WO2016079976A1 - Dispositif de circulation des gaz d'échappement pour moteur à combustion interne - Google Patents

Dispositif de circulation des gaz d'échappement pour moteur à combustion interne Download PDF

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Publication number
WO2016079976A1
WO2016079976A1 PCT/JP2015/005700 JP2015005700W WO2016079976A1 WO 2016079976 A1 WO2016079976 A1 WO 2016079976A1 JP 2015005700 W JP2015005700 W JP 2015005700W WO 2016079976 A1 WO2016079976 A1 WO 2016079976A1
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WIPO (PCT)
Prior art keywords
internal combustion
combustion engine
air
ejector
egr
Prior art date
Application number
PCT/JP2015/005700
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English (en)
Japanese (ja)
Inventor
容久 佐南
英明 市原
敬太郎 南
Original Assignee
株式会社デンソー
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from JP2015201041A external-priority patent/JP2016104977A/ja
Application filed by 株式会社デンソー filed Critical 株式会社デンソー
Priority to DE112015005244.5T priority Critical patent/DE112015005244T5/de
Priority to US15/526,069 priority patent/US20170306899A1/en
Publication of WO2016079976A1 publication Critical patent/WO2016079976A1/fr

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    • 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
    • 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
    • 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
    • F02M26/17—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories in relation to the intake system
    • 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 disclosure relates to an exhaust gas circulation device for an internal combustion engine, and more particularly to an exhaust gas circulation device that recirculates a part of exhaust gas discharged from a cylinder of the internal combustion engine to an intake system as EGR gas.
  • Patent Document 1 describes a “low pressure loop EGR system”. This EGR system is provided with an EGR passage that communicates an exhaust passage downstream of the turbine of the turbocharger and an intake passage upstream of the compressor.
  • the outlet of this EGR flow path is connected to an intake passage through which intake air that has passed through the air cleaner flows.
  • This intake passage has a structure in which it is branched into two first and second flow paths at a branching point and then joined again at a joining point on the upstream side of the compressor.
  • the outlet of the EGR channel is connected to the first channel.
  • An ejector having a nozzle, a diffuser, and a decompression chamber is installed between the first flow path and the EGR flow path.
  • an intake throttle valve is installed in the second flow path.
  • a negative pressure is generated at the junction of the first flow path and the second flow path, and the recirculation of the EGR gas to the intake passage is promoted.
  • Patent Document 2 describes a configuration in which an ejector that draws EGR gas is disposed in the intake passage downstream of the compressor.
  • the ejector is integrally formed with a casing provided with a connection portion of the EGR flow path. Inside the casing, there is provided a cylindrical throat portion whose diameter decreases toward the downstream side and whose opening end opens toward the merging chamber of the casing. An EGR introduction hole provided in the connection portion communicates with the junction chamber.
  • the EGR gas is introduced from the EGR introduction hole directly downstream of the opening end of the throat portion of the ejector. Then, it is mixed with the EGR gas into which the compressed air has been introduced at the throttle portion on the downstream side of the throat, and is quickly sent out to the intake manifold side.
  • the flow path cross-sectional area of the EGR flow path through which the EGR gas is introduced from the EGR introduction hole gradually decreases, and between the outer periphery of the ejector throat and the inner wall of the casing, When EGR gas flows through the minimum cross-sectional area flow path, the pressure loss of the EGR gas flow may increase.
  • the downstream end of the ejector throat portion is at a right angle, so that the EGR gas flow is separated or swirled at the outer peripheral edge of the throat portion. This can increase the pressure loss of the EGR gas flow.
  • This disclosure is intended to provide an exhaust gas circulation device for an internal combustion engine that can draw more EGR gas. It is another object of the present invention to provide an exhaust gas circulation device for an internal combustion engine that can reduce the pressure loss of the EGR gas flow.
  • the tip side portion of the nozzle is inserted and disposed in the negative pressure generating chamber of the ejector.
  • the air compression apparatus which supplies the nozzle with the compressed air produced
  • compressed air at atmospheric pressure or higher can be supplied from the air compressor to the ejector, so that the nozzle inlet pressure can be increased to air pressure at atmospheric pressure or higher.
  • a negative pressure is generated in the negative pressure generating chamber by the air flow of the compressed air ejected from the opening at the tip of the nozzle into the negative pressure generating chamber.
  • the EGR gas is drawn from the introduction hole of the ejector by the generated negative pressure.
  • the ejector mixes the EGR gas sucked into the negative pressure generating chamber with the air flow ejected from the nozzle tip opening into the negative pressure generating chamber and supplies it to the internal combustion engine.
  • the nozzle has an outer diameter gradually changing portion in which the outer diameter gradually decreases from the starting point (starting point) toward the outer peripheral edge of the tip.
  • the outer diameter gradually changing portion of the nozzle is arranged at a position where at least a part can be seen from the outside of the ejector through the introduction hole.
  • the position where at least a part can be seen from the outside of the ejector through the introduction hole means that the outside diameter gradually changing portion of the nozzle when the inside of the ejector (nozzle) is seen from the outside of the ejector (radially outside the nozzle) through the introduction hole. It is the position where at least a part can be seen.
  • the EGR gas introduced into the ejector from the introduction hole is introduced into the negative pressure generating chamber without colliding with the outer wall of the nozzle.
  • the gradually changing portion of the outer diameter of the nozzle guides the EGR gas from the introduction hole, and the EGR gas can be efficiently mixed with the air flow of the compressed air supplied from the air compressor.
  • FIG. 1 is a configuration diagram showing a schematic configuration of an internal combustion engine control system (Embodiment 1).
  • FIG. 2 is a front view showing an ejector and an EGR pipe (Embodiment 1).
  • FIG. 3 is a cross-sectional view taken along the line III-III in FIG. 2 (Embodiment 1).
  • FIG. 4 is a plan view showing an ejector and an EGR pipe (Embodiment 1).
  • FIG. 5 is a sectional view showing an ejector (Embodiment 1).
  • FIG. 1 is a configuration diagram showing a schematic configuration of an internal combustion engine control system (Embodiment 1).
  • FIG. 2 is a front view showing an ejector and an EGR pipe (Embodiment 1).
  • FIG. 3 is a cross-sectional view taken along the line III-III in FIG. 2 (Embodiment 1).
  • FIG. 4 is a plan view showing an ejector and an EGR
  • FIG. 6 is a schematic view showing the flow of EGR gas and compressed air in the ejector (Embodiment 1).
  • FIG. 7 is an explanatory diagram showing the EGR rate when the position of the starting point A is changed with respect to the introduction hole wall surface B (Embodiment 1, Comparative Examples 1 and 2).
  • FIG. 8 is a configuration diagram showing a schematic configuration of the engine control system (Embodiment 2).
  • the engine control system of this embodiment includes an air cleaner 1, a turbocharger TC, a bypass valve 2, an air compressor 3, an ejector 4, a throttle valve 5, an intercooler 6, an exhaust circulation device (hereinafter referred to as an EGR system), and an engine control device (electronic Control device: ECU) and the like.
  • the ejector 4 of this embodiment is installed in the intake passage of the engine E.
  • the ejector 4 includes a cylindrical housing 7 to which the EGR pipe P is connected, and a circular nozzle 9 that ejects compressed air into a negative pressure generation chamber (hereinafter referred to as a decompression chamber 8) of the housing 7. Yes.
  • the air cleaner 1 has an element for filtering foreign substances contained in fresh air (also referred to as outside air) introduced from the outside.
  • the air cleaner 1 is installed in the intake passage 11 upstream of the compressor 13.
  • the turbocharger TC is a turbocharger including a compressor 13 installed between the intake passages 11 and 12 of the engine E and a turbine 16 installed between the exhaust passages 14 and 15 of the engine E.
  • the compressor 13 compresses air flowing through an intake passage (not shown) that connects the intake passage 11 and the intake passage 12 and supplies the compressed air to the cylinder of the engine E.
  • the turbine 16 is connected to the compressor 13 through a turbine shaft 17 so as to be integrally rotatable.
  • the turbine 16 is rotationally driven by the pressure and flow rate of exhaust flowing through an exhaust passage (not shown) that communicates the exhaust passage 14 and the exhaust passage 15.
  • An air cleaner 1, a compressor 13, a bypass valve 2, an air compressor 3, an ejector 4, a throttle valve 5, an intercooler 6 and the like are installed in an intake pipe connected to a branch portion of an intake manifold of the engine E.
  • the intake passage 12 on the downstream side of the compressor 13 is branched into two first and second intake passages (flow paths 18 and 19) at a branch portion.
  • the flow paths 18 and 19 are configured to join at a joining portion on the upstream side of the throttle valve 5 and to communicate with the intake passage 20 on the upstream side of the intake manifold.
  • the throttle valve 5 constitutes a valve body of an intake throttle valve.
  • the throttle valve 5 is opened / closed (rotated) by an electric actuator such as a motor or a mechanical actuator.
  • the actuator has a built-in throttle opening sensor that detects a throttle opening corresponding to the rotation angle of the throttle valve 5.
  • the opening degree of the throttle valve 5 is energized and controlled by the ECU. Thereby, the flow rate of the compressed air (also referred to as intake air) flowing through the intake passage 20 communicating with the cylinder of the engine E is adjusted.
  • the compressed air also referred to as intake air
  • the intercooler 6 is a cooling heat exchanger that cools the compressed air, which has been compressed by the compressor 13 or the air compressor 3 and has risen in temperature, using a cooling medium such as cooling water. Thereby, the charging efficiency of the intake air supplied to the cylinder of the engine E can be increased.
  • bypass valve 2 The details of the bypass valve 2, the air compressor 3, the ejector 4, and the flow paths 18 and 19 will be described later.
  • the exhaust pipe connected to the exhaust manifold of the engine E is provided with a turbine 16, an exhaust purification device (a catalyst such as a three-way catalyst: hereinafter referred to as a catalyst) 21, a waste gate valve 22, a muffler (not shown), and the like. ing.
  • a catalyst such as a three-way catalyst: hereinafter referred to as a catalyst
  • the catalyst 21 purifies CO, HC, NOx components and the like in the exhaust gas flowing through the exhaust passage 15.
  • a diesel particulate filter (DPF), an oxidation catalyst (DOC), or a NOx catalyst may be used instead of the three-way catalyst. Alternatively, two or more of these may be arranged in series.
  • the waste gate valve 22 is installed in a waste gate flow path 23 that bypasses the turbine 16 and communicates the exhaust passage 14 and the exhaust passage 15.
  • the waste gate valve 22 is an exhaust flow control valve.
  • the waste gate valve 22 is a supercharging pressure control valve that opens when the supercharging pressure of the compressor 13 exceeds a set value and bypasses the exhaust discharged from the cylinder of the engine E from the turbine 16.
  • the opening degree of the waste gate valve 22 is energized and controlled by the ECU. As a result, the flow rate of the exhaust gas flowing through the waste gate channel 23 is adjusted. Therefore, the supercharging pressure can be lowered when the waste gate valve 22 is opened.
  • the EGR system is equipped with a “low pressure loop (LPL) -EGR system”.
  • the EGR system includes first and second EGR flow paths 31 and 32, an EGR cooler 33, a flow path switching valve 34, an EGR valve 35, and the like.
  • the first EGR passage 31 communicates the exhaust passage 15 downstream of the turbine 16 (downstream of the catalyst 21 in the first embodiment) and the intake passage 11 upstream of the compressor 13.
  • the second EGR flow path 32 communicates the exhaust passage 15 downstream of the turbine 16 and the introduction hole (described later) of the ejector 4 disposed in the flow path 18 downstream of the compressor 13.
  • the EGR cooler 33 is disposed in a shared flow path of the first and second EGR flow paths 31 and 32, that is, in an EGR flow path upstream of the flow path switching valve 34.
  • the EGR cooler 33 is a cooling heat exchanger that cools the EGR gas taken from the exhaust passage 15 downstream of the turbine 16 using a cooling medium such as cooling water.
  • the flow path switching valve 34 is installed at a branch portion of the first and second EGR flow paths 31 and 32.
  • the flow path switching valve 34 is a 2-position 3-way switching valve that selectively switches between the first EGR flow path 31 and the second EGR flow path 32.
  • the switching position of the flow path switching valve 34 is energized and controlled by the ECU.
  • the flow path switching valve 34 is switched by an electric actuator such as a motor.
  • the EGR flow path is switched to the first EGR flow path 31. Further, when the flow path switching valve 34 is opened, the EGR flow path is switched to the second EGR flow path 32.
  • the EGR valve 35 is installed in the first EGR flow path 31 on the downstream side of the flow path switching valve 34.
  • the EGR valve 35 is opened and closed (also referred to as rotational drive) by an electric actuator such as a motor.
  • the actuator has an EGR opening sensor that detects an EGR opening corresponding to the rotation angle of the EGR valve 35.
  • the opening degree of the EGR valve 35 is energized and controlled by the ECU. Thereby, the flow rate of the EGR gas flowing through the first EGR flow path 31 is adjusted.
  • the bypass valve 2 is installed in the middle of the flow path 19.
  • the bypass valve 2 is driven to open and close by an electric actuator such as a motor.
  • the opening degree of the bypass valve 2 is energized and controlled by the ECU. Thereby, the flow volume of the air flow which bypasses the flow path 18 can be adjusted. Therefore, the flow rate of the EGR gas sucked into the ejector 4 can be adjusted.
  • the flow path 18 is arranged in parallel with the flow path 19.
  • the flow path 18 communicates the intake passage 12 downstream of the compressor 13 and the intake passage 20 of the engine E.
  • the flow path 19 communicates the intake passage 12 downstream of the compressor 13 and the intake passage 20 of the engine E without passing through the air compressor 3 and the ejector 4.
  • the air compressor 3 is installed in the flow path 18 on the downstream side of the compressor 13 and on the upstream side of the ejector 4.
  • the air compressor 3 is constituted by an electric supercharger (for example, an electric supercharger or an electric compressor).
  • the air compressor 3 compresses the air supplied from the compressor 13 to generate compressed air, and supplies the generated compressed air to the nozzle 9.
  • Compressed air generated by the air compressor 3 is supplied to the ejector 4.
  • the air compressor 3 is rotationally driven by an electric actuator such as a motor. This actuator is energized and controlled by the ECU.
  • the ECU incorporates a microcomputer having a well-known structure that includes functions of a CPU, a memory (ROM, RAM), a motor drive circuit, a valve drive circuit, and the like.
  • the microcomputer is connected to various sensors such as an accelerator opening sensor that detects the amount of depression of the accelerator pedal by the driver.
  • the ejector 4 is installed in the flow path 18 on the downstream side of the air compressor 3.
  • the ejector 4 includes a cylindrical housing 7 to which an EGR pipe P that forms the second EGR flow path 32 is connected, and a nozzle 9 that ejects an air flow of compressed air into a decompression chamber 8 formed in the housing 7. It has.
  • the ejector 4 uses a negative pressure generated by an air flow of compressed air ejected from the nozzle 9 into the decompression chamber 8 and uses a large amount of EGR gas from the EGR gas introduction hole (hereinafter referred to as introduction hole 10) into the decompression chamber 8. Is to suck.
  • the EGR gas sucked into the decompression chamber 8 is mixed with the air flow of compressed air ejected from the nozzle 9 into the decompression chamber 8 and then supplied to the cylinder of the engine E.
  • a nozzle hole 36 is formed inside the nozzle 9 to introduce compressed air from the air compressor 3 and to eject an air flow of the compressed air toward the decompression chamber 8.
  • the nozzle hole 36 is an air flow path that extends straight in the axial direction of the nozzle 9.
  • the nozzle hole 36 includes an inlet opening 37, a throttle portion 38, and a tip opening 39.
  • the inlet opening 37 is provided at the opening end on the upstream side of the nozzle hole 36.
  • the inlet opening 37 opens toward the outside of the nozzle 9.
  • the inlet opening 37 is an inlet for taking in the compressed air compressed by the air compressor 3 into the ejector 4.
  • the throttle unit 38 reduces the pressure of the compressed air flowing through the nozzle hole 36 by reducing the cross-sectional area of the nozzle hole 36 and converts it from static pressure to dynamic pressure.
  • the tip opening 39 is provided at the opening end on the downstream side of the nozzle hole 36.
  • the tip opening 39 opens toward the outside of the nozzle 9.
  • the tip opening 39 is a jet outlet for jetting an air flow of compressed air toward the decompression chamber 8.
  • the housing 7 is provided with an EGR pipe connection part 42 for connecting the coupling flange 41 of the EGR pipe P and an intake pipe connection part 44 for connecting the coupling flange 43 of the nozzle 9.
  • the gasket 45 a is sandwiched between the coupling flange 41 and the EGR pipe connection portion 42.
  • the coupling flange 41 is fastened and fixed to the EGR pipe connection portion 42 by a plurality of bolts 45.
  • a gasket 46 a is sandwiched between the coupling flange 43 and the intake pipe connecting portion 44.
  • the coupling flange 43 is fastened and fixed to the intake pipe connecting portion 44 by a plurality of bolts 46.
  • the EGR pipe P includes a straight pipe portion 47 in which the second EGR flow path 32 is formed.
  • a coupling flange 41 connected to the housing 7 is provided at the downstream end of the straight pipe portion 47.
  • a coupling flange 48 connected to the flow path switching valve 34 is provided at the upstream end of the straight pipe portion 47.
  • the coupling flange 48 is fastened and fixed to an EGR pipe connection portion (not shown) of the flow path switching valve 34 by a plurality of bolts 49.
  • a gasket 49 a is sandwiched between the coupling flange 48 and the EGR pipe connection portion of the flow path switching valve 34.
  • an EGR pipe having a separate structure from the EGR pipe P may be connected between the flow path switching valve 34 and the coupling flange 48.
  • the nozzle 9 is installed in the flow path 18 on the downstream side of the air compressor 3 in the middle of the intake passage.
  • a coupling flange 43 is provided on the outer periphery of the central portion of the nozzle 9 in the axial direction.
  • a proximal end portion 51 connected to the air compressor 3 via an intake pipe (not shown) is provided.
  • the proximal end portion 51 is disposed outside the housing 7.
  • a tip side portion 52 disposed in the decompression chamber 8 is provided.
  • a decompression chamber 8 into which the tip end portion 52 in the axial direction of the nozzle 9 is inserted is formed.
  • the housing 7 is formed with an introduction hole 10 that opens to the outside and communicates the second EGR flow path 32 and the decompression chamber 8.
  • the decompression chamber 8 also serves as a mixing unit that mixes the compressed air ejected from the nozzle 9 and the EGR gas sucked from the introduction hole 10.
  • the housing 7 is provided with a diffuser 53 on the downstream side of the decompression chamber 8.
  • the diffuser 53 includes a pressure increasing portion 54 whose starting point is the downstream end of the decompression chamber 8 and whose inner diameter gradually increases from the starting point toward the outlet opening 55.
  • the pressure increasing unit 54 is a part that increases the pressure by reducing the flow rate of the mixed gas of the compressed air and the EGR gas.
  • a tip end portion 52 of the nozzle 9 is inserted and arranged.
  • the distal end portion 52 is provided with an outer diameter equal diameter portion 61 having a constant outer diameter in the axial direction and an outer diameter gradually changing portion 62 provided on the distal end side with respect to the outer diameter equal diameter portion 61.
  • the inner wall of the nozzle 9 is provided with an inner diameter gradually changing portion 63 extending from the inner diameter equal diameter portion substantially the same as the inlet opening 37 to the throttle portion 38 and an inner diameter equal diameter portion 64 having a constant inner diameter in the axial direction. ing.
  • the inner peripheral surface of the inner diameter gradually changing portion 63 is a conical tapered surface whose inner diameter gradually decreases from the starting point located on the inner periphery of the nozzle hole 36 toward the throttle portion 38. Further, the inner diameter equal diameter portion 64 extends from the inner diameter gradually changing portion 63 to the tip opening 39.
  • the outer peripheral surface of the outer diameter gradually changing portion 62 is the tip that is the end point of the outer diameter gradually changing portion 62 from the starting point (starting point: starting point) A of the outer diameter gradually changing portion 62 located at the end of the outer diameter equal diameter portion 61.
  • the starting point A of the outer diameter gradually changing portion 62 is located on the outer periphery of the tip side portion 52 of the nozzle 9.
  • the starting point A is provided on an annular ridge line between the cylindrical surface of the outer diameter equal diameter portion 61 and the conical taper surface of the outer diameter gradually changing portion 62.
  • the tip outer peripheral edge B of the outer diameter gradually changing portion 62 is provided on the outer periphery of the tip opening 39 of the nozzle 9.
  • the distal outer peripheral edge B is provided on an annular ridge line between the annular distal end surface provided on the opening peripheral edge of the distal end opening 39 and the conical tapered surface of the outer diameter gradually changing portion 62. Further, the intersection angle between the annular tip surface and the conical taper surface is an obtuse angle larger than a right angle.
  • the conical tapered surface is an inclined surface inclined from the starting point A toward the outer peripheral edge B of the tip.
  • the outer diameter gradually changing portion 62 is arranged at a position where at least a part can be seen from the outside of the housing 7 through the introduction hole 10. That is, the outer diameter gradually changing portion 62 is at least one of the outer diameter gradually changing portions 62 when the inside of the ejector 4 (nozzle 9) is viewed from the outside of the ejector 4 (outside in the radial direction of the nozzle 9) through the introduction hole 10. It is arranged so that a part can be seen.
  • extension lines L1 and L2 of the conical taper surface of the outer diameter gradually changing portion 62 intersect at a point O on the central axis of the ejector 4 before intersecting the inner wall of the housing 7.
  • the starting point A of the outer diameter gradually changing portion 62 is provided at the end of an extension line L3 obtained by extending the hole wall surface of the introduction hole 10 of the housing 7.
  • the ECU When the ignition switch is turned on (IG / ON), the ECU first obtains various sensor signals necessary for calculating the operating state (engine information) of the engine E. Then, the actuators of the bypass valve 2, the air compressor 3, the throttle valve 5, the waste gate valve 22, the flow path switching valve 34, and the EGR valve 35 are energized based on the operation status of the engine E and the program stored in the ROM. Control.
  • the target EGR amount may be determined by a sensor signal (fresh air flow signal) output from an air flow meter, an engine speed measured from a sensor signal (engine rotation signal) output from a crank angle sensor, an accelerator opening sensor, or a throttle opening. It is set corresponding to the sensor signal (engine load signal) output from the degree sensor.
  • the ECU closes the flow path switching valve 34 and fully closes the EGR valve 35 when the operating region of the engine E is a region where the engine load is low and the engine speed is low. Stop introducing EGR gas to fresh air. Thereby, the combustion state of each cylinder of the engine E is stabilized.
  • the ECU fully closes the bypass valve 2 and turns on the actuator of the air compressor 3. Further, the flow path switching valve 34 is opened and the EGR valve 35 is fully closed. As a result, EGR gas is sucked into the intake passage 20 from the exhaust passage 15 through the second EGR passage 32 and the passage 18.
  • the ECU turns off the actuator of the air compressor 3 and fully opens the bypass valve 2 when the operating region of the engine E is a medium load and the engine speed is a medium speed region. To do. At this time, the flow path switching valve 34 is closed. Then, the ECU adjusts the opening degree of the EGR valve 35 in accordance with the operating state of the engine E.
  • the ECU turns off the actuator of the air compressor 3 and fully opens the bypass valve 2 when the operating region of the engine E is a region where the engine load is high and the engine speed is high. At this time, the flow path switching valve 34 is closed and the EGR valve 35 is fully closed. Thereby, the output fall of the engine E can be avoided.
  • the turbine 16 of the turbocharger TC is driven to rotate by the pressure (exhaust energy) of the exhaust discharged from the cylinder of the engine E.
  • the EGR gas that has flowed into the second EGR flow path 32 travels toward the introduction hole 10 of the ejector 4 that is disposed downstream of the compressor 13.
  • the pressure is increased by the diffuser 53 while mixing the high-speed compressed air flow and the EGR gas in the decompression chamber 8.
  • the mixed gas of compressed air and EGR gas is sent out from the outlet opening 55 of the housing 7 to the flow path 18 on the downstream side of the ejector 4.
  • the mixed gas is sent from the flow path 18 through the intake passage 20 to the cylinder of the engine E.
  • the air supplied from the compressor 13 is compressed into the flow path 18 on the downstream side of the compressor 13 of the turbocharger TC to generate compressed air higher than the atmospheric pressure.
  • the compressed air supplied from the air compressor 3 is jetted into the decompression chamber 8 from the tip opening 39 of the nozzle 9.
  • a negative pressure is generated in the decompression chamber 8 by the air flow of the compressed air ejected into the decompression chamber 8.
  • EGR gas is drawn from the introduction hole 10 of the housing 7 by the generated negative pressure.
  • the ejector 4 mixes the EGR gas sucked into the decompression chamber 8 with the air flow of the compressed air ejected from the tip opening 39 of the nozzle 9 into the decompression chamber 8 and sends it to the cylinder of the engine E.
  • the tip end portion 52 of the nozzle 9 is provided with an outer diameter gradually changing portion 62 whose outer diameter gradually decreases from the starting point A toward the tip outer peripheral edge B. Further, the outer diameter gradually changing portion 62 of the nozzle 9 is disposed at a position where at least a part can be seen from the outside of the housing 7 of the ejector 4 through the introduction hole 10.
  • the EGR gas introduced into the housing 7 from the introduction hole 10 is introduced into the decompression chamber 8 without colliding with the outer wall of the outer diameter equal diameter portion 61 of the nozzle 9.
  • the outer diameter gradually changing portion 62 of the nozzle 9 guides the EGR gas from the introduction hole 10, and the EGR gas can be efficiently mixed with the air flow of the compressed air supplied from the air compressor 3. Therefore, the amount of EGR gas can be greatly increased as compared with the conventional technique.
  • extension lines L1 and L2 of the conical taper surface of the outer diameter gradually changing portion 62 intersect at a point O on the central axis of the ejector 4 before intersecting the inner wall of the housing 7.
  • the starting point A of the outer diameter gradually changing portion 62 is provided at the tip of an extension line L3 that extends the hole wall surface C of the introduction hole 10 of the ejector 4.
  • the downstream end (tip outer peripheral edge B) of the outer diameter gradually changing portion 62 of the ejector 4 is not at a right angle. There is no separation or vortex in the flow. Thereby, the increase in the pressure loss of an EGR gas flow can be suppressed.
  • the EGR rate in the case where the outer diameter gradually changing portion 62 of the nozzle 9 is not visible from the outside of the housing 7 through the introduction hole 10 was investigated.
  • the starting point A of the outer diameter gradually changing portion 62 is on the left side of the drawing from the tip of the extension line L3 that extends the hole wall surface C of the introduction hole 10 of the ejector 4. It is the comparative example 1 arrange
  • the EGR rate in the case where the outer diameter gradually changing portion 62 of the nozzle 9 is not visible from the outside of the housing 7 through the introduction hole 10 was investigated.
  • the starting point A of the outer diameter gradually changing portion 62 is on the right side of the drawing than the tip of the extension line L4 that extends the hole wall surface D of the introduction hole 10 of the ejector 4. It is the comparative example 2 arrange
  • the EGR gas flow drawn into the decompression chamber 8 from the introduction hole 10 is applied to the outer wall surface of the outer diameter equal diameter portion 61 that can be seen from the outside of the housing 7 through the introduction hole 10. Due to the collision (area 102), stagnation occurs in the EGR gas flow.
  • the throttle portion 104 is formed in the flow path in the ejector through which EGR gas introduced into the decompression chamber 8 from the introduction hole 10 flows. For this reason, since the flow path cross-sectional area in the flow path in the ejector decreases, the pressure loss of the EGR gas flow increases. When the nozzle 9 protrudes on the right side in the figure, it can be seen that the EGR rate tends to deteriorate as can be confirmed from the graph of FIG.
  • the EGR rate in the case where at least a part of the outer diameter gradually changing portion 62 of the nozzle 9 is located through the introduction hole 10 from the outside of the housing 7 was investigated.
  • the ejector 4 shown in FIG. 6B is Embodiment 1 in which at least a part of the outer diameter gradually changing portion 62 of the nozzle 9 is disposed at a position where it can be seen through the introduction hole 10 from the outside of the housing 7.
  • the EGR gas introduced into the housing 7 from the introduction hole 10 enters the decompression chamber 8 without colliding with the outer wall of the outer diameter equal diameter portion 61 of the nozzle 9. be introduced.
  • the outer diameter gradually changing portion 62 of the nozzle 9 functions as a guide for efficiently mixing the EGR gas from the introduction hole 10 into the air flow of the compressed air, and the EGR gas flow forms a beautiful flow (area 100). .
  • the EGR rate tends to be good.
  • the position where at least a part of the outer diameter gradually changing portion 62 of the nozzle 9 can be seen from the outside of the housing 7 through the introduction hole 10 is the outer diameter gradually changing portion 62 between the hole wall surfaces C and D of the introduction hole 10 of the ejector 4. Is the position where the starting point A or the outer peripheral edge B of the tip is arranged. That is, either the starting point A or the outer peripheral edge B of the outer diameter gradually changing portion 62 is disposed at a position (for example, in the range I-II in the graph of FIG. 7) that can be seen from the outside of the housing 7 through the introduction hole 10. Just do it.
  • FIG. 8 shows a second embodiment to which the present disclosure is applied.
  • an air cleaner 1, a bypass valve 2, an air compressor 3, an ejector 4, a compressor 13, a throttle valve 5, an intercooler 6, and the like are installed.
  • the intake passage 11 on the downstream side of the air cleaner 1 is branched into two first and second intake passages (flow paths 71 and 72) at a branching portion.
  • the flow paths 71 and 72 are configured to merge at a merge section upstream of the compressor 13 and to communicate with an intake passage 73 upstream of the compressor 13.
  • the downstream end of the compressor 13 communicates with the intake passage 12 upstream of the intake manifold.
  • the bypass valve 2 is installed in the middle of the flow path 72.
  • the opening degree of the bypass valve 2 is adjusted by energization control of the electric actuator by the ECU.
  • the flow volume of the airflow which bypasses the flow path 71 can be adjusted. Therefore, the flow rate of the EGR gas sucked into the ejector 4 can be adjusted.
  • the flow path 71 is arranged in parallel with the flow path 72.
  • the flow path 71 communicates the intake passage 11 and the intake passage 73 on the downstream side of the air cleaner 1.
  • the flow path 72 communicates the intake passage 11 and the intake passage 73 without passing through the air compressor 3 and the ejector 4.
  • the air compressor 3 is installed in the flow path 71 on the upstream side of the compressor 13 and the ejector 4.
  • the air compressor 3 is rotationally driven by an electric actuator.
  • the ejector 4 is installed in the flow path 71 on the upstream side of the compressor 13.
  • the EGR system of the present embodiment has the same effects as those of the first embodiment.
  • a turbocharger TC that compresses and supercharges intake air supplied into a combustion chamber of each cylinder of the internal combustion engine (engine) using the exhaust pressure of the internal combustion engine (engine) as a supercharger.
  • an electric (assist supercharging type) turbocharger TC that drives the turbine 16 and the compressor 13 by using the driving force of the electric motor may be used.
  • a multi-cylinder diesel engine or a multi-cylinder gasoline engine may be used.
  • a multi-cylinder engine not only a multi-cylinder engine but also a single-cylinder engine may be used.
  • a “high pressure loop (HPL) -EGR system” may be provided in addition to the “LPL-EGR system”.
  • a conical tapered surface shape in which the nozzle outer peripheral surface from the start point A of the outer diameter gradually changing portion 62 to the end outer peripheral edge B that is the end point is inclined by a predetermined inclination angle with respect to the axial direction of the nozzle 9.
  • the outer peripheral surface of the nozzle from the starting point A to the outer peripheral edge B of the outer diameter gradually changing portion 62 is a convex curved surface or the outer diameter gradually decreases from the starting point A toward the outer peripheral edge B. You may form in a concave curved surface.
  • an electric supercharger such as an electric supercharger or an electric compressor is employed as the air compressor 3, but a turbocharger TC compressor may be used.
  • an engine-driven supercharger may be used as the air compressor 3.
  • a clutch mechanism such as an electromagnetic clutch may be interposed between the crankshaft of the engine E and the drive shaft of the supercharger. Thereby, transmission and interruption of power from the engine E to the supercharger can be switched.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Exhaust-Gas Circulating Devices (AREA)

Abstract

L'invention concerne un éjecteur (4) utilisé dans un système de recirculation des gaz d'échappement (système EGR), au moins une partie d'une section changeant graduellement de diamètre extérieur (62) d'une buse (9) est disposée au niveau d'une position visible depuis l'extérieur d'un boîtier (7) au travers d'un trou d'entrée (10). De ce fait, les gaz d'EGR introduits dans le boîtier (7) au travers du trou d'entrée (10) sont introduits dans une chambre de dépressurisation (8) sans entrer en collision contre une paroi externe d'une section uniforme de diamètre extérieur (61). A ce moment, la section changeant graduellement de diamètre extérieur (62) de la buse (9) peut guider les gaz d'EGR en provenance du trou d'entrée (10) à des fins de mélange efficace des gaz d'EGR avec un flux d'air comprimé fourni en provenance d'un dispositif de compression d'air.
PCT/JP2015/005700 2014-11-20 2015-11-16 Dispositif de circulation des gaz d'échappement pour moteur à combustion interne WO2016079976A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
DE112015005244.5T DE112015005244T5 (de) 2014-11-20 2015-11-16 Abgaszirkulationsvorrichtung für eine Verbrennungskraftmaschine
US15/526,069 US20170306899A1 (en) 2014-11-20 2015-11-16 Exhaust circulating device for internal combustion engine

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP2014235731 2014-11-20
JP2014-235731 2014-11-20
JP2015-201041 2015-10-09
JP2015201041A JP2016104977A (ja) 2014-11-20 2015-10-09 内燃機関の排気循環装置

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113847124A (zh) * 2021-10-29 2021-12-28 重庆隆鑫通航发动机制造有限公司 一种通用发动机及二次进气中间部件

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000230460A (ja) * 1999-02-08 2000-08-22 Hitachi Ltd 過給エンジンの排気ガス再循環システム
JP2001165002A (ja) * 1999-11-09 2001-06-19 Caterpillar Inc 内燃機関の排気ガス循環システムのための吸入ベンチュリ
JP2012520420A (ja) * 2009-03-13 2012-09-06 スカニア シーブイ アクチボラグ 燃焼機関の再循環排気ガスを冷却するための装置
JP2013160189A (ja) * 2012-02-08 2013-08-19 Hino Motors Ltd Ｅｇｒガス混合装置

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000230460A (ja) * 1999-02-08 2000-08-22 Hitachi Ltd 過給エンジンの排気ガス再循環システム
JP2001165002A (ja) * 1999-11-09 2001-06-19 Caterpillar Inc 内燃機関の排気ガス循環システムのための吸入ベンチュリ
JP2012520420A (ja) * 2009-03-13 2012-09-06 スカニア シーブイ アクチボラグ 燃焼機関の再循環排気ガスを冷却するための装置
JP2013160189A (ja) * 2012-02-08 2013-08-19 Hino Motors Ltd Ｅｇｒガス混合装置

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113847124A (zh) * 2021-10-29 2021-12-28 重庆隆鑫通航发动机制造有限公司 一种通用发动机及二次进气中间部件

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