EP2867514A1 - Groupe moteur avec ligne de recirculation - Google Patents
Groupe moteur avec ligne de recirculationInfo
- Publication number
- EP2867514A1 EP2867514A1 EP13728491.5A EP13728491A EP2867514A1 EP 2867514 A1 EP2867514 A1 EP 2867514A1 EP 13728491 A EP13728491 A EP 13728491A EP 2867514 A1 EP2867514 A1 EP 2867514A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- exhaust
- pressure exhaust
- line
- high pressure
- phase
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
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- 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
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/08—Other arrangements or adaptations of exhaust conduits
- F01N13/10—Other arrangements or adaptations of exhaust conduits of exhaust manifolds
- F01N13/107—More than one exhaust manifold or exhaust collector
-
- 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
- F02D13/0257—Independent control of two or more intake or exhaust valves respectively, i.e. one of two intake valves remains closed or is opened partially while the other is fully opened
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D21/00—Controlling engines characterised by their being supplied with non-airborne oxygen or other non-fuel gas
- F02D21/06—Controlling engines characterised by their being supplied with non-airborne oxygen or other non-fuel gas peculiar to engines having other non-fuel gas added to combustion air
- F02D21/08—Controlling engines characterised by their being supplied with non-airborne oxygen or other non-fuel gas peculiar to engines having other non-fuel gas added to combustion air the other gas being the exhaust gas of 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
- F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D41/0047—Controlling exhaust gas recirculation [EGR]
- F02D41/005—Controlling exhaust gas recirculation [EGR] according to engine operating conditions
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
- F02M25/10—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding acetylene, non-waterborne hydrogen, non-airborne oxygen, or ozone
- F02M25/12—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding acetylene, non-waterborne hydrogen, non-airborne oxygen, or ozone the apparatus having means for generating such gases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/13—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
- F02M26/41—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories characterised by the arrangement of the recirculation passage in relation to the engine, e.g. to cylinder heads, liners, spark plugs or manifolds; characterised by the arrangement of the recirculation passage in relation to specially adapted combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/13—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
- F02M26/42—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories having two or more EGR passages; EGR systems specially adapted for engines having two or more cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/13—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
- F02M26/42—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories having two or more EGR passages; EGR systems specially adapted for engines having two or more cylinders
- F02M26/43—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories having two or more EGR passages; EGR systems specially adapted for engines having two or more cylinders in which exhaust from only one cylinder or only a group of cylinders is directed to the intake of the engine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/65—Constructional details of EGR valves
- F02M26/71—Multi-way valves
-
- 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
-
- 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
- F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D41/0047—Controlling exhaust gas recirculation [EGR]
- F02D41/0065—Specific aspects of external EGR control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/02—EGR systems specially adapted for supercharged engines
- F02M26/04—EGR systems specially adapted for supercharged engines with a single turbocharger
- F02M26/07—Mixed pressure loops, i.e. wherein recirculated exhaust gas is either taken out upstream of the turbine and reintroduced upstream of the compressor, or is taken out downstream of the turbine and reintroduced downstream of the compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/13—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
- F02M26/36—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories with means for adding fluids other than exhaust gas to the recirculation passage; with reformers
-
- 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
-
- 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
- Y02T10/40—Engine management systems
Definitions
- the invention relates to a motor unit of a motor vehicle, and in particular the recirculation line of the combustion gases.
- a motor unit comprising a combustion engine which opens, on the one hand, an exhaust line which is fed by a set of high pressure exhaust valves during a high pressure exhaust phase, and on the other hand, a recirculation line which is fed by a set of low pressure exhaust valves during a low pressure exhaust phase and which is configured to be isolated from the exhaust line.
- the invention aims to achieve a motor group configured to allow an improvement in the physics of combustion of the engine, and thus an increase in engine power consumption.
- the invention relates to a motor unit comprising a combustion engine which opens, on the one hand, an exhaust line which is fed by a set of high pressure exhaust valves during a phase high-pressure exhaust system, and on the other hand, a recirculation line which is fed by a set of low-pressure exhaust valves during a low-pressure exhaust phase and which is configured so that it can be isolated from the exhaust line, as it comprises a deactivation system which, when it is activated, is adapted to keep at least one high-pressure exhaust valve closed during the high-pressure exhaust phase, and in particular several valves, simultaneously and / or alternatively.
- the presence of the deactivation system makes it possible to send, if necessary, in the recirculation line, high pressure combustion gases that usually are sent into the exhaust line. It is thus possible to send in the recirculation line a gas richer in fuel than when the deactivation system is activated. As a result, the gases in recirculation are richer and may have a higher dihydrogen concentration than usual. As a result, the physics of combustion of the engine is improved (particularly with regard to knocking) due to the composition of the gases introduced into the engine.
- the recirculation line comprises a catalytic device for producing dihydrogen.
- the power unit comprises a bypass line which is fed by a low pressure exhaust manifold disposed between the low pressure exhaust valve assembly and the recirculation line. , which opens into the exhaust line, and which comprises an insulation system for isolating the exhaust line of the low pressure exhaust manifold.
- the isolation system is a three-way valve disposed at the junction of the low pressure exhaust manifold, the recirculation line and the bypass line.
- the invention also relates to a control method of a motor unit comprising a combustion engine which opens, on the one hand, an exhaust line which is fed by a set of high pressure exhaust valves during a high pressure exhaust phase, and, secondly, a recirculation line which is fed by a set of low pressure exhaust valves during a low pressure exhaust phase and which is configured so as to be isolated of the exhaust line, the engine comprising a system of deactivation adapted to keep closed, when it is activated, at least one high pressure exhaust valve, and in particular several simultaneously and / or alternatively, such that, when a high pressure exhaust valve is kept closed during a phase of high pressure exhaust, the recirculation line is isolated from the exhaust line during the low pressure exhaust phase that succeeds this phase of high pressure exhaust.
- the insulation of the exhaust line of the recirculation line is achieved by closing an insulation system disposed in a bypass line opening on the one hand, in the exhaust line, and, secondly, between the set of low pressure exhaust valves and the recirculation line.
- the deactivation system when activated, it keeps closed every same high pressure exhaust valve which can be deactivated. It is thus always the same high pressure exhaust valve that can be deactivated.
- the deactivation system when activated, it keeps closed in turn, during a deactivation period, each high-pressure exhaust valve which can be deactivated.
- the amount of fuel injected into a combustion chamber of the engine, the high pressure exhaust valve is intended to be kept closed during the next high pressure exhaust phase, is determined by so that the flue gas produced in this chamber has a richness of at least 1.
- Figure 1 illustrates a motor unit according to a first configuration according to the present invention
- FIG. 2 illustrates a motor unit according to a second configuration according to the present invention, the combustion gases produced in one of the combustion chambers being unable to access the high-pressure exhaust manifold, and the low-pressure exhaust manifold being isolated from the exhaust line;
- Figure 3 illustrates the displacement of the valves and the use of the combustion gases in the case where the deactivation system is not activated.
- Figure 4 illustrates the displacement of the valves and the use of combustion gases in the case where the deactivation system is activated.
- the invention relates to a motor vehicle, and more particularly to a motor unit 1 of a motor vehicle.
- the engine group 1 comprises an internal combustion engine 2, in this case, a gasoline engine.
- This engine comprises combustion chambers 3 (here, four in number) which are fueled.
- Each combustion chamber 3 is supplied with air by an air collector 4 common to all rooms 3, the air collector 4 forming the downstream end of an intake pipe 5.
- the driving of intake 5 comprises an air valve 6 which controls the air flow admitted into the engine 2.
- each combustion chamber 3 From each combustion chamber 3 opens two exhaust pipes 7, 8, one 7, high pressure, connecting the combustion chamber 3 to a high pressure exhaust manifold 9, the other 8, low pressure connecting the combustion chamber 3 to a low-pressure exhaust manifold 10.
- the engine 2 At the engine 2 are associated two exhaust manifolds 9, 10, each of these two exhaust manifolds 9, 10 being fed by all the chambers engine combustion 2.
- a camshaft of admission carries only the first set of cams. It is known today of the technologies of the camshafts with two distinct laws and interdisputedphasables. The invention applies equally to all types of engines, associated with one or more camshafts. It also applies to motors without camshaft ("camless" in English), where the valves are actuated by electromagnetic actuators.
- Both sets of exhaust cams include a series of high pressure exhaust cam for controlling the supply of the high pressure exhaust manifold 9, and a series of low pressure exhaust cams for control.
- the two sets of exhaust cams may either be carried by a single exhaust camshaft or carried by two exhaust camshafts, one bearing all the high pressure exhaust cams, the other all the low pressure exhaust cams.
- the two series of exhaust cams are angularly offset relative to one another so as to have a decoupling of the supply of the two exhaust manifolds 9, 10.
- the high pressure exhaust manifold 9 feeds an exhaust line January 1 which comprises a turbine 12 and, downstream of the latter, a pollution control system 13 for treating the gases before their exit into the atmosphere.
- the exhaust line January 1 is the only line fed by the high pressure exhaust manifold 9 so that the exhaust gas contained in the latter can only drive the turbine 12 and then be sent to the pollution control system 13.
- the pollution control system may comprise a catalytic oxidation device for oxidizing in particular the unburnt, carbon monoxide and nitrogen oxides, a catalytic reduction device to reduce in particular the oxides nitrogen.
- the low-pressure exhaust manifold 10 feeds a recirculation line 14 for the reintroduction of the exhaust gas into the engine 2.
- the recirculation line 14 opens into the intake pipe 5, upstream of the valve.
- the recirculation line 14 opens into the inlet pipe 5 upstream of a compressor 15 which is driven by the turbine 12 and which forms, with the latter, a turbocharger.
- a heat exchanger 16 is disposed in the intake duct 5 between the compressor 15 and the air valve 6 in order to allow the regulation of the temperature of the gases admitted into the engine 2 (essentially, to allow their cooling) .
- a recirculation valve 17 is disposed in the recirculation line 14 and controls the flow of gas flowing in the latter.
- the recirculation line 14 comprises a catalytic device for producing dihydrogen 18 which makes it possible to produce dihydrogen from fuel.
- the recirculation line 14 comprises, upstream of the catalytic device for producing hydrogen 18, a fuel injector 19 in order to have a sufficient quantity of fuel at the inlet of the catalytic device for producing the fuel. dihydrogen 18 to allow the production of dihydrogen.
- Other solutions are possible to allow fuel to be present in the recirculation line 14: for example, a late injection of fuel into at least one combustion chamber 3 when the low pressure exhaust valve associated with this the chamber is in an open position (and preferably when the high pressure exhaust valve associated with this chamber is in a closed position), ie a fuel injection in the intake pipe 5 when the intake valve and the valve low pressure exhaust are both in an open position (and preferably when the high pressure exhaust valve is in a closed position).
- the recirculation line 14 comprises, upstream of the catalytic device for producing hydrogen 18 and downstream of the fuel injector 19, a heater 20 allowing to increase the temperature of the gases so as to facilitate the production of dihydrogen is carried out in the catalytic device 18.
- a cooler 21 for cooling the recirculating gas is disposed in the recirculation line 14, downstream of the catalytic device for producing dihydrogen 18. This cooler 21 allows to cool the recirculation gas once the dihydrogen produced so as to reduce the bulk of the recirculation line 14.
- the recirculation line 14 comprises, in the first embodiment, upstream to downstream, from the low pressure exhaust manifold 10: the fuel injector 19, the heater 20, the device catalytic production of dihydrogen 18, the cooler 21 and the recirculation valve 17, before opening into the intake pipe 5.
- the recirculation line 14 is similar to that shown in Figure 1 with the difference that it does not include a catalytic device for producing dihydrogen or injector fuel, nor heater.
- a bypass line 22 connects the low pressure exhaust manifold 10 to the exhaust line 1 1 bypassing the turbine 12.
- the bypass line 22 opens in the exhaust line January 1 upstream of the treatment system 13.
- the bypass line 22 and the recirculation line 14 have a common origin low-pressure exhaust manifold 10.
- the bypass line 22 comprises an isolation system 23 allowing. This isolation system 23 also makes it possible to control the gas flow bypassing the turbine 12.
- the insulation system 23 is a three-way valve 23 which is arranged at the junction of the low exhaust manifold. pressure 10, the recirculation line 14 and the bypass line 22.
- the motor unit also comprises a deactivation system that, when it is activated, to keep closed at least one high pressure exhaust valve.
- the three curves 24, 25, 26 of FIG. 3 represent, respectively, the movement of the non-deactivated high pressure exhaust valves, the low pressure exhaust valves and the intake valves as a function of the angular position. crankshaft relative to the position of combustion top dead point (corresponding to 0 °).
- FIG. 3 also shows two phases 27, 28 which overlap very slightly, and which represent the use of the exhaust gases produced either by all the combustion chambers 3 when the deactivation system is not activated, or only all Combustion chambers whose high-pressure exhaust valves are not deactivated when the deactivation system is activated.
- the high and low pressure exhaust cams are angularly offset so that the opening of the non-deactivated high pressure exhaust valves is controlled in advance by an angle of about 100 °. before controlling the opening of the low pressure exhaust valves (in this case, about 90 ° for high p r ession exhaust valves, and about 190 ° for low pressure exhaust valves), and that the closure of the non-deactivated high pressure exhaust valves is controlled in advance by an angle of approximately 65 ° before the control of the closure of the low pressure exhaust valves (in this case, at approximately 340 ° for high pressure exhaust valves, and approximately 405 ° for low pressure exhaust valves).
- the non-deactivated high pressure exhaust valves are the only open valves (90 ° angle to the 190 ° angle), which corresponds to a phase 27 where the turbine 12 is activated by the high pressure exhaust gas.
- the exhaust products in the combustion chambers 3 whose high pressure exhaust valves are not deactivated are used to drive the turbine 12.
- the non-deactivated high pressure exhaust valves and the low pressure exhaust valves are the only open valves (from the angle 190 ° to the angle 340 °), which corresponds to a phase wherein the two exhaust manifolds 9, 10 are energized, the low pressure manifold 10, even when no high pressure exhaust valve is turned off, being the most fed manifold. It is thus possible, according to the opening and closing angles of the high and low pressure exhaust valves, to send to the turbine 12 the quantity of high pressure exhaust gas necessary to obtain the requested power, then to decrease the flow of the high pressure exhaust gas due to the opening of the low pressure exhaust valves.
- the low pressure exhaust valves and the intake valves are the only open valves (from the angle 340 ° to the angle 405 °), which corresponds to a time when, from With these positions, it is possible to send fuel into the low-pressure exhaust manifold 10 by injecting the fuel into the intake pipe 5.
- the second and third times form a phase 28 where the recirculation line 14 and the bypass line 22 may be fed alternately or cumulatively exhaust gas, depending on the position of the three-way valve 23.
- the high pressure exhaust phase corresponds to the moment when the non-deactivated high pressure exhaust valves are open, that is to say at the first and second time.
- the low pressure exhaust phase corresponds to the moment when the low pressure exhaust valves are open, that is to say at the second and third times.
- the intake phase corresponds to the moment when the intake valves are open, that is to say at the third and fourth time. It is thus possible, depending on the choice of sending the low pressure exhaust gas, either to use only the recirculation line 14 (with also a possibility of enriching the hydrogen gas in case of presence of a catalytic device for producing dihydrogen 18), or to use only the exhaust line January 1 by taking the bypass line 22 (used as a discharge valve of the turbine 12).
- the recirculation line 14 comprises a catalytic device for producing hydrogen 18
- the simultaneous opening of the intake valves and the low pressure exhaust valves during the third stage makes it possible to send fresh air directly upstream of the catalytic device for producing dihydrogen 18 and have a favorable richness at the inlet of this catalytic device 18.
- FIG. 4 shows the same three curves 24, 25, 26 of FIG. 3. It also represents three phases 29, 30, 31 which represent the use of the exhaust gases produced by all the combustion chambers 3 when the deactivation system is activated.
- the exhaust gases are discharged in the same way as when the deactivation system is not activated (as shown in FIG. 3).
- the exhaust gases remain confined in the chamber as long as the low pressure exhaust valves are closed.
- phase 29 represents, on the one hand, the exhaust, towards the high pressure exhaust manifold 9, of the exhaust gases produced in the combustion chambers 3, the valves of which high pressure exhaust are not deactivated, and, secondly, the confinement of the exhaust gases in the combustion chambers 3 whose high pressure exhaust valves are deactivated.
- Phase 30 represents, on the one hand, the exhaust towards the high and low pressure exhaust manifolds 9, 10 of the exhaust gases produced in the combustion chambers 3 whose high pressure exhaust valves are not deactivated, and on the other hand, the exhaust, to the low-pressure exhaust manifold 10, the exhaust gas produced in the combustion chambers 3 whose high pressure exhaust valves are deactivated.
- the phase 31 represents the exhaust, towards the low-pressure exhaust manifold 10, of the exhaust gases produced in all the combustion chambers 3.
- the deactivation system can disable the high pressure exhaust valves, one of several or all the combustion chambers 3 of the engine. Preferably, the deactivation system makes it possible to deactivate the high pressure valves of several of the combustion chambers. When several high pressure exhaust valves are thus deactivated, they can be simultaneously or alternatively.
- the deactivation system can be configured to always disable the (the) same (s) valve (s) high pressure exhaust. Instead, it can be controlled so as to alternately deactivate each of the high-pressure exhaust valves that can be deactivated, the time during which a high-pressure exhaust valve can be deactivated is the deactivated valve that can depend on a duration engine operation or a number of combustion cycles.
- the insulation system 23 is in an insulating position the exhaust line January 1 of the recirculation line during the low pressure exhaust phase that succeeds this phase of high pressure exhaust.
- the amount of fuel introduced into each combustion chamber 3 of the engine 2 can be determined so that the fuel richness of the exhaust gas produced in this chamber 3 reaches a certain value.
- the amount of fuel introduced into each combustion chamber 3 whose high pressure exhaust valve is intended to be kept closed during the next high pressure exhaust phase is determined so that the exhaust gas produced by this room 3 has a richness of at least 1.
- a control system makes it possible to control the various members of the engine group 1, in particular the deactivation system, the three-way valve 23 and the supply of the different fuel combustion chambers.
- the control system activates the deactivation system and controls the three-way valve in its position isolating the low-pressure exhaust manifold 10 of the exhaust line January 1.
- the invention thus makes it possible to optimize the recirculation loop of the engine 2 supercharged by the turbocharger in order to produce recirculating gases having a rich composition and then, for example using a catalytic device for the production of dihydrogen, which will be reinjected into the engine 2. And this without creating a penalty on the performance of the engine group 1.
- the recirculation line 14 is completely decoupled from the pollution control system 13. Therefore, when the deactivation system is activated, the gas intended for the line of recirculation 14 have a richness greater than 1 in order to increase the production of dihydrogen.
- the deactivation of the high-pressure exhaust valves makes it possible to vary the flow of exhaust gas sent to the turbine 12 with respect to the exhaust gas sent to the recirculation line 14, makes it possible to choose the number of valves.
- high-pressure exhaust system kept closed, and allows independent control of the high and low pressure exhaust valves.
- the insulation of the exhaust line 1 1 of the low pressure exhaust manifold prevents the combustion gases from the combustion chamber whose high pressure exhaust valve is deactivated. go to the turbine 12 and the pollution control system 13. There is therefore no loss of fuel and dihydrogen.
- the recirculation line 14 may not include a catalytic device for producing dihydrogen, the dihydrogen circulating in the recirculation line 14 is then produced by the fuel enrichment in the combustion chamber 3 whose exhaust valve high pressure is off.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Exhaust Gas After Treatment (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1255810A FR2992356B1 (fr) | 2012-06-21 | 2012-06-21 | Groupe moteur avec ligne de recirculation |
PCT/FR2013/051157 WO2013190198A1 (fr) | 2012-06-21 | 2013-05-24 | Groupe moteur avec ligne de recirculation |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2867514A1 true EP2867514A1 (fr) | 2015-05-06 |
Family
ID=48614058
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13728491.5A Withdrawn EP2867514A1 (fr) | 2012-06-21 | 2013-05-24 | Groupe moteur avec ligne de recirculation |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP2867514A1 (fr) |
CN (1) | CN104471229B (fr) |
FR (1) | FR2992356B1 (fr) |
WO (1) | WO2013190198A1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
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KR20180005781A (ko) | 2016-07-06 | 2018-01-17 | 현대자동차주식회사 | 차량용 연료 개질 시스템 |
US10145315B2 (en) * | 2016-12-16 | 2018-12-04 | Ford Global Technologies, Llc | Systems and methods for a split exhaust engine system |
US10683817B2 (en) * | 2016-12-16 | 2020-06-16 | Ford Global Technologies, Llc | Systems and methods for a split exhaust engine system |
US10328924B2 (en) * | 2016-12-16 | 2019-06-25 | Ford Global Technologies, Llc | Systems and methods for a split exhaust engine system |
DE102017209741B3 (de) | 2017-06-09 | 2018-12-13 | Ford Global Technologies, Llc | Aufgeladene fremdgezündete Brennkraftmaschine mit Abgasnachbehandlung und Verfahren zum Betreiben einer derartigen Brennkraftmaschine |
KR20200111523A (ko) * | 2019-03-19 | 2020-09-29 | 현대자동차주식회사 | 배기 매니폴드 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE9902491L (sv) * | 1999-06-30 | 2000-12-31 | Saab Automobile | Förbränningsmotor med avgasåtermatning |
JP3783765B2 (ja) * | 2000-07-18 | 2006-06-07 | 三菱ふそうトラック・バス株式会社 | 過給機付きエンジンのegr装置 |
US20080022680A1 (en) * | 2006-07-26 | 2008-01-31 | Gingrich Jess W | Apparatus and method for increasing the hydrogen content of recirculated exhaust gas in fuel injected engines |
WO2008033418A1 (fr) * | 2006-09-13 | 2008-03-20 | Borgwarner Inc. | Intégration d'un refroidisseur d'air d'échappement dans un turbocompresseur |
FR2909718B1 (fr) * | 2006-12-11 | 2009-02-27 | Jean Melchior | Moteur a combustion interne suralimente |
US8495992B2 (en) * | 2008-02-22 | 2013-07-30 | Borgwarner Inc. | Controlling exhaust gas flow divided between turbocharging and exhaust gas recirculating |
AT507008B1 (de) * | 2009-06-25 | 2010-12-15 | Avl List Gmbh | Verfahren zum betreiben einer brennkraftmaschine |
DE102009049614A1 (de) * | 2009-10-16 | 2011-04-21 | Emcon Technologies Germany (Augsburg) Gmbh | Abgasrückführungsventil |
US8096125B2 (en) * | 2009-12-23 | 2012-01-17 | Ford Global Technologies, Llc | Methods and systems for emission system control |
FR2957383B1 (fr) * | 2010-03-12 | 2012-06-08 | Peugeot Citroen Automobiles Sa | Moteur a combustion interne comprenant un moyen de production d'hydrogene dispose dans le flux principal de gaz d'echappement |
US8069663B2 (en) * | 2010-09-09 | 2011-12-06 | Ford Global Technologies, Llc | Method and system for turbocharging an engine |
US8479511B2 (en) * | 2010-09-09 | 2013-07-09 | Ford Global Technologies, Llc | Method and system for a turbocharged engine |
-
2012
- 2012-06-21 FR FR1255810A patent/FR2992356B1/fr not_active Expired - Fee Related
-
2013
- 2013-05-24 WO PCT/FR2013/051157 patent/WO2013190198A1/fr active Application Filing
- 2013-05-24 EP EP13728491.5A patent/EP2867514A1/fr not_active Withdrawn
- 2013-05-24 CN CN201380032508.3A patent/CN104471229B/zh not_active Expired - Fee Related
Non-Patent Citations (2)
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See also references of WO2013190198A1 * |
Also Published As
Publication number | Publication date |
---|---|
CN104471229A (zh) | 2015-03-25 |
WO2013190198A1 (fr) | 2013-12-27 |
CN104471229B (zh) | 2017-11-17 |
FR2992356A1 (fr) | 2013-12-27 |
FR2992356B1 (fr) | 2016-04-15 |
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