Turbine assembly
AssigneeCummins Engine Company, Inc.
InventorWilliam E. Woollenweber
Life of this patent
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AssigneeCummins Engine Company, Inc.
InventorWilliam E. Woollenweber
Estimating the term…
A turbine assembly is provided for use on an internal combustion engine such as a diesel engine having conventional intake and exhaust manifolds. The assembly includes a hollow section which has an inlet communicating with the exhaust manifold, and an outlet communicating with an exhaust gas entry into a chamber in which a turbine wheel is mounted. Rotatably mounted within the hollow section is a rotor which is adjustable to various selected positions. When in a first selected position, the rotor permits substantially unrestricted exhaust gas flow through the assembly. When in a second selected position, a predetermined amount of exhaust gas is diverted from the turbine wheel chamber through a bypass passageway formed in the hollow section. The end of the bypass passageway terminates downstream of the turbine wheel chamber. When in a third selected position of adjustment, the rotor effects substantial blockage of the exhaust gas flow through the assembly.
A turbine assembly for use on an internal combustion engine having an intake manifold and an exhaust manifold, said assembly comprising a housing having a chamber in which a turbine wheel is rotatably mounted, said housing chamber being provided with an exhaust gas entry and an exhaust gas exit;
Dependencies are inferred from the claim text.