초록 ▼

A supercharged internal combustion engine includes at least two exhaust-gas turbochargers arranged in series, wherein a first exhaust-gas turbocharger serves as a low-pressure stage and a second exhaust-gas turbocharger serves as a high-pressure stage. A second turbine of the second exhaust-gas turb

A supercharged internal combustion engine includes at least two exhaust-gas turbochargers arranged in series, wherein a first exhaust-gas turbocharger serves as a low-pressure stage and a second exhaust-gas turbocharger serves as a high-pressure stage. A second turbine of the second exhaust-gas turbocharger may be present upstream of a first turbine of the first exhaust-gas turbocharger, and a second compressor of the second exhaust-gas turbocharger may be arranged in an intake system downstream of a first compressor of the first exhaust-gas turbocharger and a first bypass line may branch off upstream of the second turbine and join back at a junction point between the first turbine and the second turbine.

대표청구항 ▼

1. An engine, comprising: a first cylinder group connected to a first turbine through a first exhaust line;a second cylinder group connected to a second turbine through a second exhaust line, the second turbine parallel to the first turbine;a first compressor downstream of a second compressor arrang

1. An engine, comprising: a first cylinder group connected to a first turbine through a first exhaust line;a second cylinder group connected to a second turbine through a second exhaust line, the second turbine parallel to the first turbine;a first compressor downstream of a second compressor arranged in series along an intake system; anda connecting line connecting the first exhaust line to the second exhaust line;wherein the first cylinder group includes two outer cylinders and the second cylinder group includes at least one inner cylinder. 2. The engine of claim 1, wherein the connecting line branches off from the first exhaust line upstream of the first turbine and connects to the second exhaust line upstream of the second turbine. 3. The engine of claim 1, further comprising a first bypass line with a first shut-off valve, the first bypass line branching off from the intake system between the first compressor and the second compressor, connecting back to the intake system downstream of the first compressor, and a second bypass line with a second shut-off valve, the second bypass line branching off from the intake system upstream of the second compressor, connecting back to the intake system downstream of the second compressor. 4. The engine of claim 3, further comprising a controller including instructions to regulate a position of the first shut-off valve and a position of the second shut-off valve responsive to engine operating conditions. 5. The engine of claim 1, wherein the first turbine is a fixed geometry turbine and the second turbine is a variable geometry turbine. 6. The engine of claim 1, further comprising a first turbine-side shut-off element and a second turbine-side shut-off element, wherein the first turbine-side shut-off element is arranged between the first turbine and the connecting line at the first exhaust line and the second turbine-side shut-off element is arranged between the second turbine and the connecting line at the second exhaust line. 7. The engine of claim 6, wherein, when the first turbine-side shut-off element is fully closed and the second turbine-side shut-off element is fully open, all exhaust gas from the engine flows through the second turbine. 8. The engine of claim 1, wherein the first compressor is smaller than the second compressor and the first turbine is smaller than the second turbine. 9. The engine of claim 1, wherein the first turbine is coupled to the first compressor forming a first turbocharger and the second turbine is coupled to the second compressor forming a second turbocharger.