Internal combustion engine comprising an exhaust gas recirculation system
An internal combustion engine includes a plurality of cylinders, an air intake line and an exhaust line collecting exhaust gas. The engine also includes an EGR line for rerouting a part of the exhaust gas from the exhaust line towards the air intake line and at least a first turbocharger comprising a first turbine driven by the exhaust gas flowing towards the atmosphere, linked to a first compressor located on the air intake line. The engine further includes a variable geometry EGR turbine located on the EGR line, driven by the EGR gas flowing in the EGR line. Thus, thanks to the pressure reduction occurring in the turbine, the EGR gas temperature is lowered, and less cooling power from the engine cooling system is required to cool down the EGR.
1. An internal combustion engine having a plurality of cylinders, comprising:
an air intake line capable of carrying intake air towards the cylinders;
an exhaust line capable of collecting exhaust gas from the cylinders;
an exhaust gas recirculation (EGR) line capable of rerouting a part of the exhaust gas from the exhaust line towards the air intake line;
at least a first turbocharger comprising a first turbine driven by the exhaust gas flowing towards the atmosphere, mechanically linked to a first compressor located on the air intake line;
an exhaust gas recirculation (EGR) turbine located on the EGR line, the EGR turbine being solely driven by the exhaust gas recirculation (EGR) gas flowing in the EGR line; and
a second compressor mechanically connected to the EGR turbine and capable of compressing gas flowing from an outlet of the first compressor toward the cylinders, the second compressor being arranged in parallel with an additional compressor located on the air intake line downstream from the first compressor.
2. The internal combustion engine according to claim 1 , wherein the EGR turbine is a variable geometry type, and the flow of EGR gas is regulated by varying the geometry of the turbine.
3. The internal combustion engine according to claim 1 , wherein no additional flow regulating valve is provided in the EGR line upstream of the EGR turbine.
4. The internal combustion engine according to claim 1 , wherein an outlet of the EGR line is connected to the air intake line upstream from the first compressor in the air intake line.
5. The internal combustion engine according to claim 1 , wherein an outlet of the EGR line is connected to the air intake line upstream from a compressor located most upstream of any other compressor in the air intake line.
6. The internal combustion engine according to claim 1 , wherein the air intake line further comprises at least one cooler located downstream from the EGR line outlet.
7. The internal combustion engine according to claim 1 , wherein the EGR line comprises an exhaust gas recirculation (EGR) cooler downstream of the EGR turbine.
8. An internal combustion engine having a plurality of cylinders, comprising:
an air intake line capable of carrying intake air towards the cylinders;
an exhaust line capable of collecting exhaust gas from the cylinders;
an exhaust gas recirculation (EGR) line capable of rerouting a part of the exhaust gas from the exhaust line towards the air intake line;
at least a first turbocharger comprising a first turbine driven by the exhaust gas flowing towards the atmosphere, mechanically linked to a first compressor located on the air intake line;
an exhaust gas recirculation (EGR) turbine located on the EGR line, the EGR turbine being solely driven by the exhaust gas recirculation (EGR) gas flowing in the EGR line; and
an energy recovering means linked to the EGR turbine, the energy recovering means being discrete from the first compressor and capable of recovering energy provided by the EGR turbine, wherein the energy recovering means is a second compressor mechanically connected to the EGR turbine and capable of compressing gas flowing from an outlet of the first compressor towards the cylinders.
9. The internal combustion engine according to claim 8 wherein the second compressor is arranged in parallel with an additional compressor located on the air intake line downstream from the first compressor.
10. The internal combustion engine according to claim 8 , wherein the EGR turbine is a variable geometry type, and the flow of EGR gas is regulated by varying the geometry of the turbine.
11. The internal combustion engine according to claim 8 , wherein no additional flow regulating valve is provided in the EGR line upstream of the ER turbine.
12. The internal combustion engine according to claim 8 , wherein the air intake line further comprises at least one cooler located downstream from the EGR line outlet.
13. The internal combustion engine according to claim 8 , wherein the EGR line comprises an exhaust gas recirculation (EGR) cooler downstream of the EGR turbine.
14. An internal combustion engine having a plurality of cylinders, comprising:
an air intake line capable of carrying intake air towards the cylinders;
an exhaust line capable of collecting exhaust gas from the cylinders;
an exhaust gas recirculation (EGR) line capable of rerouting a part of the exhaust gas from the exhaust line towards the air intake line;
at least a first turbocharger comprising a first turbine driven by the exhaust gas flowing towards the atmosphere, mechanically linked to a first compressor located on the air intake line;
an exhaust gas recirculation (EGR) turbine located on the EGR line, the EGR turbine being solely driven by the EGR gas flowing in the EGR line; and
an energy recovering means linked to the EGR turbine, the energy recovering means being discrete from the first compressor and capable of recovering energy provided by the EGR turbine, wherein the energy recovering means is a second compressor mechanically connected to the EGR turbine and capable of compressing gas flowing from an outlet of the first compressor towards the cylinders, wherein an outlet of the EGR line is connected to the air intake line upstream from the first compressor.
15. An internal combustion engine having a plurality of cylinders, comprising:
an air intake line capable of carrying intake air towards the cylinders;
an exhaust line capable of collecting exhaust gas from the cylinders;
an exhaust gas recirculation (EGR) line capable of rerouting a part of the exhaust gas from the exhaust line towards the air intake line;
at least a first turbocharger comprising a first turbine driven by the exhaust gas flowing towards the atmosphere, mechanically linked to a first compressor located on the air intake line;
an exhaust gas recirculation (EGR) turbine located on the EGR line, the EGR turbine being solely driven by the EGR gas flowing in the EGR line; and
an energy recovering means linked to the EGR turbine, the energy recovering means being discrete from the first compressor and capable of recovering energy provided by the EGR turbine, wherein the energy recovering means is a second compressor mechanically connected to the EGR turbine and capable of compressing gas flowing from an outlet of the first compressor towards the cylinders, wherein an outlet of the EGR line is connected to the air intake line upstream from a compressor located most upstream of any other compressor in the air intake line.