WO2006045488A1 - Condensateur d'un systeme de turbocompresseur et procede d'utilisation d'un tel systeme - Google Patents
Condensateur d'un systeme de turbocompresseur et procede d'utilisation d'un tel systeme Download PDFInfo
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- WO2006045488A1 WO2006045488A1 PCT/EP2005/011188 EP2005011188W WO2006045488A1 WO 2006045488 A1 WO2006045488 A1 WO 2006045488A1 EP 2005011188 W EP2005011188 W EP 2005011188W WO 2006045488 A1 WO2006045488 A1 WO 2006045488A1
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- condensate
- exhaust gas
- arrangement according
- charge air
- compressor
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
- F01N3/021—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters
- F01N3/033—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters in combination with other devices
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00
- F01N13/009—Exhaust or silencing apparatus characterised by constructional features ; Exhaust or silencing apparatus, or parts thereof, having pertinent characteristics not provided for in, or of interest apart from, groups F01N1/00 - F01N5/00, F01N9/00, F01N11/00 having two or more separate purifying devices arranged in series
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
- F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
- F01N3/021—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters
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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
- F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
- F02B29/04—Cooling of air intake supply
- F02B29/045—Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
- F02B29/0468—Water separation or drainage means
-
- 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
-
- 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
- F02M26/23—Layout, e.g. schematics
- F02M26/24—Layout, e.g. schematics with two or more coolers
-
- 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
- F02M26/23—Layout, e.g. schematics
- F02M26/28—Layout, e.g. schematics with liquid-cooled heat exchangers
-
- 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
- F02M26/35—Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories with means for cleaning or treating the recirculated gases, e.g. catalysts, condensate traps, particle filters or heaters
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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
- F02M35/02—Air cleaners
- F02M35/022—Air cleaners acting by gravity, by centrifugal, or by other inertial forces, e.g. with moistened walls
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
- F01N2250/00—Combinations of different methods of purification
- F01N2250/06—Combinations of different methods of purification afterburning and filtering
-
- 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
- F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
- F02B29/04—Cooling of air intake supply
- F02B29/0406—Layout of the intake air cooling or coolant circuit
- F02B29/0437—Liquid cooled heat exchangers
- F02B29/0443—Layout of the coolant or refrigerant circuit
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/02—EGR systems specially adapted for supercharged engines
- F02M26/04—EGR systems specially adapted for supercharged engines with a single turbocharger
- F02M26/05—High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M26/00—Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
- F02M26/02—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
-
- 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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- 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 invention relates to a turbocharger arrangement and a method for operating a turbocharger according to the preamble of claim 1 or claim 19.
- the return of exhaust gas is known, with both a high-pressure exhaust gas recirculation and a low-pressure exhaust gas recirculation is possible.
- the exhaust gas stream is cooled to temperatures of about 15O 0 C to 200 0 C and admixed with the intake air.
- the cooled intake air usually a partial flow of the engine coolant is used, but also the use of other coolant is known.
- Exhaust gas recirculation is all the more effective the lower the gas outlet temperatures at the exhaust gas cooler are.
- High-pressure exhaust gas recirculation In the case of high-pressure exhaust gas recirculation, exhaust gas is usually taken off in front of the turbine and the charge air is supplied to the charge air cooler. The cooling of the recirculated exhaust gas takes place by the hot engine coolant, so that due to the high temperatures usually no Exhaust gas condensate is formed. High-pressure exhaust gas recirculation achieves a significant reduction in nitrogen oxide emissions, but with a simultaneous increase in particulate emissions. The particle or particulate matter emission can be reduced by particle filters.
- the exhaust gas is removed after the turbine, preferably after a particle filter, taken from the exhaust gas flow, cooled and fed to the compressor on the suction side. Due to the greater cooling of the recirculated exhaust gas, a further reduction of the nitrogen oxide emission is possible, however, forms due to the strong cooling of the recirculated exhaust gas condensate, which is sour starK, which essentially goes back to the formed nitric acid HNO 3 , so that it Corrosion comes. If condensate mist is fed to the compressor, it can also damage the compressor because of its high speed (about 120000 to 150000 rpm).
- turbocharger arrangement and a method for operating a turbocharger, in which the risk of corrosion is as low as possible.
- This object is achieved by a turbocharger arrangement and a method having the features of claim 1 and of claim 19.
- Advantageous refinements are the subject of the claims.
- the term "charge air” is understood to mean both the intake air and the intake air mixed with the recirculated exhaust gas.
- a turbocharger arrangement in particular a motor vehicle with an internal combustion engine, is provided with exhaust gas recirculation, the arrangement having an exhaust gas cooler and a charge air cooler for cooling recirculated exhaust gas and / or charge air and a compressor for compressing the charge air and a condensate separator.
- the condensate separator By means of the condensate separator, the corrosive fraction of the exhaust gas located in the condensate, which forms when the dew point temperature is reached and reached, can be removed from the exhaust gas stream or the charge air stream and ensured that no or only minimal condensate occurs in the following region collects, which promotes an eventual corrosion of the components.
- the condensate separator is hereby preferably arranged directly after the cooler for cooling the recirculated exhaust gas and / or after the charge air cycle here and / or directly in front of the charge air compressor.
- the condensate separator may preferably be a centrifugal or cyclone separator.
- a filter for example made of stainless steel or plastic fabric or fleece, which serves as a condensate separator, is possible.
- the condensate separation can be done in several stages to increase the effectiveness. Different condensate separators can be combined as required.
- a valve for throttling the exhaust gas flow or the charge air flow is preferably provided so that the pressure level can be raised and the condensate can be discharged without additional aids.
- tools such as a pump or other arrangement, which allows a temporary increase in pressure Sammelbe ⁇ container possible.
- a check valve may be provided which allows outflow of the condensate, but prevents backflow of condensate and / or air from the outside.
- the condensate drain can have such a discharge gradient that the weight force on the condensate corresponds at least to the suction pressure, so that a suck back of condensate can be prevented.
- the condensate separator is preferably arranged directly downstream of the cooler, in particular directly downstream of the exhaust gas cooler. Also, an arrangement after the intercooler is useful. In order to protect the compressor against damage by condensate droplets, an arrangement directly in front of the compressor is also expedient. In this case, the shaft of the compressor can advantageously be used as drive or part of a centrifugal separator.
- the condensate separator must also be arranged in an area in which condensate droplets are present. This is usually the case in an area in which the temperature of the exhaust gas stream or of the exhaust gas stream Charge air flow to the dew point (taking into account the other parameters, in particular pressure and chemical composition) reaches or falls below.
- the exhaust gas or the charge air is in a region in which the exhaust gas or the charge air has a temperature which corresponds to the dew point or falls below the same deflected, in particular beauf ⁇ with a velocity component in the tangential direction, so that preferably the longitudinal movement a Rotationsbeweg is superimposed, but also a deflection of the air flow can be sufficient.
- the velocity component in the tangential direction Due to the velocity component in the tangential direction, the forming condensate droplets are moved outward and can be deposited on the wall, from where they can collect, be forwarded and discharged.
- the average tangential velocity component is preferably at least as great as the mean velocity component in the longitudinal direction, preferably at least twice as large.
- the Kondensatabscheider is preferably coupled to the shaft of the compressor or fixed, so that a high speed with little design effort and without additional drive is possible.
- the condensate separator preferably has a displacer or Schleu der Sciences, which is rotatably mounted on the shaft or formed by a Be ⁇ rich the shaft.
- This follower body is preferably made of a light metal or a light metal alloy, such as aluminum, titanium or magnesium, or made of a plastic. Alternatively or additionally, it may have a surface coating, for example an oxalic layer, which protects it from corrosion.
- the body is vorzugs ⁇ wise fluidically designed such that it despite the deflection no turbulence generated. Furthermore, it is minimized in terms of its mass to avoid mass forces.
- the displacer or spinner is preferably arranged in the normal flow direction of the charge air upstream of the impeller of the compressor and preferably directs the charge air flow by at least 90 °, preferably by two times 180 °.
- a Z-type deflection by z-about 180 ° leads to a very good separation of the condensate drops, with a part of the condensate drops knock off the body and thrown from there as a result of centrifugal force to the inner channel or housing wall.
- the kinetic energy of the condensate drops can be used for removing the condensate from the interior.
- the condensate separator is preferably arranged in the compressor housing and / or integrated in the compressor housing.
- the compressor housing preferably has bores for the condensate drain.
- the assembly includes a thermal condensate removal which enables detoxification of the condensate, so that acid, the acids condensate in Kon ⁇ contained, in particular the nitric acid, the sulfuric and are converted into their non-hazardous gases and "water, the sulfurous acid. This can then be added to the exhaust gas and delivered to the environment via the exhaust.
- a thermal condensate removal which enables detoxification of the condensate, so that acid, the acids condensate in Kon ⁇ contained, in particular the nitric acid, the sulfuric and are converted into their non-hazardous gases and "water, the sulfurous acid. This can then be added to the exhaust gas and delivered to the environment via the exhaust.
- the thermal condensate removal is preferably multi-stage, in particular three-stage, formed.
- an exhaust-heated heat exchanger for heating the condensate is preferably provided.
- a thermal reactor is preferably provided, which preferably comprises a PTC heating element and regulates automatically when no condensate is obtained.
- thermosohermal reaction Actuator provided for a Resterhitzung, in particular in the form of a elektri ⁇ 's radiator, which heats the vaporized condensate to 350 to 450 c C, so that the nitric acid vapor on its innocuous Comp components nitrogen, water and oxygen converts.
- internals are preferably provided for increasing the surface area so that the chemical process sequence can be optimized. It can be provided for each Kondensatabscheider a thermal condensate sat entsorgung, but preferably a common condensate disposal is provided for several Kondensatabscheider.
- the heating of the thermal condensate removal may preferably be at low operating temperatures (122 ° C), the lead 2 formation of NO, are operated getak ⁇ tet, to allow, for example, load-dependent metering of NO 2 so that the NO x limits to be met.
- an additional blower can be provided, which ensures egg conservation of the MAK values, irrespective of the function of the condensate discharge.
- lines are provided between the condensate separator and the condensate removal line, which lines have an automatic conveying effect as a result of capillary forces and / or their arrangement, so that pumps can be dispensed with.
- turbocharger arrangements will be explained in detail with reference to several exemplary embodiments with reference to the drawing. Show it:
- 1 is a schematic diagram of a Vorricrrtung for cooling exhaust gas, as it can be used in a turbocharger assembly according to the invention
- 2 is a schematic view of a firstticiansbei ⁇ game
- FIG. 3 is a schematic view of a second embodiment
- FIG. 6 is a schematic view of a fifth amongsbei ⁇ game
- FIG. 7 is a schematic representation of a turbocharger arrangement with high-pressure exhaust gas recirculation
- FIG. 8 is a schematic representation of a turbocharger arrangement with low-pressure exhaust gas recirculation
- Fig. 9 is a schematic view of a seventh Ausflowt! example with a first variant of a centrifugal separator
- FIG. 10 is a schematic view of an eighth Aussolidu ngsbei ⁇ game with a second variant of a centrifugal separator
- 11 is a schematic representation of a turbocharger arrangement with low-pressure exhaust gas recirculation with two-stage cooling of the recirculated exhaust gas
- 12 shows a schematic representation of a turbocharger arrangement with low-pressure exhaust gas recirculation with thermal condensate disposal
- FIG. 13 shows a schematic detail of the thermal condensate disposal of FIG. 12.
- Fig. 1 shows a small section of a turbocharger arrangement.
- a device 1 for cooling recirculated exhaust gas of a power tool is shown with an internal combustion engine which has a condensate separator 3 arranged downstream of a coolant-cooled exhaust gas cooler 2 with an exhaust gas outlet 4 and a condensate outlet 5.
- the flow direction of the exhaust stream is indicated by arrows.
- the recirculated exhaust gas stream has passed through a particle filter before the branching off of the exhaust gas stream, so that as far as possible no particles, in particular no larger particles, are separated off in addition to the condensate, which deposits and thereby reduces the maintenance effort. increase wall.
- especially small particles can serve as condensation seeds and have a positive effect on the condensation.
- the deposition of the condensate droplets takes place in the condensate separator 3 by a Ver ⁇ settlement of the exhaust gas flow in rotation, so that the condensate droplets are not only taken in the axial direction of the exhaust stream but insbesonde ⁇ re also conveyed to the outside and largely accumulate on the wall, from where they can descend due to gravity down and can be dissipated.
- the pressure loss through the condensate 3 is relatively low.
- the deposition of the aggressive condensate the components arranged behind are protected, so that the risk of corrosion can be significantly reduced.
- a centrifugal force separator which is conventional in principle is provided as condensate deflector 3, which is part of the device 1.
- the precipitate condensate flows down through the condensate outlet 5, where an opening is arranged with a collecting container 7, in which the condensate is collected.
- the collecting container 7 ⁇ / vird if allowed to emptied. It should be noted that there is a negative pressure compared to the environment, so that the condensate must be sucked n, so far no Druckhi, for example, by stopping the A-bgasstroms takes place.
- a detailed description of possible centrifugal shut-off eider takes place later with reference to Figures 9 and 10th
- a shut-off valve 8 arranged in the exhaust gas flow is provided according to the second exemplary embodiment shown in FIG. If the condensate to be removed, the Absperr ⁇ valve 8 is short-circuited, so that the pressure in the device increases and the condensate can drain off. It can be stored in a collecting container (not shown) until it is emptied.
- a pump 9 is arranged downstream of the collecting container 7, which pump is automatically actuated when a certain filling level of the collecting container 7 is reached, so that, in particular in the case of a low pressure Exhaust gas recirculation, which is connected to a pressure below the ambient level, no stopping of the exhaust gas flow as in the second embodiment erforder ⁇ is required to raise the negative pressure in the collecting container 7 to ambient level.
- a further possibility of an increase in pressure in the collecting container 7 is according to the fourth embodiment shown in FIG. 5 the provision of two valves 10 at the condensate inlet and condensate outlet thereof and a thin tube 11 with a regulating valve 12 which connects the collecting container 7 to the high-pressure side of the charge air line , so that when opening the control valve 12, the valve 10 is automatically closed at Konden ⁇ sateinlass, the pressure in the collecting container 7 increases and upon reaching a pressure level increased relative to the environment, the second valve 10 opens automatically at the condensate outlet, so that the Kon ⁇ condensate dissipated can be.
- a turbulence generator 13 is integrated in the line downstream of the exhaust gas cooler 2 in conjunction with a downstream annular channel 14 as condensate separator 3.
- the turbulence generator 13 By the turbulence generator 13, the exhaust gas stream with a Superimposed on rotational movement, so that in turn the condensate droplets forming on the basis of the reduced temperature after the exhaust gas cooler 2 are carried to the outside and deposited on the wall. Due to the speed component of the exhaust gas flow in the longitudinal direction, the condensate is entrained in the longitudinal direction and thus enters the channel 14, where it is discharged downwards and collects in a collecting container 7 according to the first embodiment. For emptying the collecting tank 7, in particular in the case of low-pressure exhaust gas recirculation, measures according to the embodiments described above are possible, for example.
- the arrangement of the condensate separator does not necessarily have to be directly downstream of the exhaust gas cooler.
- an arrangement after a subsequent intercooler is useful, especially if the temperature only reaches or falls below the dew point, so that in this case the charge air is cooled, which consists of de r intake air and the recirculated exhaust gas. Accordingly, in principle, the pure intake air can be dried.
- a filter according to the exhaust gas cooler which has a synthetic fleece, is arranged as a condensate separator.
- the condensate forming thereon collects and runs downwards, where it is collected in a collecting container.
- FIGS. 7 and 8 show examples of a possible arrangement of a condensate separator 3 in the case of high-pressure exhaust gas recirculation (FIG. 7) and in the case of low-pressure exhaust gas recirculation (FIG. 8).
- the configuration can be made in all cases according to the embodiments described above.
- the lines of Nieder ⁇ pressure side are in Figures 7 and 8 by thick solid lines shown, the high pressure side by dashed lines.
- the Strömungs ⁇ directions are each illustrated by arrows.
- the diversion of the exhaust gas to be recirculated takes place from the exhaust gas flow coming from the engine M on the high-pressure side, ie before a pressure reduction.
- the intake air is compressed in a compressor V, flows through a charge air cooler L, and is then supplied with the recirculated, cooled exhaust gas 3, which is dry after flowing through the condensate separator 3. Subsequently, the charge air flow is fed to the engine M.
- FIG. 8 shows an example of a low-pressure exhaust gas recirculation, wherein the exhaust gas to be recirculated is branched off from the exhaust gas flow coming from the engine M on the low-pressure side, that is to say after a pressure reduction.
- the exhaust gas to be recirculated is branched off from the exhaust gas flow coming from the engine M on the low-pressure side, that is to say after a pressure reduction.
- the compressor V and the subsequent charge air cooler L and to protect it from corrosion it is guided through the exhaust gas cooler 2 and the condensate separator 3 and only then supplied to the intake air.
- the charge air flow which is now formed by the recirculated exhaust gas and the intake air, is cooled in the intercooler L and fed to the engine M.
- a centrifugal separator with a rotating displacer or spinner 20 can be provided as condensate separator 3, in which case the displacer or spinner 20 on the elongated shaft 21 of the turbocharger, on which the compressor wheel 22 is arranged, is mounted before entering the Ver ⁇ denser V.
- the rotational speed of the centrifugal separator is coupled to the rotational speed of the compressor impeller 22, which is generally from 120,000 to 150,000 rpm.
- the deflection of the charge air flow due to the displacer or Schleuder ⁇ body 20 in conjunction with the compressor inlet is geometrically designed here so that more condensate drops are deposited, which have not deposited on the displacement or spinner 20.
- the displacer or spinner 20 is cup-shaped, the opening pointing in the direction of the compressor V. Due to the Z-like deflection of the charge air flow, in this case by 2 x about 180 °, were ⁇ the most condensate drops deposited before the charge air enters the compressor V.
- the presently made of an aluminum alloy displacer or spinner 20 is inserted end auf ⁇ on the shaft 21 and soldered to the same.
- FIG. 10 shows a displacer or spinner 20 for a radial condensate discharge according to the eighth exemplary embodiment of a condensate separator 3.
- the air is deflected outwards by approximately 90 °, so that the condensate droplets are displaced onto the displacer or spinner meet body 20 from which they are hurled due to the centrifugal force with high kinetic energy to the outside in an annular condensate drain leading to the channel 5, which has a schematically indicated Ven ⁇ tilmechanismus 23, which als ⁇ the high kinetic energy auf ⁇ striking condensate lets through, but prevents condensate backflow into the compressor chamber.
- the presently made of plastic displacer or spinner 20 is inserted end auf ⁇ on the shaft 21 and glued to the same, with as additional security, the Wei- lenende have a hexagonal shape and the displacer or Schleuder ⁇ body 20 have a corresponding inner shape.
- FIG. 11 shows a low-pressure exhaust gas recirculation with two-stage cooling of the recirculated exhaust gas (exhaust gas cooler 2) in addition to the (presently) one-stage charge air cooling (charge air cooler L).
- exhaust gas cooler 2 the exhaust gas coming from the engine M flows through the turbine T and, in the relaxed, cooled state, a subsequently arranged filter F is removed from the exhaust gas by means of its particles.
- Valve-controlled a part of the exhaust gas purified by particles can be recirculated at a branch, the remainder of the exhaust gas passes through the exhaust to the outside.
- the exhaust gas recirculation quantity is determined by the settling pressure gradient of exhaust back pressure and intake negative pressure, so that high exhaust gas recirculation quantities are possible with simple means.
- the recirculated part of the exhaust gas is passed through a two-stage exhaust gas cooler 2, wherein in the first stage 2 'a pre-cooling by the engine coolant, which circulates in an otherwise conventionally designed engine cooling circuit, takes place. If necessary, the exhaust gas temperature is further reduced in the second stage 2 ", while the second stage 2" is part of a low-temperature cooling circuit.
- This has an air-cooled Niedertem ⁇ temperature cooler NK, which is arranged in the air stream following the motor coolant cooling high-temperature radiator HK, a compressor K for circulating the coolant or refrigerant and in parallel branches a charge air cooler L and the second stage. 2 of the exhaust gas cooler 2, wherein the cooling or refrigerant distribution is controlled by means of valves.
- a valve-controlled if necessary available bypass B is provided, which runs parallel to the engine N / 1 and charge air can lead past the same.
- a condensate separator 3 is provided, with the aid of which condensate can be removed from the cold recirculated exhaust gas before it is mixed with the fresh air sucked in.
- a further condensate in particular a centrifugal separator as described above with clutchnah ⁇ me to the figures 9 or 10.
- a thermal condensate discharge 30 For disposal of the accumulating condensate, which is classified as hazardous substance and therefore can not be stored on board a vehicle, a thermal condensate discharge 30 is provided.
- the acids formed can be converted into non-critical components with the aid of a multi-stage thermal reactor.
- the condensate formed can be used for the precooling of the recirculated exhaust gas.
- FIG. 12 An example of the arrangement of such a condensate discharge 30 in ei ⁇ ner low-pressure exhaust gas recirculation is shown schematically in Figures 12 and 13.
- condensate which collects on the exhaust gas cooler 2, in front of the compressor V and in or after the charge air cooler L via lines gene to a central condensate collector 31 out of which it is fed via a line to a thermal reactor 32, the part of thermal condensate discharge 30 is.
- the thermal reactor 32 is subsequently integrated with the filter F in an exhaust manifold of the engine.
- the condensate-carrying lines in particular the Lei ⁇ tion from the condensate collector 31 to the thermal reactor 32, vor ⁇ lying on a cross section, which allows a promotion of the condensate due to capillary forces, so that can be despised on pumps.
- there is no essential storage of the resulting condensate in the engine system but the condensate is disturbed. directly passed to the thermal reactor 32, heated therein and then discharged.
- the condensate is used in a first stage S1 for cooling the recirculated exhaust gas, for which purpose a correspondingly formed heat exchanger forms the first stage 2 'of the exhaust duct 2, ie is arranged before the actual exhaust gas cooler 2 enters that substantially the entire enthalpy change of the condensate can be used for the first stage S 1 of the cooling of the exhaust gas.
- This causes a heating of the condensate.
- ribs or corresponding measures which increase the surface area are provided for optimizing the heat transfer of the exhaust gas heat to the condensate.
- a second step S2 the evaporation of the heated Konden ⁇ sats, whereby the further heating presently follows er ⁇ by means of a self-regulating PTC-Heizeemperents (Positive Thermal Coefficient) to about 250 to 300 0 C, and takes place in a third step S3, a Reheating to 350 to 450 0 C.
- PTC-Heizelements Positive Thermal Coefficient
- the PTC heating element is designed such that it automatically stops when no condensate has accumulated.
- the Resterhitzung the evaporated condensate in the third stage is carried out in the present case by means of an electrically heated Rohr ⁇ heater, which has a surface temperature of 350 to 450 ° C and Einbau ⁇ th or packing with a large surface area and possibly catalytic action.
- nitric acid decomposes into NO 2 , N 2 , H 2 O and O 2 and sulfuric acid or sulfurous acid in H 2 O and SO 2 or SO 3 according to the following reactions: 4 HNO 3 -> 4 NO 2 + 2 H 2 O + O 2 4 HNO 3 -> 2 N 2 + 2 H 2 O + 5 O 2 H 2 SO 4 -> SO 3 + H 2 OH 2 SO 3 -> SO 2 + H 2 O
- the now harmless condensate is fed to the exhaust gas stream and disposed of via the exhaust.
- an additional blower can be provided, which ensures compliance with the limit values regardless of the function of the condensate discharge 30.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Exhaust-Gas Circulating Devices (AREA)
Abstract
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP05812456A EP1825130A1 (fr) | 2004-10-25 | 2005-10-18 | Condensateur d'un systeme de turbocompresseur et procede d'utilisation d'un tel systeme |
US11/577,616 US20080028757A1 (en) | 2004-10-25 | 2005-10-18 | Condenser in a Turbo-Compressor System and Method for Operating One Such System |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004051922.6 | 2004-10-25 | ||
DE102004051922 | 2004-10-25 | ||
DE102005023957 | 2005-05-20 | ||
DE102005023957.9 | 2005-05-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2006045488A1 true WO2006045488A1 (fr) | 2006-05-04 |
Family
ID=35717711
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2005/011188 WO2006045488A1 (fr) | 2004-10-25 | 2005-10-18 | Condensateur d'un systeme de turbocompresseur et procede d'utilisation d'un tel systeme |
Country Status (3)
Country | Link |
---|---|
US (1) | US20080028757A1 (fr) |
EP (1) | EP1825130A1 (fr) |
WO (1) | WO2006045488A1 (fr) |
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WO2008129076A1 (fr) * | 2007-04-24 | 2008-10-30 | Mann+Hummel Gmbh | Agencement d'air comburant et de gaz d'échappement pour un moteur à combustion interne |
FR2922960A1 (fr) * | 2007-10-24 | 2009-05-01 | Valeo Systemes Thermiques | Systeme de reinjection de gaz de carter et echangeur de chaleur mis en oeuvre dans ledit systeme |
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EP1724453A1 (fr) * | 2005-05-20 | 2006-11-22 | Behr GmbH & Co. KG | Mécanisme de turbocompresseur et procédé d'utilisation de celui-ci |
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JP2010525231A (ja) * | 2007-04-24 | 2010-07-22 | マン ウント フンメル ゲゼルシャフト ミット ベシュレンクテル ハフツング | 排ガスターボチャージャを具えた内燃機関 |
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WO2008129076A1 (fr) * | 2007-04-24 | 2008-10-30 | Mann+Hummel Gmbh | Agencement d'air comburant et de gaz d'échappement pour un moteur à combustion interne |
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FR2922960A1 (fr) * | 2007-10-24 | 2009-05-01 | Valeo Systemes Thermiques | Systeme de reinjection de gaz de carter et echangeur de chaleur mis en oeuvre dans ledit systeme |
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US8151774B2 (en) | 2009-05-13 | 2012-04-10 | Deere & Company | Engine combustion air cyclonic pre-cleaner embodying throttling member adjusted in accordance with engine load |
EP2463494A3 (fr) * | 2010-12-07 | 2017-07-05 | Hyundai Motor Company | Appareil de système de refroidissement de véhicule et procédé de contrôle l'utilisant |
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Also Published As
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EP1825130A1 (fr) | 2007-08-29 |
US20080028757A1 (en) | 2008-02-07 |
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