EP2317111A1 - Mixing device for a low pressure EGR system of an internal combustion engine - Google Patents
Mixing device for a low pressure EGR system of an internal combustion engine Download PDFInfo
- Publication number
- EP2317111A1 EP2317111A1 EP10189227A EP10189227A EP2317111A1 EP 2317111 A1 EP2317111 A1 EP 2317111A1 EP 10189227 A EP10189227 A EP 10189227A EP 10189227 A EP10189227 A EP 10189227A EP 2317111 A1 EP2317111 A1 EP 2317111A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- butterfly valve
- mixing device
- inlet conduit
- shaft
- conduit
- 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.)
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Classifications
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- 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
- F02M26/74—Protection from damage, e.g. shielding means
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- 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
- F02M26/06—Low pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust downstream of the turbocharger turbine and reintroduced into the intake system upstream of the compressor
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- 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
- F02M26/21—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 with EGR valves located at or near the connection to the intake system
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- 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
- F02M26/52—Systems for actuating EGR valves
- F02M26/64—Systems for actuating EGR valves the EGR valve being operated together with an intake air throttle
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- 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
- F02M26/70—Flap valves; Rotary valves; Sliding valves; Resilient valves
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- 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
- F02M26/72—Housings
- F02M26/73—Housings with means for heating or cooling the EGR valve
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- 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
- F02M26/09—Constructional details, e.g. structural combinations of EGR systems and supercharger systems; Arrangement of the EGR and supercharger systems with respect to the engine
- F02M26/10—Constructional details, e.g. structural combinations of EGR systems and supercharger systems; Arrangement of the EGR and supercharger systems with respect to the engine having means to increase the pressure difference between the exhaust and intake system, e.g. venturis, variable geometry turbines, check valves using pressure pulsations or throttles in the air intake or exhaust system
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- 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
- F02M26/14—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories in relation to the exhaust system
- F02M26/15—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories in relation to the exhaust system in relation to engine exhaust purifying apparatus
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- 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
- F02M26/22—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories with coolers in the recirculation passage
- F02M26/29—Constructional details of the coolers, e.g. pipes, plates, ribs, insulation or materials
- F02M26/31—Air-cooled heat exchangers
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- 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
- F02M26/52—Systems for actuating EGR valves
- F02M26/53—Systems for actuating EGR valves using electric actuators, e.g. solenoids
- F02M26/54—Rotary actuators, e.g. step motors
Definitions
- the present invention relates to a mixing device for a low pressure EGR system of an internal combustion engine.
- EGR exhaust Gas Recirculation
- An EGR (Exhaust Gas Recirculation) system is often present in modern internal combustion engines, which system feeds part of the exhaust gases produced by the combustion into the intake conduit so as to mix the exhaust gases with the fresh air in order to uniform the temperature in each combustion chamber, and consequently reduce the polluting substances present in the exhaust gases which are released into the atmosphere.
- An EGR system comprises an EGR conduit, which connects the exhaust conduit to the intake conduit, and a mixing device which is arranged at the intersection between the EGR conduit and the intake conduit, and which has the function of adjusting the mixing of exhaust gas from the exhaust conduit with the fresh air present in the intake conduit.
- the mixing device comprises a butterfly valve, which is arranged at the EGR conduit, is actuated by an electrical motor and has the function of varying the section of the EGR conduit to vary the flow of exhaust gases which are introduced into the intake conduit.
- the above-described structure of the mixing device has the advantage of being cost-effective and at the same of allowing to rather accurately adjust the exhaust gas flow rate introduced into the intake conduit; however, the above-described structure of the mixing device does not allow to accurately adjust the exhaust gas flow rate introduced into the intake conduit in all operative conditions, and in particular when the introduction of a particularly high exhaust gas flow rate into the intake conduit is required. Furthermore, the known mixing devices have problems of reliability over time, because the electrical motor may be subjected to excessive overheating caused by the heat coming from the EGR conduit, which in turn is heated by the exhaust gases which flow through the EGR conduit itself, and which indicatively have a temperature of at least 350-400 °C.
- US2005145229A1 describes a mixing device for a low pressure EGR system of an internal combustion engine as described in the preamble of independent claim 1.
- a mixing device for a low pressure EGR system of an internal combustion engine is provided as disclosed in the appended claims.
- numeral 1 indicates as a whole an internal combustion engine supercharged by a turbocharger supercharging system 2.
- the internal combustion engine 1 comprises four cylinders 3, each of which is connected to an intake manifold 4 by means of at least one respective intake valve (not shown) and to an exhaust manifold 5 by means of at least one respective exhaust valve (not shown).
- the intake manifold 4 receives fresh air (i.e. air coming from the external environment) through an intake conduit 6, which is provided with an air cleaner 7 and is adjusted by a butterfly valve 8.
- An intercooler 9 for cooling the intake air is arranged along the intake conduit 6.
- An exhaust conduit 10, which feeds the exhaust gases produced by the combustion to an exhaust system, is connected to the exhaust manifold 5, which exhaust system emits the gases produced by the combustion into the atmosphere and normally comprises at least one catalyzer 11 and at least one silencer (not shown) arranged downstream of the catalyzer 11.
- the supercharging system 2 of the internal combustion engine 1 comprises a turbocharger 12 provided with a turbine 13, which is arranged along the exhaust conduit 10 for rotating at high speed under the bias of the exhaust gases expelled from the cylinders 3, and a turbocharger 14, which is arranged along the intake conduit 6 and is mechanically connected to the turbine 13 in order to be rotatably fed by the turbine 13 itself so as to increase the pressure of the air fed into the intake conduit 6.
- a bypass conduit 15 is provided along the exhaust conduit 10, which bypass conduit is connected in parallel to the turbine 13 so that the ends thereof are connected upstream and downstream of the turbine 13 itself; a wastegate 16 is arranged along the bypass conduit 15, which wastegate is adapted to adjust the exhaust gas flow rate through the bypass conduit 15 and is controlled by a pneumatic actuator 17.
- a bypass conduit 18 is provided along the intake conduit 6, which bypass conduit is connected in parallel to the turbocharger 14 so that the ends thereof are connected upstream and downstream of the turbocharger 14 itself; a Poff valve 19 is arranged along the bypass conduit 18, which Poff valve is adapted to adjust the exhaust gases which flow through the bypass conduit 18 and is controlled by an electrical actuator 20.
- the internal combustion engine 1 comprises a low pressure EGR system 21, which recalculates part of the exhaust gas present in the exhaust conduit 10 by reintroducing such exhaust gases into the intake conduit 6.
- An EGR system 21 comprises an EGR conduit 22, which connects the exhaust conduit 10 to the intake conduit 6, and a three-way mixing device 23, which is arranged at the intersection between the exhaust conduit 10 and the intake conduit 6, and which has the function of adjusting the mixing of the exhaust gases from the exhaust conduit 10 with the fresh air present in the intake conduit 6.
- a heat exchanger 24 is arranged along the EGR conduit 22 for cooling the exhaust gases from the exhaust conduit 10.
- Such a configuration is also named “Long-Route" EGR, because the EGR conduit 22 must be longer than normal to reach downstream of the catalyzer 11.
- the three-way mixing device 23 connects the intake manifold 6 to the EGR conduit 22.
- the mixing device 23 comprises an inlet conduit 25, which is connected in series to the EGR conduit 22, an inlet conduit 26, which is connected in series to a conduit coming from the air cleaner 7, and an outlet conduit 27, which is connected in series to the intake conduit 6.
- the inlet conduit 25 forms a square angle with the outlet conduit 27 and forms an obtuse angle with the inlet conduit 26, and the inlet conduit 26 forms an acute angle with the outlet conduit 27.
- the main valve 28 comprises a butterfly cap 30 and a shaft 31, which supports the butterfly cap 30 and is rotationally mounted.
- the secondary butterfly valve 28 comprises a butterfly cap 32 and a shaft 33, which supports the butterfly cap 32 and is rotationally mounted.
- the mixing device 23 comprises a common actuating device 34 which controls both the main butterfly valve 28 and the secondary butterfly valve 29.
- the common actuating device 34 comprises a single common electrical motor 35, which impresses motion to both butterfly valves 28 and 29, and a connecting element 36, which establishes a mechanical connection between the secondary butterfly valve 29 and the main butterfly valve 28 so that the reciprocal positions between the two butterfly valves 28 and 29 are mechanically linked to one another.
- the common electrical motor 35 transmits motion to the main butterfly valve 28 and thus directly controls the position of the main butterfly valve 28 itself; in turn, the main butterfly valve 28 transmits motion to the secondary butterfly valve 29 by means of the connection element 36, which links the position of the main butterfly valve 28 to the position of the secondary butterfly valve 29.
- the main butterfly valve 28 acts as "master” valve when the secondary butterfly valve 29 acts as “slave” mimicking the position of the main butterfly valve 28 by virtue of the connecting element 36.
- the actuating device 34 comprises a gear transmission 37, which transmits motion from a shaft of the electrical motor 35 to the shaft 31 of the main butterfly valve 28.
- the gear transmission 37 comprises an initial toothed wheel 38, integral with the electrical motor shaft 35, a final toothed wheel 39, integral with the shaft 31 of the main butterfly valve 28, and an intermediate toothed wheel 40, idly interposed between the initial toothed wheel 38 integral with the shaft of the electrical motor 35 and the final toothed wheel 39 integral with the shaft 31 of the main butterfly valve 28.
- the intermediate toothed wheel 40 has a first small diameter teeth crown, which is coupled to the initial toothed wheel 38, and a second larger diameter teeth crown, which is coupled to the final toothed wheel 39.
- the geared transmission 37 has a transmission ratio which de-multiplies the rotation speed of the electrical motor 35 (i.e. the electrical motor 35 turns faster than the shaft 31 of the main butterfly valve 28).
- the connecting element 36 comprises a rigid arm 41 having one end 42, which is eccentrically connected to the shaft 31 of the main butterfly valve 28 and which is opposite to the end 42 and is eccentrically connected to the shaft 33 of the secondary butterfly valve 29.
- the end 43 of the arm 41 has an elongated seat 44, which is rotationally and slidingly engaged by an eccentric pin 45 which is integral with the shaft 33 of the secondary butterfly valve 29 and is supported by a plate 46 integral with the shaft 33 itself; furthermore, the end 42 of the arm 41 is eccentrically hinged to the shaft 31 of the main butterfly valve 28, and in particular is hinged to the final toothed wheel 39, which is integral with the shaft 31 itself.
- the rigid arm 41 has a first segment, which comprises the end 42, and a second segment, which comprises the end 43 and the elongated seat 44, is shorter than the first segment and forms an obtuse angle with the first segment.
- the connecting element 36 comprises a gear set, which links the angular position of the shaft 33 of the secondary butterfly valve 29 to the angular position of the shaft 31 of the main butterfly valve 28.
- the actuating device 34 imparts to the butterfly valves 28 and 29 a law of motion in which the main butterfly valve 28 is completely closed when the secondary butterfly valve 29 is completely open and vice versa; furthermore, the actuating device 34 keeps the secondary butterfly valve 29 all open until the main butterfly valve 28 does not reach a predetermined partial opening position.
- FIG 4 the pattern of the position (i.e. of the opening/closing degree) of the secondary butterfly valve 29 is shown by a dashed line and the pattern of the position (i.e. of the opening/closing degree) of the main butterfly valve 28 is shown with a solid line according to the position ⁇ of the shaft of the electrical motor 35 (shown in abscissa).
- the relationship between the position of the main butterfly valve 28 and the position of the secondary butterfly valve 29 can be easily modified by varying the conformation (shape and/or size) of the arm 41 of the connecting element 36; thus the relationship between the position of the main butterfly valve 28 and the position of the secondary butterfly valve 29 shown in figure 4 is only an example of the many relationships which can be obtained by means of the actuating device 34.
- the relationship between the position of the main butterfly valve 28 and the position of the secondary butterfly valve 29 may be easily modified, simply by varying the angle between the two segments of the arm 41 and/or by varying the length of the two segments of the arm 41. In this manner, with a simple modification of the arm 41 of the connecting element 36, it is possible to even substantially modify the mixing features of the exhaust gas present in the inlet conduit 25 with the fresh air in the inlet conduit 26.
- the actuating device 34 also comprises a return spring which tends to push the butterfly valves 28 and 29 towards a neutral position in which the secondary butterfly valve 29 is all open and the main butterfly valve 28 is all closed and thus in complete absence of exhaust gas recirculating in the intake conduit 6.
- the return spring guarantees that the butterfly valves 28 and 29 are moved and kept in neutral position free from recirculated exhaust gases in the intake conduit 6.
- the shaft 31 of the main butterfly valve 28 has an external portion 47, which protrudes from the inlet conduit 25 (through a through hole provided with a seal) to be coupled to the actuating device 34; similarly, the shaft 33 of the secondary butterfly valve 29 also has an external portion 48, which protrudes from the inlet conduit 26 (through a through hole provided with a seal) to couple to the actuating device 34.
- the actuating device 34 comprises a box 49, inside which the external portion 47 of the shaft 31 of the main butterfly valve 28 and the external portion 48 of the shaft 33 of the secondary butterfly valve 29 penetrate.
- the electrical motor 35 and the gear transmission 37 are further accommodated in the box 49.
- the box 49 is provided with a removable cover 50, which is provided with an annular seat for ensuring an adequate tightness. Furthermore, the box 49 has a cylindrical housing 51, which extends perpendicularly to a bottom wall 52 of the box 49 and accommodates the electric motor 35 therein. The bottom wall 52 of the box 49 has two through holes (not shown) for allowing the passage of the shafts 31 and 23 of the butterfly valves 28 and 29.
- the box 49 is only supported by the inlet conduit 26 (i.e. does not touch the inlet conduit 25 in any manner and is instead arranged at a given distance from the inlet conduit 25 itself). Furthermore, the box 49 is independent and separable from the inlet conduit 26 and is fixed to the inlet conduit 26 by means of screws.
- the heat of the inlet conduit 25 may be transmitted to the box 49 only by radiation or convection and not by conduction; the overheating of the box 49 can be limited in this manner.
- at least one part of the external portion 47 of the shaft 31 of the main butterfly valve 28 is made of a heat-insulating material; in particular, the external portion 47 of the shaft 31 of the main butterfly valve 28 comprises an insert 53 made of heat-insulating material, and in particular of refractory material (typically ceramic). It is worth noting that the insert 53 has the function of both heat insulation (i.e. of obstructing the transmission of heat by conduction along the shaft 31 and towards the box 49 and the gear transmission 37) and motion transmission (i.e. of transmitting rotation motion along the shaft 31 between butterfly cap 30 and gear transmission 37).
- the insert 53 made of heat-insulating material constitutes part of the external portion 47 of the shaft 31 of the main butterfly valve 28 and is arranged between two sections of the external portion 47 so as to thermally separate the two sections of the external portion 47 (i.e. preventing a heat transmission by conduction) maintaining a mechanical continuity of the shaft 31 to transmit the rotation movement along the shaft 31 between the butterfly cap 30 and the gear transmission 37.
- each fixed joint between the insert 53 and the section of the external portion 47 comprises a cross-shaped protuberance 54, which axially rises from the insert 53 and is inserted in a seat 55, which is obtained in the section of the external portion 47 which negatively reproduces the shape of the protuberance 54.
- the cylindrical housing 51 is provided with a plurality of cooling fins 56, which thermally connect a wall of the cylindrical housing 51 to a wall of the inlet conduit 26.
- each cooling fin 54 is radially arranged with respect to the cylindrical housing 51 and fully envelops the cylinder housing 51 itself.
- the inlet conduit 25 is provided with a plurality of cooling fins 57 preferably arranged axially (i.e. parallel to the central axis of the inlet conduit 25).
- the above-described mixing device 23 has many advantages.
- the above-described mixing device 23 is simple and cost-effective to make, because a single electrical motor 35 allows to suitably control both the main butterfly valve 28 and the secondary butterfly valve 29.
- modifying the mixing features of the exhaust gases in the EGR conduit 22 with the fresh air present in the intake conduit 6 is simple by modifying the relationship between the portion of the main butterfly valve 28 and the position of the secondary butterfly valve 29 by means of a simple replacement of the arm 41 of the connecting element 36 (arm 41 which has a very low replacement cost).
- the above-described mixing device 23 is very reliable over time, because the electrical motor 35 is adequately protected from excessive overheating essentially caused by the heat transmitted by the inlet conduit 25, which is heated by the exhaust gases which indicatively have a temperature of 350-400 °C.
- the thermal protection of the electrical motor 35 is obtained by creating a separation between the box 49 and the inlet conduit 25, by inserting the insert 53 made of heat-insulating material in the external portion 47 of the shaft 31 of the main butterfly valve 28, thus making the cooling fins 56 between the housing 51 and the inlet conduit 26 and making the cooling fins 57 of the inlet conduit 25.
- the mixing device 23 has a modular structure, because the actuating device 34 is completely contained in the box 49 which can be separated from the inlet conduits 25 and 26 and from the outlet conduit 27; in this manner, the box 49 itself (i.e. the actuating device 34 itself) may be fitted on conduits 25, 26 and 27 of variable size so as to make a wide range of mixing devices 23 which differ from one another by the active flow rate.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
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- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Exhaust-Gas Circulating Devices (AREA)
Abstract
Description
- The present invention relates to a mixing device for a low pressure EGR system of an internal combustion engine.
- An EGR (Exhaust Gas Recirculation) system is often present in modern internal combustion engines, which system feeds part of the exhaust gases produced by the combustion into the intake conduit so as to mix the exhaust gases with the fresh air in order to uniform the temperature in each combustion chamber, and consequently reduce the polluting substances present in the exhaust gases which are released into the atmosphere.
- An EGR system comprises an EGR conduit, which connects the exhaust conduit to the intake conduit, and a mixing device which is arranged at the intersection between the EGR conduit and the intake conduit, and which has the function of adjusting the mixing of exhaust gas from the exhaust conduit with the fresh air present in the intake conduit. Typically, the mixing device comprises a butterfly valve, which is arranged at the EGR conduit, is actuated by an electrical motor and has the function of varying the section of the EGR conduit to vary the flow of exhaust gases which are introduced into the intake conduit.
- The above-described structure of the mixing device has the advantage of being cost-effective and at the same of allowing to rather accurately adjust the exhaust gas flow rate introduced into the intake conduit; however, the above-described structure of the mixing device does not allow to accurately adjust the exhaust gas flow rate introduced into the intake conduit in all operative conditions, and in particular when the introduction of a particularly high exhaust gas flow rate into the intake conduit is required. Furthermore, the known mixing devices have problems of reliability over time, because the electrical motor may be subjected to excessive overheating caused by the heat coming from the EGR conduit, which in turn is heated by the exhaust gases which flow through the EGR conduit itself, and which indicatively have a temperature of at least 350-400 °C.
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US2005145229A1 describes a mixing device for a low pressure EGR system of an internal combustion engine as described in the preamble ofindependent claim 1. - It is the object of the present invention to provide a mixing device for a low pressure EGR system of an internal combustion engine, which device is free from the above-described drawbacks, and in particular, is easy and cost-effective to implement.
- According to the present invention, a mixing device for a low pressure EGR system of an internal combustion engine is provided as disclosed in the appended claims.
- The present invention will now be described with reference to the appended drawings, which illustrate a non-limitative embodiment thereof, in which:
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figure 1 is a diagrammatic view of a supercharged internal combustion engine provided with an EGR system using a mixing device made according to the present invention; -
figure 2 is a section view of the mixing device infigure 1 ; -
figure 3 is a view with parts removed for clarity of an actuating device of the mixing device infigure 1 ; -
figure 4 is a chart illustrating the positions of two butterfly valves of the mixing device infigure 1 ; -
figure 5 is a perspective view of the mixing device infigure 1 ; -
figures 6 and7 are two different perspective, exploded views of the mixing device infigure 1 ; and -
figure 8 is a perspective view of an insert made of refractory material arranged along a shaft of a main butterfly valve of the mixing device infigure 1 . - In
figure 1 ,numeral 1 indicates as a whole an internal combustion engine supercharged by aturbocharger supercharging system 2. - The
internal combustion engine 1 comprises four cylinders 3, each of which is connected to anintake manifold 4 by means of at least one respective intake valve (not shown) and to an exhaust manifold 5 by means of at least one respective exhaust valve (not shown). Theintake manifold 4 receives fresh air (i.e. air coming from the external environment) through anintake conduit 6, which is provided with anair cleaner 7 and is adjusted by a butterfly valve 8. An intercooler 9 for cooling the intake air is arranged along theintake conduit 6. Anexhaust conduit 10, which feeds the exhaust gases produced by the combustion to an exhaust system, is connected to the exhaust manifold 5, which exhaust system emits the gases produced by the combustion into the atmosphere and normally comprises at least onecatalyzer 11 and at least one silencer (not shown) arranged downstream of thecatalyzer 11. - The
supercharging system 2 of theinternal combustion engine 1 comprises aturbocharger 12 provided with aturbine 13, which is arranged along theexhaust conduit 10 for rotating at high speed under the bias of the exhaust gases expelled from the cylinders 3, and aturbocharger 14, which is arranged along theintake conduit 6 and is mechanically connected to theturbine 13 in order to be rotatably fed by theturbine 13 itself so as to increase the pressure of the air fed into theintake conduit 6. - A
bypass conduit 15 is provided along theexhaust conduit 10, which bypass conduit is connected in parallel to theturbine 13 so that the ends thereof are connected upstream and downstream of theturbine 13 itself; awastegate 16 is arranged along thebypass conduit 15, which wastegate is adapted to adjust the exhaust gas flow rate through thebypass conduit 15 and is controlled by apneumatic actuator 17. Abypass conduit 18 is provided along theintake conduit 6, which bypass conduit is connected in parallel to theturbocharger 14 so that the ends thereof are connected upstream and downstream of theturbocharger 14 itself; aPoff valve 19 is arranged along thebypass conduit 18, which Poff valve is adapted to adjust the exhaust gases which flow through thebypass conduit 18 and is controlled by anelectrical actuator 20. - The
internal combustion engine 1 comprises a lowpressure EGR system 21, which recalculates part of the exhaust gas present in theexhaust conduit 10 by reintroducing such exhaust gases into theintake conduit 6. AnEGR system 21 comprises anEGR conduit 22, which connects theexhaust conduit 10 to theintake conduit 6, and a three-way mixing device 23, which is arranged at the intersection between theexhaust conduit 10 and theintake conduit 6, and which has the function of adjusting the mixing of the exhaust gases from theexhaust conduit 10 with the fresh air present in theintake conduit 6. According to a preferred embodiment, aheat exchanger 24 is arranged along the EGRconduit 22 for cooling the exhaust gases from theexhaust conduit 10. - The low
pressure EGR system 21, i.e. the EGRconduit 22, originates from theexhaust conduit 10 downstream of thecatalyzer 11 so as to take the exhaust gases which have been already treated by thecatalyzer 11 itself and which have a pressure only slightly higher than the atmospheric pressure; in this manner, the exhaust gases recirculated by theEGR conduit 22 are more "clean", i.e. have a lower content of polluting substances. Such a configuration is also named "Long-Route" EGR, because the EGRconduit 22 must be longer than normal to reach downstream of thecatalyzer 11. - The three-
way mixing device 23 connects theintake manifold 6 to theEGR conduit 22. As shown in greater detail infigure 2 , themixing device 23 comprises aninlet conduit 25, which is connected in series to the EGRconduit 22, aninlet conduit 26, which is connected in series to a conduit coming from theair cleaner 7, and anoutlet conduit 27, which is connected in series to theintake conduit 6. - As shown in
figure 3 , theinlet conduit 25 forms a square angle with theoutlet conduit 27 and forms an obtuse angle with theinlet conduit 26, and theinlet conduit 26 forms an acute angle with theoutlet conduit 27. Amain butterfly valve 28, which varies the section of theinlet conduit 25 itself, is arranged along theinlet conduit 25, and asecondary butterfly valve 26, which varies the section of theinlet conduit 26 itself, is arranged along theinlet conduit 26. Themain valve 28 comprises abutterfly cap 30 and ashaft 31, which supports thebutterfly cap 30 and is rotationally mounted. Similarly, thesecondary butterfly valve 28 comprises abutterfly cap 32 and ashaft 33, which supports thebutterfly cap 32 and is rotationally mounted. - As shown in
figure 3 , themixing device 23 comprises acommon actuating device 34 which controls both themain butterfly valve 28 and thesecondary butterfly valve 29. In particular, thecommon actuating device 34 comprises a single commonelectrical motor 35, which impresses motion to bothbutterfly valves element 36, which establishes a mechanical connection between thesecondary butterfly valve 29 and themain butterfly valve 28 so that the reciprocal positions between the twobutterfly valves - According to a preferred embodiment, the common
electrical motor 35 transmits motion to themain butterfly valve 28 and thus directly controls the position of themain butterfly valve 28 itself; in turn, themain butterfly valve 28 transmits motion to thesecondary butterfly valve 29 by means of theconnection element 36, which links the position of themain butterfly valve 28 to the position of thesecondary butterfly valve 29. In other words, themain butterfly valve 28 acts as "master" valve when thesecondary butterfly valve 29 acts as "slave" mimicking the position of themain butterfly valve 28 by virtue of the connectingelement 36. In particular, theactuating device 34 comprises agear transmission 37, which transmits motion from a shaft of theelectrical motor 35 to theshaft 31 of themain butterfly valve 28. - The
gear transmission 37 comprises aninitial toothed wheel 38, integral with theelectrical motor shaft 35, afinal toothed wheel 39, integral with theshaft 31 of themain butterfly valve 28, and an intermediatetoothed wheel 40, idly interposed between the initialtoothed wheel 38 integral with the shaft of theelectrical motor 35 and the finaltoothed wheel 39 integral with theshaft 31 of themain butterfly valve 28. The intermediatetoothed wheel 40 has a first small diameter teeth crown, which is coupled to the initialtoothed wheel 38, and a second larger diameter teeth crown, which is coupled to the finaltoothed wheel 39. As a whole, the gearedtransmission 37 has a transmission ratio which de-multiplies the rotation speed of the electrical motor 35 (i.e. theelectrical motor 35 turns faster than theshaft 31 of the main butterfly valve 28). - According to a preferred embodiment shown in the appended figures, the connecting
element 36 comprises arigid arm 41 having oneend 42, which is eccentrically connected to theshaft 31 of themain butterfly valve 28 and which is opposite to theend 42 and is eccentrically connected to theshaft 33 of thesecondary butterfly valve 29. Theend 43 of thearm 41 has anelongated seat 44, which is rotationally and slidingly engaged by aneccentric pin 45 which is integral with theshaft 33 of thesecondary butterfly valve 29 and is supported by aplate 46 integral with theshaft 33 itself; furthermore, theend 42 of thearm 41 is eccentrically hinged to theshaft 31 of themain butterfly valve 28, and in particular is hinged to the finaltoothed wheel 39, which is integral with theshaft 31 itself. Therigid arm 41 has a first segment, which comprises theend 42, and a second segment, which comprises theend 43 and theelongated seat 44, is shorter than the first segment and forms an obtuse angle with the first segment. According to a different embodiment (not shown), the connectingelement 36 comprises a gear set, which links the angular position of theshaft 33 of thesecondary butterfly valve 29 to the angular position of theshaft 31 of themain butterfly valve 28. - In the illustrated embodiment, the
actuating device 34 imparts to thebutterfly valves 28 and 29 a law of motion in which themain butterfly valve 28 is completely closed when thesecondary butterfly valve 29 is completely open and vice versa; furthermore, the actuatingdevice 34 keeps thesecondary butterfly valve 29 all open until themain butterfly valve 28 does not reach a predetermined partial opening position. The description above is illustrated infigure 4 , in which the pattern of the position (i.e. of the opening/closing degree) of thesecondary butterfly valve 29 is shown by a dashed line and the pattern of the position (i.e. of the opening/closing degree) of themain butterfly valve 28 is shown with a solid line according to the position α of the shaft of the electrical motor 35 (shown in abscissa). Infigure 4 , it is apparent that themain butterfly valve 28 is all closed when thesecondary butterfly valve 29 is all open and vice versa; furthermore, thesecondary butterfly valve 29 remains all open until a predetermined partial opening position of themain butterfly valve 28 is reached and starts to close only afterwards. - It is important to observe that the relationship between the position of the
main butterfly valve 28 and the position of thesecondary butterfly valve 29 can be easily modified by varying the conformation (shape and/or size) of thearm 41 of the connectingelement 36; thus the relationship between the position of themain butterfly valve 28 and the position of thesecondary butterfly valve 29 shown infigure 4 is only an example of the many relationships which can be obtained by means of theactuating device 34. For example, the relationship between the position of themain butterfly valve 28 and the position of thesecondary butterfly valve 29 may be easily modified, simply by varying the angle between the two segments of thearm 41 and/or by varying the length of the two segments of thearm 41. In this manner, with a simple modification of thearm 41 of theconnecting element 36, it is possible to even substantially modify the mixing features of the exhaust gas present in theinlet conduit 25 with the fresh air in theinlet conduit 26. - According to a possible embodiment (not shown), the actuating
device 34 also comprises a return spring which tends to push thebutterfly valves secondary butterfly valve 29 is all open and themain butterfly valve 28 is all closed and thus in complete absence of exhaust gas recirculating in theintake conduit 6. In case of malfunction of theelectrical motor 35, the return spring guarantees that thebutterfly valves intake conduit 6. - As shown in
figure 6 , theshaft 31 of themain butterfly valve 28 has anexternal portion 47, which protrudes from the inlet conduit 25 (through a through hole provided with a seal) to be coupled to the actuatingdevice 34; similarly, theshaft 33 of thesecondary butterfly valve 29 also has anexternal portion 48, which protrudes from the inlet conduit 26 (through a through hole provided with a seal) to couple to the actuatingdevice 34. Theactuating device 34 comprises abox 49, inside which theexternal portion 47 of theshaft 31 of themain butterfly valve 28 and theexternal portion 48 of theshaft 33 of thesecondary butterfly valve 29 penetrate. Theelectrical motor 35 and thegear transmission 37 are further accommodated in thebox 49. Thebox 49 is provided with aremovable cover 50, which is provided with an annular seat for ensuring an adequate tightness. Furthermore, thebox 49 has acylindrical housing 51, which extends perpendicularly to abottom wall 52 of thebox 49 and accommodates theelectric motor 35 therein. Thebottom wall 52 of thebox 49 has two through holes (not shown) for allowing the passage of theshafts butterfly valves - According to a preferred embodiment, the
box 49 is only supported by the inlet conduit 26 (i.e. does not touch theinlet conduit 25 in any manner and is instead arranged at a given distance from theinlet conduit 25 itself). Furthermore, thebox 49 is independent and separable from theinlet conduit 26 and is fixed to theinlet conduit 26 by means of screws. - By virtue of the fact that the
box 49 is separate from theinlet conduit 25, the heat of theinlet conduit 25 may be transmitted to thebox 49 only by radiation or convection and not by conduction; the overheating of thebox 49 can be limited in this manner. In order to further reduce the transmission of heat from theinlet conduit 25 to thebox 49 and to thegear transmission 37, at least one part of theexternal portion 47 of theshaft 31 of themain butterfly valve 28 is made of a heat-insulating material; in particular, theexternal portion 47 of theshaft 31 of themain butterfly valve 28 comprises aninsert 53 made of heat-insulating material, and in particular of refractory material (typically ceramic). It is worth noting that theinsert 53 has the function of both heat insulation (i.e. of obstructing the transmission of heat by conduction along theshaft 31 and towards thebox 49 and the gear transmission 37) and motion transmission (i.e. of transmitting rotation motion along theshaft 31 betweenbutterfly cap 30 and gear transmission 37). - As shown in
figure 8 , theinsert 53 made of heat-insulating material constitutes part of theexternal portion 47 of theshaft 31 of themain butterfly valve 28 and is arranged between two sections of theexternal portion 47 so as to thermally separate the two sections of the external portion 47 (i.e. preventing a heat transmission by conduction) maintaining a mechanical continuity of theshaft 31 to transmit the rotation movement along theshaft 31 between thebutterfly cap 30 and thegear transmission 37. The heat-insulatingmaterial insert 53 is mechanically fitted on both sides of the corresponding sections of theexternal portion 47; the fixed joints between theinsert 53 and the two sections of theexternal portion 47 also have an angular bond so as to prevent the relative rotation between theinsert 53 and the two sections of theexternal portion 47 to transmit rotary movement along theshaft 31 between thebutterfly cap 30 and thegear transmission 37. According to the embodiment shown infigure 8 , each fixed joint between theinsert 53 and the section of theexternal portion 47 comprises across-shaped protuberance 54, which axially rises from theinsert 53 and is inserted in aseat 55, which is obtained in the section of theexternal portion 47 which negatively reproduces the shape of theprotuberance 54. - As shown in
figures 5 ,6 and7 , in order to increase the cooling of the electrical motor 35 (which is heated both by effect of the heat from theinlet conduit 25 and by effect of the heat generated in use within theelectrical motor 35 itself), thecylindrical housing 51 is provided with a plurality of coolingfins 56, which thermally connect a wall of thecylindrical housing 51 to a wall of theinlet conduit 26. In particular, each coolingfin 54 is radially arranged with respect to thecylindrical housing 51 and fully envelops thecylinder housing 51 itself. - Furthermore, in order to attempt to cool the
inlet conduit 25 in proximity of thebox 49 in order to reduce the transmission of heat from theinlet conduit 25 to the box 49 (and thus to thegear transmission 37, and above all to electric motor 35), theinlet conduit 25 is provided with a plurality of coolingfins 57 preferably arranged axially (i.e. parallel to the central axis of the inlet conduit 25). - The above-described
mixing device 23 has many advantages. - Firstly, the above-described
mixing device 23 is simple and cost-effective to make, because a singleelectrical motor 35 allows to suitably control both themain butterfly valve 28 and thesecondary butterfly valve 29. - Furthermore, by virtue of the presence of the
main butterfly valve 28 along theinlet conduit 25 and of thesecondary butterfly valve 29 along theinlet conduit 26, it is possible to always optimally adjust the mixing of the fresh air present in theinlet conduit 26 with the exhaust gases present in theinlet conduit 25. In particular, by either completely closing or nearly closing thesecondary butterfly valve 29, a particularly high exhaust gas flow rate can be introduced into theintake conduit 6, and always adjustable with extreme accuracy. - In the above-described
mixing device 23, modifying the mixing features of the exhaust gases in theEGR conduit 22 with the fresh air present in theintake conduit 6 is simple by modifying the relationship between the portion of themain butterfly valve 28 and the position of thesecondary butterfly valve 29 by means of a simple replacement of thearm 41 of the connecting element 36 (arm 41 which has a very low replacement cost). - The above-described
mixing device 23 is very reliable over time, because theelectrical motor 35 is adequately protected from excessive overheating essentially caused by the heat transmitted by theinlet conduit 25, which is heated by the exhaust gases which indicatively have a temperature of 350-400 °C. The thermal protection of theelectrical motor 35 is obtained by creating a separation between thebox 49 and theinlet conduit 25, by inserting theinsert 53 made of heat-insulating material in theexternal portion 47 of theshaft 31 of themain butterfly valve 28, thus making the coolingfins 56 between thehousing 51 and theinlet conduit 26 and making the coolingfins 57 of theinlet conduit 25. - Finally, the mixing
device 23 has a modular structure, because theactuating device 34 is completely contained in thebox 49 which can be separated from theinlet conduits outlet conduit 27; in this manner, thebox 49 itself (i.e. theactuating device 34 itself) may be fitted onconduits devices 23 which differ from one another by the active flow rate.
Claims (15)
- A mixing device (23) for a low pressure EGR system (21) of an internal combustion engine; the mixing device (23) comprises:a first inlet conduit (25), which can be connected to an EGR conduit (22);a second inlet conduit (26), which can be connected to an intake of fresh air from outside;an outlet conduit (27), which can be connected to an intake conduit (6);a main butterfly valve (28), which is arranged within the first inlet conduit (25) to vary the section of the first inlet conduit (25);a secondary butterfly valve (29), which is arranged within the second inlet conduit (26) to vary the section of the second inlet conduit (26); andan actuating device (34), which controls the main butterfly valve (28) and the secondary butterfly valve (29) and is provided with a connecting element (36), which establishes a mechanical connection between the main butterfly valve (28) and the secondary butterfly valve (29), so that the positions of two butterfly valves (28, 29) are mechanically linked to one another;wherein the main butterfly valve (28) comprises a first butterfly cap (30) and a first shaft (31) that supports the first butterfly cap (30) and has a first external portion (47) protruding from the first inlet conduit (25) to mate with the actuating device (34);
wherein the secondary butterfly valve (29) comprises a second butterfly cap (32) and a second shaft (33) supporting the second butterfly cap (32) and has a second external portion (48) which protrudes from the second inlet conduit (26) to mate with the actuating device (34); and
wherein the actuating device (34) comprises a box (49), in which the first external portion (47) of the first shaft (31) of the main butterfly valve (28) and the second external portion (48) of the second shaft (33) of the secondary butterfly valve (29) penetrate, and an electric motor (35) which is inserted in a cylindrical housing (51) of the box (49);
the mixing device (23) is characterized in that:the actuating device (34) comprises single common electrical motor (35), which is inserted in an cylindrical housing (51) of the box (49); andthe cylindrical housing (51) is fitted with a plurality of first cooling fins (56), which thermally connect a wall of the cylindrical housing (51) to a wall of the second inlet conduit (26). - A mixing device (23) according to claim 1, wherein the connecting element (36) comprises a rigid arm (41) having a first end (43) eccentrically connected to a second shaft (33) of the secondary butterfly valve (29), and a second end (42) which is opposite to the first end (43) and is eccentrically connected to a first shaft (31) of the main butterfly valve (28).
- A mixing device (23) according to claim 2, wherein:the first end (43) of the arm (41) has an elongated seat (44), which is rotationally and slidingly engaged by an eccentric pin (45) integral with the second shaft (31) of the main butterfly valve (28); andthe first end (42) of the arm (41) is eccentrically hinged to the first shaft (31) of the main butterfly valve (28).
- A mixing device (23) according to claim 3, wherein the rigid arm (41) has a first segment comprising the first end (43) and the elongated seat (44), and a second segment comprising the second end (42); the second segment is longer than the first segment, and forms an obtuse angle with the first segment.
- A mixing device (23) according to claims 2, 3 or 4, wherein by changing the conformation of the arm (41) of the connecting element (36) it is possible to change the relationship between the position of the main butterfly valve (28) and the position of the secondary butterfly valve (29) in order to change the mixing features of the exhaust gases in first inlet conduit (25) with fresh air in the second inlet conduit (26).
- A mixing device (23) according to one of claims 1 to 5, wherein by virtue of the effect of the actuating device (34) the secondary butterfly valve (29) is fully open when the main butterfly valve (28) is fully closed and vice versa.
- A mixing device (23) according to claim 6, wherein the actuating device (34) keeps the secondary butterfly valve (29) fully open until the main butterfly valve (28) reaches a predetermined partial opening position.
- A mixing device (23) according to one of claims 1 to 7, wherein the main butterfly valve (28) comprises a first butterfly cap (30) and a first shaft (31) supporting the first butterfly cap (30) and has a first external portion (47) which protrudes from the first inlet conduit (25) in order to mate with the actuating device (34); at least part of the first external portion (47) of the first shaft (31) of the main butterfly valve (28) is made of thermally insulating material.
- A mixing device (23) according to claim 8, wherein the first external portion (47) of the first shaft (31) of the main butterfly valve (28) comprises an insert (53) made of heat-insulating material, and in particular, refractory material.
- A mixing device (23) according to claim 9, wherein the insert (53) made of heat-insulating material is a part of the first external portion (47) of the first shaft (31) of the main butterfly valve (28) and is interposed between two sections of the first external portion (47) in order to thermally separate the two sections of the first external portion (47) maintaining mechanical continuity on the first shaft (33).
- A mixing device (23) according to claim 10 wherein the insert (53) made of heat-insulating material mechanically fits in the corresponding sections of the first external portion (47) on both sides by means of fixed joints, which also have an angular bond so as to prevent the relative rotation between the insert (53) and the two sections of the first external portion (47) to transmit the rotational movement along the first shaft (31).
- A mixing device (23) according to one of claims from 1 to 11, wherein the box (49) is supported by the second inlet conduit (26) only.
- A mixing device (23) according to claim 12, wherein the box (49) is independent and separable from the second inlet conduit (26) and is fixed to the second inlet conduit (26) by means of screws.
- A mixing device (23) according to one of claims from 1 to 13, wherein each first cooling fin (56) is arranged radially with respect to the cylindrical housing (51) and fully envelops the cylindrical housing (51) itself.
- A mixing device (23) according to one of claims from 1 to 14, wherein the first inlet conduit (25) is provided with a plurality of second cooling fins (57) preferably in axial arrangement.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT000702A ITBO20090702A1 (en) | 2009-10-28 | 2009-10-28 | MIXER DEVICE FOR A LOW-PRESSURE ENGINE EGR SYSTEM WITH INTERNAL COMBUSTION |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2317111A1 true EP2317111A1 (en) | 2011-05-04 |
EP2317111B1 EP2317111B1 (en) | 2012-03-21 |
Family
ID=42077045
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10189227A Not-in-force EP2317111B1 (en) | 2009-10-28 | 2010-10-28 | Mixing device for a low pressure EGR system of an internal combustion engine |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2317111B1 (en) |
AT (1) | ATE550541T1 (en) |
IT (1) | ITBO20090702A1 (en) |
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EP2497921A1 (en) * | 2011-03-08 | 2012-09-12 | Delphi Automotive Systems Luxembourg SA | Throttle valve assembly |
DE102012101767A1 (en) * | 2012-03-02 | 2013-09-05 | Pierburg Gmbh | Internal combustion engine |
WO2013127763A1 (en) * | 2012-02-29 | 2013-09-06 | Continental Automotive Gmbh | Mixing valve of an internal combustion engine |
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FR3007071A1 (en) * | 2013-06-17 | 2014-12-19 | Peugeot Citroen Automobiles Sa | THERMAL MOTOR WITH COMMON ACTUATOR FOR EGR VALVE AND AIR VALVE |
US9080506B2 (en) | 2013-08-13 | 2015-07-14 | Ford Global Technologies, Llc | Methods and systems for boost control |
US9091202B2 (en) | 2013-08-13 | 2015-07-28 | Ford Global Technologies, Llc | Methods and systems for boost control |
US9109505B2 (en) | 2013-08-13 | 2015-08-18 | Ford Global Technologies, Llc | Methods and systems for condensation control |
US9151219B2 (en) | 2013-08-13 | 2015-10-06 | Ford Global Technologies, Llc | Methods and systems for surge control |
US9174637B2 (en) | 2013-08-13 | 2015-11-03 | Ford Global Technologies, Llc | Methods and systems for torque control |
WO2016012401A1 (en) * | 2014-07-25 | 2016-01-28 | Continental Automotive Gmbh | Valve device for a motor vehicle |
US9261051B2 (en) | 2013-08-13 | 2016-02-16 | Ford Global Technologies, Llc | Methods and systems for boost control |
US9279374B2 (en) | 2013-08-13 | 2016-03-08 | Ford Global Technologies, Llc | Methods and systems for surge control |
US9303557B2 (en) | 2013-08-13 | 2016-04-05 | Ford Global Technologies, Llc | Methods and systems for EGR control |
US9309836B2 (en) | 2013-08-13 | 2016-04-12 | Ford Global Technologies, Llc | Methods and systems for boost control |
US9309837B2 (en) | 2013-08-13 | 2016-04-12 | Ford Global Technologies, Llc | Methods and systems for EGR control |
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US9682685B2 (en) | 2013-08-13 | 2017-06-20 | Ford Global Technologies, Llc | Methods and systems for condensation control |
US9759135B2 (en) | 2014-04-04 | 2017-09-12 | Ford Global Technologies, Llc | Method and system for engine control |
KR20180039143A (en) * | 2015-09-07 | 2018-04-17 | 닛산 지도우샤 가부시키가이샤 | Exhaust recirculation control method and exhaust recirculation control device |
US10018157B2 (en) | 2013-03-14 | 2018-07-10 | Ford Global Technologies, Llc | Methods and systems for boost control |
FR3067062A1 (en) * | 2017-06-01 | 2018-12-07 | Peugeot Citroen Automobiles Sa | METHOD FOR CONTROLLING FLOW RATE OF AIR ASSAY MEANS AND BURNED GAS MEANS RECIRCULATED IN A MOTORPROOF GROUP |
EP3569847A4 (en) * | 2017-01-16 | 2019-12-25 | Nissan Motor Co., Ltd. | Method for controlling internal combustion engine and device for controlling internal combustion engine |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014106517A1 (en) | 2014-05-09 | 2015-11-12 | Pierburg Gmbh | Exhaust gas turbocharger with a wastegate valve |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2722927A (en) * | 1952-10-29 | 1955-11-08 | George W Cornelius | Apparatus for controlling internal combustion engine fuel mixtures |
JPS5252028A (en) * | 1975-10-24 | 1977-04-26 | Toyota Motor Corp | Internal engine exhaust recycling device |
US4960096A (en) * | 1988-11-18 | 1990-10-02 | Showa Aluminum Corporation | Adapter for intake manifold |
EP1270905A2 (en) * | 2001-06-28 | 2003-01-02 | Delphi Technologies, Inc. | Manifold inlet valve having linear response |
US20050145229A1 (en) | 1998-11-09 | 2005-07-07 | Stt Emtec Ab Ltd. | Method and device for an EGR-system and a valve as well as a regulation method and device |
US20050241702A1 (en) * | 2004-03-26 | 2005-11-03 | Stt Emtec Ab | Valve device |
JP2006214405A (en) * | 2005-02-07 | 2006-08-17 | Hitachi Ltd | Exhaust gas circulating device for internal combustion engine, and valve module for internal combustion engine |
US7320220B1 (en) * | 2006-12-15 | 2008-01-22 | Caterpillar Inc. | EGR valve having integrated motor, controller, and flow meter |
FR2926114A1 (en) * | 2008-01-03 | 2009-07-10 | Valeo Sys Controle Moteur Sas | EGR LOOP OF AN INTERNAL COMBUSTION ENGINE OF A MOTOR VEHICLE |
EP2085601A1 (en) * | 2008-02-04 | 2009-08-05 | Kamtec Inc. | Exhaust gas recirculation valve for vehicle |
-
2009
- 2009-10-28 IT IT000702A patent/ITBO20090702A1/en unknown
-
2010
- 2010-10-28 EP EP10189227A patent/EP2317111B1/en not_active Not-in-force
- 2010-10-28 AT AT10189227T patent/ATE550541T1/en active
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2722927A (en) * | 1952-10-29 | 1955-11-08 | George W Cornelius | Apparatus for controlling internal combustion engine fuel mixtures |
JPS5252028A (en) * | 1975-10-24 | 1977-04-26 | Toyota Motor Corp | Internal engine exhaust recycling device |
US4960096A (en) * | 1988-11-18 | 1990-10-02 | Showa Aluminum Corporation | Adapter for intake manifold |
US20050145229A1 (en) | 1998-11-09 | 2005-07-07 | Stt Emtec Ab Ltd. | Method and device for an EGR-system and a valve as well as a regulation method and device |
EP1270905A2 (en) * | 2001-06-28 | 2003-01-02 | Delphi Technologies, Inc. | Manifold inlet valve having linear response |
US20050241702A1 (en) * | 2004-03-26 | 2005-11-03 | Stt Emtec Ab | Valve device |
JP2006214405A (en) * | 2005-02-07 | 2006-08-17 | Hitachi Ltd | Exhaust gas circulating device for internal combustion engine, and valve module for internal combustion engine |
US7320220B1 (en) * | 2006-12-15 | 2008-01-22 | Caterpillar Inc. | EGR valve having integrated motor, controller, and flow meter |
FR2926114A1 (en) * | 2008-01-03 | 2009-07-10 | Valeo Sys Controle Moteur Sas | EGR LOOP OF AN INTERNAL COMBUSTION ENGINE OF A MOTOR VEHICLE |
EP2085601A1 (en) * | 2008-02-04 | 2009-08-05 | Kamtec Inc. | Exhaust gas recirculation valve for vehicle |
Cited By (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2012119797A1 (en) * | 2011-03-08 | 2012-09-13 | Delphi Automotive Systems Luxembourg Sa | Throttle valve assembly |
US9689308B2 (en) | 2011-03-08 | 2017-06-27 | Delphi International Operations Luxembourg S.A.R.L | Throttle valve assembly |
EP2497921A1 (en) * | 2011-03-08 | 2012-09-12 | Delphi Automotive Systems Luxembourg SA | Throttle valve assembly |
WO2013127763A1 (en) * | 2012-02-29 | 2013-09-06 | Continental Automotive Gmbh | Mixing valve of an internal combustion engine |
CN104136759B (en) * | 2012-02-29 | 2016-11-30 | 大陆汽车有限责任公司 | The mixing valve of internal combustion engine |
US9765732B2 (en) | 2012-02-29 | 2017-09-19 | Continental Automotive Gmbh | Mixing valve of an internal combustion engine |
JP2015510980A (en) * | 2012-02-29 | 2015-04-13 | コンチネンタル オートモーティヴ ゲゼルシャフト ミット ベシュレンクテル ハフツングContinental Automotive GmbH | Mixing valve for internal combustion engine |
CN104136759A (en) * | 2012-02-29 | 2014-11-05 | 大陆汽车有限责任公司 | Mixing valve of an internal combustion engine |
KR20140134654A (en) * | 2012-02-29 | 2014-11-24 | 콘티넨탈 오토모티브 게엠베하 | Mixing valve of an internal combustion engine |
DE102012101767B4 (en) * | 2012-03-02 | 2015-01-08 | Pierburg Gmbh | Internal combustion engine |
DE102012101767A1 (en) * | 2012-03-02 | 2013-09-05 | Pierburg Gmbh | Internal combustion engine |
WO2013167423A1 (en) * | 2012-05-09 | 2013-11-14 | Continental Automotive Gmbh | Mixing valve of an internal combustion engine |
US9771898B2 (en) | 2012-05-09 | 2017-09-26 | Continental Automotive Gmbh | Mixing valve of an internal combustion engine |
EP2662556A1 (en) * | 2012-05-09 | 2013-11-13 | Continental Automotive GmbH | Mixing valve of a combustion engine |
JP2015523492A (en) * | 2012-05-15 | 2015-08-13 | ヴァレオ システム ドゥ コントロール モトゥール | Two-channel metering device and its use |
FR2990726A1 (en) * | 2012-05-15 | 2013-11-22 | Valeo Sys Controle Moteur Sas | TWO-WAY DOSER AND APPLICATIONS OF THE SAME |
WO2013171413A1 (en) * | 2012-05-15 | 2013-11-21 | Valeo Systemes De Controle Moteur | Two-way metering device and applications of said metering device |
WO2014095520A1 (en) * | 2012-12-21 | 2014-06-26 | Continental Automotive Gmbh | Valve |
US9777848B2 (en) | 2012-12-21 | 2017-10-03 | Continental Automotive Gmbh | Common motor driven dual butterfly valves |
CN104884781A (en) * | 2012-12-21 | 2015-09-02 | 大陆汽车有限责任公司 | Valve |
US10018157B2 (en) | 2013-03-14 | 2018-07-10 | Ford Global Technologies, Llc | Methods and systems for boost control |
FR3007071A1 (en) * | 2013-06-17 | 2014-12-19 | Peugeot Citroen Automobiles Sa | THERMAL MOTOR WITH COMMON ACTUATOR FOR EGR VALVE AND AIR VALVE |
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WO2016012401A1 (en) * | 2014-07-25 | 2016-01-28 | Continental Automotive Gmbh | Valve device for a motor vehicle |
KR20180039143A (en) * | 2015-09-07 | 2018-04-17 | 닛산 지도우샤 가부시키가이샤 | Exhaust recirculation control method and exhaust recirculation control device |
EP3348818A4 (en) * | 2015-09-07 | 2018-09-12 | Nissan Motor Co., Ltd. | Exhaust gas recirculation control method and exhaust gas recirculation control device |
US10634075B2 (en) | 2015-09-07 | 2020-04-28 | Nissan Motor Co., Ltd. | Exhaust gas recirculation control method and exhaust gas recirculation control device |
EP3569847A4 (en) * | 2017-01-16 | 2019-12-25 | Nissan Motor Co., Ltd. | Method for controlling internal combustion engine and device for controlling internal combustion engine |
RU2721070C1 (en) * | 2017-01-16 | 2020-05-15 | Ниссан Мотор Ко., Лтд. | Control method for internal combustion engine and control device for internal combustion engine |
FR3067062A1 (en) * | 2017-06-01 | 2018-12-07 | Peugeot Citroen Automobiles Sa | METHOD FOR CONTROLLING FLOW RATE OF AIR ASSAY MEANS AND BURNED GAS MEANS RECIRCULATED IN A MOTORPROOF GROUP |
Also Published As
Publication number | Publication date |
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ITBO20090702A1 (en) | 2011-04-28 |
EP2317111B1 (en) | 2012-03-21 |
ATE550541T1 (en) | 2012-04-15 |
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