{
  "$type": "site.standard.document",
  "coverImage": {
    "$type": "blob",
    "ref": {
      "$link": "bafkreigqcjlstgieixwxr6eweyfbgbgzsi2z3pgyucboripzcpywqhwnkm"
    },
    "mimeType": "image/png",
    "size": 106156
  },
  "description": "A gas turbine engine (20) according to an exemplary aspect of the present disclosure includes, among other things, a bearing compartment (60), a shaft (66) configured to rotate during operation of the gas turbine engine (20), and a sleeve (70) configured to rotate with the shaft (66) during…",
  "path": "/patents/1409560",
  "publishedAt": "2024-04-10T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/003",
    "RTX CORP [US]"
  ],
  "textContent": "A gas turbine engine (20) according to an exemplary aspect of the present disclosure includes, among other things, a bearing compartment (60), a shaft (66) configured to rotate during operation of the gas turbine engine (20), and a sleeve (70) configured to rotate with the shaft (66) during operation of the gas turbine engine (20). The sleeve (70) includes a variable radial dimension (84) about a circumference of the sleeve (70). The engine (20) further includes a seal (68) statically mounted relative to the sleeve (70) and configured to cooperate with the sleeve (70) to seal the bearing compartment (60).",
  "title": "ROTATING SLEEVE CONTROLLING CLEARANCE OF SEAL ASSEMBLY OF GAS TURBINE ENGINE"
}