{
  "$type": "site.standard.document",
  "description": "A gas turbine engine (20) article (60) includes a ceramic body (62) that defines a flange (70), first and second cooling passages (72, 74) partitioned from each other by the flange (70), a through-hole (76) in the flange (70) that connects the first and second cooling passages (72, 74), and a…",
  "path": "/patents/1409845",
  "publishedAt": "2024-07-17T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D25/246",
    "RTX CORP [US]"
  ],
  "textContent": "A gas turbine engine (20) article (60) includes a ceramic body (62) that defines a flange (70), first and second cooling passages (72, 74) partitioned from each other by the flange (70), a through-hole (76) in the flange (70) that connects the first and second cooling passages (72, 74), and a thermal insulation bushing (78) that lines the through-hole (76).",
  "title": "GAS TURBINE ENGINE CERAMIC ARTICLE WITH THERMAL INSULATION BUSHING"
}