Forming cooling aperture(s) in a turbine engine component
US11913119B2 · kind B2 · utility
0Cited by
33References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Aug 13, 2021 |
| Grant date | Feb 27, 2024 |
| Priority date | — |
| Expiry date | Aug 18, 2042 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R2900/03042
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
A manufacturing method is provided during which a preform component for a turbine engine is provided. The preform component includes a substrate and a locating feature at an exterior surface of the substrate. An outer coating is applied over the substrate. The outer coating covers the locating feature. At least a portion of the preform component and the outer coating are scanned with an imaging system to provide scan data indicative of a location of the locating feature. A cooling aperture is formed in the substrate and the outer coating based on the scan data.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.