Classifications

• • 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
  • F02D41/0007—Controlling intake air for control of turbo-charged or super-charged engines
• • 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
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
  • F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
  • F01N3/08—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
  • F01N3/10—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
  • F01N3/24—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
  • F01N3/30—Arrangements for supply of additional air
  • F01N3/32—Arrangements for supply of additional air using air pump
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
  • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
  • F02B37/12—Control of the pumps
  • F02B37/16—Control of the pumps by bypassing charging air
• • 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
  • F02D13/0261—Controlling the valve overlap
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02D—CONTROLLING COMBUSTION ENGINES
  • F02D23/00—Controlling engines characterised by their being supercharged
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
  • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
  • F02B37/12—Control of the pumps
  • F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
• • 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

Definitions

• the present invention relates to a method of controlling turbocharger speed of a piston engine according to the preamble of claim 1.
• the present invention relates to a control system for a turbocharged piston engine according to the preamble of claim 14.
• a turbocharger is generally accepted way of improving the performance of an internal combustion engine.
• the operation of a turbocharger is influenced by the characteristics and adaptation of the interrelated compressor and turbine.
• Using high pressure ratios in the compressor i.e. using sub- stantially high charge pressure in the intake system of the engine is beneficial.
• the operation of the compressor part of the turbocharger is restricted on one hand by the limit that corresponds to maximum flow capacity of the compressor and on the other hand by the surge margin. Surging of the compressor is detrimental to the operation of the engine, since the pressure and flow of the combustion air supplied to the engine will decrease as soon as the compressor surges.
• valve timing An important issue relating to the operation of a turbocharged piston engine is valve timing.
• a device for accomplishing alterations in timing of the valve we refer to document WO 9830787 A1.
• a device for controlling the valves on an internal combustion engine which makes it possible to delay the opening of the engine's valve and closing the valve earlier making the open time of the valve shorter. According to the document this may be used for both intake and exhaust valves but the document fails to disclosed specific applications of such a device.
• WO 2008/000899A1 shows an arrangement for adjusting the closing moment of a gas exchange valve of a combustion engine making it possible e.g. make the closing of the valve later than normally e.g. in different load situations of the engine.
• US 6,105,555 disclose a turbocharged internal combustion engine having a system and method for preventing a rapid decrease of turbocharger power during rapid fuel reduction transients in engine operation.
• An exhaust valve control device capable of varying the timing of opening of the engine exhaust valves is provided. The exhaust valve control device advance the timing of opening of the exhaust valves to cause ad- ditional exhaust gas to be delivered to the turbine thereby preventing a rapid decrease of compressor speed and preventing compressor surge.
• An object of the invention is to provide a method of controlling turbocharger speed of a piston engine, the operation of which is more efficient than prior art engines. Disclosure of the invention
• percent-degrees means an integral of relative valve position over a range of crank angle, wherein the percentage means valve position in relation to cylinder diameter.
• Crank angle represent a position of the crank shaft of an engine, in which a full cycle of four stroke engine comprises 720° beginning at top dead center before the power stroke.
• Objects of the invention are met with a method of controlling turbocharger speed of a piston engine which comprises at least one intake valve and at least one exhaust valve, an intake valve operating system and an exhaust valve operating system arranged for operating the valves, and a turbocharger arrangement comprising a compressor part being in flow connection with the inlet side of the at least one intake valve and a turbine part being in flow connection with the exhaust side of the at least one exhaust valve, in which method engine is run in a first mode of operation in which the engine is operated below or at a predetermined load and combustion air is pressurised with the compressor part of the turbocharger arrangement, the intake valve is controlled by a first intake valve lift profile and the air is introduced to the cylinder, fuel is combusted in the engine by means of combustion air, the exhaust valve is controlled by a first exhaust valve lift profile and exhaust gases generated during the combustion are conveyed to the turbine part of the turbocharger arrangement.
• the engine is run in a second mode of operation above the predetermined load during which the closing of the inlet valve is advanced compared to that of the first mode of operation and that the air flow between an outlet of the compressor part and an inlet of the turbine part is increased allowing more combustion aire to flow through the compressor part.
• the engine is provided with a turbocharger equipped with a waste gate.
• the waste gate is controlled so that in the first mode of operation the waste gate is open and in the second mode of operation the waste gate is closed. This provides the higher charge air pressure during the second mode of operation. Increased charge air pressure compensates the effect of advanced closing of the inlet valve and simultaneously increases the gas flow through the engine during a scavenging phase of the engine.
• the waste gate may also be controlled so that in the first mode of operation the waste gate is closed and in the second mode of operation the waste gate is maintained closed.
• the engine is provided with a turbocharger without a waste gate.
• turbocharger is designed to provide adequately increased charge pressure in the second mode of operation as well as provide required performance in the first mode of operation.
• the closing of the inlet valve lift is controlled to be closed to 1% of cylinder bore at crank angle about 20° earlier than during the first mode of operation.
• the 1 % open-position is used in connection with this specification in the definition because in practise the 1% opening position is easily detectable and is less ambiguous than the initial beginning of opening from totally closed position.
• the closing of the inlet valve lift is controlled to be closed to 1% of cylinder bore at crank angle between 35-65° before bottom dead center.
• the air flow between an outlet of the compressor part and an inlet of the turbine part is increased by admitting more air through a bypass conduit provided in the engine extending between an outlet side of the compressor part and an inlet side of the turbine part.
• fuel is ignited by an external ignition and during the first mode of operation the closing of the exhaust valve lift and the opening of the intake valve lift are overlapped forming a scavenging area and during the second mode of operation the scavenging area is controlled to be 5 - 300% bigger than during the first mode of operation.
• compression ignition is prac- tised in the engine and during the first mode of operation the closing of the exhaust valve lift and the opening of the intake valve lift are overlapped forming a scavenging area and that during the second mode of operation the scavenging area is controlled to be 5 - 60% bigger than during the first mode of operation.
• the scavenging area is more than 150 %deg.
• the closing of the exhaust valve lift is preferably controlled to be closed to 1 % of cylinder bore at crank angle about 15° later than during the first mode of operation.
• the intake valves are operated so that during the opening movement the valve lift is at 1% position while the crank angle is between 15-50° before top dead center.
• fuel ignition timing during the second mode of operation is more than 0° and less than or equal to 5° (crank angle) advanced to that of the first mode of operation.
• fuel ignition timing is about 2-3° (crank angle) advanced.
• the predetermined load is 70-85% of the maximum load of the engine.
• the engine is operated during the second mode of operation above the predetermined engine load so that while combusting fuel by means of combustion air pressurized by a turbocharger assembly, intake valves of the engine are closed earlier than in the first mode of operation, and the boost pressure obtained by the turbocharger assembly is increased, and amount of bypass air flow between an outlet side of the compressor part and an inlet side of the turbine part is increased, increasing the air mass flow through the compressor part.
• the engine is provided with a waste gate and the boost pressure is increased by closing a waste gate of the turbocharger assembly during the second mode of operation.
• a control system for a turbocharged four stroke piston engine having a turbocharger with a waste gate intake and exhaust valves, in which at least intake or exhaust valves comprising adjustable valve operating system
• the control system comprising a processing unit, a control signal transmitting unit and a control signal receiving unit, the signal transmitting unit being in connection at least with one of the engine's valve operating system and the signal receiv- ing unit being in connection with engine sensors monitoring engine's load, speed and/or at least one combustion process variable.
• the processing unit is arranged to process the signals received by the signal receiving unit and provide the signal to be transmitted by the signal transmitting unit in such a manner that a change in the state of the valve operating system is initiated based on information from anyone of the en- gine sensors monitoring engine's load, speed and at least one combustion process variable.
• control system is arranged to operate so that, while 70-73% load is exceeded (the second mode of operation), the control system sets and/or maintains the waste gate in closed state, and advances intake valve closing time and delaying the exhaust valve closing.
• a four stroke piston engine in which the method is practised comprises at least one intake valve and at least one exhaust valve, an intake valve operating system and an exhaust valve operating system arranged for operating the valves, and a turbocharger arrangement comprising a compressor part being in flow connection with the inlet side of the at least one intake valve and a turbine part being in flow connection with the exhaust side of the at least one exhaust valve.
• the piston engine is provided with an adjustable flow connection between an outlet side of the compressor part and an inlet side of the turbine part, and that the intake valve operating system comprises means for adjusting timing of closing of the intake valve.
• the adjustable flow connection between the outlet of the compressor part and the inlet of the turbine part comprises the intake valve operating system and the exhaust valve operating system having adjustable valve overlapping during the closing of the exhaust valve lift and opening movement of the intake valve.
• the operation of the turbocharger may be controlled advantageously by controlling valve overlapping having positive effect on engine's thermal load.
• the adjustable flow connection between the outlet of the compressor part and the inlet of the turbine part comprises adjustable valve overlapping such that the intake valve operating system is provided with adjustable timing of valve opening.
• the adjustable flow connection be- tween the outlet of the compressor part and the inlet of the turbine part comprises adjustable valve overlap such that the exhaust valve operating system having adjustable closing of valve timing.
• the adjustable flow connection between an outlet side of the compressor part and an inlet side of the turbine part com- prises a bypass conduit and a control valve provided in the conduit.
• Invention has several benefits. Invention provides for example an efficient control for operation of compressor part of a turbocharger. Additionally thermal load of the engine is minimised. Specifically, the invention provides efficient way of controlling the firing pressure of the engine and turbocharger speed in the high load range of the engine. Additionally, NOx emissions are reduced due to the advanced inlet valve closing. Specific fuel consumption is also decreased at high load range of the engine.
• Figure 1 illustrates a piston engine according to the first embodiment of the invention
• Figure 2 illustrates valve lift profiles according to the first embodiment of the invention
• Figure 3 illustrates exemplary compressor map in connection with the invention
• FIG. 4 illustrates valve lift profiles according to the second embodiment of the invention
• Figure 5 illustrates valve lift profiles according to the third embodiment of the invention
• Figure 6 illustrates a piston engine according to the second embodiment of the inven- tion and
• Figure 7 illustrates a control system in a turbocharged four stroke piston engine according to an embodiment of the invention.
• Figure 1 schematically shows part of a piston engine 10.
• the engine comprises cylinders 15 arranged in the body 20 of the engine.
• the engine is a supercharged four stroke engine provided with a turbocharger arrangement 25.
• the turbocharger arrangement 25 is coupled to its gas exchange system 30.
• the turbocharger arrangement 25 comprises a compressor part 25.1 and a turbine part 25.2 the basic operation and construction is known as such.
• the compressor arrangement may comprise also a combination of more than one turbocharger.
• each cylinder 15 is provided with one intake valve 35 and one exhaust valve 40 and a valve operating system 45, 50, which is arranged to open and close the valves in respect to the crank angle of the engine.
• the valve operating system includes preferably a camshaft coupled to the crank shaft of the engine which is not shown here for clarity reasons.
• the compressor part 25.1 is arranged in flow connection with the intake valves 35 of the engine.
• the turbine part 25.2 is arranged in flow connection with the exhaust valves 40 of the engine.
• the compressor part may be coupled to an air receiver and the turbine part may be coupled to the ex- haust manifold of the engine.
• bypass conduit 55 provided in the engine extending between an outlet side of the compressor part and an inlet side of the turbine part as shown in figure 1. More specifically, in this embodiment the conduit is arranged to connect the air receiver of the engine to the exhaust manifold, but the conduit may also be integrated to the turbocharger arrangement 25.
• the bypass conduit 55 is provided with controllable flow adjusting means 60, such as a control valve.
• controllable flow adjusting means 60 such as a control valve.
• At least the valve operation system 45 of the intake valve 35 is provided with means for adjusting closing timing of the valve.
• the intake valve operation system 45 is arranged to operate so that the closing time of the intake valve may be adjusted during the operation of the engine. In this connection this means setting the operation between distinct states or continuous control. This makes it possible to practise a following method in connection with the engine according to the first embodiment of the invention, in which the mode of operation is changed based on the load of the engine.
• the exhaust valve operating system 50 and intake valve operating system 45 are operated according to an embodiment of the invention so that the valves are operated with lift profiles as is depicted with solid lines in the figure 2.
• the valve lift i.e. the position of the valve is expressed in relation to the cylinder bore diameter in question.
• the valve lift profile of the exhaust valve 210 according to which the exhaust valve operating system 45 is arranged to control the operation of the exhaust valve 40 is shown as solid line.
• the exhaust valve lift in the first embodiment of the invention is not substantially changed between the first and the second modes of operation.
• the lift profile of the intake valves 220 according to which the intake valve operat- ing system 45 is arranged to control the operation of the intake valve 35 in the first mode of operation is shown as solid line, as well.
• the exhaust valves are operated so that the lift profile during the closing movement is at 1% open-position while the crank angle is between 0-15°, preferably 3-6° after top dead center. Total opening movement of the exhaust valve is about 7,5 % and start of the closing movement takes place about at 290° crank angle.
• the so called scavenging area 230 has an area of about 95 %deg, shown in figure 2.
• the intake valves 35 in turn are operated so that during the opening the valve lift 220 is at 1% position preferably while the crank angle is between 15-50°, preferably 30-40° before top dead center.
• the valve lift 220 is at 1% position preferably while the crank angle is between 35-65°, preferably 40-50° before bottom dead center.
• the operation above the predetermined load comprises fol- lowing phases.
• the lift profile of the intake valve 220' according to which the intake valve operating system 45 is arranged to control the operation of the intake valve 35 in the second mode of operation is shown as dashed line.
• the intake valves 35 are operated so that during the closing movement the lift profile 220' is at 1 % position preferably while the crank angle is between 35-65 °, preferably 50° before bottom dead center, that is about 20° before than in the first mode of operation.
• the time during which the inlet valves are opened is decreased by closing the valves earlier compared to the first mode of operation.
• substantially the whole closing movement is advanced with about 20° compared to that of the first mode of operation.
• the boost pressure obtained from the turbocharger arrangement naturally is increased.
• the boost pressure is increased more than conventionally due to the fact that with waste-gate turbochargers the waste gate is typically opened at higher loads.
• the boost pressure obtained from the turbocharger arrangement in the second mode of operation is increased by closing the waste gate of the turbocharger.
• the boost pressure obtained from the turbocharger arrangement in the second mode of operation is increased by matching the operation of the turbocharger arrangement with the shortened inlet valve open time, for example, by proper overall dimensioning of the turbocharger.
• the obtained higher boost pressure substantially compensates the amount of air in the charge of the cylinder.
• the flow connection between an outlet side of the compressor part 25.1 and an inlet side of the turbine part, that is the bypass 55, is opened allowing more combustion air to flow through the compressor part 25.1 of the turbocharger arrangement 25. This way the working point of the compressor part 25.1 in the compressor map moves farther from the surge line.
• the predetermined load is preferably 70-85% of the maximum load of the engine.
• the engine in the first mode of operation the engine is operated below or at 70- 85% of the maximum load of the engine, and in the second mode of operation the en- gine is operated above 70-85% of the maximum load of the engine.
• FIG 3 is an exemplary compressor map of the compressor part 25.1.
• the operating line during the first mode of operation i.e. below or at the predetermined load is illustrated with the reference 310.
• the pressure obtained by the compressor part is steadily increased while the load of the engine is increased and the rotational speed of the compressor part is increased respectively.
• the second mode of operation is initiated.
• the operating line 330 is made to follow a modified operating line compared to conventional waste-gate controlled turbocharger arrangement, the operating line of which is shown as dotted lined with reference 340. In the conventional arrangement the waste-gate is opened while operating in the operating line 340.
• the position of the modified operating line 330 is controlled by the combination of controlling the intake valve closing timing as described above and the flow connection between an outlet side of the compressor part 25.1 and an inlet side of the turbine part so as to keep the operating line 330 on the right side (in the figure 3) of a certain surge margin, the hatched area 350 in the figure.
• the surge margin is about 10- 15% from the surge line 360 of the compressor part 25.1.
• FIG 3 there is also shown an imaginary operating line 330' which represents con- dition in which the second mode of operation would not include the step of, simultaneously with decreasing the open time of the inlet valves by closing the valves earlier, opening the flow connection between an outlet side of the compressor part 25.1 and an inlet side of the turbine part, thus allowing more combustion air to flow through the compressor part 25.1 of the turbocharger arrangement 25.
• This way the working point of the compressor part 25.1 in the compressor map moves farther from the surge line, 330' -> 330.
• the surge margin provides a measure of how close an operating point is to surge.
• the engine is operated during the second mode of operation above the predetermined engine load so that while combusting fuel by means of combustion air pressurized by a turbocharger assembly, intake valves of the engine are closed earlier than in the first mode of operation, and the boost pressure obtained by the turbocharger assembly is increased, and amount of bypass air flow between an outlet side of the compressor part 25.1 and an inlet side of the turbine part is increased, increasing the air mass flow through the compressor part.
• the engine 10 differs from that shown in figure 1 on one hand that the bypass conduit 55 is not needed.
• the exhaust valve operation system 50 is provided with adjustable valve operation function.
• the valve operation system 45 of the intake valve 35 is provided with means for adjusting closing timing of the valve.
• the intake valve operation system 45 is arranged to operate so that the closing time of the intake valve may be adjusted during the operation of the engine. In this connection this means setting the operation between distinct states or continuous control. This makes it possible to practise a following method in connection with the engine according to the second embodiment of the invention.
• the valve operation system 50 of the exhaust valve 40 is provided with means for adjusting closing timing of the valve.
• the exhaust valve operation system 50 is arranged to operate so that the closing time of the intake valve may be adjusted during the operation of the engine. In this connection this means setting the operation between distinct states or continuous control. This makes it possible to practise a following method in connection with the engine according to the second embodiment of the invention, in which the mode of operation is changed based on the load of the engine.
• the exhaust valve operating system 50 and intake valve operating system 45 is operated according to the second embodiment of the invention as is depicted in the figure 4.
• the valve lift profile of the exhaust valve 210 according to which the exhaust valve operating system 45 is arranged to control the operation of the exhaust valve 40 in the first mode of operation is shown as solid line.
• the lift profile of the intake valve 220 accord- ing to which the intake valve operating system 45 is arranged to control the operation of the intake valve 35 in the first mode of operation is shown as solid line, as well.
• the exhaust valves are operated in the first mode of operation so that the lift profile during the closing movement is at 1% open-position while the crank angle is between 0-15°, preferably 3-6° after top dead center.
• Total opening movement of the exhaust valve is about 7,5 % and the start of the closing movement takes place about at 290° crank angle.
• the so called scavenging area 230 has an area of about 95 %deg.
• the intake valves 35 in turn are operated so that during the opening movement of the valve the lift profile 220 is at 1% position preferably while the crank angle is between 15-50°, preferably 30-40° before top dead center. During the closing movement of the valve the valve lift profile 220 is at 1 % position preferably while the crank angle is between 35-65°, preferably 40-50° before bottom dead center.
• the exhaust valve operating system 50 and intake valve operating system 45 is operated as is depicted with dashed line in the figure 4.
• dashed line the valve lift profile of the exhaust valve 210' according to which the exhaust valve operating system 45 is arranged to control the operation of the exhaust valve 40 in the second mode of operation is shown as dashed line.
• the lift profile of the intake valves 220' according to which the intake valve operating system 45 is arranged to control the operation of the intake valve 35 in the second mode of operation is shown as dashed line, as well.
• the exhaust valves are operated so that the lift profile during the closing movement is at 1% open-position while the crank angle is between 15-25°after top dead center.
• Start of the closing movement of the exhaust valves takes place about at 310° crank angle.
• the intake valves 35 in turn are operated in the second mode of operation so that during the closing movement the lift profile 220' is at 1 % position preferably while the crank angle is between 35-65°before bottom dead center.
• the scavenging area 230 is the scavenging area 230.
• the called scavenging area 230 has an area of about 160 %deg.
• the scaveng- ing area 230 is increased about 70% while the shifting from the fist mode of operation to the second mode of operation.
• the shifting from the first mode of the operation to the second mode of operation may involve quite different changes in different kind of en- gines, also depending on the actual application of the engine.
• the common features are always advancing the closing of the inlet valve lift and arranging increased air passage between the outlet of the compressor part and the inlet of the turbine part of the turbocharger.
• the increased air passage is preferably accomplished by increasing the scavenging area as disclosed above.
• the scavenging area during the first mode of operation may be very small, sometimes even zero.
• the valve overlapping i.e. the scavenging area, during the second mode of operation may be increased several hundreds of percents.
• the scavenging area during the second mode of operation is increased typically 5 - 60 percents.
• the engine is operated during the second mode of operation so that while combusting fuel by means of combustion air pressurized by a turbocharger assembly, intake valves of the engine are closed earlier than in the first mode of operation, and that the boost pressure obtained by the turbocharger assembly is increased, and exhaust valves of the engine are closed later than in the first mode of operation increasing the airflow through the engine.
• the boost pressure obtained by the turbocharger assembly is increased preferably by maintaining the turbine by-pass closed or closing it.
• the obtained higher boost pressure substantially compensates the amount of air in the charge of the cylinder.
• the open time of the exhaust valves is increased by closing the exhaust valves later. This increases the overlap of the valve open-period during the second mode of operation allowing more air to flow through the engine 10, and thus also through the compressor part 25.1 of the turbocharger arrangement 25. This way the working point of the compressor part 25.1 in the compressor map moves farther from the surge line.
• the operation during the second mode of operation comprises increasing the valve overlapping i.e. so called scavenging area 230 while the closing of the inlet valves is advanced, more air is flown through the engine during the scavenging phase.
• the valve overlapping range during the scavenging phase in this example takes place substantially between crank angle 310 - 380°.
• the intake and exhaust valves are controlled to operate so that the scavenging area is asymmetric on the exhaust valve's side.
• Admitting the air flow through the engine 10 instead of (or in addition to) using the bypass conduit 55 has the beneficial effect of decreasing thermal load of the engine component in the cylinder and cylinder head, that is mainly the valves and the top of the piston.
• valves according to a third embodiment of the invention corresponds to that of the second embodiment i.e. the bypass conduit may be omitted.
• the operation of the third embodiment during the first mode of operation corresponds to that of the second embodiment and the operation of the third embodiment during the second mode of operation corresponds to that of the second embodiment except that the intake valve operating system 45 is arranged to operate so that both the opening timing and closing timing is advanced compared to the operation during the first mode of operation.
• the ef- feet of advancing the closing timing corresponds to that of the first and the second embodiment.
• the scavenging area 230 is increased about 50% while the shifting from the fist mode of operation to the second mode of operation.
• Increasing the air flow during the second mode of operation in the third embodiment of the invention is accomplished by combination of controlling the closing timing of the exhaust valves and the opening timing of the inlet valves, thus increasing the valve overlapping range and the scavenging area 230 during the scavenging phase.
• valve operating system 45, 50 may be realized in various manners. Changing or adjusting closing timing may be realized for example as is disclosed in WO 2008/000899.
• control system 200 which among other operations of the engine 10 is arranged control e.g. the operation of the valves 35, 40 by means of the valve operating system 45, 50 and the fuel injection and/or ignition system 61.
• the control system comprises a memory unit 207, into which the operational parameters of the engine are stored.
• the control system 200 comprises a processing unit 202, which is arranged to define the working conditions of the engine. In case the control system 200 gets the information that the load of the engine is changed so that the load is increased above the predetermined load it controls the intake valves to close earlier. In addition this, it also controls the exhaust valves to close later as describe above in connection with the second embodiment.
• the control system controls the fuel injection system 61 to advance the timing of the injection and/or ignition.
• this comprises controlling of injection of pilot fuel and/or spark or other ignition system.
• the processing unit 202 Based on the measurement of engine load and/or speed the control system controls the valve operation systems 45, 50 so that the actual surge margin is maintained between a lower and upper set value.
• the lower set value is about 10% and the upper set value is about 15%.
• Maintaining the surge margin between the lower and the upper set value comprises the following steps:
• valve operation system 45,50 is controlled to run the valves so that the size of the scavenging area 230 is increased i.e. the overlap of the valve is increased around the 360° crank angle and/or
• the inlet valve operation system 45 is controlled to run the inlet valve so that the clos- ing timing is delayed
• valve operation system 45,50 is controlled to run the valves so that the size of the scavenging area 230 is decreased i.e. the overlap of the valve is decreased around the 360° crank angle and/or - the inlet valve operation system 45 is controlled to run the inlet valve so that the closing timing is advanced.
• the inlet valve closing is advance during the second mode of operation result in sharply decreasing NOx emissions,.
• the fuel injection timing during the second mode of operation is at least 0-5° (crank angle) advanced to that of the first mode of operation.
• the fuel injection takes place at about 13-15° before top dead center, while during the second mode of operation fuel injection may take place at about 17° before top dead center. This way the specific fuel consumption during the second mode of operation may be considerably lower than in the conventional waste- gate controlled turbocharger engine.
• Figure 7 schematically shows a control arrangement for piston engine 10 according to a still another embodiment of the invention.
• the engine comprises cylinders 15 arranged in the body 20 of the engine.
• the engine is a supercharged four stroke engine provided with a turbocharger arrangement 25. More specifically the engine is a large piston engine having cylinder diameter greater or equal to 200 mm and/or arranged to produce power substantially more than 150 kW / cylinder.
• the turbocharger arrangement 25 is coupled to the gas exchange system 30 of the engine.
• the turbocharger arrangement 25 comprises a compressor part 25.1 and a turbine part 25.2 the basic operation and construction is known as such. Further, the turbocharger is provided with a waste gate system 25.3, allowing or preventing a part of the exhaust gas by-passing the turbine part.
• the compressor arrangement may comprise also a combination of more than one turbochargers.
• each cylinder 15 is provided with one intake valve 35 and one exhaust valve 40 only and a valve operating system 45, 50, which is arranged to open and close the valves in respect to the crank angle of the engine.
• the compressor part 25.1 is arranged in flow connection with the intake valves 35 of the engine.
• the turbine part 25.2 is arranged in flow connection with the exhaust valves 40 of the engine.
• the compressor part may be coupled to an air receiver and the turbine part may be coupled to the exhaust manifold of the engine.
• the engine is also provided with a fuel injection and/or ignition system 61.
• sensors arranged in connection with the engine 10 and its control system 200 in order to monitor certain variables relating to the combustion process taken place in the engine and/or relating to certain process apparatuses of the engine.
• the engine is provided with a charge air temperature sensor 151 and a charge air pressure sensor 152. These sensors provide information representing the operation of e.g. the compressor part 25.1 of the turbocharger.
• the engine is also provided with a speed sensor 154 and engine load sensor 155.
• the engine is also provided with en exhaust gas temperature sensor 153, cylinder knock / ignition timing / cylinder pressure sensor 156. These all are sensors for monitoring combustion process variables.
• combustion process variables which may be determined making use on available information such as fuel injection timing and duration.
• valve operation system 45 of the intake valve 35 is provided with means for adjusting closing timing of the valves.
• the intake valve operation system 45 is arranged to operate so that the closing time of the intake valve may be adjusted during the operation of the engine by the control system 200.
• the control system 200 is arranged to control the operation of the inlet valve operating system according to a preferred embodiment by setting the intake valve closing be- tween at least two distinct states. This makes it possible to practise a following method in connection with the engine according to the first embodiment of the invention, in which the mode of operation is changed based on the load of the engine.
• the control system 200 comprises a processing unit 202, control signal transmitting unit 204 and a control signal receiving unit 206.
• the control signal transmitting unit 204 is arranged to transmit signal from the control system to selected devices. It is arranged in connection with actuators 25.3, 45 arranged in the engine in order to change the state of engine's control apparatuses.
• the signal transmitting unit 204 is also in connection with at least with engine's intake valve operating system 45.
• the signal transmitting unit 204 is also in connection with the waste gate 25.3 of the turbocharger depending on the application.
• the signal receiving unit is arranged to receive a signal to the control system. It is arranged in connection with engine sensors monitoring en- gine's variables, particularly engine's load 154, speed 155 and/or at least one combustion process variable 151 , 152, 153, 156.
• the processing unit 202 is arranged to process the signals received by the signal receiving unit 206 and provide the signal to be transmitted by the signal transmitting unit 204.
• the control system is arranged to operate in such a manner that a change in the state of the valve operating system 45, 50 is initiated based on information from anyone of the engine sensors monitoring engine's load 155, speed 154, at least one combustion process variable and/or external activation 160. This makes it possible to control the operation of the inlet valves of the turbocharged four stroke engine with comprehensive approach.
• control system 200 operates the valves in a first mode of operation below or at a predetermined load
• the exhaust valve operating system 50 and intake valve operating system 45 are operated according to an embodiment of the invention so that the valves are operated with lift profiles as is depicted with solid lines in the figure 2.
• control system 200 initiates the change of the state of the operation from the first mode of operation to the second mode of operation, so that the valves are operated with lift profiles as is depicted with dashed lines in the figure 2.
• control system 200 is arranged to operate in such a manner that a change in the state of the intake valve operating system 45 is initiated based on information from anyone of the engine sensors monitoring engine's load, speed and at least one combustion process variable. This way the combustion of the engine is under strict control during various operating circumstances of the engine.
• the control system is provided with an individual limit value for each of the sensors monitoring engine's operation and/or other engine's operational variable.
• the variables may be divided into three base event groups: 1 ) Speed/load Activation, 2) Load transient Activation 3) External Activation.
• Speed/load Activation i.e. in the state of the inlet valve closing timing is initiated by a predetermined change in a variable belonging to anyone of the event groups.
• the speed/load activation is based on predetermined operating ranges of the engine where each defined operating range is associated with a specific state of the valve stored in or made available to the control system.
• the valve state transition due to the current speed/load is initiated when the actual value of the speed/load passes the limit value between the set of neighbouring operating ranges.
• the load transient activation is based on limit values stored in or made available to the control system relating to the engine's operational variables. There is a limit value for each monitored variable and the processing unit is arranged to initiate the change in the state of the intake valve operating system in case the actual value of the signal of anyone of variables passes the limit value of the load.
• the external activation is based on any desired external event which initiates the change in the state of the intake valve operating system.
• the speed/load activation in practise means that the load of the engine is increased or decreased so that the actual value of the speed/load passes the limit value.
• the boost pressure obtained from the turbocharger arrangement is naturally also increased.
• the control system is arranged to increase the boost pressure obtained from the turbocharger arrangement by initiating the closing of the waste gate of the turbocharger, or maintaining it closed, substantially simultaneously with advancing the closing of the inlet valve. This is done preferably when the load of the engine exceeds 70-80% of the maximum load of the engine.

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• Engineering & Computer Science (AREA)
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• Combustion & Propulsion (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Chemical Kinetics & Catalysis (AREA)
• Health & Medical Sciences (AREA)
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• Output Control And Ontrol Of Special Type Engine (AREA)
• Supercharger (AREA)
• Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
• Combined Controls Of Internal Combustion Engines (AREA)

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• 2009
  • 2009-11-19 EP EP09799657.3A patent/EP2347110B1/en active Active
  • 2009-11-19 CN CN200980146175.0A patent/CN102216592B/zh active Active
  • 2009-11-19 KR KR1020117011389A patent/KR101657322B1/ko active IP Right Grant
  • 2009-11-19 RU RU2011124881/06A patent/RU2511878C2/ru active
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