{
  "$type": "site.standard.document",
  "description": "A hot section (104) of a gas turbine engine (100) includes a stator housing wall (114) and an at least one insulating standoff (116) attached to the stator housing wall (114), extending radially away from the stator housing wall (114). The hot section (104) includes an accessory module (118)…",
  "path": "/patents/1415477",
  "publishedAt": "2023-10-11T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "B22F5/009",
    "RAYTHEON TECH CORP [US]"
  ],
  "textContent": "A hot section (104) of a gas turbine engine (100) includes a stator housing wall (114) and an at least one insulating standoff (116) attached to the stator housing wall (114), extending radially away from the stator housing wall (114). The hot section (104) includes an accessory module (118) attached to an opposite end of the at least one insulating standoff (116) away from the stator housing wall (114).",
  "title": "HOT SECTION OF A GAS TURBINE ENGINE AND METHOD OF MANUFACTURING A GAS TURBINE ENGINE WITH AN INSULATION STANDOFF"
}