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Systems and methods for internal combustion engine operation with exhaust gas recirculation and turbocharging are disclosed. The systems include an exhaust gas recirculation loop for recirculating exhaust gas flow from a first portion of the cylinders of the engine into an intake system prior to com

Systems and methods for internal combustion engine operation with exhaust gas recirculation and turbocharging are disclosed. The systems include an exhaust gas recirculation loop for recirculating exhaust gas flow from a first portion of the cylinders of the engine into an intake system prior to combustion. The system further includes a turbine with first and second inlets for receiving exhaust gas flows from respective first and second parts of the exhaust gas of the remaining portion of the cylinders.

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1. A system, comprising: an internal combustion engine including a plurality of cylinders operable to produce an exhaust flow, an exhaust system connected to the plurality of cylinders, an intake system connected to the plurality of cylinders, and a turbocharger, the turbocharger including a turbine

1. A system, comprising: an internal combustion engine including a plurality of cylinders operable to produce an exhaust flow, an exhaust system connected to the plurality of cylinders, an intake system connected to the plurality of cylinders, and a turbocharger, the turbocharger including a turbine in the exhaust system and a compressor in the intake system connected to the turbine, whereina first portion of the plurality of cylinders is operably connected to an exhaust gas recirculation system connected to the intake system for recirculation of a first portion of the exhaust flow,a second portion of the plurality of cylinders is operably connected to a first inlet to the turbine to provide a second portion of the exhaust flow to the turbine through the first inlet,a third portion of the cylinders is operably connected to a second inlet to the turbine to provide a third portion of the exhaust flow to the turbine through the second inlet, andthe first portion of the plurality of cylinders includes first and second cylinders which are positioned physically adjacent to one another in the engine, are commonly connected to a first exhaust manifold that is connected to the exhaust gas recirculation system, and are exclusively dedicated to providing the first portion of the exhaust flow to the intake system. 2. The system of claim 1, wherein the exhaust gas recirculation system is connected to the intake system downstream of the compressor. 3. The system of claim 1, wherein the second portion of the plurality of cylinders includes third and fourth cylinders commonly connected to a second exhaust manifold that is connected to the first inlet of the turbine and the third portion of the plurality of cylinders includes fifth and sixth cylinders that are commonly connected to a third exhaust manifold that is connected to the second inlet of the turbine. 4. The system of claim 3, wherein during operation of the engine the plurality of cylinders fire in order from the first cylinder, to the fifth cylinder, to the third cylinder, to the sixth cylinder, to the second cylinder, and then to fourth cylinder so that cylinders commonly connected to respective ones of the first, second and third exhaust manifolds do not fire consecutively. 5. The system of claim 1, wherein during operation of the engine the plurality of cylinders define a firing order and no two consecutive cylinders in the firing order are commonly connected to any of the exhaust gas recirculation system, the first inlet of the turbine, and the second inlet of the turbine. 6. The system of claim 1, wherein the turbine includes a housing defining a first flow passage extending from the first inlet to a turbine wheel in the housing and a second flow passage fluidly isolated from the first flow passage that extends from the second inlet to the turbine wheel. 7. The system of claim 6, wherein the first flow passage and the second flow passage define asymmetric cross-sections with the first flow passage being larger than the second flow passage. 8. A system, comprising: an engine including a plurality of cylinders;an intake system configured to direct a charge flow to all of the plurality of cylinders;an exhaust system including a turbocharger having a first inlet configured to receive a first exhaust flow from a first portion of the plurality of cylinders and a second inlet configured to receive a second exhaust flow from a second portion of the plurality of cylinders, wherein the first exhaust flow and the second exhaust flow are isolated from one another to the first and second inlets of the turbine; andan exhaust gas recirculation system configured to receive a third exhaust flow from a third portion of the plurality of cylinders and direct the third exhaust flow to the intake system,wherein the third portion of the plurality of cylinders includes two cylinders that are positioned physically adjacent to one another in the engine, and are exclusively dedicated to providing the third exhaust flow to the intake system. 9. The system of claim 8, wherein the first portion of the plurality of cylinders is exclusively dedicated to providing the first exhaust flow to the first inlet of the turbocharger and the second portion of the plurality of cylinders is exclusively dedicated to providing the second exhaust flow to the second inlet of the turbocharger. 10. The system of claim 8, wherein the turbocharger includes a turbine in the exhaust system, the turbine including a housing defining the first inlet and the second inlet, and the turbocharger further includes a compressor in the intake system connected to the turbine, wherein the exhaust gas recirculation system is connected to the intake system downstream of the compressor. 11. The system of claim 8, wherein the first portion, the second portion and the third portion of the plurality of cylinders each comprise no more than two cylinders. 12. The system of claim 8, wherein the first portion of the plurality of cylinders is connected to a first exhaust manifold, the second portion of the plurality of cylinders is connected to a second exhaust manifold, and the third portion of the plurality of cylinders is connected to a third exhaust manifold. 13. The system of claim 8, wherein during operation of the engine the plurality of cylinders define a firing order and none of the first portion, the second or the third portion of the plurality of cylinders includes two consecutive cylinders in the firing order. 14. A method, comprising: operating an engine having a plurality of cylinders;directing a charge flow into the plurality of cylinders from an intake system;combusting a mixture of the charge flow and fuel within the plurality of cylinders to generate a power output and a flow of exhaust from the plurality of cylinders;directing a first part of the flow of exhaust to an exhaust gas recirculation system to mix with the charge flow in the intake system prior to combustion, wherein the first part of the flow of exhaust is created by combustion in a first portion of the plurality of cylinders;directing a second part of the flow of exhaust to a first inlet of a turbine in an exhaust system, wherein the second part of the flow of exhaust is created by combustion in a second portion of the plurality of cylinders; anddirecting a third part of the flow of exhaust to a second inlet of the turbine in the exhaust system, wherein the third part of the flow of exhaust is created by combustion in a third portion of the plurality of cylinders, wherein the first, second and third portions of the plurality of cylinders each comprise different cylinders,wherein the first portion of the plurality of cylinders includes two cylinders that are positioned physically adjacent to one another in the engine, and are exclusively dedicated to providing the first part of the exhaust flow to the intake system. 15. The method of claim 14, wherein a compressor in the intake system is connected to the turbine, and the first part of the exhaust flow is received in the intake system downstream of the compressor. 16. The method of claim 14, wherein each of the second portion and the third portion of the plurality of cylinders includes two cylinders. 17. The method of claim 14, further comprising firing the plurality of cylinders in a firing order so that cylinders comprising respective ones of the first portion, the second portion and the third portion do not fire consecutively.