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 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 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 and capable of recovering the 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 the first compressor outlet towards the cylinders;
wherein the EGR turbine is of the variable geometry type, and the flow of EGR gas is regulated by varying the geometry of the turbine, an inlet of the EGR line is upstream of any turbine located on the exhaust line, and an outlet of the EGR line is connected to the air intake line upstream from at least one compressor in the air intake line.
2. 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.
3. The internal combustion engine according to claim 1 , wherein the second compressor is located on the air intake line, downstream from the first compressor.
4. The internal combustion engine according to claim 1 , wherein the air intake line further comprises an additional compressor located downstream from the first compressor.
5. The internal combustion engine according to claim 4 , wherein the second compressor is arranged in parallel with the additional compressor located on the air intake line downstream from the first compressor.
6. The internal combustion engine according to claim 1 , wherein the EGR line outlet is connected to the air intake line upstream from the first compressor located most upstream of any other compressor in the air intake line.
7. The internal combustion engine according to claim 1 , wherein the air intake line further comprises an additional compressor located downstream from the EGR line outlet.
8. The internal combustion engine according to claim 1 , wherein the EGR line comprises an EGR cooler downstream of EGR turbine.
9. 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 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 EGR turbine located on the EGR line, the EGR turbine being solely driven by the EGR gas flowing in the EGR line;
wherein the EGR turbine is of the variable geometry type, and the flow of EGR gas is regulated by varying, the geometry of the turbine, an inlet of the EGR line is upstream of any turbine located on the exhaust line, and an outlet of the EGR line is connected to the air intake line upstream from at least one compressor in the air intake line, wherein the EGR line outlet is connected to the air intake line downstream from the first compressor located most upstream of any other compressor in the air intake line and upstream from at least one other compressor.
10. The internal combustion engine according to claim 9 , wherein no additional flow regulating valve is provided in the EGR line upstream of the EGR turbine.
11. The internal combustion engine according to claim 9 , wherein the at least one other compressor linked to the EGR turbine and capable of recovering the energy provided by the EGR turbine, wherein the at least one other compressor mechanically connected to the EGR turbine and capable of compressing gas flowing from the first compressor outlet towards the cylinders.
12. 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 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 EGR turbine located on the EGR line, the EGR turbine being solely driven by the EGR gas flowing in the EGR line;
wherein the EGR turbine is of the variable geometry type, and the flow of EGR gas is regulated by varying the geometry of the turbine, an inlet of the EGR line is upstream of any turbine located on the exhaust line, and an outlet of the EGR line is connected to the air intake line upstream from at least one compressor in the air intake line, wherein the exhaust manifold is arranged in two parts, each connected to a corresponding EGR conduit, the two EGR conduits meeting upstream of the EGR turbine.
13. The internal combustion engine according to claim 12 , wherein no additional flow regulating valve is provided in the EGR line upstream of the EGR turbine.
14. The internal combustion engine according to claim 12 , further comprising an energy recovering means linked to the EGR turbine and capable of recovering the 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 the first compressor outlet towards the cylinders.