Method for Operating an Internal Combustion Engine of a Motor Vehicle
20230349315 ยท 2023-11-02
Inventors
Cpc classification
F02B29/0406
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B29/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02B29/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B29/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method for operating an internal combustion engine of a motor vehicle. The internal combustion engine includes a combustion chamber, an intake tract, a compressor disposed in the intake tract, and a conduit element which is fluidly connected to the intake tract. The internal combustion engine is operable in a heating mode to heat at least a compressor housing of the compressor. In the heating mode a part of the air flowing through the intake tract and compressed by the compressor is returned to the intake tract by the conduit element. The method includes recording a temperature of the air in the intake tract upstream of the compressor by a sensor and comparing the temperature with a threshold value. When the temperature is lower than the threshold value, the internal combustion engine is operated in the heating mode.
Claims
1-8. (canceled)
9. A method for operating an internal combustion engine (10) of a motor vehicle, the internal combustion engine (10) comprising: a combustion chamber; an intake tract (20), wherein air is flowable through the intake tract (20) and wherein the combustion chamber is providable with the air via the intake tract (20); a compressor (24) disposed in the intake tract (20), wherein the compressor (24) has a compressor housing (32) and a compressor wheel (28) disposed rotatably in the compressor housing (32) for compressing air flowing through the intake tract (20) and to the combustion chamber; and a conduit element (36) which is fluidly connected to the intake tract (20) at a first connection point (V1) disposed upstream of the compressor wheel (28) and at a second connection point (V2) disposed downstream of the compressor wheel (28); wherein the internal combustion engine (10) is operable in a heating mode to heat at least the compressor housing (32) and wherein in the heating mode at least a part of the air flowing through the intake tract (20) and compressed by the compressor wheel (28) is removed from the intake tract (20) at the second connection point (V2), introduced into the conduit element (36), provided to the first connection point (V1) by the conduit element (36) and introduced into the intake tract (20) at the first connection point (V1); and comprising the steps of: recording a temperature of the air in the intake tract (20) upstream of the compressor wheel (28) by a sensor; comparing the temperature with a threshold value; and when the temperature is lower than the threshold value, operating the internal combustion engine (10) in the heating mode.
10. The method according to claim 9, wherein the internal combustion engine (10) further comprises a valve element (40) which is displaceable between a closed position that blocks the conduit element (36) and an open position that releases the conduit element (36) and wherein the valve element (40) is in the open position during the heating mode.
11. The method according to claim 9, wherein the internal combustion engine (10) is in a traction mode during the heating mode.
12. The method according to claim 9, wherein the internal combustion engine (10) further comprises an intercooler (42) disposed in the intake tract (20) downstream of the compressor wheel (28) and wherein air compressed by the compressor wheel (28) is cooled by the intercooler (42).
13. The method according to claim 12, wherein the intercooler (42) is disposed downstream of the second connection point (V2).
14. The method according to claim 9, wherein the intake tract (20) does not have a cooling device for cooling the air in a longitudinal region (L) extending continuously from the compressor wheel (28) to the second connection point (V2).
Description
BRIEF DESCRIPTION OF THE DRAWING
[0021] In the single the
DETAILED DESCRIPTION OF THE DRAWING
[0022] The single the
[0023] The respective mixture of fuel and air is also referred to as a mixture, and comprises air and a fuel, in particular a liquid fuel, wherein the respective combustion chamber is provided with the air and with the fuel. In this case, the internal combustion engine 10 has an intake tract 20 that can be flowed through by the air and is also referred to as an inlet tract, by means of which intake tract the air flowing through the intake tract 20 is fed to and particularly into the combustion chambers.
[0024] The internal combustion engine comprises at least one exhaust gas turbocharger 22 here, which has a compressor 24 arranged in the intake tract 20 and a turbine 26 arranged in the exhaust gas tract 18. The compressor 24 has a compressor wheel 28 arranged in the intake tract 20. The turbine 26 comprises a turbine wheel 30 arranged in the exhaust gas tract 18. The compressor 24 additionally comprises a compressor housing 32 depicted only schematically and partially in the
[0025] The internal combustion engine 10 additionally comprises a conduit element 36 which is fluidly connected to the intake tract 20 at a first connection point V1 and at a second connection point V2. The connection point V2 is arranged downstream of the connection point V1 in the flow direction of the air flowing through the intake tract 20, and the connection point V1 is additionally arranged upstream of the compressor wheel 28, while the connection point V2 is arranged downstream of the compressor wheel 28. A method for operating the internal combustion engine 10, particularly in the traction mode, is described in the following with reference to the single the
[0026] In order to be able to guarantee a particularly advantageous operation of the internal combustion engine 10, particularly during the traction mode, in a particularly simple manner, the internal combustion engine 10 is operated in a heating mode to heat at least the compressor housing 32, particularly during at least a part of the traction mode, the heating mode thus being carried out simultaneously with the traction mode at least during the specified part, for example. In other words, it is preferably provided that the internal combustion engine 10 is in the traction mode during the heating mode. In the traction mode, at least a part of the air flowing through the intake tract 20 and compressed, and thus warmed, by means of the compressor wheel 28 is removed from the intake tract 20 at the second connection point V2, introduced into the conduit element 36, returned to the first connection point V1 by means of the conduit element 36 and introduced into the intake tract 20 at the first connection point V1. The air can then flow from the connection point V1 back to the connection point V2. The air flows through the compressor housing 32 on its way from the connection point V1 to the connection point V2, such that the compressor housing 32 is heated or kept warm by means of the returned air that has already previously been compressed, and thus heated. The air is additionally compressed again on its way from the connection point V1 and the connection point V2 by means of the compressor wheel 32, and is thus heated further, whereby a particularly high temperature of the air flowing from the connection point V1 to the connection point V2, and flowing through the compressor housing in the process, can thus be obtained. The compressor housing 32 and the component arranged in an environment 38 of the compressor housing 32 can thus be kept warm or heated efficiently and effectively with the internal combustion engine 10.
[0027] The internal combustion engine 10 has a valve element 40 arranged in the conduit element 36 here, the valve element being able to be displaced between a closed position blocking the conduit element 36 and at least one open position releasing the conduit element 36. The valve element 40 is in the open position during the heating mode here. It is preferably provided that the valve element 40 is in the closed position at least during a different part of the traction mode from the heating mode. The valve element 40 is constantly in the closed position during the traction mode, with the exception of the heating mode occurring during the traction mode.
[0028] An intercooler 42 depicted particularly schematically in the
[0029] A circulation of the air is depicted in the
[0030] It can further be seen from the
[0031] The turbine 26 is arranged in a bypass device 46, which has a bypass conduit 48 also referred to as a bypass. The bypass conduit 48 is fluidly connected to the exhaust gas tract 18 at a third connection point V3 and at a fourth connection point V4. The connection point V4 is arranged upstream of the turbine wheel 30 in the flow direction of the exhaust gas flowing through the exhaust gas tract 18, while the connection point V3 is arranged downstream of the turbine wheel 30. At least a part of the exhaust gas flowing through the exhaust gas tract 18 can be removed from the exhaust gas tract 18 at the connection point V4 by means of the bypass conduit 48 and introduced into the bypass conduit 48. The exhaust gas removed at the connection point V4 and introduced into the bypass conduit 48 can flow through the bypass conduit 48 and is guided to the connection point V3 by means of the bypass conduit 48. The exhaust gas flowing through the bypass conduit 48 can be introduced into the exhaust gas tract 18 again at the connection point V3, wherein the exhaust gas flowing through the bypass conduit 48 bypasses the turbine wheel 30, and thus does not drive the turbine wheel 30.
[0032] The bypass device 46 additionally comprises a valve 50, also referred to as a bypass valve, waste gate or waste gate valve, arranged in the bypass conduit 48, by means of which a quantity of the exhaust gas flowing through the bypass conduit 48 can be adjusted, for example. A power of the turbine 26 can be adjusted as needed by adjusting the quantity of the exhaust gas flowing through the bypass conduit 48.
[0033] The internal combustion engine 10 additionally has an exhaust gas recirculation device 52 having an exhaust gas recirculation conduit 54. The exhaust gas recirculation conduit 54 is fluidly connected to the exhaust gas tract 18 at a fifth connection point V5 and fluidly connected to the intake tract 20 at a sixth connection point V6. The connection point V6 is arranged upstream of the compressor wheel 28, and preferably downstream of the connection point V1 in the flow direction of the exhaust gas flowing through the intake tract 20, for example. The connection point V5 is arranged downstream of the turbine wheel 30 in the flow direction of the exhaust gas flowing through the exhaust gas tract 18, for example, wherein the connection point V5 can be arranged upstream or downstream of the connection point V3. At least a part of the exhaust gas flowing through the exhaust gas tract 18 can be removed from the exhaust gas tract 18 at the connection point V5 by means of the exhaust gas recirculation conduit 54 and introduced into the exhaust gas recirculation conduit 54. The exhaust gas removed from the exhaust gas tract 18 at the connection point V5 and introduced into the exhaust gas recirculation conduit 54 can flow through the exhaust gas recirculation conduit 54, and is fed, and thus returned, to the connection point V6 by means of the exhaust gas recirculation conduit 54. The exhaust gas flowing through the exhaust gas recirculation conduit 54 can flow out of the exhaust gas recirculation conduit 54 at the connection point V6, and flow into the intake tract 20. The exhaust gas recirculation device 52 comprises an exhaust gas recirculation valve 56 arranged in the exhaust gas recirculation conduit 54 here, by means of which a quantity of the exhaust gas flowing through the exhaust gas recirculation conduit 54 can be adjusted.
TABLE-US-00001 List of reference characters: 10 internal combustion engine 12 housing element 14 output shaft 16 cylinder 18 exhaust gas tract 20 intake tract 22 exhaust gas turbocharger 24 compressor 26 turbine 28 compressor wheel 30 turbine wheel 32 compressor housing 34 shaft 36 conduit element 38 environment 40 valve element 42 intercooler 44 arrow 46 bypass device 48 bypass conduit 50 bypass valve 52 exhaust gas recirculation device 54 exhaust gas recirculation conduit 56 exhaust gas recirculation valve V1 connection point V2 connection point V3 connection point V4 connection point V5 connection point V6 connection point