CN105863819A - Internal combustion engine and method for operating the same - Google Patents
Internal combustion engine and method for operating the same Download PDFInfo
- Publication number
- CN105863819A CN105863819A CN201610084599.0A CN201610084599A CN105863819A CN 105863819 A CN105863819 A CN 105863819A CN 201610084599 A CN201610084599 A CN 201610084599A CN 105863819 A CN105863819 A CN 105863819A
- Authority
- CN
- China
- Prior art keywords
- filling air
- exhaust
- aerofluxus
- turbine
- condensate
- 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.)
- Pending
Links
Classifications
-
- 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
-
- 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
- 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
-
- 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
- F02B29/0412—Multiple heat exchangers arranged in parallel or in series
-
- 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
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/013—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in series
-
- 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
- F01N2610/00—Adding substances to exhaust gases
-
- 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
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)
- Supercharger (AREA)
Abstract
The invention relates to an internal combustion engine and a method for operating the same. An internal combustion engine (10) is provided with a plurality of cylinders (11) and at least one exhaust gas turbocharger (14). In the exhaust gas turbocharger (14) or a turbine (13) of each exhaust gas turbocharger (14), exhaust gas in the leaving cylinders (11) is expandable, energy extracted in the process can be used for compressing filling air to be supplied to the cylinders (11) in a compressor (16) of a corresponding exhaust gas turbocharger (14), a filling air cooling device (19) is positioned on upstream of the compressor (16) of the corresponding exhaust gas turbocharger (14), and therefore the filling air can be cooled after being compressed via the compressor (16) of the exhaust gas turbocharger (14). When the filling air is cooled, condenstated materials accumulated in the corresponding filling air cooling device (19) can be supplied into the exhaust gas.
Description
Technical field
The present invention relates to the explosive motor of preamble according to claim 1.The invention still further relates to preamble according to claim 7 for the method operating explosive motor.
Background technology
Air-discharging and supercharging explosive motor (exhaust gas supercharged internal combustion engine) is sufficiently known from practice.Therefore, air-discharging and supercharging explosive motor includes at least one exhaust turbine supercharger, and wherein, the aerofluxus of the cylinder leaving explosive motor can expand in the turbine of this exhaust turbine supercharger or each exhaust turbine supercharger.The energy extracted during the expansion of aerofluxus is used in the compressor of corresponding exhaust turbine supercharger, in order to compress the combustion air of the cylinder to be fed to explosive motor.Typically, filling air cooler is arranged in the downstream of associated compressors of corresponding exhaust turbine supercharger, in order to be cooled in associated compressors the filling air of compression in the region of respective air cooler.
In the cooling period of the filling air of compression, in the region of corresponding filling air cooler, condensate can be accumulated, because in the cooling period of filling air, the absorbability of water is reduced by cooling air.In the case of the known explosive motor of practice, this condensate is discharged from explosive motor and is disposed.
Summary of the invention
Setting about from this, the present invention is based on creating novel internal combustion engine and for operating the target of its method.
This target is solved by explosive motor according to claim 1.According to the present invention, the condensate accumulated in corresponding filling air cooler in the cooling period of filling air can be supplied in aerofluxus.
In the case of according to the explosive motor of the present invention, the condensate accumulated in corresponding filling air cooler in filling air cooling period is not discharged from explosive motor and is disposed, but is supplied in aerofluxus.Therefore, aerofluxus is cooled down in the upstream of the respective turbine of corresponding exhaust turbine supercharger.This is favourable in so-called torrid zone operator scheme (tropical operating mode) close to exhaust temperature limit value of explosive motor.And, it is no longer necessary to dispose any condensate.
According to first other favourable development, explosive motor includes single exhaust turbine supercharger, wherein, the condensate accumulated in the filling air cooler of the compressor of exhaust turbine supercharger in the cooling period of filling air can be supplied in aerofluxus in the upstream of the turbine of exhaust turbine supercharger.According to second, alternative other favourable development, explosive motor includes having the first exhaust turbocharger of high-pressure turbine and high pressure compressor and have the second exhaust turbocharger of low-pressure turbine and low pressure compressor, wherein, the condensate accumulated in the filling air cooler of the high pressure compressor of first exhaust turbocharger in the cooling period of filling air can be supplied in aerofluxus in the upstream of the high-pressure turbine of first exhaust turbocharger.The condensate accumulated in the filling air cooler of the low pressure compressor of second exhaust turbocharger in the cooling period of filling air can be supplied in aerofluxus in the upstream of the high-pressure turbine of first exhaust turbocharger and/or be supplied in aerofluxus in the upstream of the low-pressure turbine of second exhaust turbocharger.In first other favourable development of the present invention and in the case of second other favourable development of the present invention, in the region of filling air cooler, the condensate of accumulation can be supplied in aerofluxus in a limiting fashion.
Preferably, condensate can be supplied in aerofluxus via pipeline, and this pipeline starts from filling airline or starts to extend to the direction of pumping-out line from corresponding filling air cooler.This structure is simple at design aspect.
Limit in Patent right requirement 7 for operating the method according to the invention of explosive motor.
Accompanying drawing explanation
Other development preferred of the present invention can be obtained by dependent claims and following description.The example embodiment of the present invention obtains more detailed description with the help of the attached drawing, and is not limited to it.It illustrates:
Fig. 1 is the figure of the first explosive motor according to the present invention；
Fig. 2 is the figure of the second explosive motor according to the present invention；
Fig. 3 is the figure of the 3rd explosive motor according to the present invention；And
Fig. 4 is the figure of another explosive motor according to the present invention.
List of reference characters
10 explosive motors
11 cylinders
12 aerofluxuss
13 turbines
13a high-pressure turbine
13b low-pressure turbine
14 exhaust turbine superchargers
14a exhaust turbine supercharger
14b exhaust turbine supercharger
15 aerofluxuss
16 compressors
16a high pressure compressor
16b low pressure compressor
17 burning gases
18 filling air
18a filling air
18b filling air
19 filling air coolers
19a filling air cooler
19b filling air cooler
20 filling air
21 condensates
21a condensate
21b condensate
22 pumps
23 pumping-out lines
24 filling airline
25 pipelines.
Detailed description of the invention
The present invention relates to explosive motor and the method relating to operate this kind of explosive motor.
Fig. 1 illustrates the first example embodiment of the explosive motor 10 according to the present invention with multiple cylinder 11, and wherein, fuel burns in the cylinder 11 of explosive motor 10.The aerofluxus 12 of the cylinder 11 leaving explosive motor can be supplied to the turbine 13 of exhaust turbine supercharger 14 in FIG via pumping-out line, and wherein, aerofluxus 12 expands in turbine 13 and leaves turbine 13 as the aerofluxus 15 expanded.
The energy extracted during aerofluxus 12 expands in the turbine 13 of exhaust turbine supercharger 14 is used in the compressor 16 of exhaust turbine supercharger, so that compression and combustion air 17 and the filling air 18 as compression provide to explosive motor 10 via filling airline 24, i.e. its cylinder 11.At this, the compressor 16 of exhaust turbine supercharger 14 is assigned filling air cooler 19, in the region of this filling air cooler 19, the filling air 18 compressed in compressor 16 can be cooled, in order to supplies, to the cylinder 11 of explosive motor 10, the filling air 20 cooled down.
In the case of the explosive motor 10 according to the present invention, can be supplied in aerofluxus at filling air 18 condensate 21 that cooling period is formed in filling air cooler 19, i.e. be supplied to leave in the aerofluxus 12 of the cylinder 11 of explosive motor 10.
In this process, condensate 21 is introduced in aerofluxus 12 in the case of the distance of the enough evaporation loops being available for condensate 21 of exhaust turbine supercharger 14 turbine 13 upstream, so that in the region of the turbine 13 of exhaust turbine supercharger 14, all of condensate 21 evaporates.Complicated condensate is disposed and can be omitted in the present case.By means of the condensate 21 evaporation in aerofluxus 12, the temperature of aerofluxus 12 can be lowered, and this is especially when being favourable in the so-called torrid zone operator scheme operated near its temperature extremes at turbine 13.
Fig. 2 illustrates the explosive motor 10 with two-stage air-discharging and supercharging, wherein, leave explosive motor 10 cylinder 11 aerofluxus 12 first via first exhaust turbocharger 14a high-pressure turbine 13a via pumping-out line 23 and subsequently low-pressure turbine 13b via second exhaust turbocharger 14b directed.The aerofluxus 12 expanded in two turbines 13a, 13b leaves explosive motor as the aerofluxus 15 expanded.
The energy extracted in turbine 13a, 13b is used in compressor 16a, 16b of exhaust turbine supercharger 14a, 14b, in order to compression and combustion air 17 step by step in them.Here, each compressor 16a, 16b are each assigned filling air cooler 19a, 19b, in order to filling air 18a, 18b of the compression of associated compressors 14a, 14b is left in cooling.Therefore, the filling air 18b of the low pressure compressor 16b leaving second exhaust turbocharger 14b is cooled down in the region of filling air cooler 16b.The filling air 18a of the high pressure compressor 16a leaving first exhaust turbocharger 14a is cooled down in the region of filling air cooler 19a.The filling air 20 obtaining cooling in the region of filling air cooler 19a is supplied the cylinder 11 to explosive motor 10 via filling airline 24.
In the example embodiment of Fig. 2, the condensate 21a accumulated in the filling air cooler 19a of high pressure compressor 16a in the cooling period of filling air 18a is provided to aerofluxus 12, i.e., upstream at high-pressure turbine 13a, wherein, in the region of the filling air cooler 19b of low pressure compressor 16b accumulation condensate 21b by the supplied upstream at low-pressure turbine 13b to aerofluxus.At this, corresponding condensate 21a and 21b is supplied to aerofluxus respectively by the upstream at corresponding turbine 13a and 13b respectively in the way of can obtaining the enough evaporation loops being respectively used to evaporative condenser thing 21a and 21b, so that respectively in the region of corresponding turbine 13a and 13b, all of condensate evaporative.
In the case of multistage air-discharging and supercharging, the form of Fig. 3 is preferred.In the case of the form of Fig. 3, in the region of the filling air cooler 19b of low pressure compressor 16b, the condensate 21b of accumulation is as the condensate 21a of accumulation in the region at the filling air cooler 19a of high pressure compressor 16a, in the supplied upstream of high-pressure turbine 13a of first exhaust turbocharger 14a to the aerofluxus 12 leaving cylinder 11, i.e., for equally with the evaporation of the upstream of condensate 21a, 21b in the aerofluxus 12 of to(for) high-pressure turbine 13a, the mode of the enough evaporation loops that can obtain.
In order to will in the region at the filling air cooler 19b of low pressure compressor 16b the condensate 21b of accumulation in the supplied upstream of high-pressure turbine 13a to aerofluxus 12, pump 22 is provided in figure 3, under it helps, the barometric gradient between the area of low pressure of air-discharging and supercharging and high-pressure area can be overcome.
Fig. 4 illustrates a form of the present invention, wherein, in the region of the filling air cooler 19b of low pressure compressor 16b the condensate 21b of accumulation by partly via pump 22 together with the condensate 21a of accumulation in the region at the filling air cooler 19a of high pressure compressor 16a in the supplied upstream of high-pressure turbine 13a to aerofluxus 12, and another part of condensate 21b is sent back in aerofluxus by the upstream at low-pressure turbine 13b.
Therefore, it is an object of the invention to not discharge and dispose from explosive motor, at the condensate that the cooling period of filling air is accumulated in filling air cooler, but send described condensate back to aerofluxus, in order to reduce delivery temperature from there through condensate evaporation in aerofluxus.
Corresponding filling air cooler 19,19a, 19b region in accumulation condensate 21,21a, 21b can corresponding filling air cooler 19,19a, 19b region in by so-called condensate trap (not shown) from filling air separation.
By means of pipeline 25, condensate 21,21a, 21b can be guided from corresponding filling air cooler 19,19a, 19b filling airline 24 direction started towards pumping-out line 23 respectively, in order to mixed with aerofluxus by condensate.
Claims (10)
- null1. an explosive motor (10)，There is multiple cylinder (11)，And there is at least one exhaust turbine supercharger (14、14a、14b)，Wherein，At this exhaust turbine supercharger (14、14a、14b) or each exhaust turbine supercharger (14、14a、Turbine (13 14b)、13a、In 13b)，The aerofluxus leaving cylinder (11) is inflatable，And wherein，The energy extracted in this process can be used for so that at corresponding exhaust turbine supercharger (14、14a、Compressor (16 14b)、16a、In 16b), compression is to be fed to the filling air of cylinder (11)，And wherein，Filling air cooler (19、19a、19b) it is positioned at corresponding exhaust turbine supercharger (14、14a、Compressor (16 14b)、16a、Downstream 16b)，So that at filling air at corresponding exhaust turbine supercharger (14、14a、Compressor (16 14b)、16a、This filling air is cooled down after compression in 16b)，It is characterized in that，In cooling period of filling air at corresponding filling air cooler (19、19a、The condensate (21 of accumulation in 19b)、21a、21b) can be fed in aerofluxus.
- Explosive motor the most according to claim 1, it is characterized in that, it includes single exhaust turbine supercharger (14), wherein, the cooling period condensate (21) of accumulation in the filling air cooler (19) of the compressor (16) of exhaust turbine supercharger (14) at filling air can be supplied in aerofluxus in the upstream of the turbine (13) of exhaust turbine supercharger (14).
- Explosive motor the most according to claim 1, it is characterized in that, its first exhaust turbocharger (14a) including there is high-pressure turbine (13a) and high pressure compressor (16a) and there is the second exhaust turbocharger (14b) of low-pressure turbine (13b) and low pressure compressor (16b), wherein, cooling period condensate (21a) of accumulation in the filling air cooler (19a) of the high pressure compressor (16a) of first exhaust turbocharger (14a) at filling air can be supplied in aerofluxus in the upstream of the high-pressure turbine (13a) of first exhaust turbocharger (14a).
- Explosive motor the most according to claim 3, it is characterized in that, the cooling period condensate (21b) of accumulation in the filling air cooler (19b) of the low pressure compressor (16b) of second exhaust turbocharger (14b) at filling air can be supplied in aerofluxus in the upstream of the high-pressure turbine (13a) of first exhaust turbocharger (14a).
- 5. according to the explosive motor described in claim 3 or 4, it is characterized in that, the cooling period condensate (21b) of accumulation in the filling air cooler (19b) of the low pressure compressor (16b) of second exhaust turbocharger (14b) at filling air can be supplied in aerofluxus in the upstream of the low-pressure turbine (13b) of second exhaust turbocharger (14b).
- 6. according to the explosive motor described in any one in claim 1 to 5, it is characterized in that, condensate (21,21a, 21b) can be supplied in aerofluxus via pipeline (25), and described pipeline (25) starts from filling airline (24) or starts to extend to the direction of pumping-out line (23) from corresponding filling air cooler (19,19a, 19b).
- 7. one kind has multiple cylinder and the method for the explosive motor with at least one exhaust turbine supercharger for operation, wherein, in the turbine of this exhaust turbine supercharger or each exhaust turbine supercharger, leave the exhaust expansion of cylinder, and wherein, the energy extracted in this process is for compress the filling air to be fed to cylinder in the compressor of corresponding exhaust turbine supercharger, and wherein, downstream at the compressor of corresponding exhaust turbine supercharger, filling air is cooled down in filling air cooler, it is characterized in that, the condensate accumulated in the compressor of corresponding exhaust turbine supercharger in the cooling period of filling air is supplied to aerofluxus.
- Method the most according to claim 7, it is characterized in that, the condensate accumulated in the filling air cooler of the high pressure compressor of first exhaust turbocharger in the cooling period of filling air is supplied in aerofluxus in the upstream of the high-pressure turbine of first exhaust turbocharger.
- Method the most according to claim 8, it is characterized in that, the condensate accumulated in the filling air cooler of the low pressure compressor of second exhaust turbocharger in the cooling period of filling air is supplied in aerofluxus in the upstream of the high-pressure turbine of first exhaust turbocharger.
- Method the most according to claim 8 or claim 9, it is characterized in that, the condensate accumulated in the filling air cooler of the low pressure compressor of second exhaust turbocharger in the cooling period of filling air is supplied in aerofluxus in the upstream of the low-pressure turbine of second exhaust turbocharger.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102015001663.6A DE102015001663A1 (en) | 2015-02-10 | 2015-02-10 | Internal combustion engine and method for operating the same |
| DE102015001663.6 | 2015-02-10 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105863819A true CN105863819A (en) | 2016-08-17 |
Family
ID=56498090
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610084599.0A Pending CN105863819A (en) | 2015-02-10 | 2016-02-14 | Internal combustion engine and method for operating the same |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JP6636352B2 (en) |
| KR (1) | KR102328548B1 (en) |
| CN (1) | CN105863819A (en) |
| DE (1) | DE102015001663A1 (en) |
| FI (1) | FI129817B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102016213936A1 (en) * | 2016-07-28 | 2018-02-01 | Mahle International Gmbh | Internal combustion engine with a charge air cooler |
| JP2021124181A (en) * | 2020-02-06 | 2021-08-30 | マツダ株式会社 | Automatic transmission |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2018358A (en) * | 1978-04-05 | 1979-10-17 | Maschf Augsburg Nuernberg Ag | Exhaust-gas turbocharged internal combustion engine |
| FR2940366A1 (en) * | 2008-12-22 | 2010-06-25 | Renault Sas | Gaseous mixture i.e. flue gas and air mixture, processing device for internal combustion engine, has closing unit connected to downstream portion such that inlet pipe is located between closing unit and heat exchanger |
| CN103485943A (en) * | 2012-06-07 | 2014-01-01 | 三菱自动车工业株式会社 | Condensation water drain control mechanism |
| CN103575159A (en) * | 2012-08-07 | 2014-02-12 | 福特环球技术公司 | Method for discharging condensate from a turbocharger arrangement |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE19961610A1 (en) * | 1999-12-21 | 2001-04-05 | Daimler Chrysler Ag | Internal combustion engine with two exhaust gas turbochargers for motor vehicle, has control unit that increases/decreases variable geometry turbine cross-section for high/low engine speed |
| JP2007138798A (en) * | 2005-11-17 | 2007-06-07 | Isuzu Motors Ltd | Multiple stage supercharging system |
| JP5626017B2 (en) * | 2011-02-28 | 2014-11-19 | 三菱自動車工業株式会社 | Condensate drain device |
-
2015
- 2015-02-10 DE DE102015001663.6A patent/DE102015001663A1/en not_active Withdrawn
-
2016
- 2016-02-02 KR KR1020160012780A patent/KR102328548B1/en active IP Right Grant
- 2016-02-09 JP JP2016022471A patent/JP6636352B2/en active Active
- 2016-02-09 FI FI20165091A patent/FI129817B/en active IP Right Grant
- 2016-02-14 CN CN201610084599.0A patent/CN105863819A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2018358A (en) * | 1978-04-05 | 1979-10-17 | Maschf Augsburg Nuernberg Ag | Exhaust-gas turbocharged internal combustion engine |
| FR2940366A1 (en) * | 2008-12-22 | 2010-06-25 | Renault Sas | Gaseous mixture i.e. flue gas and air mixture, processing device for internal combustion engine, has closing unit connected to downstream portion such that inlet pipe is located between closing unit and heat exchanger |
| CN103485943A (en) * | 2012-06-07 | 2014-01-01 | 三菱自动车工业株式会社 | Condensation water drain control mechanism |
| CN103575159A (en) * | 2012-08-07 | 2014-02-12 | 福特环球技术公司 | Method for discharging condensate from a turbocharger arrangement |
| US20140041381A1 (en) * | 2012-08-07 | 2014-02-13 | Ford Global Technologies, Llc | Method for discharging condensate from a turbocharger arrangement |
Also Published As
| Publication number | Publication date |
|---|---|
| DE102015001663A1 (en) | 2016-08-11 |
| JP2016148332A (en) | 2016-08-18 |
| FI129817B (en) | 2022-09-15 |
| KR102328548B1 (en) | 2021-11-17 |
| KR20160098048A (en) | 2016-08-18 |
| FI20165091A (en) | 2016-08-11 |
| JP6636352B2 (en) | 2020-01-29 |
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| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information | ||
| CB02 | Change of applicant information |
Address after: Augsburg Applicant after: MAN ENERGY SOLUTIONS SE Address before: Augsburg Applicant before: Man Diesel & Turbo SE |
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160817 |