed between them. The functions of one element can be performed by two, and vice versa. The structures and functions of one embodiment can be adopted in another embodiment. It is not necessary for all advantages to be present in a particular embodiment at the same time. Every feature which is unique from the prior art, alone or in combination with other features, also should be considered a separate description of further inventions by the applicant, including the structural and/or functional concepts embodied by such features. Thus, the foregoing descriptions of the embodiments according to the present invention are provided for illustration only, and not for the purpose of limiting the invention as defined by the appended claims and their equivalents.

Claims

1. An internal combustion engine electric discharge structure comprising:

a first electrode including a first voltage receiving end and a second engine attachment end with a long thin conductive material that discharges non-equilibrium plasma by a barrier discharge; and

a dielectric material covering the first electrode.

2. The internal combustion engine electric discharge structure of claim 1, further comprising

a second electrode facing the first electrode on a periphery of the dielectric material.

3. The internal combustion engine electric discharge structure of claim 2, wherein

the second electrode includes a tubular electrode surrounding at least a portion of the first electrode.

4. The internal combustion engine electric discharge structure of claim 3, further comprising

a cylinder head having the second electrode attached thereto, with the first electrode including a linear central electrode.

5. The internal combustion engine electric discharge structure of claim 2, wherein

the first electrode includes a linear central electrode; and

the second electrode is disposed as at least part of one of a wall surface of a combustion chamber and a top surface of a piston.

6. The internal combustion engine electric discharge structure of claim 2, further comprising

a fuel injection valve for supplying fuel into a combustion chamber of an internal combustion engine; and

a voltage application device operatively coupled to the first voltage receiving end of the first electrode for applying a voltage between the first electrode and the second electrode, such that the non-equilibrium plasma generates radicals within the combustion chamber before an air-fuel mixture in the combustion chamber undergoes autoignition.

7. The internal combustion engine electric discharge structure of claim 6, further comprising

a control unit operatively coupled to the voltage application device to vary a discharge start timing of the non-equilibrium plasma discharge in accordance with a mechanical load of the internal combustion engine.

8. The internal combustion engine electric discharge structure of claim 7, wherein

the control unit sets the discharge start timing of the non-equilibrium plasma discharge to occur during an intake stroke when the mechanical load of the internal combustion engine is comparatively low.

9. The internal combustion engine electric discharge structure of claim 8, wherein

the control unit sets the discharge start timing of the non-equilibrium plasma discharge to be increasingly advanced as the mechanical load of the internal combustion engine becomes lower.

10. The internal combustion engine electric discharge structure of claim 7, wherein

the control unit sets the discharge start timing of the non-equilibrium plasma discharge to occur during a compression stroke when the mechanical load of the internal combustion engine is comparatively high.

11. The internal combustion engine electric discharge structure of claim 10, wherein

the control unit sets the discharge start timing of the non-equilibrium plasma discharge to be increasingly delayed as the mechanical load of the internal combustion engine increases.

12. The internal combustion engine electric discharge structure of claim 6, further comprising

a control unit operatively coupled to the voltage application device to set a discharge start timing of the non-equilibrium plasma discharge to occur after an intake valve has opened.

13. The internal combustion engine electric discharge structure of claim 6, further comprising

a control unit operatively coupled to the voltage application device to set a discharge ending timing of the non-equilibrium plasma discharge to occur before an intake valve has closed.

14. The internal combustion engine electric discharge structure of claim 6, further comprising

a control unit operatively coupled to the voltage application device to set a discharge energy of the non-equilibrium plasma discharge such that the discharge energy increases as the mechanical load of the internal combustion engine becomes lower when the mechanical load of the internal combustion engine is in a low load range.

15. The internal combustion engine electric discharge structure of claim 14, wherein

the control unit increases the discharge energy of non-equilibrium plasma discharge by at least one method selected from

increasing a voltage value of an AC voltage applied between the first and second electrodes,

increasing a frequency of the AC voltage applied between the first and second electrodes, and

increasing an application duration of the AC voltage applied between the first and second electrodes.

16. The internal combustion engine electric discharge structure of claim 6, further comprising

a variable compression ratio mechanism arranged to change a mechanical compression ratio of the internal combustion engine; and

a control unit operatively coupled to the variable compression ratio mechanism to reduce the mechanical compression ratio so that an air-fuel mixture does not undergo compression ignition when a mechanical load of the internal combustion engine is in a high load range, and volumetric ignition is performed.

17. The internal combustion engine electric discharge structure of claim 6, further comprising

a fuel injection control unit operatively coupled to the fuel injection valve to control injection of fuel directly into a cylinder of the internal combustion engine such that a stratified air-fuel mixture is formed in the cylinder when a mechanical load of the internal combustion engine is in a low load range.

18. An internal combustion engine control method for controlling an operating state of an internal combustion engine, comprising:

determining a mechanical load of the internal combustion engine;

injecting fuel into a combustion chamber of the internal combustion engine;

applying a voltage to an electric discharge device having a first electrode and a second electrode to produce a non-equilibrium plasma discharge generating radicals within the combustion chamber before an air-fuel mixture of the fuel undergoes autoignition; and

setting a discharge start timing of the non-equilibrium plasma discharge such that the discharge start timing varies in accordance with the mechanical load.