SE1550267A1 - A method for controlling an internal combustion engine, an internal combustion engine controlled by such a method and avehicle comprising such an internal combustion engine. - Google Patents
A method for controlling an internal combustion engine, an internal combustion engine controlled by such a method and avehicle comprising such an internal combustion engine. Download PDFInfo
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- SE1550267A1 SE1550267A1 SE1550267A SE1550267A SE1550267A1 SE 1550267 A1 SE1550267 A1 SE 1550267A1 SE 1550267 A SE1550267 A SE 1550267A SE 1550267 A SE1550267 A SE 1550267A SE 1550267 A1 SE1550267 A1 SE 1550267A1
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- exhaust
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- valve
- combustion engine
- internal combustion
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D13/00—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing
- F02D13/02—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation
- F02D13/06—Cutting-out cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D17/00—Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling
- F02D17/02—Cutting-out
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/008—Controlling each cylinder individually
- F02D41/0087—Selective cylinder activation, i.e. partial cylinder operation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D13/00—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing
- F02D13/02—Controlling the engine output power by varying inlet or exhaust valve operating characteristics, e.g. timing during engine operation
- F02D13/0203—Variable control of intake and exhaust valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D17/00—Controlling engines by cutting out individual cylinders; Rendering engines inoperative or idling
- F02D17/02—Cutting-out
- F02D17/023—Cutting-out the inactive cylinders acting as compressor other than for pumping air into the exhaust system
- F02D17/026—Cutting-out the inactive cylinders acting as compressor other than for pumping air into the exhaust system delivering compressed fluid, e.g. air, reformed gas, to the active cylinders other than during starting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/0002—Controlling intake air
- F02D2041/001—Controlling intake air for engines with variable valve actuation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/0002—Controlling intake air
- F02D2041/001—Controlling intake air for engines with variable valve actuation
- F02D2041/0012—Controlling intake air for engines with variable valve actuation with selective deactivation of cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D2250/00—Engine control related to specific problems or objectives
- F02D2250/28—Control for reducing torsional vibrations, e.g. at acceleration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/008—Controlling each cylinder individually
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1444—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
- F02D41/1444—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases
- F02D41/1454—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases the characteristics being an oxygen content or concentration or the air-fuel ratio
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1497—With detection of the mechanical response of the engine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/02—Circuit arrangements for generating control signals
- F02D41/14—Introducing closed-loop corrections
- F02D41/1497—With detection of the mechanical response of the engine
- F02D41/1498—With detection of the mechanical response of the engine measuring engine roughness
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Description
10
To reduce the mass flow and increase the exhaust temperature, the exhaust and
inlet valves of the deactivated cylinders can be closed. The pressure in the deacti-
vated cylinders gives rise to a torque pulse per revolution per cylinder until the pres-
sure, due to leakage, becomes so low in these cylinders that no significant torque is
obtained from them. This leads to even greater vibration problems and oil carryover
across the piston rings from the crankcase to the combustion chamber during the
lower part of the piston stroke in the deactivated cylinders, due to the negative differ-
ential pressure across the piston rings. This will occur after a certain period of deacti-
vaüon.
The vibrations can be reduced if either the exhaust or the intake valves in the deacti-
vated cylinders are kept closed and the active valves do both the exhaust and inlet lift
events. Torque pulses will then be obtained from the compression/expansion pres-
sure in the deactivated cylinders. This results in essentially the same vibration level
as when the only measure is shutting off the fuel to the deactivated cylinders. More-
over, the mass flow to the exhaust treatment is reduced and the exhaust temperature
is thereby significantly increased.
By controlling the exhaust or inlet valves of the deactivated cylinders, so that they will
remain closed during all strokes, the engine exhaust treatment system will not be
cooled because no air is passed to the exhaust treatment system from the deacti-
vated cylinders.
Within the vehicle exhaust emission driving cycle, cylinder deactivation with closed
intake and/or exhaust valves might be required to prevent the exhaust temperature to
fall below its critical limit. This is done in order to maintain the conversion of the ex-
haust emissions in the exhaust treatment system.
ln order to simultaneously avoid cooling of the exhaust treatment system and reduce
vibrations, a zero flow of air through the deactivated cylinders may be created. Thus,
air will be prevented from passing through the deactivated cylinders and further to the
exhaust treatment system. Consequently, the exhaust treatment system will not be
cooled. The zero flow must be achieved in an efficient manner, so that pressure
pulses, noise and mechanical stress are reduced or eliminated.
Document US 6431154 B1 discloses how the air flow is reduced through the deacti-
vated cylinders in an internal combustion engine in order to avoid that emissions and
vibrations occur.
SUMMARY OF THE INVENTION
Despite prior art there is a need to further develop a method for controlling an internal
combustion engine in which vibrations resuiting from a zero flow of air supplied to the
exhaust gas system from one or more of the cylinders are reduced. There is also a
need to further develop a method for controlling an internal combustion engine which
reduces tail pipe exhaust emissions by introducing a zero flow of air to the exhaust
gas system from one or more of the cylinders and as a consequence increase the
exhaust gas temperature upstream the exhaust treatment system thereby facilitating
conversion of emissions.
The object of the present invention is thus to provide a method for controlling an in-
ternal combustion engine in which vibrations resuiting from a zero flow of air supplied
to the exhaust gas system from one or more of the cylinders are reduced.
Another object of the present invention is to provide a method for controlling an inter-
nal combustion engine in which the cooling of the exhaust treatment system is re-
duced.
Another object of the present invention is to provide a method for controlling an inter-
nal combustion engine in order to prevent oil from leaking into the combustion cham-
bers due to negative differential pressure in the combustion chambers when a zero
flow of air supplied to the exhaust gas system from one or more of the cylinders is
implemented.
A further object of the present invention is to provide a method for controlling an in-
ternal combustion engine which reduces tail pipe exhaust emissions when a zero
flow of air supplied to the exhaust gas system from one or more of the cylinders is
implemented.
These objectives are achieved with a method for controlling an internal combustion
engine, which is characterized by the features specified in patent ciaim 1.
According to the method, periodicaiiy no air is supplied to the exhaust gas system
from one or more of the deactivated cylinders of the internal combustion engine, and
the air mass trapped in the cylinders of the combustion engine which supply air to the
exhaust system is reduced in relation to the air mass trapped in the respective cylin-
ders which periodically not supply air to the engine exhaust system. This causes the
vibrations in the internal combustion engine to be reduced with a simultaneous in-
crease of the exhaust gas temperature upstream the exhaust treatment system,
thereby facilitating conversion of emissions.
The exhaust gas properties based on a diagnose of oxygen content and/or tempera-
ture of the exhaust gases are compared with predetermined exhaust gas properties.
Also, vibrations in the internal combustion engine based on crankshaft torsional vi-
brations, or other engine vibrations, are compared with a predetermined vibration
value of the internal combustion engine.
The internal combustion engine has preferably separate valve control means for the
inlet and exhaust valves. At an operating condition of the internal combustion engine
corresponding to normal load the control device controls the exhaust valves to open
at the bottom dead centre of the termination of the expansion stroke and so that they
close at top dead centre for start of the intake stroke, and the inlet valves open at the
top dead centre when the intake stroke starts and close at the bottom dead centre
when the compression stroke starts.
According to an aspect of the invention, when an operating condition in which the risk
of cooling the exhaust treatment system to a critical temperature exists, the intake
valves and exhaust valves in one or more of the cylinders are controlled to produce a
zero flow of air from the inlet side to the exhaust side of the cylinder when the pistons
move back and forth in these cylinders. At the same time, the fuel injection is con-
trolled to supply a first volume of fuel to the cylinders with zero ?ow of air, and also
ensure that a second volume of fuel is supplied to the other cylinders. Preferably, the
second fuel volume is greater than the first volume of fuel, which results in a reduc-
tion of vibrations of the internal combustion engine. However, under certain operating
conditions a different distribution between the first and second fuel volume is advan-
tageous. For example they may be equal, or the first volume of fuel may be greater
than the second volume of fuel.
According to another aspect of the invention, one of the first intake valves is con-
trolled to open at a bottom dead centrecentre of the piston in the first cylinder, be-
tween an expansion stroke and an exhaust stroke, and to close at a top dead centre
of the piston in the first cylinder between an exhaust stroke and an intake stroke. At
the same time the other of the first intake valves is controlled to open when one of
the first intake valves closes, and to close at bottom dead centre between an inlet
stroke and a compression stroke, and the first exhaust valves are controlled so that
they remain closed during all strokes of the engine.
According to a further aspect of the invention, one of the first exhaust valves is con-
trolled to open at a bottom dead centre of the piston in the first cylinder, between an
expansion stroke and an exhaust stroke, and to close at top dead centre of the piston
in the first cylinder between an exhaust stroke and an intake stroke, the other of the
first exhaust valves is controlled to open when one of the first exhaust valves closes,
and to close at bottom dead centre between an inlet stroke and a compression
stroke, and the first intake valves are controlled so that they remain closed during all
strokes of the engine.
The above mentioned objectives are also achieved with an internal combustion en-
gine, which is characterized by the features specified in patent claim 21.
Such combustion engine ensures that the vibrations caused by the fact that no air is
supplied to the exhaust gas system from one or more of the cylinders, are effectively
reduced. Such an internal combustion engine also increases the exhaust gas tem-
perature upstream the exhaust treatment system, thereby facilitating conversion of
emissions. By controlling the internal combustion engine so that the trapped air mass
in the second, active cylinder decreases relative to the trapped air mass of the first
deactivated cylinder, the pressure in the active cylinders will reduce and adapt to a
pressure level which substantially provide the same torque contribution to the crank-
shaft vs. crank angle, as the cylinders from which no air is supplied to the exhaust
gas system. Thus, the vibrations will be effectively reduced.
When for example 3 out of 6 cylinders are deactivated in an inline six-cylinder en-
gine, vibrations of the order 1,5 are created due to loss of torque contribution from
the deactivated cylinders. According to the invention the vibrations of order 1,5 are
suppressed by maintaining compression and expansion pressure in the deactivated
cylinders. By controlling the internal combustion engine so that the trapped air mass
in the active cylinders decreases in relation to the trapped air mass in the deactivated
cylinders, the suppression of vibrations of order 1,5 is further reduced. The invention
is particularly effective for reducing the low-frequency vibrations that arise during idle
operation of the engine.
ln order to minimize the excitation of vibrations of order 1,5, the sum of torque contri-
butions from the pressure in all cylinders should not contain the order of 1,5. This
may be achieved by reducing the difference between the torque contributions from
the deactivated and the activated cylinders by reducing the air mass trapped in the
active cylinders, while trapped air mass in the deactivated cylinders may be in-
creased. From the active cylinders air is supplied to the exhaust gas system. How
much reduction of the trapped air mass in the active cylinders that is required de-
pends on the load and speed of the engine, and is preferably controlled so that the
reduction of vibrations at idle has priority, however exhaust emissions always have
top priority. Torque vs. crank angle, produced by the active cylinders is a function of
cylinder pressure, cylinder bore and the crank mechanism, i.e. connecting rod length,
stroke of the crankshaft, and crankshaft position. The crank mechanism cannot be
affected. Therefore, the cylinder pressure is used to optimize the torque contribution.
Of particular importance is the crankshaft position approximately 25 degrees before
and after top dead centre because the combination of high cylinder pressure and the
position of the crank mechanism results in high torque.
The above mentioned objectives are also achieved with a vehicle, which is character-
ized by the features specified in patent claim 22.
A vehicle provided with such an internal combustion engine will avoid cooling of the
exhaust treatment system and ensure that vibrations due to the deactivation of the
cylinders are effectively reduced. The comfort of the persons travelling in the vehicle
increases when the vibrations of the vehicle decrease compared to previously known
concept for cylinder deactivation.
The invention also relates to a computer program and a computer program product
for performing the method according to the present invention.
BRIEF DESCRIPTION OF THE DRAWINGS
Below is a description of, as examples, preferred embodiments of the invention with
reference to the enclosed drawings, in which:
Fig. 1 shows schematically a vehicle in a side view, with an engine controlled by the
method according to the present invention,
Fig. 2 shows schematically a view from above of an engine controlled by the method
according to the present invention,
Fig. 3 shows a sectional view through the line ll-ll in fig. 2,
Fig. 4a-d shows graphs of the crankshaft torque from each cylinder of an engine con-
trolled by the method according to the present invention,
Fig. 5 shows graphs of the pressure in a cylinder vs. crank position of an engine con-
trolled by the method according to the present invention,
Fig. 6 shows graphs of the pressure in a cylinder vs. volume of an engine controlled
by the method according to the present invention, and
Fig. 7 shows a flow chart of the method for controlling an engine according to the
present invention.
DETAILED DESCRIPTION OF PREFERRED EMBODIIVIENTS OF THE INVENTION
Fig. 1 shows schematically a vehicle 1 in a side view, e.g. a truck, which comprises
an internal combustion engine 2 controlled by the method according to the present
invention. The engine 2, which may be a diesel engine, is connected to a gearbox 4
which is further connected to driving wheels 6 of the vehicle 1 via a propeller shaft 8.
The internal combustion engine controlled by the method according to the invention
will now be described with reference to figures 2 and 3. Fig. 2 shows a schematic
view from above of an internal combustion engine 2 of a four-stroke type. Preferably,
the engine is a diesel engine that is powered by diesel fuel and comprises at least a
first and second cylinder C1, C4. The engine 2 of the embodiment disclosed in fig. 2
comprises six cylinders C1 - C6, which are arranged in a row in which a piston P1 -
P6 is arranged in each cylinder C1 - C6 of the engine 2. The invention is applicable
to any cylinder configuration and not limited to inline engines only.
At least one first inlet valve 18 is provided in the first cylinder C1 and the first inlet
valve 18 is in communication with an intake system 20. At least one first exhaust
valve 24 is provided in the first cylinder C1 and the first exhaust valve 24 is in com-
munication with an exhaust system 26. At least one second inlet valve 19 is provided
in the second cylinder C4 and the second inlet valve 19 is in communication with the
intake system 20. At least one second exhaust valve 25 is provided in the second
cylinder C4 and the second exhaust valve 25 is in communication with the exhaust
system 26. Correspondingly, the inlet and exhaust valves are provided in the remain-
ing cylinders C2, C3, C5, C6.
Preferably, two inlet valves 18, 19 and two exhaust valves 24, 25 are arranged in
each cylinder C1 - C6 where each inlet valve 18, 19 communicates with the intake
system 20 and each exhaust valve 24, 25 communicates with the exhaust system 26.
According to one embodiment, a damper 23 may be arranged in the intake system
, which damper 23 can be adjusted so that it restricts the air supply to the cylinders
C4 - C6 of the engine 2.
Fig. 3 shows a cross sectional view of the internal combustion engine 2 through the
line ||-|| in Fig. 2. The piston P1 is via a connecting rod 14 connected to a crankshaft
16, which upon rotation of the crankshaft 16 reciprocates the piston P1 in the cylinder
C1. However, it is possible to replace the crankshaft 16 and use some other force
transfer means 16 for transfer force from the piston P1 to the gearbox 4 and to the
propeller shaft 8 of the vehicle 1. At least a first valve control means in the form of a
first cam shaft 22 is provided to control the first and second inlet valve 18, 19. At
least one second valve control means in the form of a second camshaft 28 is ar-
ranged to control the first and second exhaust valve 24, 25. According to the illus-
trated embodiment the valve control means comprises camshafts 22, 28, but it is
however possible to use other types of valve instruments, such as hydraulic, pneu-
matic or electric valve control means.
The crankshaft 16 is arranged to control each camshaft 22, 28. At least one control
device 34 is provided between the crankshaft 16 and each camshaft 22, 28 for con-
trolling the first inlet valve 18 and the first exhaust valve 24, so that no air is supplied
to the exhaust system 26 from the first cylinder C1 when the first piston P1 moves
back and forth in the first cylinder C1 and when the first cylinder C1 is deactivated.
Thus, a zero flow through the first cylinder C1 is created. However, it is possible to
replace the crankshaft 16 and use some other force transfer means 16 for controlling
each camshaft 22, 28.
The control device 34 is also arranged to control the internal combustion engine 2 so
that the intake air mass in the second cylinder C4 decreases relative to the intake air
mass in the first cylinder C1. At one operating condition the combustion engine cor-
responding to a normal state the control device 34 is controlled so that the exhaust
valves 24, 25 open at the bottom dead centre BDC for the termination of the expan-
sion stroke and so that they close at the top dead centre TDC for start of the inlet
stroke, and that the inlet valves 18, 19 open at the top dead centre TDC when the
inlet stroke begins, and closes at bottom dead centre BDC when the compression
stroke starts.
Depending on the type of internal combustion engine 2, two first and two second cam
shafts 22, 28 may be provided in the internal combustion engine 2. This is advanta-
geous if the engine 2 is of a V-type.
A camshaft controller 30 is provided in the internal combustion engine 2. The crank-
shaft 16 controls each camshaft 22, 28 via a camshaft transmission 32. At least one
control device 34 is provided between the crankshaft 16 and each camshaft 22, 28,
so that the valves can be controlled to a position in which the inlet and exhaust
valves 18, 19, 24, 25 are controlled so that no air is supplied to the exhaust system
26 when the pistons P1 - P3 move back and forth in the cylinders C1 - C3. Prefera-
bly, a control device 34 is provided for each camshaft 22, 28. An electronic control
unit 36 receives signals from various sensors (not shown) such as the absolute pres-
sure in the intake manifold, the charge air temperature, air mass flow, throttle posi-
tion, engine speed and engine load. The control unit 36 affects the control device 34,
which adjusts the valves 18, 19, 24, 25 opening and closing times relative to the posi-
tion of the crankshaft angle (p.
A computer program P controls the internal combustion engine 2, wherein said com-
puter program P comprises program code for making the electronic control unit 36 or
another computer 46 connected to the electronic control unit 36 performing the steps
of the method according to the present invention. The invention also relates to a
computer programme product which is directly storable in an internal memory M into
the electronic control unit 36 or the other computer 46.
A fuel pump 41 is connected to injection means 43 arranged in each cylinder C1 -
C6. The injection means 43 injecting fuel into the cylinders C1 - C6. Thus, the engine
is preferably designed as an Otto engine.
Fig. 4 a - d shovv graphs of tordue versus crankshaft angle qi ef an internal combus-
'tidn engine 2 prdvided with six cylinders Cl - C6. Tile Y axis represents tdrque T
froni the cylinders Cl - (36. The X axis represents the crankshaft angle <9 and tliereby
the position of pieion P1. Each positive tordue pulse in Pig. 4a represents en expan-
sion of cylinder Cl - (36, respeclively. išveiy iiegative terdue pulse represents a com-
pression oi cylinder Ci - (36, respectiveiy.
11
in Pig. 4h three et the engines six cyiinders (It ~ (33 has heen deactivated white the
remaining three cyiinders G4 - (26 are stiii activated. in a deactivated cylinder no air is
supplied to the exhaust gas system. ln the embodiment disclosed in fig. 4b no fuel is
supplied to the deactivated cylinders C1 - C3. in an activated cyiinder tuei and air are
supplied te the cyiinder cerresoonding te norrnai eperatien conditions of the engine 2.
Ail veives in the three deactivated cyiinders (31 - (33 are cicsed and the cyiinders (lt ~
(33 have gradualiy detiated. A prohiein anses when ene cr rnore cyiinders Ct ~ CB is
deactivated and the other cylinders (34 - (36 are activated. Then vihretions are gener-
ated hy the cemhustien engine 2 due to a different frequency spectrum ot expansions
et the engine 2, since srnaii or no toreue putsas are obtained frorn the pressure in the
deactivated cyiinders Ci « (33.
in Fig. ac the vihratiens have to scrne extent heen reduced hy controiling the corn~
hustion engine 2 se tiiat the sarne amount ot gas is trapped in cyiinders Ct ~ (33 as
in cyiinders (34 - (36, during the intet stroke. At the sarne tirne cyiinders (31 -« (33 are
centroiied in such a tyay that the net iiow et gas across these cyiiitders is zero. The
air traoped in the deactivated cyiiiwders Ct - (33 nfiii he centoressed and exoanded
and therehy transier a tordue to the crankshatt. This wiii change the order ot vibra-
tions frcrn i,5 to 3.
Fig. fiir: shews however that the positive tordue puise in the active cyiinders G4 ~ G6
is higher than the positive terdue pulse which heiids up in the deactivated cyiinders
G1 - G3. This tordue difference wili cause vihratiens in the engine 2, ttrhich hecerne
especiaiiy annoying when the engine 2 is operated et idle speed. The vihraticns ere
generated hy the iaterai forces hett-trash the eistons Ft ~ P3 and cyiiitders Ct ~ 63,
and in the hearings tor the crankshatt 16.
Ešy reduciiwg the intake air rnass to the active cyiinders (34 ~ C36 in reiation te the in-
taite air rnass in the deactivated cyiinders Ci - G3, the terdue ot the active cyiinders
C4- - (36 wiil reduce and adapt to a pressure ievei suhstantiaiiy cerresponding to the
terciue in the deactivated cyiinders Ct ~ G3, as shoe/ri hy the green in Fig. 4d. Thus
the vihrations wšii be etiectiveiy reduced.
12
When tor exarnpie 3 out ot 6 of the cyiirtders (lt - G6 are deactivated in an iniine six
cyiinder engine in the embodiment above, vibrations of order 1,5 arises. i-iovvever,
the method according to the invention changes to the order ot vibrations to 3 by
rnaintaining compression and expansion pressure in the deactivated cyiinders Ct -
(33. By controiiing the internai combustion engine 2 so that the rttass of air trapped in
the active cyiinders G4 ~ G6 decreases in reiation to the mass oi air trappen in the
deactivated cylinders (31 - (33 the mass fiow ot air to the active cyiinders (34 ~ (36 wiii
decrease. According to one enthodirnent the intet vaives 19 in the active cylinders G4
- (36 are controiied to reduce the intake air rriass to the active cviinders (34 - (36. This
is achieved by controiiing the intet vaives 19 in the active cyiinders (34 ~ G6 to ciose
before or after the closirtg tirne of inlet valves 19 during normai operation ot the inter-
nai combustion engine 2.
According to an embodiment of the invention the inlet and exhaust valves 18, 24 in
one or more of the cylinders (31 - (33 are controlled to produce a zero flow of air from
the inlet side to the exhaust side of the cylinder when the pistons move back and
forth in these cylinders. At the same time, the fuel injector is controlled to supply a
first volume of fuel to the cylinders with zero ?ow of air during these cylinders expan-
sion stroke, and also a second volume of fuel is supplied to the cylinders in which a
flow ofgas from the inlet side to the exhaust side is executed, during these cylinders
expansion. Under these conditions the pressure in the cylinders C1 - C3 will increase
and be adapted to a pressure level which substantially corresponds to the pressure
in the cylinders C4 - C6, which is shown by the graph in Fig. 4d. Thus vibrations will
be effectively reduced. The ratio between the first and second fuel volume can vary
depending on the internal combustion engine and vehicle operating conditions. The
first and second fuel volume may also be substantially equal.
The graphs in Fig. 4 represent an internet combustion engine 2 of the tounstroke
type, where vvithin the cranitshatt 16 rotates 7213 ° CA and each piston P1 ~ P6 traveis
tour strokes to coinpiete a tuii cycie.
Fig. 5 iiiustrates cyiinder pressure vs. crankshaft position e ot an internai combustion
engine 2. The Y-axis represents the pressure p in the cyiinder G1, and in the cyiinder
C34. The X-axis represents the crankshait tiosition to and thus the position of the pis-
13
ton P in the cylinder. Graph A in Fig, 5 iiiustrates the pressure in the deactivated oyi-
inder Ct vs. orankshatt position o. (šraph B iiiustrates the pressure in the active ovi-
inder (134 vs. orankshatt position o. The additionai pressure irierease arising atter top
dead centre, TÜC in the graohs B and CI is due to oornhustion ot tuei.
in order to cornpieteiy eiiminate the exoitation ot vihrations ot the order i ,5, the pres-
sure in aii cyiinders (It - (35 must he identioai. This is airhost achieved hy reduoing
the difference between tordue puises trom the deactivated and the active cytinders
(lt - (36, hy redueing the air rnass trapped in the active cyiinders Ca - (36, vtfhiie the
trapped air rtiass in the deaotivated cyiinders Ct - (33 may he increased. Graph C
shovvs that the trapped air mass ~ and hence presstire - in the active oyiinder (34 has
heen reduced and varies with the cranirshatt position o. The required reduction ot
traphed air in the active eytinders G4 ~ C63, depends on the ioad and is preterahiy
controiied so that reduction ot vihrations at idie is ttrioritized. Toroue vs. orank angie
produced hy the active oyiinders (34 ~ Cd is a tunotion ot cyiinder pressure, oyiinder
hore and the crank mechanism, ie. eonnecting rod iength, stroke ot the crankshatt
16, and erankshatt position, e. "the crank ntecitanisnt cannot he intiuenoed, and
theretore the cyiinder pressure is used to optirnize the addition ot tordue. Üt partiet:-
iar importance is the crank position approxirnateiy 25 degrees hetore and etter piston
top dead centre TDC, since the oonthiriation ot high inet/tänder pressure. and the
crank rnechanisrn position vviii resutt in high toroue. in an ernhodiment, the second
iniet vaives are controiied to reduce the intake air mass to the active eyiinders G4 «
(36. This is achieved hy controiiing the intet vaives 'iQ in the aetivated cyiinders (34 -
G6 to oiose hetore or efter the ciosing tirrie ot iniet vaives 19 during normai operation
ot the internet corrihustion engine 2.
According to the tirst ernhodiment the intet vaives ti) in the oyiinders C34 - G6 are
controiied to oiose in the range eorrespondiitg to 30” cranksiiatt angies hetore hos
torn dead centre (CA hEšDCI) to Bi? crankshatt angies atter bottom dead centre (CA
aBDC), preterahiy at the hottoni dead centre (aBDC).
According to the second ernhodinient the intet vaives 'is in the oyiinders (34 ~ (36 are
controiied to ciose in the range eorresponding to St? CA aBDC to 9=Ci° CA aBDG,
preterahiy 6G” CA aBÛC. According to a third ernhodirnent the darnper, eg. a throttie
14
23 arranged in the intaite system 20 is activated. By ciosing the throttie 23 in order to
restrict the air iiow to the active cyiinders (34 » Co of engine 2 the trapped rnass ot air
in the active cyiinders G4 - Co wii! decrease. The throttie 23 can he oseci in combina-
tion iivith the controi ot the intaite valves 19 to the active cyiinders G4 - (36.
ln order to controi the intake vaives 18 and exhaust vaives 24 of the deactivated cyt~
inders (31 ~ (33, so that no air enters the exhaust system 26 frorn the deactivated cyt-
inders Ct ~ G3 when the pistons P1 ~ P3 rhoves hack and forth in the deactit/ated
cyiihders Ct - (33 the intaite vaives ot the deactivated cyiinoers (lt ~ (33 are con-
troiied, according to a 'tirst ernhodintent, to open in the exhaust stroke and in the in-
take stroke, ifvhiie the exhaust vaives ot the deactivated cyiinders G1 - C33 are con-
'troiieci to a closed position 'tor aii strokes,
According to a second ernioociirnent the exhaust vaives 24 of the deactivated cyiin-
dere (lt - G3 are controiied to open in tite exhaust stroke and in the intake stroke,
white the intake vaives ot the deactivated cyiinders (Ii ~ (33 are controiied to a ciosed
position for aii strokes.
Therehy the resoiting 'fiow to the exhaust systern 26 'irorn the cieactivateo cyiinders
G1 - (33 wiii become zero. Since there is no het tiow of air through these cyiinders ot
'the interna! comoustioit engine 2, cooiing and oxygenation of the exhaust 'treatment
systern 38 is avoided. Since no suh atmospheric pressure is deveioped in the cylin-
ciers (31 - G3, no oii carryover across the piston rings from the cranitcase to the corn-
hostion charriher takes piace. it shouid he rnentioned in this context that it is possihie
to supply tuei to the deactivated cyiinders (It-Gå, white no net iiow oi air is gerierateci
hy these cyiinders. Then the cyiinder pressure increases in the deactivated cyiinciers
during comoostion, irvhich contrihutes to a reduction of vibrations.
To completely eliminate the excitation of vibrations of the order 1,5, the pressure in
all cylinders C1 - C6 must be identical. ln order to substantially achieve this the in-
take valves and exhaust valves of cylinders C1 - C3 are controlled so that a zero ?ow
of air from the inlet side to the exhaust side is achieved, and so that no air is supplied
to the exhaust system from these cylinders, when the pistons move back and forth in
the cylinders C1 - C3. Meanwhile, the fuel injectors 43 are controlled to supply a first
volume of fuel to the cylinders G1 - G3 at TDGf (Top Dead Centre firing). A second
volume of fuel is supplied to the cylinders G4 - G6 at TDGf for these cylinders. As a
result, the pressure in the cylinders G1 - G3 will increase and be adapted to a pres-
sure level which substantially corresponds to the pressure in the cylinders G4 - G6.
Thus, the vibrations will be effectively reduced. lf the first and second fuel volume are
equal an essentially complete elimination of the order of 1,5 is achieved.
According to a further embodiment disclosed in Pig. 6 the inlet valves 18 and 19 and
the exhaust valves 24 and 25 in all cylinders G1 - G6 are kept closed so that no air is
supplied to the exhaust system 26 from the cylinders G1 - G6 when the pistons P1 -
P6 move back and forth in the cylinders G1 - G6. The fuel injectors 42 are controlled
to supply fuel at TDGf to all of the cylinders G1 - G6, through which a zero flow of air
from the inlet side to the exhaust side prevail.
According to this embodiment fuel is supplied during several consecutive expansion
strokes in the cylinders G1 - G6. As a result the pressure in the cylinders G1 - G6
will increase in consecutive steps A1 - A3.
When the irapped air within the cylinders has been cohsumed by the consecutive
combustions during the expansion strokes, the inlet valves 18 and 19 and the ex-
haust valves 24 and 25 in the cylinders G1 - G6 are controlled to an opening and
closing procedure corresponding to a normal operation condition for the engine 2 so
that fresh air is supplied to the cylinders G1 - G6. Thereafter, if the exhaust gas
properties and/or exhaust temperature deviate from the predetermined exhaust gas
properties and/or exhaust temperature the inlet valves 18 and 19 and the exhaust
valves 24 and 25 in all cylinders G1 - G6 are kept closed so that no air is supplied to
the exhaust system 26, and fuel is supplied during several consecutive expansion
strokes in the cylinders G1 - G6.
The method for controllirig the internal combustion engine 2 of the present inventioiw
will be described along with the flowchart of Fig. ff, comprises the steps of:
a) driving the internal combustion engine 2 at least one cycle of opening and closing
of the inlet and exhaust valves 18,19,24,25 corresponding to normal operation of the
combustion engine 2,
16
b) comparing the exhaust gas properties with a predetermined value for exhaust gas
properties, such as exhaust temperature,
d) supplying fuel to the second cylinder C4, and
e) controlling the first inlet valve 18 and the first exhaust valve 24, so that no air is
supplied to the exhaust system 26 from the first cylinder C1 when the first piston P1
moves back and forth in the first cylinder C1, if the exhaust gas properties deviate
from the predetermined exhaust gas properties.
The method comprises the additional step: c) diagnosing vibrations of the internal
combustion engine 2 and compare the vibrations with a predetermined value of vibra-
tions of the internal combustion engine 2.
Step b) and step c) are performed in any order or are performed substantially simul-
taneously.
ln step b) the exhaust gas properties may for example be the amount of oxygen in
the exhaust gases and/or the exhaust temperature of the exhaust gases.
During step a) information about the present air-fuel ratio Åpres and present vibrations
Vpres of the engine 2 are collected and the collected present air-fuel ratio Apms is in
step b) compared to a predetermined reference value for the air-fuel ratio Åref and the
collected present value of vibrations Vpæs is in step c) compared to a predetermined
reference value for the vibrations Vref. lf the exhaust gas properties deviate from the
predetermined exhaust gas properties, i.e. Apres > Aref the first inlet valve 18 and the
first exhaust valve 24 are controlled, so that no air is supplied to the exhaust system
26 from the first cylinder C1 when the first piston P1 moves back and forth in the first
cylinder C1. However, if Åpres < Åref the first inlet valve 18 and the first exhaust valve
24 are controlled to open and close in accordance to normal engine operation condi-
tions.
The method comprises the additional step: f) reducing the intake air mass to the sec-
ond cylinder C4 in relation to the intake air mass to the first cylinder C1, if the vibra-
17
tions in the internal combustion engine 2 are greater than the predetermined value
for the vibrations in the internal combustion engine 2.
ln step f) if the collected present value of vibrations Vpres in the internal combustion
engine 2 is greater than the predetermined reference value for the vibrations Vref in
the internal combustion engine 2, i.e. Vpres > Vref the intake air mass to the second
cylinder C4 is reduced in relation to the intake air mass to the first cylinder C1. Thus,
the pressure in the second cylinder C4 is reduced and the vibrations in the engine 2
will be effectively reduced.
ln step f) the second inlet valve 19 is controlled to reduce the trapped mass of air in
the second cylinder C4. This may be achieved by controlling the second inlet valve
19 to close before or after the time of closing of the second inlet valve 19 during nor-
mal operation of the combustion engine 2.
According to an embodiment the force transfer means 16 for controlling each valve
control means 22, 28 Es a crankshaft 1ß and the second inlet valve 19 is controlled to
close in the range corresponding to 30° CA bBDC to 30° CA aBDC, preferably at
BDC.
According to another embodiment the force transfer means 16 for controlling each
valve control means 22, 28 ls a crankshafl: 16 and the second inlet valve 19 is con-
trolled to close in the range corresponding to 30° CA aBDC to 90° CA aBDC, pref-
erably 60° CA aBDC.
According to an embodiment the first inlet valve 18 is in step e) preferably controlled
to open during the exhaust stroke and the intake stroke, while the first exhaust valve
24 is controlled to a closed position during all strokes.
According to another embodiment the first exhaust valve 24 is in step e) preferably
controlled to open during the exhaust stroke and the intake stroke, while the first inlet
valve 18 is controlled to a closed position for all strokes.
18
Preferably, the supplied fuel to the engine 2 is diesel fuel. Since an engine 2 powered
by diesel works according to the compression ignition principle, pistons, valves and
valve timing are designed with a suitable geometry, so that a functional interaction
between the pistons and valves is obtained.
The method comprises the additional step: g) control respective valve 18,19,24,25 by
means of two first and two second valve control means 22, 28.
Preferably, the valve control means 22, 28 are camshafts 22, 28. The inlet and ex-
haust valves are controlled and driven by a separate valve control device, which is in
turn driven by the crankshaft. The respective valve control device has control means
which controls the valve and thus the opening and closing times of the valve. The
control device is preferably coupled to a control unit which controls the control device
to a position which is adapted to the internal combustion engine operating conditions.
The control unit also controls a fuel injection device that supplies fuel to the cylinders.
The method comprises the additional steps:
h) supply a first volume of fuel to the first cylinder C1 to be combusted in total or
mostly during the expansion stroke of the first cylinder C1, and
i) supply a second volume of fuel to the second cylinder C4 to be combusted in total
or mostly during the expansion stroke of the second cylinder C4.
By controlling the inlet valves and exhaust valves of the cylinders where within a zero
flow from the inlet side to the exhaust side prevails and consequently no air is sup-
plied to the exhaust system from these cylinders when the pistons move back and
forth in the cylinders, while the fuel injectors 43 are controlled to supply a first volume
of fuel at TDCf to the cylinders through which a zero flow from the inlet side to the
exhaust side prevails and also ensure that a second volume of fuel is supplied at
TDCf to the cylinders in which a flow of gas from the inlet side to the exhaust side
takes place, the pressure in the cylinders C1 - C3 will increase and be adapted to a
pressure level substantially corresponding to the pressure in the cylinders C4 - C6.
Thus, the vibrations will be effectively reduced. The ratio between the first and sec-
ond fuel volume can vary depending on the combustion engine and operating condi-
tions of the vehicle. The first and second volume of fuel may be substantially equal,
19
but preferably the second volume of fuel is greater than the first volume of fuel, so
that vibrations are effectively reduced.
Preferably, the method comprises the additional step:
j) control two inlet valves 18, 19 and two exhaust valves 24, 25 by means of respec-
tive valve control means 22, 28. ln such an internal combustion engine, the applica-
tion of the invention may be very efficient, since the number of valves per cylinder
affects the air flow and the filling and emptying of the cylinders.
According to an embodiment in step j):
-control one of the first intake valves 18 to open at a bottom dead centre BDC of the
piston P1 in the first cylinder C1 between an expansion stroke and an exhaust stroke,
and to close at a top dead centre TDC for the piston P1 in the first cylinder C1 be-
tween an exhaust stroke and an intake stroke;
-control the other of the first intake valves 18 to open when one of the first intake
valves 18 closes, and to close at the bottom dead centre BDC between an intake
stroke and a compression stroke, and
-control the first exhaust valve 24, so that they remain closed during all strokes of the
engine 2.
According to another embodiment in step j):
-control one of the first exhaust valves 24 to open at a bottom dead centre BDC of
the piston P1 in the first cylinder C1 between an expansion stroke and an exhaust
stroke, and to close at a top dead centre TDC of the piston P1 in the first cylinder C1
between the exhaust stroke and an intake stroke;
-control the other of the first exhaust valves 24 to open when one of the first exhaust
valve 24 closes, and to close at the bottom dead centre BDC between the intake
stroke and a compression stroke, and
-control the first intake valves 18, so that they remain closed during all strokes of the
engine 2.
The method comprises the additional step: k) controlling the second inlet valve 19
and the second exhaust valve 25, so that no air is supplied to the exhaust system 26
from the second cylinder C4 when the second piston P4 moves back and forth in the
second cylinder C4, if the exhaust gas properties deviate from the predetermined
exhaust gas properties.
Preferably, in steps e) and k) fuel is supplied during several consecutive cycles in the
first and second cylinders C1, C4.
lf the diagnosed exhaust gas properties comprises information about the present air-
fuel ratio Apres and the predetermined exhaust gas properties comprises information
about a predetermined reference value for the air-fuel ratio Åref and if the present air-
fuel ratio Åpres is less than the air-fuel ratio Aref the inlet and exhaust valves 18, 19, 24,
are controlled to open and close in accordance with normal operation of the com-
bustion engine 2.
The present invention also relates to a computer programme P (fig. 3) and a com-
puter programme product for performing the steps of the method. The computer pro-
gram P controls the internal combustion engine, wherein said computer program P
comprises program code for making the electronic control unit 36 or another com-
puter 46 connected to the electronic control unit 36 performing the steps of the
method according to the present invention as mentioned herein, when said computer
programme P is run on the electronic control unit 36 or another computer 46 con-
nected to the electronic control unit 36.
The computer programme product comprises a program code stored on a, by an
electronic control unit 36 or another computer 46 connected to the electronic control
unit 36 readable, media for performing the steps of the method according to the pre-
sent invention as mentioned herein, when said computer programme P is run on the
electronic control unit 36 or another computer 46 connected to the electronic control
unit 36. Alternatively, the computer programme product is directly storable in an in-
ternal memory M into the electronic control unit 36 or another computer 46 connected
to the electronic control unit 36, comprising a computer programme P for performing
the steps of the method according to the present invention, when said computer pro-
21
gramme P is run on the electronic control unit 36 or another computer 46 connected
to the electronic control unit 36.
The components and features specified above may within the framework of the in-
vention be combined between the different embodiments specified.
Claims (24)
1. A method for cchtreiâtrtg an internet combustion engine, (2) cemprising, at teast a first and second cyiinder (Ci, 04); one first pister: (P1) arranged in the first cyiirtder ((31); one second pistcn (P4) arrangeci än the second cytinder (C42 at teast ene tšrst intet vaive (18) arranged in the first cyiinder (C1), the tšrst šniet vaive (18) comrnunicates With an intake system (203 at teast a first exhaust vaive (24) arranged in the fšrst cylinder ((31), the first exhaust vaive (24) ccmmunicates with ah exhaust system (263 at teast a second intet vatve (tät) arranged ih the second cytinder (C34), the second intet vaâve (19) cemmunicates with the intake system (2ü); at teast a second exhaust vatve (25) arranged in the second cyiiewder ((34), the sec- ond exhaust vatve (25) ccmmunicates with the exhaust system (2tš); at teast a first vaive controi means (22) vvhich contrcis the first and second inlet valve (18, 1Q); at teast a second vaive centret means (28) which centrets the first and second ex~ haust vaive (24, 25); and at least one force transfer means (16) for controttihg each vaive centret means (22, 28), cherecterized än that the method comprises the following steps: a) driving the internal combustion engine (2) at least one cycle of opening and clos- ing of the inlet and exhaust valves (18,19,24,25) corresponding to normal operation of the combustion engine (2), b) comparing the exhaust gas properties with a predetermined value for exhaust gas properties, d) supplying fuel to the second cylinder (4), and e) controlling the first inlet valve (18) and the first exhaust valve (24), so that no air is supplied to the exhaust system (26) from the first cylinder (C1) when the first piston (P1) moves back and forth in the first cylinder (C1), if the exhaust gas properties de- viate from the predetermined exhaust gas properties. 10 15 20 25 30 23
2. The method of claim 1, characterized by the additional step: c) diagnosing vibra- tions of the internal combustion engine (2) and comparing the vibrations with a pre- determined value of vibrations of the internal combustion engine (2).
3. The method of claim 2, characterized in that in step b) and step c) are performed in any order or are performed substantially simultaneously.
4. The method according to any of claim 2 and claim 3, characterized by the addi- tional step: f) reducing the intake air mass to the second cylinder (C4) in relation to the intake air mass to the first cylinder (C1), if the vibrations in the internal combus- tion engine (2) are greater than the predetermined value for the vibrations in the in- ternal combustion engine (2).
5. The method of claim 4, characterized in that in step f) the second inlet valve (19) is controlled to reduce the trapped mass of air in the second cylinder (C4).
6. The method of claim 5, characterized in that the second inlet valve (19) is con- trolled to close before or after the time of closing of the second inlet valve (19) during normal operation of the combustion engine (2).
7. The method according to claim 6, characterized in that the force transfer means (16) for controlling each valve control :Haans (22, 26) comprises a crankshaft (16) and En that the second inlet valve (19) is controlled to close in the range correspond- ing to 30° crank angle before bottom dead centre (CA bBDC) to 30° after bottom dead centre (CA aBDC), preferably at the bottom dead centre (atBDC) .
8. The method of claim 6, characterized in that the force transfer means (16) for con- trolling each valve control means (22, 28) comprisas a crankshaft (16) and in that the second inlet valve (19) is controlled to close in the range corresponding to 30° after bottom dead centre (CA aBDC) to 90° after bottom dead centre (CA aBDC), prefera- bly 60° crank angles after bottom dead centre (CA aBDC). 10 15 20 25 30 24
9. The method according to any of the preceding claims, characterized by the addi- tional step: g) control respective valve (18,19,24,25) by means of two first and two second valve control means (22, 28).
10. The method according to any of the preceding claims, characterized in that the valve control means (22, 28) are camshafts (22, 28).
11. The method according to any of the preceding claims, characterized in that the method comprises the further steps of: h) supply a first volume of fuel to the first cylinder (C1) to be combusted in total or mostly during the expansion stroke of the first cylinder (C1), and i) supply a second volume of fuel to the second cylinder (C4) to be combusted in total or mostly during the expansion stroke of the second cylinder (C4).
12. The method of claim 11, wherein the second volume of fuel is greater than the first volume of fuel.
13. The method according to any of the preceding claims, characterized by the addi- tional step: j) control two inlet valves (18, 19) and two exhaust valves (24, 25) by means of re- spective valve control means (22, 28).
14. The method of claim 13 , characterized in that in stepj): -control one of the first intake valves (18) to open at a bottom dead centre (BDC) of the piston (P1) in the first cylinder (C1) between an expansion stroke and an exhaust stroke, and to close at a top dead centre (TDC) for the piston (P1) in the first cy- cylinder (C1) between the exhaust stroke and an intake stroke; -control the other of the first intake valves (18) to open when one of the first intake valves (18) closes, and to close at the bottom dead centre (BDC) between the intake stroke and a compression stroke, and -control the first exhaust valve (24), so that they remain closed during all strokes of the engine (2). 10 15 20 25 30 25
15. The method of claim 13, characterized in that in step j): -control one of the first exhaust valves (24) to open at a bottom dead centre (BDC) of the piston (P1) in the first cylinder (C1) between an expansion stroke and an exhaust stroke, and to close at a top dead centre (TDC) of the piston (P1) in the first cy- cylinder (C1) between the exhaust stroke and an intake stroke; -control the other of the first exhaust valves (24) to open when one of the first ex- haust valve (24) closes, and to close at the bottom dead centre (BDC) between the intake stroke and a compression stroke, and -control the first intake valves (18), so that they remain closed during all strokes of the engine (2).
16. The method according to any of the preceding claims, characterized by the addi- tional step: k) controlling the second intake valve (19) and the second exhaust valve (25), so that no air is supplied to the exhaust system (26) from the second cylinder (C4) when the second piston (P4) moves back and forth in the second cylinder (C4), if the exhaust gas properties deviate from the predetermined exhaust gas properties.
17. The method of claim 16, characterized in steps e) and k) fuel is supplied during several consecutive cycles in the first and second cylinders (C1, C4).
18. The method of claim 17, characterized in that the inlet and exhaust valves (18, 19, 24, 25) are controlled to open and close in accordance to normal operation of the combustion engine (2) if the diagnosed exhaust gas properties comprises information about the present air-fuel ratio (Apres) and the predetermined exhaust gas properties comprises information about a predetermined reference value for the air-fuel ratio (Åref) and if the present air-fuel ratio (Åpres) is less than the air-fuel ratio (Åref).
19. The method according to any of claims 1-8, characterized in that in step e) the first inlet valve (18) is controlled to open during the exhaust stroke and the intake stroke, while the first exhaust valve (24) is controlled to a closed position during all strokes. 10 15 20 26
20. The method according to any of claims 1-8, characterized in that in step e), the first exhaust valve (24) is controlled to open during the exhaust stroke and the intake stroke, while the first inlet valve (18) is controlled to a closed position for all strokes.
21 _ An internal combustion engine (2) characterized in that the engine (2) is con- trolled according to the method of claims 1 - 20.
22. A vehicle (1 ), characterized in that the vehicle (1) comprises an internal com- bustion engine (2) according to claim 21.
23. A computer program (P) for controlling an internal combustion engine (2), wherein said computer program (P) comprises program code for making an elec- tronic control unit (36) or another computer (46) connected to the electronic control unit (36) performing the steps according to any of the claims 1 - 20.
24. A computer program product comprising a program code stored on a media readable by a computer (36, 46) to perform the steps of the method according to any of the claims 1 - 20, when said program code runs on an electronic control unit (36) or another computer (46) connected to the electronic control unit (36).
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
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SE1550267A SE1550267A1 (sv) | 2014-03-07 | 2015-03-05 | A method for controlling an internal combustion engine, an internal combustion engine controlled by such a method and avehicle comprising such an internal combustion engine. |
PCT/SE2015/000013 WO2015133957A1 (en) | 2014-03-07 | 2015-03-09 | A method for controlling an internal combustion engine, an internal combustion engine controlled by such a method and a vehicle comprising such an internal combustion engine. |
DE112015000774.1T DE112015000774T5 (de) | 2014-03-07 | 2015-03-09 | Verfahren zum Steuern eines Verbrennungsmotors, durch ein solches Verfahren gesteuerter Verbrennungsmotor und Fahrzeug mit einem solchen Verbrennungsmotor |
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SE1450258A SE539424C2 (sv) | 2014-03-07 | 2014-03-07 | Förbränningsmotor, fordon som innefattar en sådan förbränningsmotor och förfarande för att styra en sådan förbränningsmotor |
SE1450259A SE538790C2 (sv) | 2014-03-07 | 2014-03-07 | Förbränningsmotor, fordon som innefattar en sådan förbränningsmotor och förfarande för att styra en sådan förbränningsmotor |
SE1450260 | 2014-03-07 | ||
SE1550267A SE1550267A1 (sv) | 2014-03-07 | 2015-03-05 | A method for controlling an internal combustion engine, an internal combustion engine controlled by such a method and avehicle comprising such an internal combustion engine. |
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DE (1) | DE112015000774T5 (sv) |
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JP3733786B2 (ja) * | 1999-05-21 | 2006-01-11 | トヨタ自動車株式会社 | 電磁駆動弁を有する内燃機関 |
JP2001132484A (ja) * | 1999-11-05 | 2001-05-15 | Denso Corp | 内燃機関の可変気筒制御装置 |
CN100368671C (zh) * | 2002-01-31 | 2008-02-13 | 马自达汽车株式会社 | 火花点火发动机的控制装置 |
US8020525B2 (en) * | 2007-07-12 | 2011-09-20 | Ford Global Technologies, Llc | Cylinder charge temperature control for an internal combustion engine |
US8667953B2 (en) * | 2009-10-14 | 2014-03-11 | GM Global Technology Operations LLC | Cylinder deactivation to reduce fuel enrichment after fuel cutoff modes |
GB2496407B (en) * | 2011-11-10 | 2017-11-08 | Ford Global Tech Llc | A three cylinder engine with a deactivatable cylinder. |
US8955498B2 (en) * | 2012-07-24 | 2015-02-17 | Ford Global Technologies, Llc | Variable valve timing for EGR control |
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2015
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DE112015000774T5 (de) | 2016-11-24 |
WO2015133957A1 (en) | 2015-09-11 |
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