Dual flow turbine housing for a turbocharger in a divided manifold exhaust system having E.G.R. flow

Claim 1

An internal combustion engine, comprising: a plurality of combustion cylinders; a first exhaust manifold and a second exhaust manifold, each said first exhaust manifold and said second exhaust manifold coupled with a plurality of said combustion cylinders; an intake manifold coupled with said plurality of combustion cylinders; an EGR system disposed in fluid flow communication between said first exhaust manifold and said intake manifold; a turbocharger including a compressor having an inlet receiving combustion gas and an outlet in fluid flow communication with said intake manifold, and a turbine drivingly coupled to said compressor, said turbine having a turbine casing and a turbine wheel disposed in said casing, said casing defining a bifurcated inlet and an outlet, said turbine bifurcated inlet having a first inlet path in fluid flow communication with said first exhaust manifold and a second inlet path in fluid flow communication with said second exhaust manifold, said first inlet path being of smaller volume than said second inlet path; a mixer in fluid flow communication to receive fluid flows from said EGR system and from said compressor outlet, and to provide a mixture of said flows to said intake manifold; and a fluid bypass conduit interconnecting said compressor outlet and said intake manifold for selectively bypassing said mixer.

Claim 15

A method of operating an internal combustion engine, comprising, the steps of: providing a plurality of combustion cylinders, a first exhaust manifold, a second exhaust manifold and an intake manifold; transporting exhaust gas from a first group of said plurality of said combustion cylinders to said first exhaust manifold and from a second group of said plurality of combustion cylinders to said second exhaust manifold; providing a turbocharger including a turbine having an inlet and an outlet, and a compressor having an inlet and an outlet; providing a first inlet path and a second inlet path in said turbine inlet; rotatably driving said turbine with exhaust gas introduced at said first inlet path from said first exhaust manifold, and with exhaust gas introduced at said second inlet path from said second exhaust manifold; introducing combustion gas at said compressor inlet; transporting combustion gas from said compressor outlet to said intake manifold; and providing an exhaust gas recirculation duct interconnecting said first exhaust manifold with said intake manifold, and re-circulating exhaust gas in said exhaust gas re-circulation duct; preserving pulse energy in exhaust gas flow from said second exhaust manifold to said second inlet path; and providing restricted flow in said first inlet path in comparison to said second inlet path, for increasing back pressure and compensating for reduced exhaust flow in said first inlet path; providing a mixer, and mixing combustion gas from said compressor with exhaust gas from said exhaust gas recirculation duct; and providing a conduit in fluid flow communication with said compressor outlet and said intake manifold, and bypassing said mixer with combustion gas flow through said conduit.

Claim 16

A method of operating an internal combustion engine, comprising, the steps of: providing a plurality of combustion cylinders, a first exhaust manifold, a second exhaust manifold and an intake manifold; transporting exhaust gas from a first group of said plurality of said combustion cylinders to said first exhaust manifold and from a second group of said plurality of combustion cylinders to said second exhaust manifold; providing a turbocharger including a turbine having an inlet and an outlet, and a compressor having an inlet and an outlet; providing a first inlet path and a second inlet path in said turbine inlet; rotatably driving said turbine with exhaust gas introduced at said first inlet path from said first exhaust manifold, and with exhaust gas introduced at said second inlet path from said second exhaust manifold; introducing combustion gas at said compressor inlet; transporting combustion gas from said compressor outlet to said intake manifold; and providing an exhaust gas recirculation duct interconnecting said first exhaust manifold with said intake manifold, and re-circulating exhaust gas in said exhaust gas re-circulation duct; preserving pulse energy in exhaust gas flow from said second exhaust manifold to said second inlet path; and providing restricted flow in said first inlet path in comparison to said second inlet path, for increasing back pressure and compensating for reduced exhaust flow in said first inlet path; providing a mixer, and mixing combustion gas from said compressor with exhaust gas from said exhaust gas recirculation duct; and providing a conduit in fluid flow communication with said compressor outlet and said intake manifold, and bypassing said mixer with combustion gas flow through said conduit.