DE1526448A1 - Internal combustion engine with exhaust gas turbocharger - Google Patents
Internal combustion engine with exhaust gas turbochargerInfo
- Publication number
- DE1526448A1 DE1526448A1 DE19661526448 DE1526448A DE1526448A1 DE 1526448 A1 DE1526448 A1 DE 1526448A1 DE 19661526448 DE19661526448 DE 19661526448 DE 1526448 A DE1526448 A DE 1526448A DE 1526448 A1 DE1526448 A1 DE 1526448A1
- Authority
- DE
- Germany
- Prior art keywords
- internal combustion
- exhaust gas
- combustion engine
- gas turbocharger
- intercooler
- 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.)
- Granted
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
- F02B29/045—Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
- F02B29/0462—Liquid cooled heat exchangers
-
- 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
- F02B29/0475—Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly the intake air cooler being combined with another device, e.g. heater, valve, compressor, filter or EGR cooler, or being assembled on a special engine location
-
- 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
- F02B67/00—Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for
- F02B67/10—Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for of charging or scavenging apparatus
-
- 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)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Description
den 28. März 1966 klöckner-humboldt-deutzag-köln r ^ς / / λ TP R/Dar D 66/30March 28, 1966 klöckner-humboldt-deutzag-köln r ^ ς / / λ TP R / Dar D 66/30
Brennkraftmaschine mit AbgasturboJt^3wr'^, ^Internal combustion engine with exhaust gas turboJt ^ 3wr '^, ^
Die Erfindung betrifft eine Brennkraftmaschine mit Abgasturbolader und Ladeluftkühler.The invention relates to an internal combustion engine with an exhaust gas turbocharger and intercooler.
Bei bekannten Brennkraftmaschinen wird die vorverdichtete Ladeluft vom Abgasturbolader zum Ladeluftkühler durch Luftleitungen zugeführt, die selbständige Bauteile darstellen. Diese Leitungen nehmen, insbesondere bei Brennkraftmaschinen mit hohen Aufladegraden, sehr viel Bauraum in Anspruch und müssen aus Platzmangel in strömungstechnisch ungünstigen formen verlegt den. Der Erfindung liegt die Aufgabe zugrunde, eine raumsparende und strömungsgünstige Luftführung zwischen Abgasturbolader und Ladeluftkühler zu ermöglichen. Dies wird erfindungsgemäß dadurch gelöst, daß der Abgasturbolader"<und der Ladeluftkühler an einem gemeinsamen Geräteträger angeordnet sind, der als Teil der Luftleitung zwischen Abgasturbolader und Ladeluftkühler ausgebildet ist.In known internal combustion engines, the pre-compressed charge air from the exhaust gas turbocharger to the intercooler through air lines supplied, which represent independent components. These lines take, especially in internal combustion engines with high Charging degrees, take up a lot of installation space and have to be laid in aerodynamically unfavorable shapes due to lack of space the. The invention is based on the object of a space-saving and aerodynamically favorable air duct between the exhaust gas turbocharger and intercooler to allow. This is according to the invention solved in that the exhaust gas turbocharger "<and the intercooler are arranged on a common device carrier, which is designed as part of the air line between the exhaust gas turbocharger and intercooler is.
Durch den erfindungsgemäßen Vorschlag erreicht man den Torteil, daß ein äußerst geringer Bauraum beansprucht wird, ohne dabei strömungsungünstige Leitungen in Kauf zu nehmen. Nach einer weiteren Ausgestaltung der Erfindung kann durch die Anordnung des Luftdurchtritts symmetrisch zu der in Strömungsrichtung liegenuun Mittelebene des Geräteträgers der weitere Yorteil erreicht werden, daß unabhängig von der Lage des Luftaustritts desThe proposal according to the invention achieves the gate part, that an extremely small installation space is required without having to accept lines that are unfavorable to the flow. After another The arrangement of the air passage means that the configuration of the invention can be symmetrical to that in the direction of flow Central plane of the device carrier of the further Yorteil can be achieved that regardless of the location of the air outlet of the
BADORK31NAL 909887/0668 -2-BADORK 31 NAL 909887/0668 -2-
D 66/50D 66/50
Abgasturboladers, rechts oder, links, ane kurze raumsparende Yerbindungsleitung zwischen Abgasturbolader und Geräteträger verwendet werden kann.Exhaust gas turbocharger, on the right or, on the left, ane short space-saving connection line can be used between the exhaust gas turbocharger and the equipment rack.
Der Geräteträger ist als selbständiges Bauteil der Maschinenart einfach anzupassen. Man ist daher in der konstruktiven Gestaltung dieses Leitungsteiles frei. Es können ohne bedeutenden Hehraufwand Mittel vorgesehen werden, die die Strömungsverhältnisse und die Kühlung dieses Teiles verbessern. Bei weiteren Ausgestaltungen der Erfindung wird daher vorgeschlagen, daß sich der Querschnitt das Luftdurchtritts im Geräteträger zum Ladeluftkühler hin erweitert, wodurch ein besonders strömungsgünstiger und verlustarmer Eintritt der Ladeluft in den Ladeluftkühler ermöglicht wird. Des weiteren wird vorgeschlagen, die Wandungen des Luftdurchtritts des Geräteträgers nur an einem Ende mit diesem fest zu verbinden. Dadurch können sie sich an dem anderen Ende frei unter Wärmeeinfluß ausdehnen. Schließlich kann es ebenfalls von Vorteil sein, die Wandungen des Luftdurchtrittes dee Geräteträgers zu kühlen. In diesem Fall werden in dem Geräteträger Kühlräume oder Kühlrippen vorgesehen.The device carrier is simple as an independent component of the machine type adapt. You are therefore free in the structural design of this line part. There can be funds without significant additional expenditure be provided that improve the flow conditions and the cooling of this part. In further embodiments of the invention it is therefore proposed that the cross-section of the air passage in the equipment rack to the intercooler widens, whereby a particularly streamlined and low-loss entry of the charge air into the charge air cooler is made possible. It is also proposed to connect the walls of the air passage of the device carrier to this only at one end. This allows them to get involved the other end freely expand under the influence of heat. Finally can It may also be advantageous to cool the walls of the air passage of the device carrier. In this case, in the equipment rack Cold rooms or cooling fins provided.
In den Zeichnungen werden beispielsweise Ausführungsformen der Erfindung dargestellt.In the drawings, for example, embodiments of the invention are shown.
Die Abb. 1 zeigt im Teilschnitt die Anordnung eines Abgasturbolader zum Ladeluftkühler.Fig. 1 shows a partial section of the arrangement of an exhaust gas turbocharger to the intercooler.
Die Abb. 2 zeigt ergänzend zu Abb. 1 die Ancrlnung von Kühlräumen im Geräteträger.Fig. 2 shows, in addition to Fig. 1, the alignment of cold rooms in the equipment rack.
909887/0556 - 3 -909887/0556 - 3 -
ORIGINALORIGINAL
28.3.1966March 28, 1966
-3ϊ52644β D66/3°- 3 ϊ52644β D66 / 3 °
Die Abb. 3 stellt einen Schnitt entsprechend der Linie III - III in Abb. 2 dar.Fig. 3 shows a section along the line III - III in Fig. 2.
An einer Brennkraftmaschine 1 ist ein Geräteträger 2 angeflanscht, der als Teil einer Luftleitung 3 zwischen einem Abgasturbolader 4 und einem Ladeluftkühler 5 ausgebildet ist. Der Abgasturbolader 4 und der Ladeluftkühler 5 sind am Geräteträger 2 befestigt und mit einem Flansch 6 bzw. 7 mit einem Luftdurchtritt 8 des Geräteträgers verbunden. Der Querschnitt des Luftdurchtritts im Geräteträger erweitert sich zum Ladeluftkühler hin, wodurch eine besonders strö- g mungstechnisch günstige Lösung erreicht wird. Die Wandungen des Luftdurchtrittes 8 sind an der Ladeluftkühlerseite 7 mit dem Geräteträgei verbunden, während sie an der Abgasturboladerseite 6 frei durch eine Öffnung des Geräteträgers geführt sind.An equipment carrier 2 is flanged to an internal combustion engine 1, which is designed as part of an air line 3 between an exhaust gas turbocharger 4 and a charge air cooler 5. The exhaust gas turbocharger 4 and the charge air cooler 5 are attached to the equipment rack 2 and with a flange 6 or 7 with an air passage 8 of the equipment rack tied together. The cross-section of the air passage in the equipment rack expands towards the charge air cooler, which creates a particularly streamlined system metrologically favorable solution is achieved. The walls of the air passage 8 are connected to the intercooler side 7 with the equipment carrier, while they are free on the exhaust gas turbocharger side 6 by a Opening of the device carrier are performed.
In der Abb. 2 sind die Wandungen für die Luftdurchtritte an beiden Enden mit dem Geräteträger fest verbunden, wodurch die Wandungen des Luftdurchtritts 8 mit den Wandungen des Geräteträgers 2 einen Kühlraum 9 bilden. Die Kühlmittelzufuhr erfolgt durch eine ÖffnungIn Fig. 2 the walls for the air passages are on both Ends firmly connected to the device carrier, whereby the walls of the air passage 8 with the walls of the device carrier 2 a Form refrigerator 9. The coolant is supplied through an opening
10, der Kühlmittelabfluß erfolgt durch eine Öffnung 11. '10, the coolant is drained through an opening 11. '
Die Abb. 3 zeigt einen Schnitt entsprechend der Linie III - III in Abb. 2, aus dem hervorgeht, daß der Luftdurchtritt symmetrisch su der in Strömungsrichtung liegenden Kittelebene 12 des Geräteträgers 2 angeordnet ist. Mit 13 sind Kühlrippen bezeichnet, die im Luftdurchtritt 8 angeordnet sind und eine Vorkühlung der Ladeluft bewirken. Fig. 3 shows a section along the line III - III in Fig. 2, from which it can be seen that the air passage is symmetrical su the center plane 12 of the device carrier lying in the direction of flow 2 is arranged. With 13 cooling fins are designated, which in the air passage 8 are arranged and cause a pre-cooling of the charge air.
909887/0556
BAD ORiG1NAL909887/0556
BAD ORiG 1 NAL
Claims (5)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEK0058908 | 1966-04-01 |
Publications (3)
Publication Number | Publication Date |
---|---|
DE1526448A1 true DE1526448A1 (en) | 1970-02-12 |
DE1526448B2 DE1526448B2 (en) | 1973-03-15 |
DE1526448C3 DE1526448C3 (en) | 1973-09-27 |
Family
ID=7228891
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1526448A Expired DE1526448C3 (en) | 1966-04-01 | 1966-04-01 | Device carrier designed as an independent structural unit for fastening a charging fan and other auxiliary devices to an internal combustion engine |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE1526448C3 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2389764A1 (en) * | 1977-05-05 | 1978-12-01 | Sulzer Ag | |
DE2833790A1 (en) * | 1978-08-02 | 1980-03-13 | Kloeckner Humboldt Deutz Ag | Water cooled IC engine - has turbocharger on bracket at engine front with charge air line near common chamber for charger and engine coolant |
EP0091066A1 (en) * | 1982-04-01 | 1983-10-12 | Bayerische Motoren Werke Aktiengesellschaft, Patentabteilung AJ-3 | Internal-combustion engine with a turbo charger |
DE102005012756A1 (en) * | 2005-03-19 | 2006-09-21 | Man B & W Diesel Ag | Internal combustion engine has low pressure loading device which is so formed that it is decoupled from engine by separating module whereby low pressure loading device is supported at separate framework or frame |
WO2011054515A1 (en) * | 2009-11-06 | 2011-05-12 | Mtu Friedrichshafen Gmbh | Charger/intercooler assembly |
DE102005039459B4 (en) * | 2005-08-20 | 2015-03-05 | Daimler Ag | Internal combustion engine with an exhaust gas turbocharger |
-
1966
- 1966-04-01 DE DE1526448A patent/DE1526448C3/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2389764A1 (en) * | 1977-05-05 | 1978-12-01 | Sulzer Ag | |
DE2833790A1 (en) * | 1978-08-02 | 1980-03-13 | Kloeckner Humboldt Deutz Ag | Water cooled IC engine - has turbocharger on bracket at engine front with charge air line near common chamber for charger and engine coolant |
EP0091066A1 (en) * | 1982-04-01 | 1983-10-12 | Bayerische Motoren Werke Aktiengesellschaft, Patentabteilung AJ-3 | Internal-combustion engine with a turbo charger |
DE102005012756A1 (en) * | 2005-03-19 | 2006-09-21 | Man B & W Diesel Ag | Internal combustion engine has low pressure loading device which is so formed that it is decoupled from engine by separating module whereby low pressure loading device is supported at separate framework or frame |
DE102005039459B4 (en) * | 2005-08-20 | 2015-03-05 | Daimler Ag | Internal combustion engine with an exhaust gas turbocharger |
WO2011054515A1 (en) * | 2009-11-06 | 2011-05-12 | Mtu Friedrichshafen Gmbh | Charger/intercooler assembly |
Also Published As
Publication number | Publication date |
---|---|
DE1526448C3 (en) | 1973-09-27 |
DE1526448B2 (en) | 1973-03-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
SH | Request for examination between 03.10.1968 and 22.04.1971 | ||
C3 | Grant after two publication steps (3rd publication) |