Partially integrated exhaust manifold
US-8935917-B2 · Jan 20, 2015 · US
US9347367B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9347367-B2 |
| Application number | US-201313938682-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 10, 2013 |
| Priority date | Jul 10, 2013 |
| Publication date | May 24, 2016 |
| Grant date | May 24, 2016 |
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A turbocharger is disclosed for use with an engine system. The turbocharger may have a housing at least partially defining a compressor shroud and a turbine shroud. The turbine shroud may form a first volute and a second volute, each having an inlet configured to receive exhaust from an exhaust manifold of the engine in a tangential direction, and an axial channel disposed downstream of the inlet. The turbocharger may also have a turbine wheel disposed within the turbine shroud and configured to receive exhaust from the axial channels of the first and second volutes, a compressor wheel disposed within the compressor shroud, and a shaft connecting the turbine wheel to the compressor wheel. The turbocharger may further have a nozzle ring in fluid communication with the axial channels of the first and second volutes at a location upstream of the turbine wheel.
Opening claim text (preview).
What is claimed is: 1. A turbocharger for an engine, comprising: a housing at least partially defining a compressor shroud and a turbine shroud, the turbine shroud forming a first volute and a second volute each having: a volute inlet configured to receive exhaust from an exhaust manifold of the engine in a tangential direction; and an axial channel disposed downstream of the volute inlet; the first volute having an inner annular wall and an annular tongue disposed coaxially…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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