[Technical Field]
[0001] The present invention relates to a fuel injection pressure control apparatus for
an internal combustion engine typified by a diesel engine. In particular, the present
invention relates to strategies for optimizing the combustion state of air-fuel mixtures.
[Background Art]
[0002] As is conventionally known, in a diesel engine used as an automobile engine or the
like, fuel injection control is performed that adjusts periods and amounts of fuel
injection from a fuel injection valve (also referred to below as "injector") according
to engine revolution, amount of accelerator operation, coolant temperature, intake
air temperature, and the like (e.g., see Patent Literature 1 listed below).
[0003] Diesel engine combustion is achieved by premixed combustion and diffusion combustion.
When fuel injection from a fuel injection valve begins, first a combustible mixture
is produced by the vaporization and diffusion of fuel (ignition delay period). Next,
this combustible mixture self-ignites at about the same time at numerous places in
a combustion chamber, and combustion rapidly progresses (premixed combustion). Further,
fuel is injected into the combustion chamber, so that combustion is continuously performed
(diffusion combustion). Thereafter, unburned fuel is present even after fuel injection
has ended, so heat continues to be produced for some period of time (afterburning
period).
[0004] In diesel engines, as the vaporization of fuel in the cylinder grows more intense,
flame propagation speed after ignition rises. When this flame propagation speed becomes
high, the amount of fuel that burns at once becomes too great, pressure inside the
cylinder drastically increases, thus generating vibration or noise. This phenomenon
is called diesel knocking, and often occurs particularly when operating at a low load.
Also, in this sort of situation, a drastic elevation in combustion temperature is
accompanied by an increase in the amount of nitrogen oxide (referred to below as "NOx")
produced, and thus exhaust emissions become worse.
[0005] In order to overcome these problems, the fuel pressure (may also be referred to as
"fuel injection pressure" below) is adjusted as disclosed in the Patent Literatures
2 to 4 listed below. Ordinarily, the fuel pressure is set high in order to increase
the combustion speed within the cylinder, or conversely, the fuel pressure is set
low in order to control the generation of vibration or noise.
[Citation List]
[Patent Literature]
[Summary of Invention]
[Technical Problem]
[0007] However, in today's diesel engines, as a procedure for setting the fuel pressure
in accordance with the operation state, the fuel pressure is adapted to each of the
engine operation states of engine revolution and engine torque (corresponding to the
engine load). That is to say, an adapted value of the fuel pressure is determined
experimentally by trial and error for each engine operation state, and the adapted
values of the fuel pressure corresponding to a large number of individual engine operation
states are turned into a map, thus preparing a fuel pressure setting map. Then, by
following this fuel pressure setting map, a target fuel pressure is set that is appropriate
for the current engine operation state, and for example a high pressure fuel pump
is controlled accordingly.
[0008] The following is an explanation of an example of a procedure for preparing a fuel
pressure setting map that has been used up to now. In this procedure for preparing
a fuel pressure setting map, first, a fuel pressure setting map as shown in Fig. 9(a)
is prepared, and this fuel pressure setting map is changed as shown in Fig. 9(b) and
Fig. 9(c) in that order, by determining experimentally by trial and error adapted
values for the fuel pressure.
[0009] First, Fig. 9(a) is a fuel pressure setting map in which the fuel pressure gradually
becomes higher, over the entire operation region, as the engine revolution increases.
In this fuel pressure setting map, the lines of equal fuel pressure (the straight
lines indicated as broken lines in the figure) are parallel to the vertical axis (engine
torque axis) in the figure, so that they coincide with the lines of equal revolution.
With this fuel pressure setting map, a favorable drivability is realized and even
in a region of low revolution, the fuel pressure is quickly increased in accordance
with an increase in engine revolution, so that delays in increasing the fuel pressure
can be prevented.
[0010] However, with the fuel pressure setting map shown in Fig. 9(a), problems with regard
to the quietness of the engine remain. Accordingly, a low fuel pressure region in
a low torque region is enlarged towards the high revolution side compared to the fuel
pressure setting map shown in Fig. 9(a), and thus the map is changed to the fuel pressure
setting map shown in Fig. 9(b), in which a favorable quietness of the engine is attained
in this operation region. The amount of change for this is determined experimentally
by trial and error.
[0011] However, with the fuel pressure setting map shown in Fig. 9(b), problems with regard
to exhaust emissions of the engine remain. Accordingly, a high fuel pressure region
in an intermediate torque region is enlarged towards the low revolution side compared
to the fuel pressure setting map shown in Fig. 9(b), and thus the atomization of the
fuel in this operation region (in particular in the operation region enclosed by the
dash-dotted line in Fig. 9(c)) is enhanced, so that the map is changed to a fuel pressure
setting map as shown in Fig. 9(c), in which an improvement of the exhaust emissions
is attained. The amount of change for this is determined experimentally by trial and
error. In the fuel pressure setting map shown in Fig. 9(c), the low fuel pressure
region near the maximum torque line is enlarged towards the high revolution side,
and thus also a suppression of oil dilution is attained.
[0012] Since the above-described preparation procedure was used, the preparation of the
fuel pressure setting map required a considerable effort. And what is more, since
an adapted value for the fuel pressure had to be determined experimentally by trial
and error for each engine operation state individually, there was also no guarantee
that appropriate fuel pressures are set across the entire engine operation region.
That is to say, there were cases in which, even though a reduction of combustion noise
and a reduction of the generated amount of NOx may be achieved in a given operation
region, the combustion efficiency worsens and a sufficient engine torque cannot be
attained, and there were cases in which, conversely, even though a sufficiently high
engine torque is attained, there is a tendency that the combustion noise increases
and the generated amount of NOx increases.
[0013] Thus, conventionally, since the adapted values of the fuel pressure were decided
through trial and error, the adaptation tended to be complicated, it was impossible
to implement a systematic procedure for setting the fuel pressure that is common to
a number of engine types, and an optimization of the fuel pressure could not be said
to be accomplished across the entire engine operation region, so that there was still
room for improvement.
[0014] The present invention was conceived in view of these problems, and it is an object
thereof to provide a fuel injection pressure control apparatus with which it is possible
to carry out fuel injection with a fuel injection pressure that is set by a systematic
procedure for setting the fuel injection pressure, when setting a fuel injection pressure
that is suitable for the operation state of the internal combustion engine.
[Solution to Problem]
- Principle by which the Problem is Solved -
[0015] The solving principle by which the present invention attains the above-noted object
is to provide an unambiguous correlation between requested output (requested power)
of the internal combustion engine and fuel injection pressure (for example the target
fuel pressure within the common rail). Moreover, in a situation in which the output
of the internal combustion engine changes due to a change in at least one of the revolution
and torque of the internal combustion engine, a fuel injection with a correspondingly
suitable fuel pressure can be carried out, whereas conversely in a situation in which
the output of the internal combustion engine does not change even though the revolution
or the torque of the internal combustion engine changes, the fuel pressure is not
changed from the suitable value that was set so far. Thus, it becomes possible to
let the change of the heat generation rate approach an ideal state during combustion
of the air-fuel mixture.
- Means for Solving the Problem -
[0016] More specifically, the present invention is based on a fuel injection pressure control
apparatus for an internal combustion engine of the compression ignition type that
controls the pressure of fuel that is injected into a cylinder of the internal combustion
engine. The fuel injection pressure is adjusted in accordance with the output requested
by the internal combustion engine by allocating in advance a region of equal fuel
injection pressure to a region of equal power requested by the internal combustion
engine, across substantially the entire region in which the internal combustion engine
can be operated.
[0017] Due to these characterizing features, when the output requested by the internal combustion
engine has changed during operation of the internal combustion engine, the fuel injection
pressure (target fuel injection pressure) is set such that it becomes the fuel injection
pressure that has been allocated in advance in correspondence with the requested output
of the internal combustion engine. Moreover, the fuel injection pressure is obtained
by allocating a region of equal fuel injection pressure to a region of equal output,
so that a systematic procedure for setting the fuel pressure can be implemented that
is common to a number of engine types, and the preparation of the fuel setting map
for setting a fuel injection pressure that is suitable for the operation state of
the internal combustion engine can be simplified.
[0018] By adjusting the fuel injection pressure, for example, it is possible to let the
change of the heat generation rate during combustion of the air-fuel mixture approach
an ideal state. More specifically, if the fuel injection pressure is set to be high,
the amount by which the heat generation rate increases per unit time during the initial
period of the combustion can be made large (the slope angle of the waveform of the
heat generation rate can be made large), and the injection period over which the same
injection amount is attained can be made short, so that the combustion period can
be shortened (the lowering of the heat generation rate can be set to an earlier timing).
That is to say, the phase of the heat generation rate waveform with respect to the
advancement of the crank angle can be made short (the timing at which the heat generation
rate is lowered can be shifted in the advance direction of the crank angle). Moreover,
also the peak of the heat generation rate (local maximum of the heat generation rate
waveform) can be increased. Conversely, if the fuel injection pressure is set to be
low, the slope angle of the heat generation rate waveform during the initial period
of the combustion can be made small, the phase of the heat generation rate waveform
with respect to the advancement of the crank angle can be made large, and moreover,
the local maximum (peak) of the heat generation rate waveform can be lowered. Thus,
the change of the heat generation rate waveform can be changed by adjusting the fuel
injection pressure, and it becomes possible to let this heat generation rate waveform
approach an ideal waveform. Accordingly, it becomes possible to satisfy several requirements
at the same time, namely to improve the exhaust emissions by reducing the amount of
NOx generated, to reduce combustion noise during the combustion stroke, and to ensure
a sufficient engine torque. Furthermore, it becomes possible to simplify the preparation
of the fuel pressure setting map for obtaining this ideal combustion waveform.
[0019] As a way to allocate the region of equal fuel injection pressure to the region of
equal output of the internal combustion engine, it is possible to allocate a region
of equal fuel injection pressure to the region of equal power of the internal combustion
engine, such that the fuel injection pressure does not change if the output that is
determined from a revolution and a torque of the internal combustion engine does not
change even though the revolution and the torque of the internal combustion engine
has changed.
[0020] Thus, it is possible to change the fuel injection pressure only when the requested
output of the internal combustion engine changes, and to set a suitable fuel injection
pressure unambiguously with respect to the requested output of the internal combustion
engine. For example, if the revolution of the internal combustion engine rises but
there is no change of the requested output due to a lowering of the torque, or conversely,
if the torque of the internal combustion engine rises but there is no change of the
requested output due to a lowering of the revolution, then the fuel injection pressure
is not changed, and the suitable value that has been set up to then is maintained.
[0021] As a way to allocate the fuel injection pressure region, it is possible to allocate
a fuel injection pressure that is higher the higher the output requested by the internal
combustion engine is. That is to say, in a high-torque operation state or in a high-revolution
state of the internal combustion engine, the requested output is attained by increasing
the heat generation rate within the cylinder.
[0022] As a way to allocate the fuel injection pressure region, it is possible to set a
fuel injection pressure region where the fuel injection pressure increases in any
of the cases that both the revolution and the torque of the internal combustion engine
increase, that the torque increases at constant revolution of the internal combustion
engine, and that the revolution increases at constant torque of the internal combustion
engine. That is to say, the fuel injection pressure can be adjusted such that the
fuel injection pressure increases only in situations in which the requested output
of the internal combustion engine rises.
[0023] Moreover, a proportion of a change of the fuel injection pressure with respect to
a change of the output requested by the internal combustion engine can be set to become
smaller the lower the revolution of the internal combustion engine becomes. That is
to say, in a region of low revolutions of the internal combustion engine, the change
of the fuel injection pressure can be made smooth, and a sharp increase of the combustion
pressure within the cylinder is avoided in this operation state, so that the generation
of vibrations or noise accompanying the combustion can be suppressed. Conversely,
in a region of high revolutions of the internal combustion engine, the fuel injection
pressure changes considerably with an increase of the torque, for example, and the
requested output is attained quickly, so that the responsiveness of the internal combustion
engine becomes favorable.
[0024] Furthermore, the fuel pressure setting map that is looked up in order to adjust the
fuel injection pressure is as follows: Lines of equal output and lines of equal fuel
injection pressure drawn within a map where a horizontal axis denotes revolution of
the internal combustion engine and a vertical axis denotes torque of the internal
combustion engine substantially match across substantially the entire region in which
the internal combustion engine can be operated.
[0025] The following example can be given for a specific procedure for deciding the fuel
injection pressure in accordance with the output requested by the internal combustion
engine: The fuel injection pressure can be made proportional, with a predetermined
proportionality constant, to the output requested by the internal combustion engine,
and the fuel injection pressure can be determined by adding a predetermined pressure
offset to a provisional fuel injection pressure obtained by multiplying this requested
output with the proportionality constant.
[0026] In this case, the pressure offset can be set such that a heat generation rate reaches
a local maximum at a time when a crank angle has reached about 10° after compression
top dead center, if the fuel of a main injection that is injected by a fuel injection
valve starts to combust at a time when a piston of the internal combustion engine
has reached compression top dead center.
[0027] Thus, it becomes possible to specifically decide the fuel injection pressure in accordance
with the output requested by the internal combustion engine. Moreover, if the fuel
injection is carried out at the thusly decided fuel injection pressure, then 50% of
the air-fuel mixture within the cylinder will be completely combusted at the time
of 10° after compression top dead center of the piston (ATDC 10°). That is to say,
about 50% of the total amount of generated heat in the expansion stroke is generated
until ATDC 10°, and it becomes possible to operate the internal combustion engine
with high thermal efficiency.
[0028] The following example can be given for a specific procedure for deciding the fuel
injection pressure in an output region where combustion noise is addressed, which
is an output region where the output requested by the internal combustion engine is
relatively low: The fuel injection pressure at the output region where combustion
noise is addressed may be determined by determining a reference pressure by adding
a predetermined pressure basic offset to a provisional fuel injection pressure that
is determined by multiplying a predetermined proportionality constant to the output
requested by the internal combustion engine, and then correctively decreasing this
reference pressure.
[0029] In this case, the fuel injection pressure may be determined by setting the amount
by which the reference pressure is correctively decreased in the output region where
combustion noise is addressed to become larger the smaller the output requested by
the internal combustion engine becomes.
[0030] If the pressure offset is set in this manner, it is possible to suppress combustion
noise in the combustion chamber and to improve the quietness of the internal combustion
engine in situations in which the output of the internal combustion engine is relatively
low.
[0031] The following example can be given for a specific procedure for deciding the fuel
injection pressure in an output region where NOx is addressed, which is an output
region where the output requested by the internal combustion engine is relatively
high: The fuel injection pressure at an output region where NOx is addressed may be
determined by determining a reference pressure by adding a predetermined pressure
basic offset to a provisional fuel injection pressure determined by multiplying a
predetermined proportionality constant to the output requested by the internal combustion
engine, and then correctively decreasing this reference pressure.
[0032] In this case, the fuel injection pressure may be determined by setting the amount
by which the reference pressure is correctively decreased in the output region where
NOx is addressed to become larger the larger the output requested by the internal
combustion engine becomes.
[0033] If the pressure offset is set in this manner, then it is possible to suppress the
combustion speed within the combustion chamber to a low level and to considerably
reduce the amount of NOx generated in the course of combustion within the cylinder
in situations in which the output of the internal combustion engine is relatively
high
[0034] The following example can be given for a specific procedure for deciding the fuel
injection pressure in an output region where smoke is addressed, which is an output
region where the output requested by the internal combustion engine is substantially
intermediate: The fuel injection pressure at an output region where smoke is addressed
may be determined by determining a reference pressure by adding a predetermined pressure
basic offset to a provisional fuel injection pressure determined by multiplying a
predetermined proportionality constant to the output requested by the internal combustion
engine, and then correctively increasing this reference pressure.
[0035] If the pressure offset is set in this manner, then even if the main injection is
implemented by a plurality of partial injections, the injection amount per unit time
can be increased, a shortening of the injection period can be accomplished, and a
deterioration of the efficiency accompanying a lengthening of the injection period
can be overcome.
[Advantageous Effects of Invention]
[0036] In the present invention, a fuel injection pressure of an internal combustion engine
of the compression ignition type is set in such a manner that a region of equal fuel
injection pressure is allocated to an equal output region across substantially the
entire region in which the internal combustion engine can be operated. Thus, it becomes
possible to implement a systematic procedure for setting the fuel pressure that is
common to a number of engine types.
[Brief Description of Drawings]
[0037]
[FIG. 1]
Fig. 1 is a conceptual diagram of an engine according to an embodiment and its control
system.
[FIG. 2]
Fig. 2 is a cross-sectional view showing a combustion chamber of a diesel engine and
its surroundings.
[FIG. 3]
Fig. 3 is a block diagram showing the configuration of a control system, such as an
ECU.
[FIG. 4]
Fig. 4 is a waveform diagram illustrating the change of the heat generation ratio
at an expansion stroke.
[FIG. 5]
Fig. 5 is a diagram showing the relation between the requested engine output and the
target fuel pressure set in accordance with this requested output, in a first embodiment.
[FIG. 6]
Fig. 6 is a diagram showing a fuel setting map that is looked up when deciding the
target fuel pressure in the first embodiment.
[FIG. 7]
Fig. 7 is a diagram showing a fuel setting map that is looked up when deciding the
target fuel pressure in the second embodiment.
[FIG. 8]
Fig. 8 is a diagram showing the relation between the requested engine output and the
target fuel pressure set in accordance with this requested output, in a third embodiment.
[FIG. 9]
Fig. 9 is a diagram illustrating an example of a conventional method for preparing
a fuel pressure setting map.
[Description of Embodiments]
[0038] The following is a description of an embodiment of the present invention based on
the drawings. In the present embodiment, a case is described in which the present
invention is applied to a common rail in-cylinder direct injection multi-cylinder
(for example, inline four-cylinder) diesel engine (compression ignition internal combustion
engine) mounted in an automobile.
- Engine configuration -
[0039] First, the overall configuration of a diesel engine (referred to below as simply
"engine") according to the present embodiment will be described. FIG. 1 is a schematic
configuration diagram of an engine 1 and a control system for the same according to
the present embodiment. FIG. 2 is a cross-sectional view that shows a combustion chamber
3 of the diesel engine and parts in the vicinity of the combustion chamber 3.
[0040] As shown in FIG. 1, the engine 1 according to the present embodiment is configured
as a diesel engine system whose main portions are a fuel supply system 2, combustion
chambers 3, an intake system 6, an exhaust system 7, and the like.
[0041] The fuel supply system 2 is provided with a supply pump 21, a common rail 22, injectors
(fuel injection valves) 23, a cutoff valve 24, a fuel addition valve 26, an engine
fuel path 27, an added fuel path 28, and the like.
[0042] The supply pump 21 draws fuel from a fuel tank, and after putting the drawn fuel
under high pressure, supplies that fuel to the common rail 22 via the engine fuel
path 27. The common rail 22 functions as an accumulation chamber where high pressure
fuel supplied from the supply pump 21 is held (accumulated) at a predetermined pressure,
and this accumulated fuel is distributed to each injector 23. The injectors 23 are
configured from piezo injectors within which a piezoelectric element (piezo element)
is provided, and which supply fuel by injection into the combustion chambers 3 by
opening a valve as suitable. The details of the control of fuel injection from the
injectors 23 will be described later.
[0043] Also, the supply pump 21 supplies part of the fuel drawn from the fuel tank to the
fuel addition valve 26 via the added fuel path 28. In the added fuel path 28, the
aforementioned cutoff valve 24 is provided in order to stop fuel addition by cutting
off the added fuel path 28 during an emergency.
[0044] The fuel addition valve 26 is configured from an electronically controlled opening/closing
valve whose valve opening period is controlled with an addition control operation
by an ECU 100 described later such that the amount of fuel added to the exhaust system
7 becomes a target addition amount (an addition amount such that the exhaust A/F becomes
a target A/F), or such that a fuel addition timing becomes a predetermined timing.
That is, a desired amount of fuel from the fuel addition valve 26 is supplied by injection
to the exhaust system 7 (to an exhaust manifold 72 from exhaust ports 71) at an appropriate
timing.
[0045] The intake system 6 is provided with an intake manifold 63 connected to an intake
port 15a formed in a cylinder head 15 (see FIG. 2), and an intake tube 64 that constitutes
an intake path is connected to the intake manifold 63. Also, in this intake path,
an air cleaner 65, an airflow meter 43, and a throttle valve 62 are disposed in that
order from the upstream side. The airflow meter 43 outputs an electrical signal corresponding
to the amount of air that flows into the intake path via the air cleaner 65.
[0046] The exhaust system 7 is provided with the exhaust manifold 72 connected to the exhaust
ports 71 formed in the cylinder head 15, and exhaust tubes 73 and 74 that constitute
an exhaust path are connected to the exhaust manifold 72. Also, in this exhaust path,
a maniverter (exhaust purification apparatus) 77 is disposed that is provided with
a NOx storage catalyst (NSR catalyst: NOx storage reduction catalyst) 75 and a DPNR
catalyst (diesel particulate-NOx reduction catalyst) 76, which are described later.
The following is a description of the NSR catalyst 75 and the DPNR catalyst 76.
[0047] The NSR catalyst 75 is an NOx storage and reduction catalyst, and is configured using,
for example, alumina (Al
2O
3) as a support, with, for example, an alkali metal such as potassium (K), sodium (Na),
lithium (Li), or cesium (Cs), an alkaline earth element such as barium (Ba) or calcium
(Ca), a rare earth element such as lanthanum (La) or Yttrium (Y), and a precious metal
such as platinum (Pt) supported on this support.
[0048] In a state in which a large amount of oxygen is present in the exhaust, the NSR catalyst
75 stores NOx, and in a state in which the oxygen concentration in the exhaust is
low and a large amount of a reduction component (for example, an unburned component
(HC) of fuel) is present, the NSR catalyst 75 reduces NOx to NO
2 or NO and releases the resulting NO
2 or NO. NOx that has been released as NO
2 or NO is further reduced due to quickly reacting with HC or CO in the exhaust and
becomes N
2. Also, by reducing NO
2 or NO, HC and CO themselves are oxidized and thus become H
2O and CO
2. In other words, by appropriately adjusting the oxygen concentration or the HC component
in the exhaust introduced to the NSR catalyst 75, it is possible to purify HC, CO,
and NOx in the exhaust. In the configuration of the present embodiment, adjustment
of the oxygen concentration or the HC component in the exhaust can be performed with
an operation to add fuel from the aforementioned fuel addition valve 26.
[0049] On the other hand, in the DPNR catalyst 76, an NOx storage and reduction catalyst
is supported on a porous ceramic structure, for example, and PM in exhaust gas is
captured when passing through a porous wall. When the air-fuel ratio of the exhaust
gas is lean, NOx in the exhaust gas is stored in the NOx storage and reduction catalyst,
and when the air-fuel ratio is rich, the stored NOx is reduced and released. Furthermore,
a catalyst that oxidizes/burns the captured PM (for example, an oxidization catalyst
whose main component is a precious metal such as platinum) is supported on the DPNR
catalyst 76.
[0050] Here, the configuration of the combustion chamber 3 of the diesel engine and parts
in the vicinity of the combustion chamber 3 will be described. The following description
makes reference to FIG. 2. As shown in FIG. 2, in a cylinder block 11 that constitutes
part of the main body of the engine, a cylindrical cylinder bore 12 is formed in each
cylinder (each of four cylinders), and a piston 13 is housed within each cylinder
bore 12 such that the piston 13 can slide in the vertical direction.
[0051] The aforementioned combustion chamber 3 is formed on the top side of a top face 13a
of the piston 13. More specifically, the combustion chamber 3 is defined by a lower
face of the cylinder head 15 installed on top of the cylinder block 11 via a gasket
14, an inner wall face of the cylinder bore 12, and the top face 13a of the piston
13. Cavities 13b are concavely provided in approximately the center of the top face
13a of the piston 13, and these cavities 13b also constitute part of the combustion
chamber 3.
[0052] A small end 18a of a connecting rod 18 is linked to the piston 13 by a piston pin
13c, and a large end of the connecting rod 18 is linked to a crankshaft serving as
an engine output shaft. Thus, back and forth movement of the piston 13 within the
cylinder bore 12 is transmitted to the crankshaft via the connecting rod 18, and engine
output is obtained due to rotation of this crankshaft. Also, a glow plug 19 is disposed
facing the combustion chamber 3. The glow plug 19 glows due to the flow of electrical
current immediately before the engine 1 is started, and functions as a starting assistance
apparatus whereby ignition and combustion are promoted due to part of a fuel spray
being blown onto the glow plug.
[0053] In the cylinder head 15, the intake port 15a that introduces air to the combustion
chamber 3 and the exhaust port 71 that discharges exhaust gas from the combustion
chamber 3 are respectively formed, and an intake valve 16 that opens/closes the intake
port 15a and an exhaust valve 17 that opens/closes the exhaust port 71 are disposed.
The intake valve 16 and the exhaust valve 17 are disposed facing each other on either
side of a cylinder center line P. That is, the engine 1 is configured as a cross flow-type
engine. Also, the injector 23 that injects fuel directly into the combustion chamber
3 is installed in the cylinder head 15. The injector 23 is disposed approximately
at the center above the combustion chamber 3, in an erect orientation along the cylinder
center line P, and injects fuel introduced from the common rail 22 toward the combustion
chamber 3 at a predetermined timing.
[0054] Furthermore, as shown in FIG. 1, the engine 1 is provided with a turbocharger 5.
This turbocharger 5 is provided with a turbine wheel 5B and a compressor wheel 5C
that are linked via a turbine shaft 5A. The compressor wheel 5C is disposed facing
the inside of the intake tube 64, and the turbine wheel 5B is disposed facing the
inside of the exhaust tube 73. Thus the turbocharger 5 uses exhaust flow (exhaust
pressure) received by the turbine wheel 5B to rotate the compressor wheel 5C, thereby
performing a so-called turbocharging operation that increases the intake pressure.
In the present embodiment, the turbocharger 5 is a variable nozzle-type turbocharger,
in which a variable nozzle vane mechanism (not shown) is provided on the turbine wheel
5B side, and by adjusting the opening degree of this variable nozzle vane mechanism
it is possible to adjust the turbocharging pressure of the engine 1.
[0055] An intercooler 61 for forcibly cooling intake air heated due to supercharging with
the turbocharger 5 is provided in the intake tube 64 of the intake system 6. The throttle
valve 62 provided on the downstream side from the intercooler 61 is an electronically
controlled opening/closing valve whose opening degree is capable of stepless adjustment,
and functions to constrict the area of the path of intake air under predetermined
conditions, and thus adjust (reduce) the supplied amount of intake air.
[0056] Also, the engine 1 is provided with an exhaust gas recirculation path (EGR path)
8 that connects the intake system 6 and the exhaust system 7. The EGR path 8 decreases
the combustion temperature by appropriately recirculating part of the exhaust to the
intake system 6 and resupplying that exhaust to the combustion chamber 3, thus reducing
the amount of NOx produced. Also, provided in the EGR path 8 are an EGR valve 81 that
by being opened/closed steplessly under electronic control is capable of freely adjusting
the amount of exhaust flow that flows through the EGR path 8, and an EGR cooler 82
for cooling exhaust that passes through (recirculates through) the EGR path 8.
- Sensors -
[0057] Various sensors are installed at respective sites in the engine 1, and these sensors
output signals related to environmental conditions at the respective sites and the
operating state of the engine 1.
[0058] For example, the above airflow meter 43 outputs a detection signal corresponding
to an intake air flow amount (intake air amount) on the upstream side of the throttle
valve 62 within the intake system 6. An intake temperature sensor 49 is disposed in
the intake manifold 63, and outputs a detection signal corresponding to the temperature
of intake air. An intake pressure sensor 48 is disposed in the intake manifold 63,
and outputs a detection signal corresponding to the intake air pressure. An A/F (air-fuel
ratio) sensor 44 outputs a detection signal that continuously changes according to
the oxygen concentration in the exhaust on the downstream side of the maniverter 77
of the exhaust system 7. An exhaust temperature sensor 45 likewise outputs a detection
signal corresponding to the temperature of the exhaust gas (exhaust temperature) on
the downstream side of the maniverter 77 of the exhaust system 7. A rail pressure
sensor 41 outputs a detection signal corresponding to the pressure of fuel accumulated
in the common rail 22. A throttle opening degree sensor 42 detects the opening degree
of the throttle valve 62.
-ECU-
[0059] As shown in FIG. 3, the ECU 100 is provided with a CPU 101, a ROM 102, a RAM 103,
a backup RAM 104, and the like. In the ROM 102, various control programs, maps that
are referred to when executing those various control programs, and the like are stored.
The CPU 101 executes various computational processes based on the various control
programs and maps stored in the ROM 102. The RAM 103 is a memory that temporarily
stores data resulting from computations with the CPU 101 or data that has been input
from the respective sensors, and the backup RAM 104, for example, is a nonvolatile
memory that stores that data or the like to be saved when the engine 1 is stopped.
[0060] The CPU 101, the ROM 102, the RAM 103, and the backup RAM 104 are connected to each
other via a bus 107, and are connected to an input interface 105 and an output interface
106 via the bus 107.
[0061] The rail pressure sensor 41, the throttle opening degree sensor 42, the airflow meter
43, the A/F sensor 44, the exhaust temperature sensor 45, the intake pressure sensor
48, and the intake temperature sensor 49 are connected to the input interface 105.
Further, a water temperature sensor 46 that outputs a detection signal corresponding
to the coolant temperature of the engine 1, an accelerator opening degree sensor 47
that outputs a detection signal corresponding to the amount that an accelerator pedal
is depressed, a crank position sensor 40 that outputs a detection signal (pulse) each
time that the output shaft (crankshaft) of the engine 1 rotates a fixed angle, and
the like are connected to the input interface 105. On the other hand, the aforementioned
injectors 23, fuel addition valve 26, throttle valve 62, EGR valve 81, and the like
are connected to the output interface 106.
[0062] The ECU 100 executes various controls of the engine 1 based on the output of the
various sensors described above. Furthermore, the ECU 100 executes pilot injection,
pre-injection, main injection, after-injection, and post injection, as control of
fuel injection of the injectors 23.
[0063] The fuel injection pressure when executing these fuel injections is determined by
the internal pressure of the common rail 22. As the common rail internal pressure,
ordinarily, the target value of the fuel pressure supplied from the common rail 22
to the injectors 23 (i.e., the target rail pressure) is set to increase as the engine
load increases, and as the engine revolution increases. That is, when the engine load
is high, a large amount of air is drawn into the combustion chamber 3, so it is necessary
to inject a large amount of fuel into the combustion chamber 3 from the injectors
23, and therefore it is necessary to set a high injection pressure from the injectors
23. Also, when the engine revolution is high, the period during which injection is
possible is short, so it is necessary to inject a larger amount of fuel per unit time,
and therefore it is necessary to set a high injection pressure from the injectors
23. In this way, the target rail pressure is ordinarily set based on the engine load
and the engine revolution. As one of the features of the present invention, a specific
method for setting the target value of the fuel pressure is explained later.
[0064] The optimum values of fuel injection parameters for fuel injection such as the above
pilot injection, main injection, and the like differ depending on temperature conditions
of the engine, intake air, and the like.
[0065] For example, the ECU 100 adjusts the amount of fuel discharged by the supply pump
21 such that the common rail pressure becomes the same as the target rail pressure
set based on the engine operating state, i.e., such that the fuel injection pressure
matches the target injection pressure. Also, the ECU 100 determines the fuel injection
amount and the form of fuel injection based on the engine operating state. Specifically,
the ECU 100 calculates an engine revolution speed based on the value detected by the
crank position sensor 40 and obtains an amount of accelerator pedal depression (accelerator
opening degree) based on the value detected by the accelerator opening degree sensor
47, and determines the total fuel injection amount (the sum of the injection amount
in pre-injection and the injection amount in main injection) based on the engine revolution
speed and the accelerator opening degree.
- Setting of Target Fuel Pressure -
[0066] The following is an explanation of a procedure for setting the target fuel pressure
and of a fuel pressure setting map, which are characteristic for the present embodiment.
First, the technical idea behind setting the target fuel pressure in the present embodiment
is explained.
[0067] In the diesel engine 1, it is important to satisfy several requirements at the same
time, namely to improve the exhaust emissions by reducing the amount of NOx generated,
to reduce combustion noise during the combustion stroke, and to ensure a sufficient
engine torque. The inventors of the present invention recognized that, as a way to
satisfy these requirements at the same time, it is effective to suitably control the
change of the heat generation rate within the cylinder during the combustion stroke
(the change represented by the waveform of the heat generation rate), and, as a way
to control this change of the heat generation rate, found the procedure of setting
the target fuel pressure described in the following.
[0068] The solid line in Fig. 4 indicates the ideal waveform of the heat generation rate
for the combustion of fuel injected at the main injection, where the horizontal axis
denotes the crank angle and the vertical axis denotes the heat generation rate. TDC
in the drawing indicates the crank angle position corresponding to the compression
top dead center of the piston 13. As this heat generation rate waveform, the combustion
of the fuel injected at the main injection commences from the compression top dead
center (TDC) of the piston 13, the heat generation rate reaches its local maximum
(peak) at a predetermined piston position after compression top dead center (for example
at the time of 10° after compression top dead center (ATDC 10°)), and the combustion
of the fuel injected at the main injection is finished at a further predetermined
piston position after compression top dead center (for example at the time of 25°
after compression top dead center (ATDC 25°). If the combustion of the air-fuel mixture
is carried out with such a change of the heat generation ratio, then for example 50%
of the air-fuel mixture within the cylinder will be completely combusted at the time
of 10° after compression top dead center (ATDC 10°). That is to say, about 50% of
the total amount of heat generated in the expansion stroke is generated until ATDC
10°, and it becomes possible to operate the engine 1 with high thermal efficiency.
[0069] The waveform denoted by the dash-dotted line in Fig. 4 denotes the waveform of the
heat generation rate for the combustion of fuel that is injected at the pre-injection.
Thus, a stable diffusion combustion of the fuel injected at the main injection is
realized. For example, a heat amount of 10[J] is generated by the combustion of the
fuel injected at this pre-injection. There is no limitation to this value. For example,
it may be set as appropriate in accordance with the total amount of the fuel injection.
Furthermore, while not shown in the drawings, also a pilot injection is carried out
prior to the pre-injection, sufficiently raising the temperature inside the cylinder,
so that favorable ignition characteristics of the fuel injected at the main injection
can be maintained.
[0070] Thus, in the present embodiment, sufficient pre-warming inside the cylinder is carried
out by the pilot injection and the pre-injection. Due to this pre-warming, when the
main injection, which is explained later, begins, the fuel injected at this main injection
is immediately exposed to a temperature environment of at least its own self-ignition
temperature, so that thermal decomposition advances, and the combustion begins immediately
after the injection.
[0071] More specifically, there are physical delays and chemical delays as fuel ignition
delays in diesel engines. A physical delay is the time required for the vaporization
and mixing of the fuel drops, which depends on the gas temperature of the combustion
space. On the other hand, a chemical delay is the time required for the chemical breakdown
of compounds of the fuel vapor and for the heat generation by oxidation. The physical
delay can be suppressed to a minimum in situations in which there is pre-heating within
the cylinder, as described above, and as a result, also the ignition delay can be
suppressed to a minimum.
[0072] Consequently, as a combustion form of fuel injected by the main injection, almost
no pre-mixing combustion takes place. As a result, controlling the fuel injection
timing becomes almost the same as controlling the combustion timing, and the controllability
of the combustion can be greatly improved. That is to say, up to now, this premixing
combustion took up a large proportion of the combustion in diesel engines, but in
the present embodiment, the proportion of this premixing combustion is suppressed
to a minimum, making it possible to largely improve the controllability of the combustion
by controlling the waveform of the heat generation rate (ignition period and heat
generation amount) through control of the fuel injection timing and fuel injection
amount (control of the injection rate waveform). In the present embodiment, this new
form of combustion is referred to as "successive combustion (combustion that begins
immediately after the fuel has been injected)" or "controlled combustion (combustion
that is actively controlled through the fuel injection timing and the fuel injection
amount)".
[0073] The waveform of the dash-dot-dot line a in Fig. 4 shows waveform of the heat generation
rate for the case that the fuel injection pressure is set to be higher than an appropriate
value, leading to a state where the combustion speed and the peak value are both too
high, and there is the concern that the combustion noise becomes large and there is
an increased amount of NOx generated. On the other hand, the waveform of the dash-dot-dot
line β in Fig. 4 shows the heat generation rate waveform for the case that the fuel
injection pressure is set to be lower than an appropriate value, leading to a state
where the combustion speed is low and the timing of the peak is shifted considerably
towards later angles, so that there is the concern that a sufficient engine torque
cannot be ensured.
[0074] As explained above, the procedure for setting the target fuel pressure in accordance
with the present embodiment is based on the technical idea of achieving increased
combustion efficiency by optimizing the change of the heat generation rate (optimizing
the heat generation rate waveform). In order to realize this, the target fuel pressure
is set as described below. In the following, several embodiments of procedures for
setting the target fuel pressure are described.
First Embodiment
[0075] A first embodiment is described first.
[0076] The solid line in Fig. 5 shows the relation between the required output (required
power) of the engine 1 according to the present embodiment and the target fuel pressure
set in accordance with this required output. Thus, the required output and the target
fuel pressure are proportional to each other, and the target fuel pressure can be
determined unambiguously from the required output. In other words, a target fuel pressure
is allocated in advance to each requested output.
[0077] Referring to Fig. 5, the following is a more specific explanation of the procedure
for setting the target fuel pressure in accordance with the requested output.
[0078] First, a provisional fuel pressure line as indicated by the broken line in Fig. 5
is set. This provisional fuel pressure line is set such that when the requested output
is "0", also the target fuel pressure becomes "0", as a straight line passing through
the origin in the graph of Fig. 5 and having a predetermined slope.
[0079] The slope of this provisional fuel pressure line is determined for example by the
exhaust amount of the engine 1. That is to say, the larger the exhaust amount of the
engine 1 is, the smaller the slope of the provisional fuel pressure line is set, for
example. The target fuel pressures on this provisional fuel pressure line correspond
to the provisional fuel injection pressures of the present invention, and these provisional
fuel injection pressures are determined through the proportional relation with the
requested output, which is given by a predetermined proportionality constant (corresponding
to the slope of the provisional fuel pressure line). That is to say, the provisional
fuel injection pressures can be determined by multiplying the requested output with
the predetermined proportionality constant, and the set of these provisional fuel
injection pressures constitutes the provisional fuel pressure line.
[0080] Then, the provisional fuel pressure line is shifted parallel towards the high fuel
pressure side (upwards in Fig. 5) by a predetermined pressure offset with respect
to a power centroid (the point of 40 kW requested output in the graph shown in Fig.
5) on the provisional fuel pressure line, whereby the fuel pressure line shown by
the solid line in the figure is set. It should be noted that there is no limitation
to the above-noted value as the power centroid.
[0081] Here, the power centroid is set as the value corresponding to that output that is
used with the highest frequency among the outputs of the engine 1.
[0082] Furthermore, the pressure offset amount is set such that the heat generation rate
within the cylinder reaches its local maximum (peak) at a predetermined piston position
after compression top dead center (at the time of 10° after compression top dead center
(ATDC 10°), if the fuel of the main injection injected by the injector 23 begins its
combustion at the compression top dead center (TDC) of the piston 13. That is to say,
the pressure offset amount is set such that at the power centroid the ideal heat generation
rate waveform shown by the solid line in Fig. 4 is attained. It should be noted that
this pressure offset amount depends on the exhaust amount and the number of cylinders
of the engine 1, and is set individually for each type of engine 1 through advance
experimentation or simulation. Moreover, the fuel supply system 2 of the engine 1
according to the present embodiment is set to 200 MPa as an upper limit of the target
fuel pressure (maximum rail pressure).
[0083] Fig. 6 is a fuel pressure setting map that is looked up when deciding the target
fuel pressure. This fuel pressure setting map is prepared in accordance with the fuel
pressure line shown by the solid line in Fig. 5, and is stored for example in the
ROM 102. In this fuel pressure setting map, the horizontal axis denotes engine revolution
and the vertical axis denotes engine torque. Tmax in Fig. 6 denotes the maximum torque
line.
[0084] As a feature of this fuel pressure setting map the lines of equal fuel injection
pressures (regions of equal fuel injection pressures) denoted by A - I in the figure
are allocated to equal power lines (regions of equal output) of the requested output
(requested power) of the engine 1 that is determined based on, for example, the amount
by which the accelerator pedal is pressed down. That is to say, this fuel pressure
setting map is set such that the lines of equal power and the lines of equal fuel
injection pressure substantially match.
[0085] More specifically, the curve A in Fig. 6 is the line where the requested engine output
is 10 kW, and the line of a fuel injection pressure of 66 MPa is allocated to this
line. Similarly, the curve B is the line where the requested engine output is 20 kW,
and the line of a fuel injection pressure of 83 MPa is allocated to this line. The
curve C is the line where the requested engine output is 30 kW, and the line of a
fuel injection pressure of 100 MPa is allocated to this line. The curve D is the line
where the requested engine output is 40 kW, and the line of a fuel injection pressure
of 116 MPa is allocated to this line. The curve E is the line where the requested
engine output is 50 kW, and the line of a fuel injection pressure of 133 MPa is allocated
to this line. The curve F is the line where the requested engine output is 60 kW,
and the line of a fuel injection pressure of 150 MPa is allocated to this line. The
curve G is the line where the requested engine output is 70 kW, and the line of a
fuel injection pressure of 166 MPa is allocated to this line. The curve H is the line
where the requested engine output is 80 kW, and the line of a fuel injection pressure
of 183 MPa is allocated to this line. The curve I is the line where the requested
engine output is 90 kW, and the line of a fuel injection pressure of 200 MPa is allocated
to this line. There is no limitation to these values, and they can be set as appropriate
in view of the performance characteristics of the engine 1.
[0086] Moreover, in these lines A - I, the proportion of change of the fuel injection pressure
with respect to a change in the requested engine output is set to be substantially
equivalent.
[0087] Accordingly, a fuel injection pressure control apparatus in accordance with the present
invention is constituted by the ROM 102 in which this fuel pressure setting map is
stored, the supply pump 21, and the CPU 101.
[0088] Thus, the target fuel pressure that is appropriate for the requested output of the
engine 1 is set in accordance with the fuel pressure setting map prepared in this
manner, and the supply pump 21 is controlled accordingly, for example.
[0089] Moreover, the fuel injection pressure increases when the engine revolution and the
engine torque increase simultaneously (see arrow I in Fig. 6), when the engine torque
increases at constant engine revolution (see arrow II in Fig. 6), or when the engine
revolution increases at constant engine torque (see arrow III in Fig. 6). Thus, when
the engine torque (engine load) is high, a fuel injection amount that is suitable
for the intake air amount can be ensured, and when the engine revolution is high,
the necessary fuel injection amount can be ensured within a short period of time by
increasing the fuel injection amount per unit time. Therefore, it is possible to consistently
realize a combustion form of the ideal heat generation rate waveform shown by the
solid line in Fig. 4, regardless of the engine output and the engine revolution, and
it becomes possible to satisfy the requirements of improving the exhaust emissions
by reducing the amount of NOx generated, reducing combustion noise during the combustion
stroke, and ensuring a sufficient engine torque.
[0090] On the other hand, if the engine output does not change following a change in the
engine revolution and the engine torque (corresponding to the arrow IV in Fig. 6),
the optimal value of the fuel injection pressure that was set until then is maintained
without changing the fuel injection pressure. That is to say, the fuel injection pressure
is not changed due to the change of the engine operation following this line of equal
fuel injection pressure (coinciding with the line of equal power), and the combustion
form of the above-noted ideal heat generation rate waveform is continued. In this
case, it becomes possible to continuously satisfy the requirements of improving the
exhaust emissions by reducing the amount of NOx generated, reducing combustion noise
during the combustion stroke, and ensuring a sufficient engine torque.
[0091] As noted above, in the present embodiment, an unambiguous correlation is maintained
between the requested output (requested power) of the engine 1 and the fuel injection
pressure (common rail pressure), and in a situation in which the engine output changes
due to a change in at least one of the engine revolution and engine torque, a fuel
injection with a correspondingly suitable fuel pressure can be carried out, whereas
conversely in a situation in which the engine output does not change even though the
engine revolution or the engine torque changes, the fuel pressure is not changed from
the suitable value that was set so far. Thus, it becomes possible to let the change
of the heat generation rate approach an ideal state across the entire engine operation
region. Moreover, in the present embodiment, a systematic procedure for setting the
fuel pressure is implemented that is common to a number of engine types, so that it
is possible to simplify the preparation of the fuel pressure setting map for setting
the suitable fuel injection pressure in accordance with the operation state of the
engine 1.
Second Embodiment
[0092] The following is an explanation of a second embodiment. In this embodiment, a modified
example of the fuel pressure setting map is used, whereas the remaining configuration
and control method are the same as in the first embodiment. Accordingly, only the
fuel pressure setting map is explained.
[0093] Fig. 7 shows a fuel pressure setting map that is referenced when deciding the target
fuel pressure in the present embodiment. This fuel pressure setting map is stored
for example in the above-mentioned ROM 102.
[0094] As in the above-described first embodiment, a feature of this fuel pressure setting
map is that the lines of equal fuel injection pressure (regions of equal fuel injection
pressure), which are indicated by A - L in the figure, are allocated to lines of equal
power (regions of equal power) of the requested output (requested power) for the engine
1 that is determined based on the amount by which the accelerator pedal is pressed
down. That is to say, also in this fuel pressure setting map, the lines of equal power
and the lines of equal fuel injection pressure are set to substantially match each
other.
[0095] More specifically, the curve A in Fig. 7 is the line where the requested engine output
is 10 kW, and the line of a fuel injection pressure of 30 MPa is allocated to this
line. Similarly, the curve B is the line where the requested engine output is 20 kW,
and the line of a fuel injection pressure of 45 MPa is allocated to this line. The
curve C is the line where the requested engine output is 30 kW, and the line of a
fuel injection pressure of 60 MPa is allocated to this line. The curve D is the line
where the requested engine output is 40 kW, and the line of a fuel injection pressure
of 75 MPa is allocated to this line. The curve E is the line where the requested engine
output is 50 kW, and the line of a fuel injection pressure of 90 MPa is allocated
to this line. The curve F is the line where the requested engine output is 60 kW,
and the line of a fuel injection pressure of 105 MPa is allocated to this line. The
curve G is the line where the requested engine output is 70 kW, and the line of a
fuel injection pressure of 120 MPa is allocated to this line. The curve H is the line
where the requested engine output is 80 kW, and the line of a fuel injection pressure
of 135 MPa is allocated to this line. The curve I is the line where the requested
engine output is 90 kW, and the line of a fuel injection pressure of 150 MPa is allocated
to this line. The curve J is the line where the requested engine output is 100 kW,
and the line of a fuel injection pressure of 165 MPa is allocated to this line. The
curve K is the line where the requested engine output is 110 kW, and the line of a
fuel injection pressure of 180 MPa is allocated to this line. The curve L is the line
where the requested engine output is 120 kW, and the line of a fuel injection pressure
of 200 MPa is allocated to this line. There is no limitation to these values, and
they can be set as appropriate in view of the performance characteristics of the engine
1.
[0096] Moreover, in these lines A - L, the proportion of change of the fuel injection pressure
with respect to a change in the requested engine output is set to become smaller as
the engine revolution becomes lower. That is to say, the distance between the lines
is set to be wider in the region of small revolutions than in the region of high revolutions.
[0097] Thus, the target fuel pressure that is appropriate for the requested output of the
engine 1 is set in accordance with the fuel pressure setting map prepared in this
manner, and the supply pump 21 is controlled accordingly, for example.
[0098] Moreover, the fuel injection pressure increases when the engine revolution and the
engine torque increase simultaneously (see arrow I in Fig. 7), when the engine torque
increases at constant engine revolution (see arrow II in Fig. 7), or when the engine
revolution increases at constant engine torque (see arrow III in Fig. 7). Thus, when
the engine torque (engine load) is high, a fuel injection amount that is suitable
for the intake air amount can be ensured, and when the engine revolution is high,
the necessary fuel injection amount can be ensured within a short period of time by
increasing the fuel injection amount per unit time. Therefore, it is possible to consistently
realize a combustion form of the ideal heat generation rate waveform shown by the
solid line in Fig. 4, regardless of the engine output and the engine revolution, and
it becomes possible to satisfy the requirements of improving the exhaust emissions
by reducing the amount of NOx generated, reducing combustion noise during the combustion
stroke, and ensuring a sufficient engine torque.
[0099] On the other hand, if the engine output does not change following a change in the
engine revolution and the engine torque (corresponding to the arrow IV in Fig. 7),
the suitable value of the fuel injection pressure that was set until then is maintained
without changing the fuel injection pressure. That is to say, the fuel injection pressure
is not changed due to the change of the engine operation following this line of equal
fuel injection pressure (coinciding with the line of equal power), and the combustion
form of the above-noted ideal heat generation rate waveform is continued. In this
case, it becomes possible to continuously satisfy the requirements of improving the
exhaust emissions by reducing the amount of NOx generated, reducing combustion noise
during the combustion stroke, and ensuring a sufficient engine torque.
[0100] As noted above, in the present embodiment, an unambiguous correlation is maintained
between the requested output (requested power) of the engine 1 and the fuel injection
pressure (common rail pressure). Thus, it becomes possible to let the change of the
heat generation rate approach an ideal state across the entire engine operation region.
Moreover, in the present embodiment, a systematic procedure for setting the fuel pressure
is implemented that is common to a number of engine types, so that it is possible
to simplify the preparation of the fuel pressure setting map for setting the suitable
fuel injection pressure in accordance with the operation state of the engine 1.
[0101] And as noted above, with the fuel pressure setting map of the present embodiment,
the proportion of the change amount of the fuel injection pressure with respect to
change of the engine output is set to become smaller as the engine revolution becomes
lower. Therefore, changes in the fuel injection pressure in the region of lower revolutions
of the engine 1 become smooth, so that a sudden increase of the combustion pressure
within the cylinder can be avoided in this operation state, and the generation of
oscillations and noise accompanying combustion can be suppressed. On the other hand,
in the region of high revolutions of the engine 1, there is a large change of the
fuel injection pressure as the torque increases, for example, so that the requested
output can be quickly attained and a favorable responsiveness of the engine 1 is achieved.
Third Embodiment
[0102] The following is an explanation of a third embodiment. In the above-described first
embodiment, the fuel pressure line (see Fig. 5) was set such that the target fuel
pressure was proportional to the requested output of the engine 1. Instead, in the
present embodiment, an optimization of the fuel pressure line is attained through
a corrective decrease or a corrective increase of the target fuel pressure with respect
to the fuel pressure line shown in Fig. 5 (in the present embodiment, this fuel pressure
line is a second provisional fuel pressure line, explained below, for determining
the provisional fuel injection pressure of the present invention). This is explained
in detail in the following.
[0103] The solid line in Fig. 8 denotes the relation between the requested output (requested
power) of the engine 1 according to the present embodiment and the target fuel pressure
that is set in accordance with this requested output. As shown, the requested output
power and the target fuel pressure are not proportional to each other, but the target
fuel pressure can be decided unambiguously from the requested power. In other words,
the target fuel pressures are allocated in advance to the requested outputs.
[0104] Referring to Fig. 8, the following is a more specific explanation of a procedure
for setting the target fuel pressure in accordance with the requested output.
[0105] First, as in the case of the above-described first embodiment, a first provisional
fuel pressure line (provisional fuel pressure line of the first embodiment) as indicated
by the dash-dotted line in Fig. 8 is set. This first provisional fuel pressure line
is set such that when the requested output is "0", also the target fuel pressure becomes
"0", as a line passing through the origin in the graph of Fig. 8 and having a predetermined
slope.
[0106] As in the case of the above-described first embodiment, the slope of this first provisional
fuel pressure line is determined for example by the exhaust amount of the engine 1.
The target fuel pressures on this first provisional fuel pressure line correspond
to the provisional fuel injection pressures of the present invention, and these provision
fuel injection pressures are determined by the proportional relation with the requested
output, which is given by a predetermined proportionality constant (corresponding
to the slope of the first provisional fuel pressure line). That is to say, the provisional
fuel injection pressures can be determined by multiplying the requested output with
the predetermined proportionality constant, and the set of these provisional fuel
injection pressures constitute the first provisional fuel pressure line.
[0107] Then, the first provisional fuel pressure line is shifted parallel towards the high
fuel pressure side (upwards in Fig. 8) by a predetermined pressure offset (a pressure
basic offset according to the present invention) with respect to a power centroid
on the first provisional fuel pressure line (the point where the requested output
is 40 kW in the graph shown in Fig. 8), whereby a second provisional fuel pressure
line shown by the broken line in the figure is set.
It should be noted that there is no limitation to the above-noted value as the power
centroid.
[0108] The power centroid and the pressure offset amount are determined in the same manner
as in the case of the above-described first embodiment, so that further explanations
are omitted here.
[0109] The final fuel pressure line is set by subjecting the second provisional pressure
line that has been set in this manner to a corrective decrease or a corrective increase
of the target fuel pressure, as explained below.
[0110] First, the fuel injection pressure in the output region where combustion noise is
addressed, which is a region where the output requested by the engine 1 is relatively
low, is determined by correctively decreasing the fuel pressure on the second provisional
fuel pressure line (the reference pressure in the present invention). The amount by
which the reference pressure on the second provisional fuel pressure line is correctively
reduced is set such that it becomes larger the smaller the output requested by the
engine 1 is. That is to say, the smaller the output requested by the engine 1 is,
the more the reference pressure on the second provisional pressure line is reduced,
and the lower the target fuel pressure is set.
[0111] The fuel injection pressure at the output region where NOx is addressed, which is
a region where the output requested by the engine 1 is relatively high, is determined
by correctively decreasing the reference pressure on the second provisional fuel pressure
line. The amount by which the reference pressure on the second provisional fuel pressure
line is correctively reduced is set to become larger the larger the output requested
by the engine 1 is. That is to say, the larger the output requested by the engine
1 is, the more the reference pressure on the second provisional fuel pressure line
is reduced, and the lower the target fuel pressure is set.
[0112] Furthermore, the fuel injection pressure at the output region where smoke is addressed,
which is roughly an output region, of the possible output regions of the internal
combustion engine 1, where the output requested by the engine 1 is intermediate, is
determined by correctively increasing the reference pressure on the second provisional
fuel pressure line. The amount by which the reference pressure on the second provisional
fuel pressure line is correctively increased is set to become smaller towards the
output region where the combustion noise is addressed and towards the output region
where the NOx is addressed, so that continuity of the fuel pressure line (continuity
between the output region where combustion noise is addressed and the output region
where smoke is addressed, and continuity between the output region where NOx is addressed
and the output region where smoke is addressed) can be ensured.
[0113] The following effects can be achieved by setting the fuel pressure line in this
manner and setting the target fuel pressure accordingly.
[0114] Since the fuel injection pressure is correctively decreased in the output region
where combustion noise is addressed, the combustion noise in the combustion chamber
3 can be suppressed to a low level in situations where the output of the engine 1
is relatively low, and the quietness of the engine 1 can be improved.
[0115] Moreover, since the fuel injection pressure is correctively decreased in the output
region where NOx is addressed, the combustion speed in the combustion chamber 3 can
be suppressed to a low level in situations where the output of the engine 1 is relatively
high, and the amount of NOx generated with the combustion in the cylinder can be reduced
considerably. Also, the requested output reaching the upper limit of the target fuel
pressure (maximum rail pressure) can be shifted towards the high output side.
[0116] Moreover, since the fuel injection pressure is correctively increased in the output
region where smoke is addressed, the fuel injection amount per unit time can be increased,
even when the main injection is implemented by a plurality of partial injections,
for example accompanying an increase in EGR, and a shortening of the injection period
can be accomplished, so that it is possible to overcome the deterioration of efficiency
that accompanies a lengthening of the injection period.
- Other Embodiments -
[0117] The above-described embodiments were explained for the case that the present invention
is applied to an inline four-cylinder diesel engine mounted in an automobile. However,
the present invention is not limited to use in automobiles, and can also be applied
to engines utilized for other uses. Moreover, there is no particular limitation concerning
the number of cylinders or the engine type (in-line engine, V-type engine, etc.)
[0118] Moreover, in the above-described embodiments, an NSR catalyst 75 and a DPNR catalyst
76 were provided as the maniverter 77, but it is also possible to provide an NSR catalyst
75 and a DPF (diesel particulate fitter).
[0119] Moreover, in the above-described embodiments, the lines of equal fuel injection pressure
are allocated to the lines of equal power across the entire engine operation region.
However, the present invention is not limited to this, and it is also possible to
provide a region where the lines of equal fuel injection pressure do not match the
lines of equal power, in a portion of the engine operation region (for example near
the maximum torque line Tmax).
[0120] Moreover, in the above-described embodiments, the provisional fuel pressure line
(the broken line in Fig. 5) and the first provisional fuel pressure line (the dash-dotted
line in Fig. 8) are straight lines, and the requested outputs and the target fuel
pressures are proportional on this line, but it is also possible to set the provisional
fuel pressure line and the first provisional fuel pressure line as curves (quadratic
curves), as shown by the dash-dot-dot lines in Fig. 5 and Fig. 8. However, also in
this case, it is necessary that the target fuel pressure can be decided unambiguously
from the requested output.
[Industrial Applicability]
[0121] The present invention can be applied to the control of the fuel injection pressure
in common-rail in-cylinder direct injection multi-cylinder diesel engines mounted
in automobiles.
[Reference Signs List]
[0122]
- 1
- engine (internal combustion engine)
- 3
- combustion chamber
- 13
- piston
- 23
- injector (fuel injection valve)