Engine with exhaust gas recirculation system and variable geometry turbocharger

1. An engine assembly comprising:

an intake assembly;

a spark-ignited internal combustion engine defining a plurality of cylinders and configured to combust a fuel;

wherein the plurality of cylinders includes a first cylinder, a second cylinder, a third cylinder, and a fourth cylinder;

wherein each of the plurality of cylinders is in fluid communication with the intake assembly;

wherein combustion of the fuel occurs within the plurality of cylinders and produces an exhaust gas;

an exhaust assembly in fluid communication with a first subset of the plurality of cylinders, the exhaust assembly including a first exhaust manifold, a second exhaust manifold, and an EGR manifold;

wherein the first exhaust manifold and the second exhaust manifold converge at a manifold interface, wherein the manifold interface defines a first manifold flow path in fluid communication with the first exhaust manifold and defines a second manifold flow path in fluid communication with the second exhaust manifold, and wherein the first manifold flow path is separated from the second manifold flow path by a manifold flow divider;

wherein the first exhaust manifold receives the produced exhaust gas from the first cylinder;

wherein the second exhaust manifold receives the produced exhaust gas from both the second cylinder and the third cylinder;

wherein the EGR manifold is a dedicated EGR manifold that receives all of the produced exhaust gas from the fourth cylinder and is configured to route all of the exhaust gas from the fourth cylinder to the intake assembly; and

a turbocharger including:

a compressor in fluid communication with the intake assembly;

a variable geometry turbine in fluid communication with the first exhaust manifold and with the second exhaust manifold; and

wherein the compressor and variable geometry turbine are operatively connected through a shaft.

2. The engine assembly of claim 1 , wherein the variable geometry turbine includes a turbine housing defining a turbine inlet; and

wherein the turbine inlet is coupled with the manifold interface and is in fluid communication with the manifold interface.

3. The engine assembly of claim 2 , further comprising a turbine flow divider disposed within the turbine inlet;

wherein the turbine flow divider partially defines a first turbine channel and a second turbine channel;

wherein the first turbine channel is in fluid communication with the first manifold flow path, the second turbine channel is in fluid communication with the second manifold flow path; and

wherein the turbine flow divider abuts the manifold flow divider.

4. The engine assembly of claim 3 , wherein the variable geometry turbine includes a rotatable turbine wheel disposed within the housing; and

a plurality of articulating veins circumferentially disposed about the rotatable turbine wheel, and configured to controllably nozzle the exhaust gas to the turbine wheel.

5. The engine assembly of claim 4 , wherein the plurality of articulating veins are transitionable between a first state and a second state, wherein the second state provides a greater resistance to exhaust flow than the first state;

wherein each of the plurality of articulating veins respectively extend to a first radial position apart from the center of the rotatable turbine wheel when in the first state; and

wherein the turbine flow divider extends to a position proximate the first radial position for each of the plurality of articulating veins.

6. The engine assembly of claim 3 , wherein the turbine flow divider only extends within the turbine inlet.

7. The engine assembly of claim 1 , wherein the plurality of cylinders combust fuel sequentially in the order of the first cylinder, the third cylinder, the fourth cylinder, and the second cylinder.

8. The engine assembly of claim 1 , wherein the variable geometry turbine includes: a rotatable turbine wheel; and

a plurality of articulating veins circumferentially disposed about the rotatable turbine wheel, and configured to controllably nozzle the exhaust gas to the turbine wheel.

9. An engine assembly comprising:

an intake assembly;

a spark-ignited internal combustion engine defining a plurality of cylinders and configured to combust a fuel;

wherein the plurality of cylinders includes a first cylinder, a second cylinder, a third cylinder, and a fourth cylinder, wherein the plurality of cylinders combust fuel sequentially in the order of the first cylinder, the third cylinder, the fourth cylinder, and the second cylinder;

wherein each of the plurality of cylinders is in fluid communication with the intake assembly;

wherein combustion of the fuel occurs within the plurality of cylinders and produces an exhaust gas;

an exhaust assembly in fluid communication with a first subset of the plurality of cylinders, the exhaust assembly including a first exhaust manifold, a second exhaust manifold, and an EGR manifold;

wherein the first exhaust manifold receives the produced exhaust gas from the first cylinder;

wherein the second exhaust manifold receives the produced exhaust gas from both the second cylinder and the third cylinder;

wherein the EGR manifold is a dedicated EGR manifold that receives all of the produced exhaust gas from the fourth cylinder and is configured to route all of the exhaust gas from the fourth cylinder to the intake assembly; and

a turbocharger including:

a compressor in fluid communication with the intake assembly;

a variable geometry turbine in fluid communication with the first exhaust manifold and with the second exhaust manifold; and

wherein the compressor and variable geometry turbine are operatively connected through a shaft.

10. The engine assembly of claim 9 , wherein the first exhaust manifold and the second exhaust manifold converge at a manifold interface;

wherein the manifold interface defines a first manifold flow path in fluid communication with the first exhaust manifold and defines a second manifold flow path in fluid communication with the second exhaust manifold; and

wherein the first manifold flow path is separated from the second manifold flow path by a manifold flow divider.

11. The engine assembly of claim 10 , wherein the variable geometry turbine includes a turbine housing defining a turbine inlet; and

wherein the turbine inlet is coupled with the manifold interface and is in fluid communication with the manifold interface.

12. The engine assembly of claim 11 , further comprising a turbine flow divider disposed within the turbine inlet;

wherein the turbine flow divider partially defines a first turbine channel and a second turbine channel;

wherein the first turbine channel is in fluid communication with the first manifold flow path, the second turbine channel is in fluid communication with the second manifold flow path; and

wherein the turbine flow divider abuts the manifold flow divider.

13. The engine assembly of claim 12 , wherein the variable geometry turbine includes

a rotatable turbine wheel disposed within the housing; and

a plurality of articulating veins circumferentially disposed about the rotatable turbine wheel, and configured to controllably nozzle the exhaust gas to the turbine wheel.

14. The engine assembly of claim 13 , wherein the plurality of articulating veins are transitionable between a first state and a second state, wherein the second state provides a greater resistance to exhaust flow than the first state;

wherein each of the plurality of articulating veins respectively extend to a first radial position apart from the center of the rotatable turbine wheel when in the first state; and

wherein the turbine flow divider extends to a position proximate the first radial position for each of the plurality of articulating veins.

15. The engine assembly of claim 12 , wherein the turbine flow divider only extends within the turbine inlet.

16. An engine assembly comprising:

an intake assembly;

a spark-ignited internal combustion engine defining a plurality of cylinders and configured to combust a fuel;

wherein the plurality of cylinders includes a first cylinder, a second cylinder, a third cylinder, and a fourth cylinder;

wherein each of the plurality of cylinders is in fluid communication with the intake assembly;

wherein combustion of the fuel occurs within the plurality of cylinders and produces an exhaust gas;

an exhaust assembly in fluid communication with a first subset of the plurality of cylinders, the exhaust assembly including a first exhaust manifold, a second exhaust manifold, and an EGR manifold;

wherein the first exhaust manifold receives the produced exhaust gas from the first cylinder;

wherein the second exhaust manifold receives the produced exhaust gas from both the second cylinder and the third cylinder;

wherein the EGR manifold is a dedicated EGR manifold that receives all of the produced exhaust gas from the fourth cylinder and is configured to route all of the exhaust gas from the fourth cylinder to the intake assembly; and

a turbocharger including:

a compressor in fluid communication with the intake assembly;

a variable geometry turbine in fluid communication with the first exhaust manifold and with the second exhaust manifold, the variable geometry turbine including a rotatable turbine wheel and a plurality of articulating veins circumferentially disposed about the rotatable turbine wheel, wherein the plurality of articulating veins are configured to controllably nozzle the exhaust gas to the rotatable turbine wheel; and

wherein the compressor and variable geometry turbine are operatively connected through a shaft.

17. The engine assembly of claim 16 , wherein the first exhaust manifold and the second exhaust manifold converge at a manifold interface;

wherein the manifold interface defines a first manifold flow path in fluid communication with the first exhaust manifold and defines a second manifold flow path in fluid communication with the second exhaust manifold; and

wherein the first manifold flow path is separated from the second manifold flow path by a manifold flow divider.

18. The engine assembly of claim 17 , wherein the variable geometry turbine includes a turbine housing defining a turbine inlet; and

wherein the turbine inlet is coupled with the manifold interface and is in fluid communication with the manifold interface.

19. The engine assembly of claim 18 , further comprising a turbine flow divider disposed within the turbine inlet;

wherein the turbine flow divider partially defines a first turbine channel and a second turbine channel;

wherein the first turbine channel is in fluid communication with the first manifold flow path, the second turbine channel is in fluid communication with the second manifold flow path; and

wherein the turbine flow divider abuts the manifold flow divider.