BACKGROUND OF THE INVENTION
1. FIELD OF THE INVENTION
[0001] The present invention relates to an internal combustion engine introducing an inert
gas into a combustion chamber so as to perform combustion in accordance with the preamble
of claim 1.
2. DESCRIPTION OF THE RELATED ART
[0002] Conventionally, in an internal combustion engine, for example, in a diesel engine,
in order to restrict generation of NOx, it is structured an engine exhaust passage
and an engine intake passage are connected by an exhaust gas recirculation (hereinafter,
refer to an EGR: an Exhaust Gas Recirculation) so as to recirculate the exhaust gas,
that is, EGR gas into the engine intake passage via the EGR passage. In this case,
since the EGR gas has a relatively high specific heat and accordingly can absorb a
large amount of heat, a combustion temperature within the combustion chamber is lowered
as an amount of the EGR gas is increased, that is, a rate of the EGR (EGR gas amount/(EGR
gas amount + intake air amount)) is increased. When the combustion temperature is
lowered, the generation amount of NOx is lowered, so that the more the EGR rate is
increased, the less the generation amount of NOx becomes.
[0003] As mentioned above, it has been conventionally known that the generation amount of
NOx can be lowered when the EGR rate is increased. However, in the case where the
EGR rate is increased, the generation amount of a soot, that is, the smoke suddenly
starts increasing when the EGR rate exceeds a certain limit. With respect to this
point, it has been conventionally considered that the smoke is unlimitedly increased
when the EGR rate is increased further, so that it has been considered that the EGR
rate at which the smoke suddenly starts increasing is the maximum allowable limit
of the EGR rate.
[0004] Accordingly, the EGR rate has been conventionally defined within a range which does
not exceed the maximum allowable limit. The maximum allowable limit of the EGR rate
is significantly different in correspondence to a type of the engine and a fuel, however,
is within a range from about 30 % to 50 %. Therefore, in the conventional diesel engine,
the EGR rate is restricted to the range from about 30 % to 50 % at the maximum.
[0005] As mentioned above, since it has been conventionally considered that the maximum
allowable limit exists with respect to the EGR rate, the EGR rate has been defined
within the range which does not exceed the maximum allowable limit and so that the
generation amount of NOx and the smoke becomes as least as possible. However, even
when the EGR rate is defined so that the generation amount of NOx and the smoke becomes
as least as possible, the reduction of the generation amount of NOx and the smoke
has a limit, so that actually a significant amount of NOx and smoke are still generated.
[0006] However, in the process of researching combustion in the diesel engine, it has been
found that when making the EGR rate greater than the maximum allowable limit, the
smoke is suddenly increased as mentioned above, however, the generation amount of
the smoke has a peak, and when further increasing the EGR rate to exceed the peak,
then the smoke suddenly starts reducing at this time. When setting the EGR rate to
the value equal to or more than 70 % at a time of an idling operation or strongly
cooling the EGR gas, the smoke becomes substantially 0, that is, the soot is hardly
generated when setting the EGR rate to the value equal to or more than 55 %. Further,
it has been found that the generation amount of NOx becomes significantly small amount
at this time. Thereafter, on the basis of this information, a consideration has been
performed with respect to the reason why the soot is not generated, as a result, a
new combustion system which has not been obtained and can simultaneously reduce the
soot and NOx has been constructed. The new combustion system will be in detail described
below. In a word, it is based on a principle that the growth of a hydrocarbon is stopped
in the middle of a step by which the hydrocarbon grows the soot.
[0007] That is, it is ascertained as a result of many experiments and researches that the
growth of the hydrocarbon stops in the middle of the step before becoming the soot
when the temperature of the fuel and the surrounding gas at a time of combustion within
the combustion chamber is equal to or less than a certain temperature, and that the
hydrocarbon grows the soot at a stroke when the temperature of the fuel and the surrounding
gas reaches a certain temperature. In this case, the temperature of the fuel and the
surrounding gas is greatly influenced by an endothermic effect of the gas surrounding
the fuel at a time when the fuel is burned, so that it is possible to control the
temperature of the fuel and the surrounding gas by adjusting the heat absorption amount
of the gas surrounding the fuel in correspondence to the generation amount at a time
of the fuel combustion.
[0008] Accordingly, when restricting the temperature of the fuel and the surrounding gas
at a time of the combustion within the combustion chamber to a level equal to or less
than the temperature at which the growth of the hydrocarbon stops halfway, the soot
is not generated, so that it is possible to restrict the temperature of the fuel and
the surrounding gas at a time of the combustion within the combustion chamber to the
level equal to or less than the temperature at which the growth of the hydrocarbon
stops on the way by adjusting the heat absorption amount of the gas surrounding the
fuel. On the contrary, the hydrocarbon that stops growing on the way before becoming
the soot can be easily purified by the after treatment using an oxidation catalyst
or the like. This is a basic principle of the new combustion system. The internal
combustion engine employing the new combustion system was already filed as EP 879,946
A2 by the present applicant.
[0009] Here, in a vehicle in which an automatic transmission is provided in an internal
combustion engine performing a conventional combustion, when the automatic transmission
is shifted up, for example, due to the increase in a vehicle speed, an ignition timing
of the internal combustion engine is delayed in order to reduce a shift change shock,
an amount of the intake air is reduced or an output torque of the engine is reduced.
[0010] Further, in the new combustion system as mentioned above, it is desired to reduce
the shock due to the torque change generated together with the shift change by the
automatic transmission.
SUMMARY OF THE INVENTION
[0011] An object of the present invention is to provide an internal combustion engine which
can reduce a shock generated together with a change of a torque generated by the engine
when the shift change is performed by the automatic transmission while simultaneously
preventing a soot (a smoke) from being discharged from the internal combustion engine
and preventing NOx from being discharged.
[0012] The above object is solved by combination of features of the main claim, the sub-claims
disclose further advantageous embodiments of the invention.
[0013] In accordance with the present invention, there is provided an internal combustion
engine structured such that a generation amount of a soot is gradually increased to
the peak when increasing an amount of an inert gas supplied within a combustion chamber,
a temperature of a fuel and a surrounding gas thereof at a time of burning within
the combustion chamber becomes lower than a temperature for generating a soot when
further increasing the amount of the inert gas supplied within the combustion chamber,
so that a soot is hardly generated, and an automatic transmission is connected to
the internal combustion engine, wherein it is possible to execute a combustion structured
such that an amount of an inert gas supplied within the combustion chamber is more
than an amount of the inert gas when the generation amount of the soot becomes peak
and a soot is hardly generated, and an air fuel ratio is reduced, an injection timing
of the fuel is delayed, or an amount of a recirculated exhaust gas is corrected to
be increased when the combustion such that the soot is hardly generated is performed
and the automatic transmission is under a control state.
[0014] Accordingly, in the case where the air fuel ratio is reduced, since the combustion
in which the soot is hardly generated is performed under a condition that an air tends
to be insufficient, the combustion is deteriorated due to the reduction of the air
fuel ratio when the combustion in which the soot is hardly generated is performed,
so that the torque generated by the engine is reduced. Accordingly, it is possible
to soften the shock due to the torque change when the torque generated by the engine
is changed together with the shift change by the automatic transmission.
[0015] Further, in the case where the injection timing of the fuel is delayed, the combustion
is deteriorated in accordance that the fuel supply is too late for the combustion
when the injection timing of the fuel supplied within the combustion chamber is delayed,
thus lowering the torque generated in the engine is lowered. Accordingly, it is possible
to reduce the shock due to the torque change when the torque generated in the engine
is changed in accordance that the shift change by the automatic transmission is performed.
[0016] Still further, in the case where the amount of the recirculated exhaust gas is corrected
to be increased, since the combustion in which the soot is hardly generated is performed
under a condition where the air tends to be insufficient, it is hard that the air
is supplied to the combustion chamber when the amount of the recirculated exhaust
gas is corrected to be increased when the combustion in which the soot is hardly generated
is performed, so that the air tends to be further insufficient. Accordingly, the combustion
is deteriorated and the torque generated in the engine is lowered. Therefore, it is
possible to reduce the shock generated by the torque change when the torque generated
in the engine is changed in accordance that the shift change by the automatic transmission
is performed.
[0017] Although this summary does not describe all the features of the present invention,
it should be understood that any combination of the features stated in the dependent
claims is within the scope of the present invention.
BRIEF DESCRIPTION OF THE DRAWINGS
[0018]
Fig. 1 is a total view of a compression ignition type internal combustion engine in
accordance with the present invention;
Fig. 2 is a graph which shows a change of a smoke, HC, CO and NOx in correspondence
to a change of an output torque and an air fuel ratio;
Figs. 3A and 3B are graphs which show a combustion pressure;
Fig. 4 is a view which shows a molecule of a fuel;
Fig. 5 is a graph which shows a relation between a generation amount of a smoke and
an EGR rate;
Fig. 6 is a graph which shows a relation between a total amount of an intake gas and
a required load;
Fig. 7 is a graph which shows a first operation area I and a second operation area
II;
Fig. 8 is a graph which shows an output of an air fuel ratio sensor;
Fig. 9 is a graph which shows an opening degree of a throttle valve, an opening degree
of an EGR control valve, an EGR rate, an air fuel ratio, an injection timing and an
injection amount in the required load;
Fig. 10 is a graph which shows an air fuel ratio in the first operation area I;
Figs. 11A and 11B are views which shows a map of a target opening degree of the throttle
valve and the like;
Fig. 12 is a graph which shows an air fuel ratio in a second combustion;
Figs. 13A and 13B are views which show a map of a target opening degree of the throttle
valve and the like;
Fig. 14 is a view which shows a map of a fuel injection amount;
Figs. 15 and 16 are flow charts for controlling an operation of an engine in accordance
with a first embodiment;
Fig. 17 is a graph which shows a relation between an air fuel ratio and a torque generated
in the engine;
Figs. 18 and 19 are flow charts for controlling an operation of an engine in accordance
with a second embodiment; and
Figs. 20 and 21 are flow charts for controlling the operation of the engine in accordance
with the second embodiment.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0019] Fig. 1 shows an embodiment in which the present invention is applied to a 4-stroke
compression ignition type internal combustion engine.
[0020] With reference to Fig. 1, a reference numeral 1 denotes a main body of an engine,
reference numeral 2 denotes a cylinder block, reference numeral 3 denotes a cylinder
head, reference numeral 4 denotes a piston, reference numeral 5 denotes a combustion
chamber, reference numeral 6 denotes an electrically controlled type fuel injection
valve, reference numeral 7 denotes an intake valve, reference numeral 8 denotes an
intake port, reference numeral 9 denotes an exhaust valve, and reference numeral 10
denotes an exhaust port, respectively. The intake port 8 is connected to a surge tank
12 via a corresponding intake branch pipe 11, and the surge tank 12 is connected to
a supercharger, for example, an outlet portion of a compressor 16 of an exhaust turbo
charger 15 via an intake duct 13 and an inter cooler 14. An inlet portion of the compressor
16 is connected to an air cleaner 18 via an air intake pipe 17, and a throttle valve
20 driven by a step motor 19 is arranged within the air intake pipe 17. Further, a
mass flow amount detecting device 21 for detecting a mass flow amount of a intake
air is arranged within the air intake pipe 17 disposed upward the throttle valve 20.
[0021] An automatic transmission 60 is connected to a crank shaft 69 serving as an output
shaft of the engine main body 1. The automatic transmission 60 is provided with a
torque converter 61 and a transmission 62, and an output shaft 71 of the transmission
62 is connected to a drive wheel of a vehicle via a differential gear (not shown).
[0022] The transmission 62 is of a known type which is provided with a planetary gear train
and frictional elements (a brake, a clutch and the like), and is structured to switch
an engaging state of the frictional elements by switching a control hydraulic pressure
and perform a fixation and connection of each of the elements in the planetary gear
train, thereby performing a shift change operation. The torque converter 61 is of
a known type which is provided with a pump directly connected to the engine output
shaft and a turbine driven by a fluid discharged by the pump, and an output shaft
of the turbine (hereinafter, referred to as

a converter output shaft") is directly connected to an input shaft of the transmission
62. The torque converter 61 has a known torque amplification function of amplifying
the torque input from the engine output shaft so as to output to the converter output
shaft. The automatic transmission 60 is provided with a converter output shaft rotating
speed sensor 63 which outputs a pulse signal having a frequency corresponding to a
rotating speed of the converter output shaft (that is, a rotating speed of the input
shaft of the transmission 62), and a transmission output shaft rotating speed sensor
64 which outputs a pulse signal having a frequency corresponding to a rotating speed
of the output shaft of the transmission 62, respectively.
[0023] A lockup mechanism 73 is provided within the torque converter 61. That is, the torque
converter 61 is connected to the crank shaft 69 so as to be rotated together with
the crank shaft 69, however, is provided with a pump cover 74, a pump impeller 75
supported by the pump cover 74, a turbine runner 77 mounted to an input shaft 76 of
an automatic transmission 70 and a stator, and a rotational movement of the crank
shaft 69 is transmitted to the input shaft 76 via the pump cover 74, the pump impeller
75 and the turbine runner 77.
[0024] The lockup mechanism 73 is mounted to the input shaft 76 in such a manner as to freely
move in an axial direction thereof, and is provided with a lockup clutch plate 78
which rotates together with the input shaft 76. In general, that is, when the lockup
is in on-state, a pressurized oil is supplied within a room 79 between the lockup
clutch plate 28 and the pump cover 74 via an oil passage within the input shaft 76,
and next the pressurized oil flown out from the room 79 is discharged via the oil
passage within the input shaft 76 after being fed within a room 80 around the pump
impeller 75 and the turbine runner 77. At this time, since a pressure difference between
the rooms 79 and 80 disposed in both sides of the lockup clutch plate 78 is hardly
generated, the lockup clutch plate 78 is apart from an inner wall surface of the pump
cover 74, so that at this time, a rotational force of the crank shaft 69 is transmitted
to the input shaft 76 via the pump cover 74, the pump impeller 75 and the turbine
runner 77.
[0025] When the lockup should be turned on, the pressurized oil is supplied within the room
80 via the oil passage within the input shaft 76, and the oil within the room 79 is
discharged via the oil passage within the input shaft 76. At this time, the pressure
within the room 80 becomes higher than the pressure within the room 79 and the lockup
clutch plate 78 is press contacted onto the inner peripheral surface of the pump cover
74, so that the crank shaft 69 and the input shaft 76 are in a directly connected
state in which they are rotated at a constant speed. A control of supplying an oil
within the rooms 79 and 80, that is, an on/off control of the lockup mechanism 73
is controlled by a control valve provided within the automatic transmission 70, and
the control valve is controlled on the basis of an output signal of an electronic
control unit 40. Further, a large number of clutches for performing a shift change
operation are provided within the automatic transmission 70, and these clutches are
controlled on the basis of the output signal of the electronic control unit 40.
[0026] On the contrary, the exhaust port 10 is connected to an inlet portion of an exhaust
turbine 23 of the exhaust turbo charger 15 via an exhaust manifold 22, and an outlet
portion of the exhaust turbine 23 is connected to a catalytic convener 26 containing
a catalyst 25 having an oxidation function therein via an exhaust pipe 24. An air
fuel ratio sensor 27 is arranged within the exhaust manifold 21.
[0027] An exhaust pipe 28 connected to an outlet portion of the catalyst converter 26 and
the air intake pipe 17 disposed downstream the throttle valve 20 are connected to
each other via an exhaust gas recirculation (hereinafter, referred to as an EGR) passage
29, and an EGR control valve 31 driven by a step motor 30 is arranged within the EGR
passage 29. Further, an inter cooler 32 for cooling an EGR gas flowing within the
EGR passage 29 is arranged within the EGR passage 29. In the embodiment shown in Fig.
1, an engine cooling water is introduced into the inter cooler 32, and the EGR gas
is cooled by the engine cooling water.
[0028] On the contrary, the fuel injection valve 6 is connected to a fuel reservoir, so-called
a common rail 34 via a fuel supply pipe 33. A fuel is supplied into the common rail
34 from an electrically controlled type fuel pump 35 in which a discharge amount is
variable, and the fuel supplied into the common rail 34 is supplied to the fuel injection
valve 6 via each of the fuel supply pipe 33. A fuel pressure sensor 36 for detecting
a fuel pressure within the common rail 34 is mounted to the common rail 34, so that
a discharge amount of the fuel pump 35 can be controlled. Therefore, the fuel pressure
within the common rail 34 becomes a target fuel pressure on the basis of an output
signal of the fuel pressure sensor 36.
[0029] An electronic control unit 40 is constituted by a digital computer, and is provided
with a read only memory (ROM) 42, a random access memory (RAM) 43, a microprocessor
(CPU) 44, an input port 45 and an output port 46 mutually connected by a two way bus
41. An output signal of the mass flow amount detecting device 21 is input to the input
port 45 via a corresponding AD converter 47, and output signals of the air fuel ratio
sensor 27 and the fuel pressure sensor 36 are also input to the input port 45 via
the corresponding AD converter 47, respectively. Pulse signals from the converter
output shaft rotating speed sensor 63 and the transmission output shaft rotating speed
sensor 64 are respectively input to the input port 45. A load sensor 51 for generating
an output voltage in proportion to a depression amount L of an accelerator pedal 50
is connected to the accelerator pedal 50, and an output voltage of the load sensor
51 is input to the input port 45 via the corresponding AD converter 47. Further, a
crank angle sensor 52 for generating an output pulse every time when the crank shaft
rotates, for example, at 30 degrees is connected to the input port 45. The engine
speed is calculated on the basis of the output value of the crank angle sensor 52.
On the contrary, the output port 46 is connected to the fuel injection valve 6, the
throttle valve controlling step motor 19, the EGR control valve controlling step motor
30 and the fuel pump 35 via the corresponding drive circuit 48.
[0030] Fig. 2 expresses an experimental embodiment which shows a change of an output torque
and a change of a discharge amount of a smoke, HC, CO and NOx when changing an air
fuel ratio A/F (an axis of abscissas in Fig. 2) by changing an opening degree of the
throttle valve 20 and the EGR rate at a time of operating the engine at a low load.
As is understood from Fig. 2, in this experimental embodiment, the smaller the air
fuel ratio A/F becomes, the greater the EGR rate is, and the EGR rate becomes equal
to or more than 65 % when the air fuel ratio is equal to or less than a stoichiometric
air fuel ratio (14.6).
[0031] As shown in Fig. 2, in the case of making the air fuel ratio A/F smaller by increasing
the EGR rate, the generation amount of the smoke starts increasing when the EGR rate
becomes near 40 % and the air fuel ratio A/F becomes about 30 %. Next, when further
increasing the EGR rate and making the air fuel ratio A/F smaller, the generation
amount of the smoke is suddenly increased to the peak. Next, when further increasing
the EGR rate and making the air fuel ratio A/F smaller, the smoke is suddenly reduced
at this time, and when the air fuel ratio A/F becomes near 15.0 with the EGR rate
set to a value equal to or more than 65 %, the amount of the smoke is substantially
0. That is, the soot is hardly generated. At this time, the output torque of the engine
is slightly reduced and the generation amount of NOx is significantly reduced. On
the contrary, the generation amount of HC and CO starts increasing at this time.
[0032] Fig. 3A shows a change of a combustion pressure within the combustion chamber 5 when
the air fuel ratio A/F is near 18 and the generation amount of the smoke is the largest,
and Fig. 3B shows a change of a combustion pressure within the combustion chamber
5 when the air fuel ratio A/F is near 13 and the generation amount of the smoke is
substantially 0. As is understood from comparison between Figs. 3A and 3B, the combustion
pressure in the case as shown in Fig. 3B in which the generation amount of the smoke
is substantially 0 is lower than that shown in Fig. 3A in which the generation amount
of the smoke is large.
[0033] The following results can be introduced from the experimental results shown in Figs.
2 and 3. That is, at first, when the air fuel ratio A/F is equal to or less than 15.0
and the generation amount of the smoke is substantially 0, the generation amount of
NOx is significantly reduced as shown in Fig. 2. The reduction of the generation amount
of NOx means the reduction of the combustion temperature within the combustion chamber
5, so that it is said that the combustion temperature within the combustion chamber
5 becomes low when the soot is hardly generated. The same matter can be applied to
the case as shown in Fig. 3. That is, in a state shown in Fig. 3B where the soot is
hardly generated, the combustion pressure becomes low, so that the combustion temperature
within the combustion chamber 5 becomes low.
[0034] Secondly, when the generation amount of the smoke, that is, the generation amount
of the soot becomes substantially 0, the discharge amount of HC and CO is increased
as shown in Fig. 2. This means that the hydrocarbon is discharged without growing
to the soot. That is, in a straight chain hydrocarbon or an aromatic hydrocarbon as
shown in Fig. 4 and contained in the fuel, when the temperature is increased in an
oxygen poor state, a precursor of the soot is formed due to a thermal decomposition,
and the soot containing a solid mainly formed by an aggregation of carbon atoms is
produced. In this case, the process of actually producing the soot is complex and
it is indefinite what aspect the precursor of the soot forms, however, in any event,
the hydrocarbon as shown in Fig. 4 grows to the soot via the precursor of the soot.
Accordingly, as mentioned above, when the generation amount of the soot becomes substantially
0, the discharge amount of HC and CO is increased as shown in Fig. 2, however, HC
at this time corresponds to the precursor of the soot or the hydrocarbon in the preceding
state.
[0035] Putting in order the considerations on the basis of the experimental results as shown
in Figs. 2 and 3, when the combustion temperature within the combustion chamber 5
is low, the generation amount of the soot becomes substantially 0, so that the precursor
of the soot or the hydrocarbon in the preceding state is discharged from the combustion
chamber 5. As a result of further performing the experiments and researches with respect
to the matter in detail, it becomes clear that the growing process of the soot stops
on the way, that is, no soot is generated, in the case where the temperature of the
fuel and the surrounding gas within the combustion chamber 5 is equal to or less than
a certain temperature, and that the soot is generated when the temperature of the
fuel and the surrounding gas within the combustion chamber 5 is equal to or more than
a certain temperature.
[0036] In this case, since the temperature of the fuel and the surrounding gas when the
growing process of the hydrocarbon stops in a state of the precursor of the soot,
that is, the certain temperature as mentioned above is changed due to various reasons,
for example, a kind of the fuel, a compression ratio of the air fuel ratio and the
like, it is not exactly said what degree the temperature is. However, the certain
temperature has a great relation to the generation amount of NOx, so that the certain
temperature can be defined from the generation amount of NOx at a certain level. That
is, as the EGR rate is increased, the temperature of the fuel and the surrounding
gas at a time of combustion is reduced, so that the generation amount of NOx is reduced.
At this time, the soot is hardly generated when the generation amount of NOx becomes
near 10 p.p.m. or less. Accordingly, the certain temperature mentioned above substantially
coincides with the temperature when the generation amount of NOx becomes near 10 p.p.m.
or less.
[0037] Once the soot is generated, the soot can not be purified in accordance with the after
treatment using the catalyst having an oxidation function. On the contrary, the precursor
of the soot or the hydrocarbon in the preceding state can be easily purified in accordance
with the after treatment using the catalyst having an oxidation function. As mentioned
above, considering the after treatment by the catalyst having an oxidation function,
there is a significantly great difference between the case of discharging the hydrocarbon
from the combustion chamber 5 as the precursor of the soot or the preceding state,
and the case of discharging the hydrocarbon from the combustion chamber 5 as the soot.
The new combustion system employed in the present invention is mainly structured so
as to discharge the hydrocarbon from the combustion chamber 5 as the precursor of
the soot or the preceding state without generating the soot within the combustion
chamber 5 and oxidize the hydrocarbon by the catalyst having the oxidation function.
[0038] Further, in order to stop the growth of the hydrocarbon in the state prior to the
generation of the soot, it is necessary to restrict the temperature of the fuel and
the surrounding gas at a time of the combustion within the combustion chamber 5 to
a temperature lower than the temperature at which the soot is generated. In this case,
it is clearly understood that an endothermic effect of the gas around the fuel when
the fuel is burned affects restriction of the temperature of the fuel and the surrounding
gas at a significantly great amount.
[0039] That is, when only an air exists around the fuel, the evaporated fuel immediately
reacts with an oxygen in the air so as to be burned. In this case, the temperature
of the air apart from the fuel is not increased so much, only the temperature around
the fuel becomes locally increased in a significant manner. That is, at this time,
the air apart from the fuel hardly perform an endothermic effect of the combustion
heat in the fuel. In this case, since the combustion temperature becomes locally high
in a significant manner, an unburned hydrocarbon to which the combustion heat is applied
generates the soot.
[0040] On the contrary, in the case where the fuel exists in the mixed gas including a large
amount of inert gas and a small amount of air, the condition becomes slightly different.
In this case, the evaporated fuel diffuses to the periphery and reacts with an oxygen
contained in the inert gas in a mixed manner so as to burn. In this case, since the
combustion heat is absorbed into the peripheral inert gas, the combustion temperature
is not increased so much. That is, it is possible to restrict the combustion temperature
to a low level. That is, the existing inert gas plays an important part to restrict
the combustion temperature to a low level due to the endothermic effect of the inert
gas.
[0041] In this case, in order to restrict the temperature of the fuel and the surrounding
gas to the temperature lower than the temperature at which the soot is generated,
the inert gas amount sufficient for absorbing sufficient heat is required. Accordingly,
when the fuel amount increases, the required inert gas amount increases accordingly.
Here, in this case, the greater the specific heat of the inert gas is, the stronger
the endothermic effect is. Therefore, a gas having a great specific heat is preferable
for the inert gas. In view of this, since CO
2 and the EGR gas have the relatively higher specific heat, it is said that employing
the EGR gas as the inert gas is preferable.
[0042] Fig. 5 shows a relation between the EGR rate and the smoke when using the EGR gas
as the inert gas and changing the cooling degree of the EGR gas. That is, in Fig.
5, a curve A shows the case where the EGR gas is strongly cooled so as to maintain
the EGR gas temperature to substantially 90 , a curve B shows the case where the EGR
gas is cooled by a compact cooling apparatus and a curve C shows the case where the
EGR gas is not forcibly cooled.
[0043] As shown by the curve A in Fig. 5, in the case where the EGR gas is strongly cooled,
the generation amount of the soot becomes peak when the EGR rate is slightly lower
than 50 %, and in this case, the soot is hardly generated when setting the EGR rate
to the level equal to or more than substantially 55 %. On the contrary, as shown by
the curve B in Fig. 5, in the case where the EGR gas is slightly cooled, the generation
amount of the soot becomes peak when the EGR rate is slightly higher than 50 %, and
in this case, the soot is hardly generated when setting the EGR rate to the level
equal to or more than substantially 65 %.
[0044] Further, as shown by the curve C in Fig. 5, in the case where the EGR gas is not
forcibly cooled, the generation amount of the soot becomes peak when the EGR rate
is near 55 %, and in this case, the soot is hardly generated when setting the EGR
rate to the level equal to or more than substantially 70 %.
[0045] In this case, Fig. 5 shows a generation amount of the smoke when the engine load
is comparatively high, when the engine load becomes small, the EGR rate at which the
generation amount of the soot becomes peak is slightly reduced, and a lower limit
of the EGR rate at which the soot is hardly generated is slightly reduced. As mentioned
above, the lower limit of the EGR rate at which the soot is hardly generated changes
in correspondence to a cooling degree of the EGR gas and the engine load.
[0046] Fig. 6 shows a mixed gas amount of the EGR gas and an air necessary for making the
temperature of the fuel and the surrounding gas at a time of combustion in the case
of employing the EGR gas for the inert gas lower than the temperature at which the
soot is generated, a rate of the air in the mixed gas, and a rate of the EGR gas in
the mixed gas. Here, in Fig. 6, an axis of ordinates shows a total intake gas amount
admitted within the combustion chamber 5, and a chain line Y shows a total intake
gas amount capable of being admitted within the combustion chamber 5 when supercharging
is not performed. Further, an axis of abscissas shows a required load.
[0047] Fig. 6 shows a mixed gas amount of the EGR gas and an air necessary for making the
temperature of the fuel and the surrounding gas at a time of combustion in the case
of employing the EGR gas for the inert gas lower than the temperature at which the
soot is generated, a rate of the air in the mixed gas, and a rate of the EGR gas in
the mixed gas. Referring to Fig. 6, an axis of ordinates shows a total intake gas
amount admitted within the combustion chamber 5, and a single dot chain line Y shows
a total intake gas amount capable of being admitted within the combustion chamber
5 when supercharging is not performed. Further, an axis of abscissas shows a required
load.
[0048] With reference to Fig. 6, the rate of the air, that is, the air amount in the mixed
gas shows an amount of the air necessary for completely burning the injected fuel.
That is, in the case shown in Fig. 6, a ratio between the air amount and the injection
fuel amount corresponds to a stoichiometric air fuel ratio. On the contrary, in Fig.
6, the rate of the EGR gas, that is, the EGR gas amount in the mixed gas shows the
EGR gas amount necessary at the lowest for setting the temperature of the fuel and
the surrounding gas to the temperature lower than the temperature at which the soot
is formed when the injected fuel is burned. The EGR gas amount is equal to or more
than 55 % of the EGR rate, and that of the embodiment shown in Fig. 6 is equal to
or more than 70 %. That is, when setting the total intake gas amount admitted into
the combustion chamber 5 to a solid line X in Fig. 6 and setting the rate between
the air amount and the EGR gas amount among the total intake gas amount X to a rate
shown in Fig. 6, the temperature of the fuel and the surrounding gas becomes lower
than the temperature at which the soot is generated, and accordingly the soot is not
completely generated. Further, the generation amount of NOx at this time is about
10 p.p.m. or less, so that the generation amount of NOx is significantly small.
[0049] Since the heat generated when the fuel is burned is increased as the fuel injection
amount is increased, in order to maintain the temperature of the fuel and the surrounding
gas to the temperature lower than the temperature at which the soot is generated,
it is necessary to increase the absorption amount of the heat due to the EGR gas.
Accordingly, as shown in Fig. 6, the EGR gas amount should be increased in accordance
that the injection fuel amount is increased. That is, the EGR gas amount should be
increased as a required load becomes high.
[0050] Here, in the case where the supercharging is not performed, an upper limit of the
amount X of the total intake gas admitted into the combustion chamber 5 is Y, so that
in Fig. 6, in the area having a required load larger than L
0, the air fuel ratio can not be maintained to the stoichiometric air fuel ratio unless
the EGR gas rate is reduced in accordance that the required load becomes greater.
In other words, in the case where it is intended to maintain the air fuel ratio to
the stoichiometric air fuel ratio in the area having the desired load larger than
L
0 when the supercharging is not performed, the EGR rate is reduced in accordance that
the required load becomes high, and accordingly, in the area having the desired load
larger than L
0, it is impossible to maintain the temperature of the fuel and the surrounding gas
to the temperature lower than the temperature at which the soot is produced.
[0051] However, as shown in Fig. 1, when recirculating the EGR gas into the inlet side of
the supercharger, that is, the air intake pipe 17 of the exhaust turbo charger 15
via the EGR passage 29, in the area having the required load larger than L
0, it is possible to maintain the EGR rate to the level equal to or more than 55 %,
for example, 70 %, so that it is possible to maintain the temperature of the fuel
and the surrounding gas to the temperature lower than the temperature at which the
soot is produced. That is, when recirculating the EGR gas so that the EGR rate within
the air intake pipe 17 becomes, for example, 70 %, the EGR rate of the intake gas
at the pressure increased by the compressor 16 of the exhaust turbo charger 15 also
becomes 70 %, so that it is possible to maintain the temperature of the fuel and the
surrounding gas to the temperature at which the soot is produced as long as the compressor
16 can increase the pressure. Accordingly, it is possible to expand an operation range
of the engine which can produce the low temperature combustion.
[0052] Here, in this case, when setting the EGR rate to the level equal to or more than
55 % in the area having the required load larger than L
0, the EGR control valve 31 is fully opened and the throttle valve 20 is slightly closed.
[0053] As mentioned above, Fig. 6 shows the case where the fuel is burned under the stoichiometric
air fuel ratio, however, even when setting the air amount to the level less than the
air amount shown in Fig. 6, that is, setting the air fuel ratio to rich, it is possible
to restrict the generation amount of NOx near to 10 p.p.m. or less while restricting
the generation of the soot, and further, even when setting the air amount to the level
more than the air amount shown in Fig. 6, that is, setting an average value of the
air fuel ratio to the lean value such as 17 to 18, it is possible to restrict the
generation amount of NOx near to 10 p.p.m. or less while restricting the generation
of the soot.
[0054] That is, when the air fuel ratio is made rich, the fuel becomes excessive, however,
since the combustion temperature is restricted to the low temperature, the excessive
fuel does not grow to the soot, so that the soot is not produced. Further, at this
time, a significantly small amount of NOx is only produced. On the contrary, when
the average air fuel ratio is lean, or even when the air fuel ratio is the stoichiometric
air fuel ratio, a small amount of soot is produced if the combustion temperature becomes
high. However, in accordance with the present invention, since the combustion temperature
is restricted to the low temperature, the soot is not produced at all. Further, only
a significantly small amount of NOx is generated.
[0055] As mentioned above, when the low temperature combustion is performed, the soot is
not produced irrespective of the air fuel ratio, that is, whether or not the air fuel
ratio is rich, stoichiometric, or lean. As a result, the generation amount of NOx
is significantly small. Accordingly, in view of the improvement of a specific fuel
consumption, it is said that it is preferable to make the average air fuel ratio lean.
[0056] In this case, it is limited to an engine at the middle or low load operation at which
the amount of heat generated by the combustion is relatively small to restrict the
temperature of the fuel and the surrounding gas at a time of combustion within the
combustion chamber to the level equal to or less than the temperature at which the
growth of the hydrocarbon stops on the way. Accordingly, in the embodiment in accordance
with the present invention, at a time of operating the engine at the middle or low
load, the temperature of the fuel and the surrounding gas at a time of combustion
is restricted to the temperature equal to or less than the temperature at which the
growth of the hydrocarbon stops on the way so as to perform the first combustion,
that is, the low temperature combustion, and at a time of operating the engine at
high load, the second combustion, that is, the conventionally performed combustion
is performed. In this case, the first combustion, that is, the low temperature combustion
means the combustion in which the amount of the inert gas within the combustion chamber
is larger than the amount of the inert gas at which the generation amount of the soot
becomes peak and the soot is hardly generated, as is apparent from the explanation
as mentioned above. The second combustion, that is, the conventionally performed combustion
means the combustion in which the amount of the inert gas within the combustion chamber
is smaller than the amount of the inert gas at which the generation amount of the
soot becomes peak.
[0057] Fig. 7 shows a first operation area I in which the first combustion, that is, the
low temperature combustion is performed and a second operation area II in which the
second combustion, that is, the combustion in accordance with the conventional combustion
method is performed. In this case, in Fig. 7, an axis of ordinates L indicates a depression
amount of the acceleration pedal 50, that is, a required load, and an axis of abscissas
N indicates an engine speed. Further, in Fig. 7, X(N) shows a first boundary between
the first operation area I and the second operation area II, and Y(N) shows a second
boundary between the first operation area I and the second operation area II. A change
of the operation area from the first operation area I to the second operation area
II is judged on the basis of the first boundary X(N), and a change of the operation
area from the second operation area II to the first operation area I is judged on
the basis of the second boundary Y(N).
[0058] That is, when the required load L exceeds the first boundary X(N) corresponding to
a function of the engine speed N when the operation state of the engine is in the
first operation area I and the low temperature combustion is performed, it is judged
that the operation area is moved to the second operation area II, so that the combustion
in accordance with the conventional combustion method is performed. Next, when the
required load L becomes lower than the second boundary Y(N) corresponding to a function
of the engine speed N, it is judged that the operation area goes to the first operation
area I, so that the low temperature combustion is performed again.
[0059] As mentioned above, two boundaries comprising the first boundary X(N) and the second
boundary Y(N) closer to the lower load than the first boundary X(N) are provided for
the following two reasons. The first reason is that since the combustion temperature
is relatively high in a side of the high load in the second operation area II, the
low temperature combustion can not be immediately performed even when the required
load L becomes lower than the first boundary X(N) at this time. That is, because the
low temperature combustion is started only when the required load L becomes significantly
low, that is, lower than the second boundary Y(N). The second reason is that the hysteresis
is provided with respect to the change in the operation area between the first operation
area I and the second operation area II.
[0060] In this case, when the engine operation state exists in the first operation area
I and the low temperature combustion is performed, the soot is hardly generated, and
in place thereof, unburned hydrocarbon is discharged from the combustion chamber 5
as the precursor of the soot or the state prior thereto. At this time, the unburned
hydrocarbon discharged from the combustion chamber 5 is well oxidized by the catalyst
25 having an oxidization function. As the catalyst 25, an oxidation catalyst, a three
way catalyst or an NOx absorbent can be employed. The NOx absorbent has the function
of absorbing NOx when the average air fuel ratio within the combustion chamber 5 is
lean and discharging NOx when the average air fuel ratio within the combustion chamber
5 becomes rich.
[0061] The NOx absorbent is structured such that, for example, an alumina is set as a carrier
and at least one selected from an alkaline metal such as a potassium K, a sodium Na,
a lithium Li and a cesium Cs, an alkaline earth metal such as a barium Ba and a calcium
Ca and a rare earth metal such as a lanthanum La and an yttrium Y, and a noble metal
such as a platinum Pt are carried on the carrier.
[0062] As well as the oxidation catalyst, the three way catalyst and the NOx absorbent have
the oxidation function. As mentioned above, the three way catalyst and the NOx absorbent
can be used as the catalyst 25.
[0063] Fig. 8 shows the output of the air fuel ratio sensor 27. As shown in Fig. 8, an output
current I of the air fuel ratio sensor 27 is changed in accordance with the air fuel
ratio A/F. Accordingly, the air fuel ratio can be derived from the output current
I of the air fuel ratio sensor 27.
[0064] Next, the outline of the operation control in the first operation area I and the
second operation area II is described with reference to Fig. 9.
[0065] Fig. 9 shows an opening degree of the throttle valve 20 with respect to the required
load L, an opening degree of the EGR control valve 31, an EGR rate, an air fuel ratio,
an injection timing and an injection amount. As shown in Fig. 9, in the first operation
area I having a low required load L, the opening degree of the throttle valve 20 is
gradually increased to about two-third of the opening degree from a nearly full close
state as the required load L is increased, and the opening degree of the EGR control
valve 31 is gradually increased to the full open state from a nearly full closed state
as the required load L is increased. Further, in the embodiment shown in Fig. 9, the
EGR rate is set to substantially 70 % in the first operation area I, and the air fuel
ratio is set to the lean air fuel ratio which is slightly leaner.
[0066] In other words, in the first operation area I, the opening degree of the throttle
valve 20 and the opening degree of the EGR control valve 31 are controlled so that
the EGR rate becomes substantially 70 % and the air fuel ratio becomes lean which
is slightly leaner. Further, in the first operation area I, a fuel injection is performed
prior to a compression top dead center TDC. In this case, an injection start timing
S is delayed in accordance that the required load L becomes high, and an injection
end timing E is also delayed in accordance that the injection start timing S is delayed.
[0067] Further, at a time of an idling operation, the throttle valve 20 is closed near to
the full closed state, and at this time, the EGR control valve 31 is also closed near
to the full closed state. When closing the throttle valve 20 near to the full closed
state, a pressure within the combustion chamber 5 at the beginning of the compression
becomes low, so that the compression pressure becomes small. When the compression
pressure becomes small, a compression work by the piston 4 is reduced. Accordingly,
a vibration of the engine main body 1 is restricted. That is, at a time of the idling
operation, in order to restrict the vibration of the engine main body 1, the throttle
valve 20 is closed near to the fully closed state.
[0068] On the contrary, the operation area of the engine changes from the first operation
area I to the second operation area II, the opening degree of the throttle valve 20
is increased stepwise from about two-third of the opening degree to the fully open
direction. At this time, in the embodiment shown in Fig. 9, the EGR rate is reduced
stepwise from substantially 70 % to 40 % or less and the air fuel ratio is increased
stepwise. That is, since the EGR rate flies over the EGR rate range (Fig. 5) in which
a lot of smoke is generated, a lot of smoke is not generated when the operation area
of the engine changes from the first operation area I to the second operation area
II.
[0069] In the second operation area II, the conventionally performed combustion is performed.
In this second operation area II, the throttle valve 20 is kept in the fully open
state except a portion thereof, and the opening degree of the EGR control valve 31
is gradually reduced as the required load L becomes high. Further, in this operation
area II, the EGR rate becomes low as the required load L becomes high, and the air
fuel ratio becomes small as the required load L becomes high. However, the air fuel
ratio is set to lean even when the required load L becomes high. Further, in the second
operation area II, the injection start timing S is set near the compression top dead
center TDC.
[0070] Fig. 10A shows a target air fuel ratio A/F in the first operation area I. In Fig.
10A, curves indicated by A/F = 15.5, A/F = 16, A/F = 17 and A/F = 18 respectively
show states having air fuel ratios 15.5, 16, 17 and 18, each of the air fuel ratios
between the curves is defined in accordance with a proportional allotment. As shown
in Fig. 10A, the air fuel ratio becomes lean in the first operation area I, and further,
in the first operation area I, the air fuel ratio A/F is made lean in accordance that
the required load L becomes low.
[0071] That is, the heat generated by the combustion is reduced as the required load L becomes
low. Accordingly, the low temperature combustion can be performed even when lowering
the EGR rate as the required load L becomes low. When lowering the EGR rate, the air
fuel ratio becomes large, so that as shown in Fig. 10A, the target air fuel ratio
A/F is made large as the required load L becomes low. As the target air fuel ratio
A/F is increased, the specific fuel consumption is improved, so that in order to make
the air fuel ratio as lean as possible, in accordance with the embodiment of the present
invention, the target air fuel ratio A/F is made large as the required load L becomes
low.
[0072] In this case, the target air fuel ratio A/F shown in Fig. 10A is preliminarily stored
within the ROM 42 as a function of the required load L and the engine speed N in the
form of a map as shown in Fig. 10B. Further, a target opening degree ST of the throttle
valve 20 necessary for setting the air fuel ratio to the target air fuel ratio A/F
as shown in Fig. 10A is preliminarily stored within the ROM 42 as a function of the
required load L and the engine speed N in the form of a map as shown in Fig. 11A,
and a target opening degree SE of the EGR control valve 31 necessary for setting the
air fuel ratio to the target air fuel ratio A/F shown in Fig. 10A is preliminarily
stored within the ROM 42 as a function of the required load L and the engine speed
N in the form of a map as shown in Fig. 11B.
[0073] Fig. 12A shows a target air fuel ratio A/F when the second combustion, that is, the
combustion in accordance with the conventional combustion method is performed. In
this case, in Fig. 12A, curves indicated by A/F = 24, A/F = 35, A/F = 45 and A/F =60
respectively show states having target air fuel ratios 24, 35, 45 and 60. The target
air fuel ratio A/F shown in Fig. 12A is preliminarily stored within the ROM 42 as
a function of the required load L and the engine speed N in the form of a map as shown
in Fig. 12B. Further, a target opening degree ST of the throttle valve 20 necessary
for setting the air fuel ratio to the target air fuel ratio A/F as shown in Fig. 12A
is preliminarily stored within the ROM 42 as a function of the required load L and
the engine speed N in the form of a map as shown in Fig. 13A, and a target opening
degree SE of the EGR control valve 31 necessary for setting the air fuel ratio to
the target air fuel ratio A/F is preliminarily stored within the ROM 42 as a function
of the required load L and the engine speed N in the form of a map as shown in Fig.
13B.
[0074] Further, the fuel injection amount Q when the second combustion is performed is calculated
on the basis of the required load L and the engine speed N. The fuel injection amount
Q is preliminarily stored within the ROM 42 as a function of the required load L and
the engine speed N in the form of a map as shown in Fig. 14.
[0075] Next, the operation control in accordance with the present embodiment will be described
below with reference to Figs. 15 and 16. With reference to Figs. 15 and 16, at first,
in step 100, it is judged whether or not a flag I indicating that the operation area
of the engine is in the first operation area I. When the flag I is set, that is, the
operation area of the engine is in the first operation area I, the operation control
goes to step 101 where it is judged whether or not the required load L becomes greater
than the first boundary X1 (N). When a relation L X1 (N) is established, the operation
control goes to step 105 where the low temperature combustion is performed.
[0076] In step 101, when it is judged that the relation L > X(N) is established, the operation
control goes to step 102 where a flag I is reset, and next, the operation control
goes to step 112 where the second combustion is performed.
[0077] On the contrary, in step 100, when it is judged that the flag I indicating that the
operating state of the engine is the first operation area I is not set, that is, when
the operation state of the engine is in the second operation area II, the operation
control goes to step 103 where it is judged whether or not the required load L becomes
lower than the second boundary Y(N). When the relation L Y(N) is established, the
recirculation goes to step 112 where the second combustion is performed at a lean
air fuel ratio.
[0078] On the contrary, in step 103, when it is judged that the relation L < Y(N) is established,
the process goes to step 104 where the flag I is set, and next the process goes to
step 105 where the low temperature combustion is performed.
[0079] In step 105, the target opening degree ST of the throttle valve 20 is calculated
from a map shown in Fig. 11 A, and the opening degree of the throttle valve 20 is
set to the target opening degree ST. Next, in step 106, the target opening degree
SE of the EGR control valve 31 is calculated from a map shown in Fig. 11 B, and the
opening degree of the EGR control valve 31 is set to the target opening degree SE.
Next, in step 107, a mass flow amount of the intake air detected by the mass flow
amount detecting device 21 (hereinafter, simply refer to as the intake air amount)
Ga is taken in, and next in step 108, the target air fuel ratio A/F is calculated
on the basis of the map shown in Fig. 10B. Next, in step 109, the fuel injection amount
Q required for setting the air fuel ratio to the target air fuel ratio A/F is calculated
on the basis of the intake air amount Ga and the target air fuel ratio A/F.
[0080] Next, in step 110, it is judged whether or not the automatic transmission 60 is under
operation. Since the torque generated in the engine is changed during the operation
of the automatic transmission 60, it is desired to soften the shock. Accordingly,
when it is judged YES in step 110, the process goes to step 111 where it is intended
to soften the shock on the basis of the change of the torque generated in the engine.
Hereinafter, the description will be given with respect to the idea for softening
the shock on the basis of the change of the torque generated in the engine.
[0081] Fig. 17 is a graph which shows the relation between the air fuel ratio and the torque
generated in the engine. In Fig. 17, an axis of abscissas indicates an air fuel ratio
A/F and an axis of ordinates indicates a torque T generated in the engine. As shown
in Fig. 17, the second combustion (the combustion in accordance with the conventional
combustion method) is performed in an area where the air amount is sufficiently excessive
and the air fuel ratio is relatively lean. Accordingly, in the case where the second
combustion is performed, when the fuel injection amount is corrected to be reduced,
that is, the air fuel ratio is increased from A/F3 to A/F4 (becomes leaner) together
with the correction for reducing the fuel injection amount, the torque generated in
the engine is reduced by T2 as the fuel amount serving for the combustion is reduced.
On the contrary, the low temperature combustion (the first combustion) is performed
in an area where the air amount is likely to be insufficient and the air fuel ratio
is richer than that of the case in the second combustion. Accordingly, in the case
where the low temperature combustion is performed, when the fuel injection amount
is corrected to be increased, that is, the air fuel ratio is reduced from A/F1 to
A/F2 (becomes richer) together with the correction for increasing the fuel injection
amount, the combustion is deteriorated and the torque generated in the engine is reduced
by T1.
[0082] Returning to the explanation of Figs. 15 and 16, the fuel injection amount is corrected
to be increased in step 111 on the basis of the idea as mentioned above (Q ← Q + Q1).
In accordance with step 111, when the low temperature combustion is performed and
the shift change is performed by the automatic transmission 60, the fuel injection
amount is corrected to be increased and the air fuel ratio is reduced, such that the
shock of the torque change due to the automatic transmission 60 is softened. On the
contrary, when it is judged NO in step 110, it is not required to soften the shock
of the torque change due to the automatic transmission. Accordingly, the present routine
is finished without correcting the fuel injection amount to increase. In this case,
in accordance with another embodiment, in place of correcting the fuel injection amount
to increase in step 111, it is possible to reduce the intake air amount by reducing
the opening degree of the throttle valve 20.
[0083] As mentioned above, in the case where the low temperature combustion is performed,
when the required load L or the engine speed N is changed, the opening degree of the
throttle valve 20 and the opening degree of the EGR control valve 31 is immediately
made to be coincident with the target opening degree ST and SE corresponding to the
required load L and the engine speed N. Accordingly, for example, when the required
load L is increased, the amount of the air within the combustion chamber 5 is immediately
increased, thus immediately increasing the torque generated in the engine.
[0084] On the contrary, when the opening degree of the throttle valve 20 or the opening
degree of the EGR control valve 31 is changed and the intake air amount is changed,
the change of the intake air amount Ga is detected by the mass flow amount detecting
device 21, and the fuel injection amount Q is controlled on the basis of the detected
intake air amount Ga. That is, the fuel injection amount Q is changed after the intake
air amount Ga is actually changed.
[0085] In step 112 where the second combustion is performed, the target fuel injection amount
Q is calculated on the basis of the map shown in Fig. 14, and the fuel injection amount
is set to the target fuel injection amount Q. Next, in step 113, in the same manner
as step 110, it is judged whether or not the shift change by the automatic transmission
60 is going to be performed. Since the torque generated in the engine is changed during
the shift change of the automatic transmission 60, it is desired to soften the shock.
Accordingly, when it is judged YES in step 113, the process goes to step 114 where
the shock on the basis of the change of the torque generated in the engine is aimed
to be softened. In step 114, on the basis of the idea as mentioned above, the fuel
injection amount is corrected to be reduced ((Q ← Q - Q2). In accordance with step
114, when the second combustion is performed and the shift change is performed by
the automatic transmission 60, the fuel injection amount is corrected to be reduced
and the air fuel ratio is increased, such that the shock of the torque change due
to the automatic transmission 60 is softened. On the contrary, when it is judged NO
in step 113, it is not required to soften the shock of the torque change due to the
automatic transmission. Therefore, the process goes to step 115 without correcting
to reduce the fuel injection amount.
[0086] Next, in step 115, the target opening degree ST of the throttle valve 20 is calculated
on the basis of the map shown in Fig. 13A. Next, in step 116, the target opening degree
SE of the EGR control valve 31 is calculated on the basis of the map shown in Fig.
13B, and the opening degree of the EGR control valve 31 is set to the target opening
degree SE.
[0087] Next, in step 117, the intake air amount Ga detected by the mass flow amount detecting
device 21 is taken in. Next, in step 118, an actual air fuel ratio (A/F)
R is calculated on the basis of the fuel injection amount Q and the intake air amount
Ga. Next, in step 119, the target air fuel ratio A/F is calculated on the basis of
the map shown in Fig. 12B. Next, in step 120, it is judged whether or not the actual
air fuel ratio (A/F)
R is larger than the target air fuel ratio A/F. When the relation (A/F)
R > A/F is established, the process goes to step 121, a correcting value ST of the
throttle opening degree is reduced at a fixed value , and next the process goes to
step 123. On the contrary, when the relation (A/F)
R A/F is established, the process goes to step 122, the correcting value ST is increased
at the fixed value , and next the process goes to step 123. In step 123, a final target
opening degree ST is calculated by adding the correcting value ST to the target opening
degree ST of the throttle valve 20, and the opening degree of the throttle valve 20
is set to the final target opening degree ST. That is, the opening degree of the throttle
valve 20 is controlled such that the actual air fuel ratio (A/F)
R becomes the target air fuel ratio A/F.
[0088] As mentioned above, in the case where the second combustion is performed, when the
required load L or the engine speed N is changed, the fuel injection amount is immediately
made to be coincident with the target fuel injection amount Q corresponding to the
required load L and the engine speed N. For example, when the required load L is increased,
the fuel injection amount is immediately increased, thus immediately increasing the
torque generated in the engine.
[0089] On the contrary, when the fuel injection amount Q is increased and the air fuel ratio
is shifted from the target air fuel ratio A/F, the opening degree of the throttle
valve 20 is controlled so that the air fuel ratio becomes the target air fuel ratio
A/F. That is, the air fuel ratio is changed after the fuel injection amount Q is changed.
[0090] In the embodiments as mentioned above, the fuel injection amount Q is controlled
in accordance with an open loop when the low temperature combustion is performed,
and the air fuel ratio is controlled by changing the opening degree of the throttle
valve 20 when the second combustion is performed. However, it is possible to feedback
control the fuel injection amount Q on the basis of the output signal of the air fuel
ratio sensor 27 when the low temperature combustion is performed, and it is possible
to control the air fuel ratio by changing the opening degree of the EGR control valve
31 when the second combustion is performed.
[0091] Hereinafter, a second embodiment of an internal combustion engine in accordance with
the present invention will be described below. A structure of the present embodiment
is substantially the same as the structure of the first embodiment as shown in Fig.
1.
[0092] Next, the description will be given with respect to the operation control in accordance
with the present embodiment below with reference to Figs. 18 and 19. Since steps 100
to 109 are the same as those of the first embodiment, the explanation thereof will
be omitted.
[0093] In step 110, it is judged whether or not the shift change is going to be performed
by the automatic transmission 60. Since the torque generated in the engine is changed
during the shift change of the automatic transmission 60, it is desired to soften
the shock. Accordingly, when it is judged YES in step 110, the process goes to step
1800 where the shock on the basis of the change of the torque generated in the engine
is aimed to be softened.
[0094] That is, in step 1800, the fuel injection timing is delayed in comparison with the
case where the shift change is not performed. In this case, when the injection timing
of the fuel supplied within the combustion chamber 5 is delayed, the combustion is
deteriorated as the fuel supply is too late for the combustion, thus lowering the
torque generated in the engine. Accordingly, when the low temperature combustion is
performed in step 1800 where the shift change is performed by the automatic transmission
60, the fuel injection timing is delayed, softening the shock of the torque change
by the automatic transmission 60. On the contrary, when it is judged NO in step 110,
it is not required to soften the shock of the torque change by the automatic transmission,
the present routine is finished without delaying the fuel injection timing.
[0095] As mentioned above, in the case where the low temperature combustion is performed,
when the required load L or the engine speed N is changed, the opening degree of the
throttle valve 20 and the opening degree of the EGR control valve 31 is immediately
made to be coincident with the target opening degree ST and SE corresponding to the
required load L and the engine speed N. Accordingly, for example, when the required
load L is increased, the amount of the air within the combustion chamber 5 is immediately
increased, thus immediately increasing the torque generated in the engine.
[0096] On the contrary, when the opening degree of the throttle valve 20 or the opening
degree of the EGR control valve 31 is changed and the intake air amount is changed,
the change of the intake air amount Ga is detected by the mass flow amount detecting
device 21, and the fuel injection amount Q is controlled on the basis of the detected
intake air amount Ga. That is, the fuel injection amount Q is changed after the intake
air amount Ga is actually changed.
[0097] Since the same operations are performed in steps 112 to 123 where the second combustion
is performed as those of the first embodiment, the explanation thereof will be omitted.
[0098] Hereinafter, a third embodiment of an internal combustion engine in accordance with
the present invention will be described below. The present embodiment has substantially
the same structure as that of the first embodiment shown in Fig. 1.
[0099] Next, the description will be given with respect to the operation control in accordance
with the present embodiment below with reference to Figs. 20 and 21. Since steps 100
to 106 are the same as those of the first embodiment, the explanation thereof will
be omitted.
[0100] In step 2000, it is judged whether or not the shift change is going to be performed
by the automatic transmission 60. Since the torque generated in the engine is changed
during the shift change of the automatic transmission 60, it is desired to soften
the shock. Accordingly, when it is judged YES in step 2000, the process goes to step
2001 where the shock on the basis of the change of the torque generated in the engine
is intended to be softened.
[0101] That is, in step 2001, the target opening degree SE of the EGR control valve 31 is
corrected to be increased, and the opening degree of the EGR control valve 31 is set
to the target opening degree SE (SE ← SE + SE). In this case, as explained with reference
to Fig. 17, since the low temperature combustion is performed under the state where
the air amount tends to be insufficient, the air admitted via the throttle valve 20
is hard to be supplied to the combustion chamber 5 when the target opening degree
SE of the EGR control valve 31 is corrected to be increased and the amount of the
EGR gas is corrected to be increased in the case where the low temperature combustion
is performed. Then the air within the combustion chamber 5 tends to be further insufficient.
As a result, the combustion is deteriorated and the torque generated in the engine
is lowered. Accordingly, when the low temperature combustion is performed in step
2001 and the shift change by the automatic transmission 60 is performed, the target
opening degree SE of the EGR control valve 31 is corrected to be increased and the
amount of the EGR gas is corrected to be increased, whereby the shock of the torque
change due to the automatic transmission 60 is softened. On the contrary, when it
is judged NO in step 2000, it is not required to soften the shock of the torque change
by the automatic transmission, the process goes to step 107 without delaying the fuel
injection timing.
[0102] Next, in step 107, a mass flow amount of the intake air detected by the mass flow
amount detecting device 21 (hereinafter, simply refer to as the intake air amount)
Ga is taken in, and next in step 108, the target air fuel ratio A/F is calculated
on the basis of the map shown in Fig. 10B. Next, in step 109, the fuel injection amount
Q required for setting the air fuel ratio to the target air fuel ratio A/F is calculated
on the basis of the intake air amount Ga and the target air fuel ratio A/F.
[0103] As mentioned above, in the case where the low temperature combustion is performed,
when the required load L or the engine speed N is changed, the opening degree of the
throttle valve 20 and the opening degree of the EGR control valve 31 is immediately
made to be coincident with the target opening degree ST and SE corresponding to the
required load L and the engine speed N. Accordingly, for example, when the required
load L is increased, the amount of the air within the combustion chamber 5 is immediately
increased, so that the torque generated in the engine is immediately increased.
[0104] On the contrary, when the opening degree of the throttle valve 20 or the opening
degree of the EGR control valve 31 is changed and the intake air amount is changed,
the change of the intake air amount Ga is detected by the mass flow amount detecting
device 21, and the fuel injection amount Q is controlled on the basis of the detected
intake air amount Ga. That is, the fuel injection amount Q is changed after the intake
air amount Ga is actually changed.
[0105] Since the same operations are performed in steps 112 to 123 in which the second combustion
is performed as those of the first embodiment, the explanation thereof will be omitted.
[0106] Next, at a time of switching between the low temperature combustion corresponding
to the first combustion and the second combustion, the intake air amount supplied
within the combustion chamber 5 and the fuel injection amount are changed. In this
case, since the intake air amount supplied within the combustion chamber 5 is actually
changed with respect to the timing at which the fuel injection amount is changed,
the generated torque is temporarily changed. Accordingly, in the internal combustion
engine provided with the automatic transmission 60, there is a risk that the shock
of the generated torque is increased in accordance with the control state of the automatic
transmission 60. Then, the description will be given with respect to the control content
of performing a switching control of the combustion in accordance with the control
state of the automatic transmission 60 in order to reduce the torque shock.
[0107] At first, the generated torque is changed at a time of switching the shift change
ratio of the automatic transmission 60. In this case, it is judged whether the shift
change ratio is at the switching state after judging the switching of the combustion
state against the required load. At a time of switching the shift change ratio, it
is structured so as to inhibit the switching between the first combustion and the
second combustion. Accordingly, it is possible to reduce the increase in the torque
change due to the change of the torque generated together with the switching between
the first combustion and the second combustion. Further, at a time of switching the
shift change ratio, it is possible to change the first combustion and the second combustion
in synchronous with the switching of the shift change. By synchronously switching
the combustion, it is possible to reduce the change of the torque in comparison with
the case in which the switching of the shift change ratio and the switching of the
combustion are performed at the different timing.
[0108] The generated torque is also changed at a time when the lockup mechanism 73 of the
automatic transmission 60 is turned between on-state and off-state. Also, in this
case, after judging the switching of the combustion state with respect to the required
load, it is judged whether the shift change ratio is at the switching state. When
the lockup mechanism 73 is turned between on-state and off-state, it is structured
so as to inhibit the switching between the first combustion and the second combustion.
Further, at a time of switching the lockup mechanism 73, it is possible to switch
the first combustion and the second combustion in synchronous with the switching between
on-state and off-state of the lockup mechanism 73. By synchronously switching the
combustion, it is possible to reduce the change of the torque in comparison with the
case in which the switching between on-state and off-state of the lockup mechanism
73 and the switching of the combustion are performed at the different timing.
[0109] Further, in addition to the torque change generated at a time of switching between
the low temperature combustion corresponding to the first combustion mentioned above
and the second combustion, the generated torque is also changed when the air fuel
ratio of a mixed gas to be burned in the engine for discharging NOx from the NOx absorbent
25 is switched to a rich state. That is, in the case of being switched to the rich
air fuel ratio operation in the engine. In the switching of the operation state of
the engine as mentioned above, it is also possible to synchronously perform a switching
control of the rich air fuel ratio operation in accordance with the control state
of the automatic transmission.
[0110] The control state of the automatic transmission includes a shift change state called
as a power down shift. It is different from the down shift which is performed in the
case where a speed reduction is performed in a vehicle, and corresponds to the shift
down operation which is performed in a state where a positive drive torque is transmitted
from the engine side to the transmission side. When the rotational synchronism at
a time of operating the power down shift is detected, the generated torque is changed.
In the control state of the automatic transmission as mentioned above, it is possible
to inhibit the switching control between the first combustion and the second combustion.
Further, in the case where it is required to increase the engine speed at a time of
operating the power down shift, it is possible to switch the air fuel ratio of the
mixed gas to be burned in the engine for discharging NOx from the NOx absorbent 25
to the rich state.
[0111] In the internal combustion engine described in the present embodiment, since an amount
of an inert gas supplied within the combustion chamber is large in the low temperature
combustion corresponding to the first combustion state, the combustion is performed
under the condition where oxygen is relatively insufficient, that is, the combustion
is performed under a relatively severe combustion condition. Accordingly, when the
engine stall is generated if the low temperature combustion corresponding to the first
combustion is performed, it is also possible to inhibit the low temperature combustion,
whereby the engine stall is not generated. In this case, it is judged whether or not
the condition is at a state where the engine stall is likely to occur, for example,
whether or not the braking operation is performed, whether or not the engine speed
becomes lower than a predetermined engine speed (for example, 2000 rpm), whether or
not an external load (an air conditioner and the like) connected to the engine is
increased, a reduction amount of the engine speed at a unit time is greater than a
predetermined amount, and the like, such that it is possible to inhibit the low temperature
combustion.
[0112] At a time of executing a low temperature combustion in which an amount of an EGR
gas supplied within a combustion chamber (5) is more than an amount of the EGR gas
when a generation amount of a soot becomes peak and the soot is hardly generated and
changing a speed of an automatic transmission (60), in order to reduce a generated
torque, an injection amount of a fuel injected from a fuel injection valve (6) is
corrected to be increased so as to reduce an air fuel ratio, or a fuel injection timing
is delayed, or an opening degree of an EGR control valve (31) is corrected to be increased
so as to correct an amount of the EGR gas to increase, and further at a time of executing
a combustion in which the amount of the EGR gas supplied within a combustion chamber
(5) is less than the amount of the EGR gas when a generation amount of a soot becomes
peak and the soot is hardly generated and changing a speed of an automatic transmission
(60), in order to reduce a generated torque, the injection amount of the fuel injected
from the fuel injection valve (6) is corrected to be reduced.