Internal combustion engine comprising an exhaust gas recirculation system
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02B-033/44
F02M-025/07
F02B-029/04
출원번호
US-0908429
(2013-06-03)
등록번호
US-8893494
(2014-11-25)
우선권정보
WO-PCT/IB2006/004061 (2006-11-23)
발명자
/ 주소
Auffret, Nicolas
Dronniou, Nicolas
출원인 / 주소
Renault Trucks
대리인 / 주소
WRB-IP LLP
인용정보
피인용 횟수 :
0인용 특허 :
8
초록▼
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
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.
대표청구항▼
1. An internal combustion engine having a plurality of cylinders, comprising: an air intake line capable of carrying intake air towards an engine intake manifold;an exhaust line capable of collecting exhaust gas from an exhaust manifold;an exhaust gas recirculation (EGR) line capable of rerouting a
1. An internal combustion engine having a plurality of cylinders, comprising: an air intake line capable of carrying intake air towards an engine intake manifold;an exhaust line capable of collecting exhaust gas from an exhaust manifold;an exhaust gas recirculation (EGR) line capable of rerouting a part of the exhaust gas from the exhaust line, towards the air intake line;a low pressure turbocharger comprising a first turbine driven by the exhaust gas flowing towards an atmosphere, mechanically linked to a first compressor located on the air intake line; anda high pressure turbocharger comprising an additional turbine located on the exhaust line upstream of the first turbine and a high pressure compressor located downstream of the first compressor,wherein an EGR line outlet is connected to the air intake line upstream from the compressor located most upstream, and wherein the EGR line is connected to the exhaust manifold or to the exhaust line upstream of the turbine located most upstream, such that the exhaust line upstream of the turbine located most upstream is in direct fluid communication with the air intake line upstream from the compressor located most upstream through the EGR line. 2. The internal combustion engine according to claim 1, wherein the EGR line is provided with an EGR cooler. 3. The internal combustion engine according to claim 2, wherein the EGR cooler uses an engine coolant. 4. The internal combustion engine according to claim 2, wherein the engine further comprises an EGR turbine located on the EGR line upstream from the EGR cooler, driven by the EGR gas flowing in the EGR line. 5. The internal combustion engine according to claim 4, wherein it further comprises an energy recovering means linked to the EGR turbine and capable of recovering the energy provided by the EGR turbine. 6. The internal combustion engine according to claim 5, 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 intake manifold. 7. The internal combustion engine according to claim 6, wherein the second compressor is located on the air intake line, downstream from the first compressor. 8. The internal combustion engine according to claim 6, wherein the second compressor is arranged in parallel with the high pressure compressor located on the air intake line downstream from the first compressor. 9. The internal combustion engine according to claim 5, wherein the energy recovering means is an energy storage component such as a battery. 10. The internal combustion engine according to claim 5, wherein the energy recovering means is a crankshaft mechanically or electrically connected to the EGR turbine. 11. The internal combustion engine according to claim 5, wherein the energy recovering means is an electrical device connected to the EGR turbine. 12. The internal combustion engine according, to claim 4, wherein the exhaust manifold is arranged in two parts, each connected to a corresponding EGR conduit, the two EGR conduits meeting upstream from the EGR turbine. 13. The internal combustion engine according to claim 1, wherein the EGR line is provided with a valve, and an additional compressor is located downstream of the first compressor in the intake line, the additional compressor being part of an additional turbocharger having a turbine that is driven by exhaust gases. 14. 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. 15. An internal combustion engine having a plurality of cylinders, comprising: an air intake line capable of carrying intake air towards an engine intake manifold;an exhaust line capable of collecting exhaust gas from an exhaust manifold;an exhaust gas recirculation (EGR) line capable of rerouting a part of the exhaust gas, towards the air intake line;a low pressure turbocharger comprising a first turbine driven by the exhaust gas flowing towards an atmosphere, mechanically linked to a first compressor located on the air intake line; anda high pressure turbocharger comprising an additional turbine located on the exhaust line upstream of the first turbine and a high pressure compressor located in the intake line downstream of the first compressor,wherein an EGR line outlet is connected to the air intake line upstream from the first compressor, and wherein the EGR line is connected, at a point downstream of the engine, to the exhaust manifold or to the exhaust line upstream of the additional turbine, such that the exhaust line upstream of the additional turbine is in direct fluid communication with the air intake line upstream from the first compressor through the EGR line. 16. An internal combustion engine having a plurality of cylinders, comprising an air intake line capable of carrying intake air towards an engine intake manifold,an exhaust line capable of collecting exhaust gas from an exhaust manifold,an exhaust gas recirculation (EGR) line capable of rerouting a part of the exhaust gas from the exhaust line, towards the air intake line,a low pressure turbocharger comprising a first turbine driven by the exhaust gas flowing towards an atmosphere, mechanically linked to a first compressor located on the air intake line,a high pressure turbocharger comprising an additional turbine located on the exhaust line upstream of the first turbine and a high pressure compressor located downstream of the first compressor,an outlet of the EGR line being connected to the air intake line upstream from the compressor located most upstream, the EGR line being connected to the exhaust manifold or to the exhaust line upstream of the turbine located most upstream,an EGR turbine located on the EGR line, driven by EGR gas flowing in the EGR line, andan 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 front the first compressor outlet towards the intake manifold. 17. The internal combustion engine according to claim 16, wherein the second compressor is located on the air intake line, downstream from the first compressor. 18. The internal combustion engine according to claim 16, wherein the second compressor is arranged in parallel with the high pressure compressor located on the air intake line downstream from the first compressor.
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이 특허에 인용된 특허 (8)
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