Method for manufacturing a turbine wheel
US-10370972-B2 · Aug 6, 2019 · US
US10823009B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10823009-B2 |
| Application number | US-201916676115-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 6, 2019 |
| Priority date | Nov 7, 2018 |
| Publication date | Nov 3, 2020 |
| Grant date | Nov 3, 2020 |
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A method for working a housing of a turbocharger, namely a bearing housing or a compressor housing or a turbine housing of the turbocharger has the following steps: providing the housing to be worked, filling at least one hollow space of the housing to be worked with an incompressible fluid; and building-up a fluid pressure in the respective hollow space filled with the incompressible fluid, at least locally deforming plastically a housing portion of the housing limiting the respective hollow space of the housing at least in portions.
Opening claim text (preview).
We claim: 1. A method for processing a housing ( 10 , 20 , 30 ) of a turbocharger, the housing including one selected from the group of: (a) a bearing housing ( 10 ) of the turbocharger, (b) a compressor housing of the turbocharger ( 20 ); and (c) a turbine housing ( 30 ) of the turbocharger, the method comprising: providing the housing ( 10 , 20 , 30 ) to be processed, wherein the housing comprises metal and at least one housing portion ( 13 , 25 , 34 ); filling at least one hollow space ( 12 , 22 , 32 , 33 ) of the housing ( 10 , 20 , 30 ) to be worked with an incompressible fluid; and increasing a fluid pressure in the respective at least one hollow space ( 12 , 22 , 33 , 33 ) filled with the incompressible fluid so as to locally plastically deform the at least one housing portion ( 13 , 25 , 34 ) of the housing ( 10 , 20 , 30 ) limiting the respective at least one hollow space ( 12 , 22 , 32 , 33 ) of the housing ( 10 , 20 , 30 ), at least in portions. 2. The method according to claim 1 , wherein the fluid pressure for the local plastic deformation of the at least one housing portion ( 13 , 25 , 34 ) limits the respective hollow space ( 12 , 22 , 32 , 33 ) of the housing ( 10 , 20 , 30 ) is determined dependent on a geometry and/or a wall thickness and/or a metallic material of the housing portion ( 13 , 25 , 34 ) to be locally deformed plastically. 3. The method according to claim 2 , wherein the respective housing portion ( 13 , 25 , 34 ) of the housing ( 10 , 20 , 30 ) to be a plastically deformed is deformed plastically such that an amount of internal stress introduced into the respective housing portion ( 13 , 25 , 34 ) corresponds to a stress loading of the respective housing portion ( 13 , 25 , 34 ) expected during the local plastic deformation. 4. The method according to claim 3 , wherein the respective housing portion ( 13 , 25 , 34 ) of the housing ( 10 , 20 , 30 ) to be plastically deformed is deformed plastically such that a residual stress introduced into the respective housing portion ( 13 , 25 , 34 ) in the plastic deformation has an opposite sign to a mean stress loading to be expected during the plastic deformation. 5. The method according to claim 4 , wherein the incompressible fluid, during the operation of the turbocharger, performs process gas conduction. 6. The method according to claim 5 , wherein the hollow space ( 22 , 32 ) that is filled with the incompressible fluid is a spiral process gas flow conduction passage of the turbine housing ( 30 ), or a spiral process gas flow conduction passage of the compressor housing ( 20 ), wherein the housing portion ( 25 , 43 ) at least locally deformed plastically comprises a wall limiting the spiral process gas flow conduction passage at least in portions, the incompressible fluid emanating from an inside portion of the wall that conducts process gas during operation of the turbocharger. 7. The method according to claim 4 , wherein the incompressible fluid, during the operation of the turbocharger, performs a coolant conduction. 8. The method according to claim 7 , wherein the hollow space ( 33 ) is a coolant passage of the housing that is separated from a process gas flow conduction passage of the housing by a wall, configured as the housing portion ( 34 ), the wall limiting the coolant passage at least in portions and adjoining a spiral process gas flow conduction passage, the incompressible fluid emanating from an outside portion of the wall that does not conduct process gas during the operation of the turbocharger. 9. The method according to claim 7 , wherein the hollow space ( 12 ) which is filled incompressible fluid is a coolant passage of the bearing housing ( 10 ).
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