CHARGING SYSTEM OF AN INTERNAL COMBUSTION ENGINE

Abstract

A charging system (20) of an internal combustion engine has a compressor (22) that compresses intake air (41) to a pressure higher than a boost pressure of the internal combustion engine. A first energy recovery turbine (25) recovers energy from an exhaust gas mass flow (45) discharged from a cylinder (12). The compressor (22) and the first energy recovery turbine (25) are disposed on a first shaft (31) and the recovered energy is transmitted directly to the compressor (22). A cooling turbine (24) expands and cools the (intake) air (41) compressed by the compressor (22) to the boost pressure required by the cylinder (12). A second energy recovery turbine (26) recovers energy from the exhaust gas mass flow (45). The second energy recovery turbine (26) and the cooling turbine (24) are on a common second shaft (32), and the second shaft (32) is coupled to at least one energy sink.

Claims

1. A charging system (20) for an internal combustion engine (10) having at least one cylinder (12), comprising: a compressor (22) that compresses intake air (41) and produces a pressure that is higher than a boost pressure of a boost air (44) when the cylinder (12) is being filled; a first energy recovery turbine (25) that recovers energy from an exhaust gas mass flow (45) discharged from the cylinder (12), the compressor (22) and the first energy recovery turbine (25) being disposed on a first shaft (31); a cooling turbine (24) that expands and cools the compressed air (42) to the required boost pressure; and a second energy recovery turbine (26) that recovers energy from an exhaust gas mass flow (45) discharged from the cylinder (12), wherein the cooling turbine (24) and the second energy recovery turbine (26) are disposed on a second shaft (32), wherein the second shaft (32) is coupled to at least one energy sink.

2. The charging system (20) of claim 1, further comprising a boost air cooler (23) that cools the air (42) compressed by the compressor (22) so that the air (42) compressed by the compressor (22) is cooled by the cooling turbine (24) and the boost air cooler (23).

2. The charging system (20) of claim 3, wherein the boost air cooler (23) is disposed between the compressor (22) and the cooling turbine (24).

3. The charging system (20) of claim 1, wherein the cooling turbine (24) is configured to expand and cool the compressed air (42) such that the temperature of the compressed air (42) is the same as or less than an ambient temperature of the intake air (41).

4. The charging system (20) of claim 1, wherein the second shaft (32) is coupled to the drive train as an energy sink.

5. The charging system (20) of claim 4, wherein the second shaft (32) is coupled to the energy sink by a planetary gear.

6. The charging system (20) of claim 1, wherein the second shaft (32) is coupled to the energy sink between the cooling turbine (24) and the second energy recovery turbine (26).

7. The charging system (20) of claim 4, wherein the coupling between the second shaft (32) and the energy sink on the side of the cooling turbine (24) takes place outside a portion on the second shaft (32) between the cooling turbine (24) and the second energy recovery turbine (26).

8. The charging system (20) of claim 1, further comprising an air filter (21) that is configured to filter the intake air.

9. A method for providing boost air (44) for a cylinder (12) of an internal combustion engine (10), comprising: operating a compressor (22) to compress intake air (41) to compressed air (42) at a pressure that is higher than a boost pressure of the internal combustion engine (10), operating a cooling turbine (24) for cooling the compressed air (42) and then relaxing the compressed air (42) to the boost pressure and feeding a resulting boost air (44) to the cylinder (12), recovering energy from the exhaust gas mass flow (45) by a first energy recovery turbine (25) and a second energy recovery turbine (26), wherein the recovered energy from the first energy recovery turbine (25) is used to operate the compressor (22), wherein the second energy recovery turbine (26) and the cooling turbine (24) transmit energy to a second shaft (32) and the energy from the second shaft (32) is transmitted to an energy sink.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0020] FIG. 1 shows a charging system 20 for an internal combustion engine according to an embodiment of the invention.

DETAILED DESCRIPTION

[0021] FIG. 1 shows an embodiment of the charging system 20 for an internal combustion engine 10 that has an engine block 11 and six cylinders 12. The charging system 20 is responsible for supplying the boost air 44 required for combustion in the cylinders 12. The components of the charging system 20 are a compressor 22, an intercooler 23, a cooling turbine 24 and first and second energy recovery turbine 25, 26.

[0022] Intake air 41 drawn in by the internal combustion engine 10 first reaches an air filter 21 that first filters the intake air 41 and thus removes from the air pollutants or constituents that are harmful to the components of the charging system 20. The intake air 41 then enters a compressor 22 that compresses the intake air 41 to a pressure that is higher than the boost pressure of the boost air when it flows into the cylinder 12. Compression also increases the temperature of the compressed air 42. To lower the temperature again, the compressed air 42 is directed into the boost air cooler 23 and the cooled air 43 then passes to the cooling turbine 24 where the air is expanded to the boost pressure and cooled. This arrangement makes it possible to cool the boost air 44 to such an extent that its temperature is below the temperature of the intake air 41 and thus also below the ambient temperature and the necessary boost pressure is nonetheless present. The cooled boost air 44 then enters the cylinders 12.

[0023] After combustion in the cylinders 12, an exhaust gas mass flow 45 is discharged during the exhaust stroke of the cylinder, is divided and enters the first and the second energy recovery turbines 25, 26. The two energy recovery turbines are disposed in parallel. The first energy recovery turbine 25 is disposed with the compressor 22 on a common first shaft 31, and the first energy recovery turbine 25 can then operate the compressor 22. The second energy recovery turbine 26 is disposed with the cooling turbine 24 on a common second shaft 32. Thus, both the second energy recovery turbine 26 and the cooling turbine 24 transmit an accelerating torque to the second shaft 32. The second shaft 32 is coupled to an energy sink via a gearing 33, so that the rotational energy transmitted to the second shaft 32 can either be reused directly, for example to operate the boost air cooler 23, or temporarily stored in a battery or other energy store. The gearing 33 is embodied as a planetary gear, for example, and in the shown embodiment is disposed in the vicinity of the cooling turbine 24 on a portion of the second shaft 32 that is not located between the cooling turbine 24 and the second energy recovery turbine 26.

[0024] This embodiment provides a compact charging system 20 with efficient cooling of the boost air pressure and makes the best possible use of the expended energy. The arrangement of the first and the second energy recovery turbines 25, 26 enables optimal recovery of the energy contained in the exhaust gas mass flow 45. Even if a maximum boost pressure is exceeded by the compression, the boost air 44 can be expanded again by the cooling turbine 24 and thus cooled. This greater expansion results in greater cooling. The exhaust gas mass flow can alternatively be directed more to the second energy recovery turbine 26, so that the compressor is driven to a lesser extent by the first energy recovery turbine 25. Supplying the second energy recovery turbine 26 with a larger exhaust gas mass flow causes a larger proportion of its energy to be transmitted to the second shaft 32 and passed from there via the coupling to an energy sink for further use. The energy of the exhaust gas mass flow can thus always be recovered in the best possible way, even if the compressor already is compressing the intake air to a maximum pressure level.

LIST OF REFERENCE SIGNS

[0025] 10 Internal combustion engine [0026] 11 Engine block [0027] 12 Cylinder [0028] 20 Charging system [0029] 21 Air filter [0030] 22 Compressor [0031] 23 Boost air cooler [0032] 24 Cooling turbine [0033] 25 First energy recovery turbine [0034] 26 Second energy recovery turbine [0035] 31 First shaft [0036] 32 Second shaft [0037] 33 Gearing [0038] 41 Intake air [0039] 42 Compressed air [0040] 43 Cooled air [0041] 44 Boost air [0042] 45 Exhaust gas mass flow