WO2012099146A1 - 過給機およびこれを備えたディーゼル機関 - Google Patents
過給機およびこれを備えたディーゼル機関 Download PDFInfo
- Publication number
- WO2012099146A1 WO2012099146A1 PCT/JP2012/050911 JP2012050911W WO2012099146A1 WO 2012099146 A1 WO2012099146 A1 WO 2012099146A1 JP 2012050911 W JP2012050911 W JP 2012050911W WO 2012099146 A1 WO2012099146 A1 WO 2012099146A1
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- WO
- WIPO (PCT)
- Prior art keywords
- mixing member
- air
- side wall
- exhaust gas
- diesel engine
- 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.)
- Ceased
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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
- 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
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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
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
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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
-
- 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
- F02M26/02—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
-
- 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
- F02M26/19—Means for improving the mixing of air and recirculated exhaust gases, e.g. venturis or multiple openings to the intake system
-
- 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
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
- F02M35/1205—Flow throttling or guiding
- F02M35/1216—Flow throttling or guiding by using a plurality of holes, slits, protrusions, perforations, ribs or the like; Surface structures; Turbulence generators
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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
- F02M35/00—Combustion-air cleaners, air intakes, intake silencers, or induction systems specially adapted for, or arranged on, internal-combustion engines
- F02M35/12—Intake silencers ; Sound modulation, transmission or amplification
- F02M35/1288—Intake silencers ; Sound modulation, transmission or amplification combined with or integrated into other devices ; Plurality of air intake silencers
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to a supercharger and a diesel engine equipped with the same, and in particular, exhaust gas from a marine diesel engine, an onshore power generation diesel engine or the like is recirculated and used for a supercharger.
- exhaust gas of a diesel engine contains harmful substances such as NOx, SOx and dust, and substances that give a load to the environment.
- harmful substances such as NOx, SOx and dust
- various methods that do not discharge such harmful substances have been proposed.
- EGR exhaust gas recirculation
- Air diluted with exhaust gas has a lower oxygen concentration than normal air. Therefore, the speed of combustion, which is a reaction between fuel and oxygen, can be delayed. Further, carbon dioxide and water vapor contained in a large amount in the exhaust gas have a larger specific heat capacity than air, and even if the calorific value is the same, a rise in temperature can be kept low. Due to these effects, the maximum temperature of the flame is lowered, so that NOx generation (Thermal NOx) can be suppressed.
- NOx generation Thermal NOx
- Patent Document 1 discloses that exhaust gas is circulated through a suction pipe connected to a small turbocharger mounted on a diesel engine of an automobile.
- the present invention has been made in view of such circumstances, and prevents the temperature deviation of the mixed air obtained by mixing the recirculated exhaust gas and the sucked air, thereby reducing the efficiency and reliability.
- An object of the present invention is to provide a supercharger capable of suppressing a decrease and a diesel engine equipped with the same.
- the supercharger of the present invention and the diesel engine equipped with the same employ the following means. That is, the supercharger according to the first aspect of the present invention includes a turbine that is rotationally driven by exhaust gas discharged from a diesel engine, a rotary shaft that is provided with the turbine at one end, and a rotary shaft that is provided at the other end of the rotary shaft. And a compressor that compresses air sucked from the suction port when the turbine is driven to rotate, and mixing means provided upstream of the suction port, the mixing means comprising the air and the exhaust gas. A part of the mixture is mixed and led to the suction port.
- a small turbocharger mounted on a diesel engine such as an automobile has an exhaust gas recirculation system that lowers the combustion temperature by circulating a part of the exhaust gas discharged from the diesel engine through an intake pipe connected to the turbocharger.
- a circulation (EGR) scheme is implemented.
- large turbochargers mounted on marine and onshore power generation diesel engines have a suction port in front of the compressor and do not have a suction pipe. Therefore, when a part of the exhaust gas discharged from the diesel engine is led between the suction port and the compressor, the distance between the suction port and the compressor is short, so a drift occurs, and the sucked air and Mixing with the exhaust gas becomes uneven and the temperature is biased.
- a mixing means for mixing the air sucked by the compressor and a part of the exhaust gas discharged from the diesel engine is provided upstream of the suction port of the compressor.
- air and exhaust gas can be mixed uniformly and can be led to the compressor.
- the mixing means is provided with a substantially cylindrical mixing member provided therein and having a plurality of holes in the side wall, and a part of the exhaust gas is introduced.
- the mixing member may have a configuration in which one end portion in the axial direction is connected to the suction port and the air is sucked into the other end portion.
- a substantially cylindrical mixing member having a plurality of holes in the side wall, one end of the mixing member in the axial direction is connected to the suction port, and air is sucked from the other end.
- the exhaust gas guided from the inlet to the inside of the mixing means is guided from the hole provided in the side wall of the mixing member to the inside of the mixing member, and the air and the exhaust gas are mixed inside the mixing member. it can. Therefore, the mixed air that has passed through the mixing member and is uniformly mixed can be supplied to the suction port.
- the number of holes provided in the side wall facing the introduction port of the mixing member may be smaller than the number of holes provided in the side wall not facing the introduction port. Good.
- the number of holes provided in the side wall of the mixing member facing the inlet is less than the number of holes provided in the side wall not facing the inlet.
- the exhaust gas introduced into the mixing means from the inlet can be guided to the side of the side wall of the mixing member that does not face the inlet and guided to the inside of the mixing member. Therefore, the exhaust gas can be uniformly mixed from the substantially circumferential direction of the air passing through the inside of the mixing member. Therefore, the mixed air that has passed through the mixing member and is uniformly mixed can be supplied to the suction port.
- the hole provided in the side wall facing the introduction port of the mixing member may have a smaller diameter than the hole provided in the side wall not facing the introduction port. Good.
- the hole diameter provided on the side wall of the mixing member facing the inlet is made smaller than the hole diameter provided on the side wall not facing the inlet.
- the hole area of the hole provided in the side wall facing the introduction port of the mixing member has a hole area of the hole provided in the side wall not opposed to the introduction port.
- the size may be 0.3 to 0.8 times the area.
- the hole area of the hole provided on the side wall of the mixing member facing the inlet is made 0.3 to 0.8 times the hole area of the hole provided on the side wall not facing the inlet.
- the mixing means is a substantially cylindrical silencer into which the air is introduced from the side wall, and the silencer has a plurality of holes in the side wall.
- a substantially conical mixing member, the mixing member being provided so that an axial direction of the mixing member and an axial direction of the silencer are substantially coaxial, and from the other end of the substantially conical diverging side from the diesel engine Part of the exhaust gas discharged is introduced.
- a substantially conical mixing member having a plurality of holes on the side wall is provided, and exhaust gas is introduced from the end of the substantially conical end-spreading side. Exhaust gas introduced into the mixing member from the end of the diverging side is led out from a plurality of holes provided in the side wall of the mixing member, and introduced into the silencer from the side wall of the silencer and the inside of the silencer Mix evenly. For this reason, it is possible to prevent the drift of the air guided to the compressor and the exhaust gas, and to guide the mixed air having a uniform temperature to the suction port. Therefore, it is possible to suppress a decrease in supercharger efficiency and a decrease in reliability due to temperature nonuniformity of the supplied mixed air.
- a diesel engine according to the second aspect of the present invention includes the supercharger described above.
- the mixing means for mixing the air sucked by the compressor and a part of the exhaust gas discharged from the diesel engine is provided upstream of the suction port of the compressor.
- air and exhaust gas can be mixed uniformly and can be led to the compressor.
- FIG. 1 is a longitudinal sectional view showing a schematic configuration of a supercharger according to a first embodiment of the present invention. It is a perspective view of the mixing member provided in the casing for return gas of the supercharger which concerns on 2nd Embodiment of this invention. It is a perspective view of the mixing member provided in the casing for return gas of the supercharger which concerns on the modification 1 of 2nd Embodiment of this invention. It is a perspective view of the mixing member provided in the casing for return gas of the supercharger which concerns on the modification 2 of 2nd Embodiment of this invention. It is a perspective view of the mixing member provided in the casing for return gas of the supercharger which concerns on 4th Embodiment of this invention. It is the longitudinal cross-sectional view which showed schematic structure of the supercharger which concerns on 5th Embodiment of this invention. It is the longitudinal cross-sectional view which showed schematic structure of the conventional large sized supercharger.
- FIG. 1 shows a supercharger 1 mounted on a large marine diesel engine (not shown) used as a main engine of a ship.
- the marine diesel engine is equipped with a plurality of superchargers 1.
- the turbocharger 1 includes a turbine 2 driven by exhaust gas discharged from a marine diesel engine, a rotary shaft 6 driven to rotate by the turbine 2, and a compressor that compresses air by rotating the rotary shaft 6. 3 and a bearing stand 4 that is provided between the turbine 2 and the compressor 3 and supports the rotating shaft 6.
- the turbine 2 includes a turbine casing 7, a turbine disk 8 that is rotated by exhaust gas (exhaust gas) supplied from a marine diesel engine, and turbine blades 9 that are provided in the circumferential direction of the turbine disk 8.
- the turbine casing 7 is provided so as to cover the turbine disk 8 and the turbine blades 9.
- the turbine casing 7 includes a turbine casing inlet 7a through which exhaust gas is guided from an exhaust gas collecting pipe (not shown) of the marine diesel engine, an exhaust gas passage 7b that guides exhaust gas of the marine diesel engine to the turbine blades 9, and a turbine.
- a turbine casing outlet 7 c that guides the exhaust gas that has passed through the blades 9 to the outside of the turbine 2 is provided.
- the turbine disk 8 has a disk shape, and a plurality of turbine blades 9 extending radially outward from the center of rotation are provided along the circumferential direction.
- the turbine blade 9 is covered with a turbine casing 7 so as to surround the outside in the radial direction. Exhaust gas is guided to the turbine blade 9 from the exhaust gas passage 7b.
- the turbine disk 8 and the rotating shaft 6 are rotationally driven by the exhaust gas guided to the turbine blade 9.
- the exhaust gas that rotationally drives the turbine disk 8 and the rotating shaft 6 flows out from the turbine blade 9 to the turbine casing outlet 7c.
- the compressor 3 includes a compressor casing 11 and an impeller 12 that compresses air (fresh air) by being driven to rotate.
- the compressor casing 11 is provided so as to cover the impeller 12.
- the compressor casing 11 is a compressor casing inlet (suction port) for taking in air and exhaust gas (hereinafter referred to as “EGR gas”) from outside through a silencer 13 and a return gas casing (mixing means) 20 described later.
- EGR gas air and exhaust gas
- the impeller 12 has a substantially disk shape, and a plurality of blades (not shown) extending from the center toward the radially outer side are provided on one surface thereof.
- the impeller 12 is covered with a spiral chamber 11b so as to surround the radially outer side. Air and EGR gas sucked from the compressor casing inlet 11a are guided to the impeller 12.
- the impeller 12 is rotationally driven when the turbine 2 provided on the coaxial 6 is rotationally driven.
- the air and EGR gas sucked from the compressor casing inlet 11 a are compressed by the rotationally driven impeller 12, and the compressed air and EGR gas are sent out radially outward of the impeller 12.
- the air and EGR gas compressed by the impeller 12 pass through the spiral chamber 11b and are led out from the compressor casing outlet 11c.
- the compressor casing 11 is provided so as to sandwich the return gas casing 20 between the compressor casing 11 and the silencer 13.
- the return gas casing 20 has an introduction port 20a that is connected to an EGR return pipe (not shown) that guides EGR gas that is part of the exhaust gas of the marine diesel engine.
- the return gas casing 20 is provided with a substantially cylindrical mixing member 21 therein.
- the mixing member 21 has a substantially cylindrical shape, and its diameter is substantially equal to the diameter of the compressor casing inlet 11a.
- the mixing member 21 has one axial end connected to the compressor casing inlet 11a and the other end connected to the silencer 13, so that the air introduced from the silencer 13 into the mixing member 21 is compressed by the compressor. It can pass to the casing inlet 11a.
- the mixing member 21 is formed by forming a perforated plate having a plurality of holes 22 on its side wall into a cylindrical shape. For example, each of the plurality of holes 22 provided in the mixing member 21 has a substantially circular shape.
- Rotating shaft 6 with one end protruding toward turbine 2 and the other end protruding toward compressor 3 passes through bearing stand 4. Further, a turbine casing 7 and a compressor casing 11 are connected to the bearing stand 4. The turbine casing 7, the bearing stand 4, and the compressor casing 11 are integrally fastened by a plurality of bolts (not shown).
- the bearing stand 4 is provided with a journal bearing (not shown) and a thrust bearing (not shown). These journal bearings are provided in the vicinity on the turbine 2 side and in the vicinity on the compressor 3 side. With these journal bearings, the rotary shaft 6 can be rotated about the axis and supported by the bearing base 4.
- exhaust gas acts on the turbine blade 9 by the thrust bearings disposed on both sides of a thrust collar (not shown) provided so as to protrude toward the outer periphery in the radial direction of the rotating shaft 6, so that the rotating shaft 6 is pivoted.
- a thrust collar (not shown) provided so as to protrude toward the outer periphery in the radial direction of the rotating shaft 6, so that the rotating shaft 6 is pivoted.
- rotation about the rotation axis 6 is possible.
- Exhaust gas is led from the exhaust gas collecting pipe of the marine diesel engine to the turbine casing inlet 7 a of the turbine casing 7.
- the exhaust gas guided to the turbine casing inlet 7a is guided to the turbine blade 9 through the exhaust gas passage 7b.
- the turbine disk 8 and the rotating shaft 6 are rotationally driven by the exhaust gas guided to the turbine blade 9.
- the exhaust gas that rotationally drives the turbine disk 8 and the rotating shaft 6 flows out from the turbine blade 9 to the turbine casing outlet 7c.
- the rotary shaft 6 Since the rotary shaft 6 is provided with the impeller 12 at the end opposite to the end where the turbine disk 8 is provided, the rotary shaft 6 is rotationally driven by the exhaust gas, so that the impeller 12 is rotationally driven.
- the impeller 12 When the impeller 12 is driven to rotate, air is sucked into the silencer 13 from the outer periphery of the silencer 13.
- a part of the exhaust gas of the marine diesel engine is introduced into the return gas casing 20 as EGR gas from the opening 20a of the return gas casing 20 provided between the silencer 13 and the compressor casing 11. Is done.
- the air (fresh air) sucked through the silencer 13 is guided to the inside of the substantially cylindrical mixing member 21 provided inside the return gas casing 20 by the rotational drive of the impeller 12. Further, the EGR gas introduced into the return gas casing 20 from the inlet 20 a of the return gas casing 20 is guided to the inside of the mixing member 21 through a plurality of holes 22 provided in the mixing member 21. As a result, the EGR gas can be uniformly mixed with the air passing through the inside of the mixing member 21.
- the air and EGR gas uniformly mixed inside the mixing member 21 are mixed air and sucked into the compressor casing 11 from the compressor casing inlet 11a.
- the mixed air sucked into the compressor casing 11 is compressed by the impeller 12 that is driven to rotate.
- the mixed air compressed by the impeller 12 is discharged from the compressor casing outlet 11c through the spiral chamber 11b.
- the compressed mixed air discharged from the supercharger 1 is supplied to the marine diesel engine.
- the marine diesel engine is supplied with mixed air in which air and EGR gas are sufficiently mixed by the supercharger 1.
- the supercharger 1 according to this embodiment and a marine diesel engine equipped with the same provide the following operational effects.
- a return gas casing (mixing means) 20 that mixes EGR gas, which is part of the gas, is provided.
- EGR gas which is part of the gas
- air and EGR gas can be mixed uniformly and can be led to the compressor casing inlet 11a. Therefore, it is possible to prevent the mixed air, which is a mixture of the air guided to the compressor casing inlet 11a and the exhaust gas, from drifting, and to guide the mixed air having a uniform temperature to the compressor casing inlet 11a. Therefore, it is possible to suppress a decrease in efficiency and a decrease in reliability of the supercharger 1 due to temperature nonuniformity of the sucked mixed air.
- one end of the mixing member 21 in the axial direction is connected to the compressor casing inlet 11a, and the other of the mixing member 21 in the axial direction is connected. Air was inhaled from the end. Thereby, the EGR gas can be guided to the inside of the mixing member 21 from the hole 22 provided in the side wall of the mixing member 21, and the air and the EGR gas can be mixed inside the mixing member 21. Therefore, mixed air that has passed through the mixing member 21 and is uniformly mixed can be supplied to the compressor casing inlet 11a.
- the supercharger 1 which can suck
- FIG. 2 is a perspective view of the side wall of the mixing member provided in the return gas casing (mixing means) according to the present embodiment.
- FIG. 2 shows a side wall of the mixing member 21 facing an inlet (not shown) provided in a return gas casing (not shown). A broken line shown in FIG. The hole 22 provided in the side wall on the opposite side to the side wall facing is shown.
- six holes 22a, 22b, 22c, 22d, 22e, and 22f are formed in a circle at substantially equal intervals on the side wall of the mixing member 21 that faces the introduction port.
- the holes 22a, 22b, 22c, 22d, 22e, and 22f are provided in a circle at substantially equal intervals.
- a hole 22g is provided at a substantially central portion of a circle formed by the six holes 22a, 22b, 22c, 22d, 22e, and 22f as indicated by a broken line.
- the number of the holes 22a, 22b, 22c, 22d, 22e, 22f provided on the side wall of the mixing member 21 facing the introduction port (six) is the mixing member facing the introduction port.
- the number (seven) of holes 22a, 22b, 22c, 22d, 22e, 22f, and 22g provided in positions other than the side wall of 21 is increasing.
- the number of the holes 22 provided in the side wall of the mixing member 21 facing the introduction port is made smaller than the number of the holes 22 provided in the other side walls, thereby returning the return gas casing.
- the EGR gas (a part of the exhaust gas) introduced into the return gas casing from the inlet of the gas moves between the mixing member 21 and the return gas casing to the side opposite to the inlet side. It goes around and is guided to the inside of the mixing member 21.
- the supercharger according to the present embodiment and the marine diesel engine equipped with the same provide the following operational effects.
- the number of holes 22a, 22b, 22c, 22d, 22e and 22f (six) provided in the side wall of the mixing member 21 facing the inlet (not shown) is mixed so as not to face the inlet.
- the number of holes 22a, 22b, 22c, 22d, 22e, 22f, and 22g provided on the side wall of the member 21 is set to be smaller than the number (seven).
- the EGR gas (a part of the exhaust gas) guided from the introduction port into the return gas casing (mixing means) is caused to wrap around the side wall of the mixing member 21 that does not face the introduction port. Can be led inside.
- the exhaust gas can be uniformly mixed with the air (fresh air) passing through the inside of the mixing member 21 from the substantially circumferential direction of the mixing member 21. Therefore, mixed air that has passed through the mixing member 21 and is uniformly mixed can be supplied to the compressor casing inlet (suction port).
- the side wall other than the side wall of the mixing member 21 facing the introduction port has a hole at a substantially circular center formed by the holes 22a, 22b, 22c, 22d, 22e, and 22f.
- 22 g is provided, the present invention is not limited to this.
- the side wall of the mixing member 21 facing the inlet is not provided with a hole 22 in the vicinity of the axial end of the mixing member 21. Or it is good also as what does not provide the some hole 22 in the approximate center part of the axial direction of the mixing member 21 like the modification 2 shown with the broken line of FIG.
- the diameter of the hole provided in the side wall of the mixing member facing the inlet of the return gas casing is provided in the side wall at other positions. It is different from the first embodiment in that it is smaller than the diameter of the hole, and the others are the same. Therefore, the description of the same configuration and the flow of EGR gas and air is omitted.
- the diameter of the hole provided in the side wall of the mixing member facing the inlet of the return gas casing (introducing means) is larger than the diameter of the hole provided at a position other than the side wall facing the inlet. Are also considered small.
- the casing for return gas (not shown)
- the EGR gas (a part of the exhaust gas) introduced into the return gas casing from the introduction port of (1) moves between the mixing member and the return gas casing to the opposite side of the introduction port side. It goes around and is led into the mixing member.
- the supercharger according to the present embodiment and the marine diesel engine equipped with the same provide the following operational effects.
- the hole diameter provided in the side wall of the mixing member facing the inlet of the return gas casing (introducing means) was made smaller than the hole diameter provided in the side wall not facing the inlet.
- the EGR gas (a part of the exhaust gas) introduced into the mixing means from the introduction port can be guided to the side of the side wall not facing the introduction port and introduced into the mixing member. Therefore, the EGR gas can be uniformly mixed from the substantially circumferential direction of the air (fresh air) passing through the inside of the mixing member. Therefore, mixed air that has passed through the mixing member and is uniformly mixed can be supplied to the compressor casing inlet (suction port).
- FIG. 5 shows a perspective view of the side wall of the mixing member provided in the return gas casing (mixing means) according to the present embodiment.
- a plurality of substantially rectangular holes 23 are provided in the side wall of the mixing member 21 so as to have a long axis in the longitudinal direction of the mixing member 21.
- the rectangular holes 23 are provided in the side wall of the mixing member 21 so that the major axes are parallel to each other.
- a part of the side wall of the mixing member 21 facing the inlet (not shown) of the return gas casing (not shown) is a portion near the compressor casing inlet (suction port) (right side in FIG. 5).
- a substantially circular hole 22 is provided instead of a substantially rectangular hole 23.
- the inner diameter of the hole 22 is substantially the same as the short axis of the substantially rectangular hole 23, and the hole area of the hole 22 is 0.3 times the hole area of the substantially rectangular hole 23.
- the supercharger according to the present embodiment and the marine diesel engine equipped with the same provide the following operational effects.
- the hole area of the hole 22 provided on the side wall of the mixing member 21 facing the inlet (not shown) of the return gas casing (introducing means) is provided on the side wall not facing the inlet.
- the hole area of the hole 23 is 0.3 times.
- the EGR gas (a part of the exhaust gas) introduced into the mixing means 21 from the introduction port is guided to the side of the side wall of the mixing member 21 not facing the introduction port, and is introduced into the mixing member 21.
- Can do. Therefore, the EGR gas can be mixed uniformly from the substantially circumferential direction of the air (fresh air) passing through the inside of the mixing member 21. Therefore, mixed air that has passed through the mixing member 21 and is uniformly mixed can be supplied to the compressor casing inlet (suction port).
- the hole area of the hole 22 provided in the side wall of the mixing member 21 facing the introduction port of the return gas casing is the hole 23 provided in the side wall not facing the introduction port.
- the present invention is not limited to this, and the hole area of the hole 22 may be 0.3 to 0.8 times the hole area of the hole 23. What is necessary is just the magnitude
- FIG. 6 is a longitudinal sectional view showing a schematic configuration of the supercharger according to the present embodiment.
- a silencer (mixing means) 13 having the same diameter as the outer diameter of the compressor casing 11 is provided at the compressor casing inlet (suction port) 11 a of the compressor casing 11.
- the silencer 13 has a substantially cylindrical shape, and silences by introducing air (fresh air) from the side wall thereof. Further, a silencer inlet 13a into which EGR gas (a part of the exhaust gas) is introduced opens on the surface of the silencer 13 opposite to the compressor 3 side (left end surface in FIG. 6).
- a substantially conical mixing member 30 is provided inside the silencer 13.
- the mixing member 30 has a plurality of holes 31 on its side wall, and is provided so that the axial direction of the mixing member 30 and the axial direction of the silencer 13 are substantially coaxial.
- the mixing member 30 provided in the silencer 13 has an introduction port 30a into which EGR gas discharged from a marine diesel engine (diesel engine) is introduced at the other end portion on the substantially conical end-spreading side.
- the introduction port 30a has a flange structure, and is fixed to the silencer introduction port 13a from the inside of the silencer 13 by bolts (not shown).
- the EGR gas is guided from an EGR return pipe (not shown) through the silencer inlet 13a to the inside of the mixing member 30 from the inlet 30a of the mixing member 30.
- the EGR gas introduced into the mixing member 30 is led out into the silencer 13 through a plurality of holes 31 provided in the side wall of the mixing member 30.
- the supercharger according to the present embodiment and the marine diesel engine equipped with this one have the following operational effects.
- a substantially conical mixing member 30 having a plurality of holes 31 on the side wall is provided, and an introduction port 30 a provided at the end of the mixing member 30 on the end spreading side.
- EGR gas (a part of the exhaust gas) was introduced.
- the EGR gas introduced into the mixing member 30 from the introduction port 30a is led into the silencer 13 through a plurality of holes 31 provided in the side wall of the mixing member 30, and the inside of the silencer 13 from the side wall of the silencer 13 Mix evenly with the air (fresh air) introduced into the.
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Abstract
Description
すなわち、本発明の第1の態様に係る過給機は、ディーゼル機関が排出する排気ガスにより回転駆動されるタービンと、一端に前記タービンを設けた回転軸と、該回転軸の他端に設けられて、前記タービンが回転駆動することにより吸込み口から吸引した空気を圧縮する圧縮機と、前記吸込み口の上流に設けられる混合手段と、を備え、該混合手段は、前記空気と前記排気ガスの一部とを混合して前記吸込み口へと導く。
以下に、本発明の第1実施形態について、図1を参照して説明する。
図1には、船舶の主機として用いられている大型の舶用ディーゼル機関(図示せず)に搭載されている過給機1が示されている。
舶用ディーゼル機関には、複数台の過給機1が搭載されている。
タービンケーシング7は、タービンディスク8とタービン翼9とを覆うように設けられている。タービンケーシング7は、舶用ディーゼル機関の排気ガス集合管(図示せず)から排気ガスが導かれるタービンケーシング入口7aと、舶用ディーゼル機関の排気ガスをタービン翼9へと導く排気ガス通路7bと、タービン翼9を通過した排気ガスをタービン2外へと導くタービンケーシング出口7cとを有している。
圧縮機ケーシング11は、インペラ12を覆うように設けられている。圧縮機ケーシング11は、サイレンサ13および後述する戻りガス用ケーシング(混合手段)20を介して外部からの空気および排気ガス(以下、「EGRガス」という。)を取り入れる圧縮機ケーシング入口(吸込み口)11aと、インペラ12が圧縮した空気が導かれる渦巻き室11bと、インペラ12が圧縮した空気(新気)を排出する圧縮機ケーシング出口11cとを有している。
舶用ディーゼル機関の排気ガス集合管からタービンケーシング7のタービンケーシング入口7aへと排気ガスが導かれる。タービンケーシング入口7aに導かれた排気ガスは、排気ガス通路7bを経てタービン翼9へと導かれる。タービン翼9に導かれた排気ガスによってタービンディスク8および回転軸6が回転駆動される。タービンディスク8および回転軸6を回転駆動した排気ガスは、タービン翼9からタービンケーシング出口7cへと流出する。
圧縮機3の圧縮機ケーシング入口(吸込み口)11aの上流であってサイレンサ13との間に、圧縮機3が吸引する空気(新気)と、舶用ディーゼル機関(ディーゼル機関)から排出される排気ガスの一部であるEGRガスとを混合する戻りガス用ケーシング(混合手段)20を設けることとした。これにより、空気とEGRガスとを均一に混合させて、圧縮機ケーシング入口11aに導くことができる。そのため、圧縮機ケーシング入口11aに導かれる空気と排気ガスとを混合した混合空気の偏流を防止して、温度が均一化した混合空気を圧縮機ケーシング入口11aに導くことができる。したがって、吸引される混合空気の温度不均一を起因とする過給機1の効率低下や信頼性の低下を抑制することができる。
本実施形態の過給機およびこれを備えている舶用ディーゼル機関は、戻りガス用ケーシングの導入口に対向している混合部材の側壁に設けられる孔数がそれ以外の位置の側壁に設けられる孔数と異なる点で、第1実施形態と相違しその他は同様である。したがって、同一の構成およびEGRガスと空気との流れについては、同一の符号を付してその説明を省略する。
図2には、本実施形態に係る戻りガス用ケーシング(混合手段)に設けられている混合部材の側壁の斜視図が示されている。
導入口に対向している混合部材21の側壁以外の位置に設けられる孔22は、略等間隔に円状に設けられている6つの孔22a、22b、22c、22d、22e、22fに加えて、6つの孔22a、22b、22c、22d、22e、22fによって形成される円の略中心部に破線で示すように孔22gが設けられている。
導入口(図示せず)に対向している混合部材21の側壁に設けられている孔22a、22b、22c、22d、22e、22fの数(6つ)を、導入口に対向していない混合部材21の側壁に設けられている孔22a、22b、22c、22d、22e、22f、22gの数(7つ)よりも少なくすることとした。これにより、導入口から戻りガス用ケーシング(混合手段)内に導かれたEGRガス(排気ガスの一部)を導入口に対向していない混合部材21の側壁側に回り込ませて、混合部材21の内部に導くことができる。そのため、混合部材21の内部を通過する空気(新気)に混合部材21の略円周方向から均一に排気ガスを混合させることができる。したがって、圧縮機ケーシング入口(吸込み口)には、混合部材21を通過して均一に混合した混合空気を供給することができる。
本実施形態の過給機およびこれを備えている舶用ディーゼル機関は、戻りガス用ケーシングの導入口に対向している混合部材の側壁に設けられる孔の径がそれ以外の位置の側壁に設けられる孔の径よりも小さい点で、第1実施形態と相違しその他は同様である。したがって、同一の構成およびEGRガスと空気との流れについては、その説明を省略する。
戻りガス用ケーシング(導入手段)の導入口に対向している混合部材の側壁に設けられている孔径を、導入口に対向していない側壁に設けられている孔径よりも小さくすることとした。これにより、導入口から混合手段内に導かれたEGRガス(排気ガスの一部)を導入口に対向していない側壁側に回り込ませて、混合部材の内部に導くことができる。そのため、混合部材の内部を通過する空気(新気)の略円周方向から均一にEGRガスを混合させることができる。したがって、圧縮機ケーシング入口(吸込み口)には、混合部材を通過して均一に混合した混合空気を供給することができる。
本実施形態の過給機およびこれを備えている舶用ディーゼル機関は、戻りガス用ケーシングの導入口に対向している混合部材の側壁に設けられる孔面積がそれ以外の位置の側壁に設けられる孔面積と異なる点で、第1実施形態と相違しその他は同様である。したがって、同一の構成およびEGRガスと空気との流れについては、同一の符号を付してその説明を省略する。
図5には、本実施形態に係る戻りガス用ケーシング(混合手段)に設けられている混合部材の側壁の斜視図が示されている。
戻りガス用ケーシング(導入手段)の導入口(図示せず)に対向している混合部材21の側壁に設けられている孔22の孔面積を、導入口に対向していない側壁に設けられている孔23の孔面積の0.3倍にすることとした。これにより、導入口から混合手段21内に導かれたEGRガス(排気ガスの一部)を導入口に対向していない混合部材21の側壁側に回り込ませて、混合部材21の内部に導くことができる。そのため、混合部材21の内部を通過する空気(新気)の略円周方向から均一にEGRガスを混合させることができる。したがって、圧縮機ケーシング入口(吸込み口)には、混合部材21を通過して均一に混合した混合空気を供給することができる。
本実施形態の過給機およびこれを備えている舶用ディーゼル機関は、サイレンサの内部に混合部材を設ける点で、第1実施形態と相違しその他は同様である。したがって、同一の構成およびEGRガスと空気との流れについては、同一の符号を付してその説明を省略する。
図6には、本実施形態に係る過給機の概略構成を示した縦断面図が示されている。
サイレンサ(混合手段)13の内部には、側壁に複数の孔31を有している略円錐状の混合部材30を設けて、混合部材30の末広がり側の端部に設けられている導入口30aからEGRガス(排気ガスの一部)を導入することとした。導入口30aから混合部材30の内部に導かれたEGRガスは、混合部材30の側壁に設けられている複数の孔31からサイレンサ13の内部に導出されて、サイレンサ13の側壁からサイレンサ13の内部に導入された空気(新気)と均一に混合する。そのため、圧縮機3の圧縮機ケーシング入口(吸込み口)11aに導かれる空気とEGRガスとの偏流を防止して、温度が均一化した混合空気を圧縮機ケーシング入口11aに導くことができる。したがって、供給される混合空気の温度不均一を起因とする過給機1の効率の低下や信頼性の低下を抑制することができる。
2 タービン
3 圧縮機
6 回転軸
11a 圧縮機ケーシング入口(吸込み口)
20 戻りガス用ケーシング(混合手段)
Claims (7)
- ディーゼル機関が排出する排気ガスにより回転駆動されるタービンと、
一端に前記タービンを設けた回転軸と、
該回転軸の他端に設けられて、前記タービンが回転駆動することにより吸込み口から吸引した空気を圧縮する圧縮機と、
前記吸込み口の上流に設けられる混合手段と、を備え、
該混合手段は、前記空気と前記排気ガスの一部とを混合して前記吸込み口へと導く過給機。 - 前記混合手段は、その内部に設けられて側壁に複数の孔を有する略円筒状の混合部材と、前記排気ガスの一部が導入される導入口と、を備え、
前記混合部材は、その軸方向の一端部が前記吸込み口に接続されて、他端部には、前記空気が吸入される請求項1に記載の過給機。 - 前記混合部材の前記導入口に対向する前記側壁に設けられる前記孔は、前記導入口に対向しない前記側壁に設けられる前記孔よりも数が少ない請求項2に記載の過給機。
- 前記混合部材の前記導入口に対向する前記側壁に設けられる前記孔は、前記導入口に対向しない前記側壁に設けられる前記孔よりも孔径が小さい請求項2または請求項3に記載の過給機。
- 前記混合部材の前記導入口に対向する前記側壁に設けられる前記孔の孔面積は、前記導入口に対向しない前記側壁に設けられる前記孔の孔面積の0.3倍から0.8倍の大きさである請求項2から請求項4のいずれかに記載の過給機。
- 前記混合手段は、前記空気が側壁から導入される略円筒状のサイレンサであって、
該サイレンサの内部には、側壁に複数の孔を有する略円錐状の混合部材を備え、
該混合部材は、その軸方向と前記サイレンサの軸方向とが略同軸になるように設けられて、略円錐状の末広がり側の他端部から前記ディーゼル機関から排出された前記排気ガスの一部が導入される請求項1に記載の過給機。 - 請求項1から請求項6のいずれかに記載の過給機を備えたディーゼル機関。
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| EP12736594.8A EP2666989B1 (en) | 2011-01-19 | 2012-01-18 | Turbocharger and diesel engine comprising the same |
| KR1020187011965A KR20180049829A (ko) | 2011-01-19 | 2012-01-18 | 과급기 및 이것을 구비한 디젤 기관 |
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| CN201280002213.7A CN103038477B (zh) | 2011-01-19 | 2012-01-18 | 增压器及具备该增压器的柴油机 |
| KR1020177010369A KR20170044217A (ko) | 2011-01-19 | 2012-01-18 | 과급기 및 이것을 구비한 디젤 기관 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016092897A1 (ja) * | 2014-12-09 | 2016-06-16 | 三菱重工業株式会社 | 吸音装置、遠心圧縮機、および過給機 |
| JP2016109085A (ja) * | 2014-12-09 | 2016-06-20 | 三菱重工業株式会社 | 吸音装置、遠心圧縮機、および過給機 |
| US10132216B2 (en) | 2016-05-31 | 2018-11-20 | Progress Rail Locomotive Inc. | Crankcase ventilation system for an internal combustion engine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104314667A (zh) | 2015-01-28 |
| KR20130021468A (ko) | 2013-03-05 |
| EP2666989B1 (en) | 2015-12-09 |
| JP5825791B2 (ja) | 2015-12-02 |
| EP2666989A4 (en) | 2014-07-02 |
| JP2012149579A (ja) | 2012-08-09 |
| EP2915974A1 (en) | 2015-09-09 |
| KR20140111351A (ko) | 2014-09-18 |
| CN103038477B (zh) | 2015-04-22 |
| KR20170044217A (ko) | 2017-04-24 |
| KR20180049829A (ko) | 2018-05-11 |
| CN103038477A (zh) | 2013-04-10 |
| EP2666989A1 (en) | 2013-11-27 |
| KR20160017118A (ko) | 2016-02-15 |
| KR101506820B1 (ko) | 2015-03-27 |
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