Exhaust system for an internal combustion engine
View Patent ↗A combustion chamber of an internal combustion engine has at least a first and a second exhaust port, which are decoupled downstream of the combustion chamber. The first exhaust port is opened before the second exhaust port during an expansion stroke of the piston. The first exhaust port is coupled to a high-pressure turbine and the second exhaust port is coupled to a low-pressure turbine. By directing exhaust gases at higher pressure to the high-pressure turbine and gases at lower pressure to the low-pressure turbine, the overall energy recovery from the exhaust gases is greater than a system with one or more exhaust turbines coupled in series with all of the exhaust ports.
1. An internal combustion engine, comprising:
a cylinder wall;
a crankshaft;
an exhaust piston disposed in the cylinder wall and coupled to the crankshaft via a connecting rod wherein the exhaust piston reciprocates within the cylinder wall when the crankshaft rotates;
a combustion chamber delimited at least by a top of the exhaust piston and the cylinder;
a plurality of primary exhaust ports defined in the cylinder wall;
a plurality of secondary exhaust ports defined in the cylinder wall wherein the pluralities of primary and secondary exhaust ports are covered and uncovered by the exhaust piston as the exhaust piston reciprocates within the cylinder wall; and
a first turbine fluidly coupled to the plurality of primary exhaust ports and fluidly decoupled from the plurality of secondary exhaust ports wherein the plurality of primary exhaust ports is covered and uncovered by the same exhaust piston that covers and uncovers the plurality of secondary exhaust ports.
2. The engine of claim 1 , further comprising: a second turbine fluidly coupled to the plurality of secondary exhaust ports.
3. The engine of claim 2 wherein the second turbine is a dual-volute turbine with a first inlet and a second inlet, the first inlet coupled to the plurality of secondary exhaust ports and the second inlet coupled to an outlet of the first turbine.
4. The engine of claim 2 , further comprising:
an intake piston disposed within the cylinder wall and adapted to reciprocate with the cylinder with the intake piston opposed from the exhaust piston wherein:
the intake piston further defines the combustion chamber;
the pluralities of primary and secondary exhaust ports are defined in the cylinder wall such that the primary exhaust port is nearer the intake piston than the secondary exhaust port; and
during reciprocating movement of the exhaust piston from a top dead center position to a bottom dead center position in which the exhaust ports are fully closed toward a position in which the exhaust ports are open, the primary exhaust port is fully uncovered prior to the secondary exhaust port becoming uncovered.
5. An internal-combustion engine system, comprising:
a cylinder wall;
an opposed-piston arrangement having:
an intake piston disposed within the cylinder wall; and
an exhaust piston disposed within the cylinder wall;
a combustion chamber delimited by the cylinder wall, the intake piston, and the exhaust piston;
a first plurality of exhaust ports defined in the cylinder wall;
a second plurality of exhaust ports defined in the cylinder wall;
a plurality of intake ports defined in the cylinder wall;
a first turbine fluidly coupled to the first plurality of exhaust ports; and
a second turbine fluidly coupled to the second plurality of exhaust ports wherein the first and second pluralities of exhaust ports and the plurality of intake ports are defined in the same cylinder wall.
6. The engine of claim 5 , further comprising:
a crankshaft coupled to the exhaust piston via a connecting rod;
wherein:
the exhaust piston reciprocates within the cylinder wall when the crankshaft rotates;
the intake ports are uncovered by the intake piston;
the first and second pluralities of exhaust ports are uncovered by the exhaust piston;
the first plurality of exhaust ports defined in the cylinder wall are located a first predetermined distance from an axis of rotation of the crankshaft; and
the second plurality of exhaust ports defined in the cylinder wall are located a second predetermined distance from the axis of rotation of the crankshaft.
7. The engine of claim 6 , further comprising:
a compressor disposed in an engine intake duct coupled to the intake ports; and
a shaft coupling the first turbine with the compressor.
8. The engine of claim 7 , further comprising: an electric motor coupled to the shaft.
9. The engine of claim 5 wherein the second turbine has two inlets, a first inlet coupled to the second plurality of exhaust ports and a second inlet coupled to the outlet of the first turbine.