Flow body for a gas turbine, gas turbine, method for manufacturing a flow body for a gas turbine, and method for repairing a flow body of a gas turbine
US-2024376825-A1 · Nov 14, 2024 · US
US8974183B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8974183-B2 |
| Application number | US-201313742749-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 16, 2013 |
| Priority date | May 24, 2010 |
| Publication date | Mar 10, 2015 |
| Grant date | Mar 10, 2015 |
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A core die for creating an airfoil includes a first section, a second section mating with the first section, and an insert for creating a slot. The first section and the second section define a body having an outer dimension. The insert is disposed at an angle to the outer dimension. A trip strip includes a first portion disposed in the second section. The first portion is in register with the insert and a thickness is maintained between the first portion and the insert along a length of the insert. The first portion tapers towards the outer dimension and the thickness is filled by the ceramic material between the slot and the first portion.
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What is claimed is: 1. An airfoil comprising; a body including; an inner passageway for cooling said body, a trip strip having a first portion disposed within said inner passageway and a second portion disposed within said inner passageway, said first portion tapering into an area requiring increased cooling, said second portion disposed at an angle from said first portion; said first portion comprises a first section and a second section; said second portion comprises a s…
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