Film growing method
US-2015368779-A1 · Dec 24, 2015 · US
US9260784B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9260784-B2 |
| Application number | US-201013384462-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 31, 2010 |
| Priority date | Aug 6, 2009 |
| Publication date | Feb 16, 2016 |
| Grant date | Feb 16, 2016 |
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The present invention relates to a method for producing a component, in particular a blade for a gas turbine, wherein a main body ( 2 ) is provided, to which a running-in layer ( 6 ) is applied, which can be worn away at least partially during operation to form an accurately fitting surface ( 11 ), wherein the running-in layer is applied by kinetic cold-gas compacting, and a component, in particular a blade for a gas turbine, comprising a main body, to which a running-in layer is applied, which can be worn away at least partially during operation to form an accurately fitting surface, wherein the running-in layer is a porous layer made of a Ti alloy.
Opening claim text (preview).
The invention claimed is: 1. A method for producing a blade for a gas turbine, the method comprising the steps of: providing a main body ( 2 ) having a blade tip, applying onto the main body ( 2 ) a running-in layer ( 6 ), which can be rubbed away at least partially to form an accurately fitting surface ( 11 ) during operation, wherein the running-in layer is applied by kinetic cold-gas compacting; the running-in layer is introduced on the blade tip; and wherein the running…
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