{
  "$type": "site.standard.document",
  "description": "An assembly for a turbine engine is provided. This turbine engine assembly includes a shell (80) and a heat shield (82) attached to the shell with a cooling cavity (84) between the shell and the heat shield. The heat shield defines a plurality of cooling apertures (104) and an indentation (106) in…",
  "path": "/patents/1412276",
  "publishedAt": "2023-07-05T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/12",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "An assembly for a turbine engine is provided. This turbine engine assembly includes a shell (80) and a heat shield (82) attached to the shell with a cooling cavity (84) between the shell and the heat shield. The heat shield defines a plurality of cooling apertures (104) and an indentation (106) in a side of the heat shield opposite the cooling cavity. The cooling apertures are fluidly coupled with the cooling cavity. An outlet (150) of a first of the cooling apertures is located at an edge of the indentation.",
  "title": "ASSEMBLY FOR A TURBINE ENGINE"
}