Internal combustion engine comprising a compressor in the induction tract
View Patent ↗In an internal combustion engine which includes in the intake section a compressor with an impeller that is mounted rotatably in a compressor intake passage, the compressor includes an additional passage which opens out into the compressor intake passage and through which a mass flow of exhaust gas can be transferred from the exhaust section into the intake section via an exhaust-gas recirculation device, the exhaust gas recirculation line of the exhaust-gas recirculation system of the engine being connected to the additional passage extending directly to the compressor.
1. An internal combustion engine having an intake section ( 6 ), a compressor ( 5 ) disposed in the intake section ( 6 ), a compressor impeller ( 19 ) rotatably supported in the compressor ( 5 ), the compressor ( 5 ) including an intake passage ( 18 ) by means of which combustion air is supplied to the compressor to be compressed therein to an elevated boost pressure, and an additional passage ( 11 ) formed separately and sealed off in a pressure-tight and flow-tight manner with respect to the axial compressor intake passage ( 18 ), the additional passage ( 11 ) being connected to the compressor intake passage ( 18 ) in an area surrounding the compressor impeller ( 19 ) at its upstream end, and an exhaust gas recirculation device ( 10 ) having a recirculation line ( 29 ) connected to the additional passage ( 11 ) for conducting an adjustable mass flow of exhaust gas from the exhaust section ( 4 ) of the engine into the intake section ( 6 ), such that the re-circulated exhaust gas is admitted directly to the impeller ( 19 ) while applying a swirl force to the impeller ( 19 ) of the compressor ( 5 ).
2. The internal combustion engine as claimed in claim 1 , wherein a swirl vane structure ( 14 , 21 ) is arranged in the flow passage ( 17 ) where the additional passage ( 11 ) opens out into the compressor intake passage ( 18 ) for controlling the swirl force applied to the impeller ( 19 ).
3. The internal combustion engine as claimed in claim 2 , wherein the swirl vane structure ( 14 , 21 ) is of adjustable design.
4. The internal combustion engine as claimed in claim 3 , wherein the swirl vane structure comprises a swirl grate disposed in the opening region ( 17 ), and an axial slide ( 21 ), which is movable between an open position and a closed position in which the swirl plate ( 21 ) blocks the flow passage ( 17 ).
5. The internal combustion engine as claimed in claim 4 , wherein a receiving recess ( 23 ) for receiving the swirl vane structure ( 14 ) is formed in the end side of the axial slide ( 21 ).
6. The internal combustion engine as claimed in claim 1 , wherein an adjustable blocking member ( 13 ) is arranged in the compressor intake passage ( 18 ) upstream of the compressor impeller ( 19 ).
7. The internal combustion engine as claimed in claim 1 , wherein a recirculation valve ( 28 ) is arranged in the exhaust-gas recirculation line ( 29 ).
8. The internal combustion engine as claimed in claim 1 , wherein the compressor ( 5 ) is part of an exhaust-gas turbocharger ( 2 ), including an exhaust-gas turbine ( 3 ) which is equipped with a variable turbine geometry ( 8 ) in order to variably control the active turbine inlet cross section.