{
  "$type": "site.standard.document",
  "description": "A seal assembly (100) for a gas turbine engine (20) may include a seal body (70) coupled to an engine static structure (36) of the gas turbine engine and a seal seat insert (110; 210) coupled to a radially extending portion (68; 268) of a shaft (66) of the gas turbine engine. The seal body may be…",
  "path": "/patents/1425479",
  "publishedAt": "2024-11-27T00:00:00.000Z",
  "site": "at://did:plc:oql6ds5vnff4ugar6rruliwd/site.standard.publication/3mn3ohu7oxx5w",
  "tags": [
    "F01D11/003",
    "RTX CORP [US]"
  ],
  "textContent": "A seal assembly (100) for a gas turbine engine (20) may include a seal body (70) coupled to an engine static structure (36) of the gas turbine engine and a seal seat insert (110; 210) coupled to a radially extending portion (68; 268) of a shaft (66) of the gas turbine engine. The seal body may be generally configured to be biased into contact with the seal seat insert to provide a sealing pressure between the seal body and the seal seat insert. In various embodiments, the seal seat insert is made from a ceramic material or a ceramic matrix composite.",
  "title": "SEAL SEAT INSERT FOR GAS TURBINE ENGINES"
}