Turbine blade with modal response adapted tip shroud
US-2024011401-A1 · Jan 11, 2024 · US
US9506372B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9506372-B2 |
| Application number | US-201113990338-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 29, 2011 |
| Priority date | Nov 30, 2010 |
| Publication date | Nov 29, 2016 |
| Grant date | Nov 29, 2016 |
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A damper ( 2 ) for damping a blade movement of a turbomachine ( 1 ), and to a method for producing the damper ( 2 ). The damper ( 2 ) has at least one side surface ( 21, 21 ′) which can be brought into frictional contact with a friction surface of the turbomachine ( 1 ) in order to damp a blade movement. The side surfaces ( 21, 21 ′) are asymmetrically convex in shape.
Opening claim text (preview).
What is claimed is: 1. A damper for damping a blade movement of a turbomachine, the damper comprising: a single piece body having a polygonal shape in a cross section normal to a rotor axis of the turbomachine, wherein the single piece body includes a first side surface intended to damp the blade movement by frictional contact with a friction surface of a first blade of the turbomachine, the first side surface being asymmetrically convex in shape, the asymmetrically convex first…
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