Turbine blade cooling hole arrangement
US11060408B1 · kind B1 · utility
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5References
20Claims
0Family size
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Key dates
| Filing date | Feb 3, 2020 |
| Grant date | Jul 13, 2021 |
| Priority date | — |
| Expiry date | Feb 3, 2040 |
Classification
- Technology area (CPC —)General
Abstract
A turbine blade for a gas turbine engine. The turbine blade having a plurality of cooling holes defined therein, wherein the plurality of cooling holes are located in the turbine blade according to the coordinates of Table 1 and at least some of the plurality of cooling holes are located in an airfoil of the turbine blade.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.