Turbine with a shroud ring around rotor blades and method of limiting leakage of working fluid in a turbine
US-2024280031-A1 · Aug 22, 2024 · US
US8951007B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8951007-B2 |
| Application number | US-201113136540-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 3, 2011 |
| Priority date | Feb 5, 2009 |
| Publication date | Feb 10, 2015 |
| Grant date | Feb 10, 2015 |
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In the turbine housing for an exhaust gas turbocharger of a drive assembly at least one spiral channel, which can be coupled to an exhaust gas line of the drive assembly is provided A receiving chamber for a turbine wheel to which exhaust gas can be supplied is disposed upstream of the at least one spiral channel. The turbine wheel is disposed in the turbine housing so as to be rotatable about a rotational axis. A guide baffle is arranged fixed to the turbine housing in a transition region between the at least one spiral channel, the guide baffle being connected to the turbine housing by a metal-to-metal joint whereby the guide baffle is connected to the turbine housing in a particular tight manner.
Opening claim text (preview).
What is claimed is: 1. A turbine housing ( 10 ) for an exhaust gas turbocharger of a drive assembly, with at least first and second spiral channels ( 12 , 16 ) which can be coupled to an exhaust gas line of the drive assembly, with a receiving chamber for a turbine wheel ( 18 ) arranged downstream of the spiral channels ( 12 , 16 ) to which exhaust gas can be applied, said turbine wheel ( 18 ) being received in the turbine housing ( 10 ) so as to be rotatable around a rotational…
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