The invention relates to a circuit arrangement for cooling charge air in a motor vehicle equipped with a turbocharger, and to a method for operating a circuit arrangement of this type. According to the prior art, to increase the power of engines, turbochargers are used in order to increase the throughput of air in the engine. In the compression needed for this, the air, designated below as charge air, is heated because of the compression in the turbocharger. To compensate for the loss of density associated with the heating of the charge air, i.e. in order to increase the air density, air coolers are used which are arranged at the front of the cooling module and serve for cooling the charge air. The charge air in this case flows through a heat exchanger, through which ambient air flows and which is consequently cooled. It is thereby possible to cool the charge air to a temperature which is approximately 15 K above the temperature of the ambient air.
It is furthermore known that the cooling of the charge air takes place via a coolant circuit, for example a low-temperature circuit, in which the coolant is cooled to very low temperatures. By means of this cold coolant, the charge air is cooled down to a predetermined cooling temperature in a charge air/coolant cooler. For the connection of the low-temperature circuit, there are two variants, namely an integration of the low-temperature circuit into a secondary circuit of the engine cooling system or a design in the form of a separate circuit.
If the engine output is to be further increased, the known supercharging systems have their limits, with respect to supercharging rates and response characteristics, at low load.
The object of the invention is to improve a circuit arrangement of the type mentioned in the introduction.
According to the invention, a circuit arrangement is proposed comprising a low-temperature circuit for cooling charge air that is fed to an engine in a motor vehicle equipped with a turbocharger, characterized in that the charge air is compressed in two stages in a first low-pressure turbocharger and a second high-pressure turbocharger, where, in order to cool the charge air, a first cooler is provided downstream of the low-pressure turbocharger and upstream of the high-pressure turbocharger, and a second cooler is provided downstream of the high-pressure turbocharger and upstream of the engine. By means of the intermediate cooling downstream of the first low-pressure turbocharger, it is possible to ensure that excessively high air temperatures do not arise, as a result of which the service time of the used components, which are exposed to the high temperatures, can be increased. The two-stage cooling exhibits an advantageous dynamic behavior. Since the intermediate cooling in partial load takes up scarcely any thermal loads, the coolant contained in the low-temperature circuit is cooled to a low temperature level just above the ambient temperature. This results in a substantial cooling power reserve which can be utilized when switching to high engine load.
The installation space required is relatively small compared to the known solutions, since, despite the intermediate cooling, there is only one charge air line to and from the cooling module, and only one coolant-cooled charge air cooler to be arranged near the engine.
A low-pressure charge air/coolant cooler is preferably provided for the first cooling of the charge air, and a high-pressure charge air/air cooler is provided for the second cooling of the charge air. In this case, stability problems are avoided in the air-cooled high-pressure charge air/air cooler particularly through the intermediate cooling.
The installation space can be utilized optimally by virtue of the fact that the high-pressure charge air/air cooler is arranged directly alongside a low-temperature cooler and, seen in the direction of air flow of the cooling air, upstream of a main coolant cooler. The front face of the low-temperature cooler takes up preferably 20% to 50% of the total front surface.
According to a preferred variant, the low-temperature circuit is part of an engine cooling circuit, but it can also be designed separately from this, and a control system for cutting down on costs is not absolutely essential. Also possible is an intermediate cooling with air and/or a cooling of the charge air downstream of the second compression stage with the aid of a coolant.
The invention is explained in detail below on the basis of two illustrative embodiments and with reference to the drawing, in which:
After the cooling in the low-pressure charge air/coolant cooler 3, the charge air 13 passes into the high-pressure turbocharger 2 in which it is further compressed to its end pressure, which is in turn associated with heating. In order to increase the charge air density in the (combustion) engine 8, the hot charge air 13 is cooled in a charge air/air cooler 4 before being fed to the engine 8. As a result of the intermediate cooling, it is possible to ensure that the maximum charge air temperatures after the last turbocharger stage remain limited to a degree which permits the use of air-cooled charge air coolers (cf.
The low-pressure charge air/coolant cooler 3 for the intermediate cooling is arranged near the engine and is supplied by the separate low-temperature circuit NK. An air cooler, hereinafter referred to as low-temperature cooler 5, is provided in the low-temperature circuit NK and is traversed by the low-temperature coolant 14 flow in connection with the low-pressure charge air/coolant cooler 3.
As is shown in
The coolers are in this case arranged in such a way that coolers which are at a low medium temperature level are positioned in the cold cooling air stream and coolers which are at a high temperature level are positioned in the warm cooling air stream.
The low-temperature coolant 14 flows onward to the pump 10, which ensures circulation of the coolant 14, and from there back to the low-pressure charge air/coolant cooler 3.
According to the present illustrative embodiment, the low-temperature coolant circuit NK is not controlled; it can be set in such a way that the best possible charge air cooling is achieved but boiling problems in the coolant 14 cannot however occur. The low-temperature coolant circuit NK contains relatively little coolant 14. The boiling problems are easily avoided because very high charge air temperatures do not occur at the outlet of the first compressor stage.
The engine 8 is cooled by an engine cooling circuit MK in which an engine coolant 12 flows. The coolant 12 cooled in the main coolant cooler 6 is fed to the engine 8 via the pump 9. The control of the cooling performance is effected via a bypass thermostat 11 in a manner known per se.
In a departure from the first illustrative embodiment, no separate low-temperature circuit NK is provided in the second illustrative embodiment. The coolant 14 is instead branched off from the engine cooling circuit MK from the pressure side of the pump 9 and is fed to the low-temperature cooler 5. In the low-temperature cooler 5, the coolant 14 is sharply cooled and then flows to the coolant-cooled low-pressure charge air/coolant cooler 3, where it serves for the intermediate cooling of the charge air 13. The coolant 14 is then mixed again at the engine outlet with the coolant stream of the engine cooling circuit MK.
Number | Date | Country | Kind |
---|---|---|---|
103 35 567 | Jul 2003 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/EP2004/007827 | 7/15/2004 | WO | 00 | 1/26/2006 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2005/012707 | 2/10/2005 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3257797 | Lieberherr | Jun 1966 | A |
3355877 | Chaffiotte | Dec 1967 | A |
3977195 | Treuil | Aug 1976 | A |
4485624 | Melchior | Dec 1984 | A |
5269143 | Cikanek et al. | Dec 1993 | A |
5394854 | Edmaier et al. | Mar 1995 | A |
5598705 | Uzkan | Feb 1997 | A |
6273076 | Beck et al. | Aug 2001 | B1 |
6378308 | Pfluger | Apr 2002 | B1 |
6397598 | Pierpont | Jun 2002 | B1 |
6412279 | Coleman et al. | Jul 2002 | B1 |
6460519 | Pierpont | Oct 2002 | B1 |
6564783 | Chou et al. | May 2003 | B2 |
6619379 | Ambros et al. | Sep 2003 | B1 |
6651618 | Coleman et al. | Nov 2003 | B1 |
6688280 | Weber et al. | Feb 2004 | B2 |
6782849 | Roithinger | Aug 2004 | B2 |
6848397 | Haase | Feb 2005 | B2 |
6877317 | Kurihara et al. | Apr 2005 | B2 |
6883314 | Callas et al. | Apr 2005 | B2 |
6918251 | Yanagisawa et al. | Jul 2005 | B2 |
6981375 | Sisken et al. | Jan 2006 | B2 |
20020056444 | Chou et al. | May 2002 | A1 |
Number | Date | Country |
---|---|---|
006 051 | Mar 2003 | AT |
006 106 | Apr 2003 | AT |
2923852 | Dec 1979 | DE |
199 48 220 | Jan 2001 | DE |
696 17 090 | Jun 2002 | DE |
0 522 471 | Jan 1993 | EP |
1270896 | Jan 2003 | EP |
1 336 735 | Oct 2005 | EP |
2001-342839 | Dec 2001 | JP |
2004116489 | Apr 2004 | JP |
1546683 | Feb 1990 | SU |
WO 2006086211 | Aug 2006 | WO |
Number | Date | Country | |
---|---|---|---|
20060185362 A1 | Aug 2006 | US |