{
  "$type": "site.standard.document",
  "description": "A manufacturing method is provided during which a preform component (60') for a turbine engine is provided. The preform component includes a substrate (74') and a locating feature (140) at an exterior surface of the substrate. An outer coating (78') is applied over the substrate. The outer coating…",
  "path": "/patents/1402227",
  "publishedAt": "2025-07-09T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "C23C28/34",
    "RTX CORP [US]"
  ],
  "textContent": "A manufacturing method is provided during which a preform component (60') for a turbine engine is provided. The preform component includes a substrate (74') and a locating feature (140) at an exterior surface of the substrate. An outer coating (78') 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 (64) is formed in the substrate and the outer coating based on the scan data.",
  "title": "METHOD FOR FORMING COOLING APERTURES IN A COATED TURBINE ENGINE COMPONENT"
}